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

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

                                  (R)
                      Code_Saturne

                      Version 4.0.6


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

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


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

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

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


Local case configuration:

  Date:                06/23/17 15:20:12
  Processor:           
  Directory:           C:\Users\GIFFARD_Q\Desktop\Stage GIFFARD Quentin\prise en main code_saturne\defraeye\essai_SIMPLE\DEBUT\RESU\20170623-1520
  MPI ranks:           3 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    SCOTCH 6.0.0

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

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


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

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

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

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

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


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

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


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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             70 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.10880E+02 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - Spalart-Allmaras    (ITURB = 70)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       RELAXV =    0.70000E+00 for nu (Relaxation)

   - Rotation/curvature correction
       IRCCOR =              0 (0: desactivated             )
                               (1: activated                )

 --- Constants

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

   - Spalart-Allmaras    (ITURB = 70)
       CSAB1  =    0.13550E+00 (b1 constant                 )
       CSAB2  =    0.62200E+00 (b2 constant                 )
       CSASIG =    0.66667E+00 (sigma constant              )
       CSAV1  =    0.71000E+01 (v1 constant                 )
       CSAW1  =    0.32011E+01 (w1 constant                 )
       CSAW2  =    0.30000E+00 (w2 constant                 )
       CSAW3  =    0.20000E+01 (w3 constant                 )


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


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

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


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


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

    STEADY ALGORITHM

 --- Global parameters

       IDTVAR =             -1 (-1: steady algorithm        )
       RELXST =    0.70000E+00 (Reference relaxation coeff. )


 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per variable relaxation coefficient

-----------------------------
 Variable          RELAXV
-----------------------------
 Velocity          0.7000E+00
 Pressure          0.3000E+00
 nu_tilda          0.7000E+00
 TempC             0.7000E+00
----------------------------

       RELAXV =  [0.,1.]       (relaxation coefficient      )


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


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

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

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       ARAK   =    0.10000E+01 (Arakawa factor              )

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


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


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

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

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

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

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


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


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


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


 ** WALL DISTANCE COMPUTATION
    -------------------------

       ICDPAR =             -1 ( 1: std, reread if restart
                               (-1: std, recomputed if restrt
                               ( 2: old, reread if restart
                               (-2: old, recomputed if restrt


       NITMAY =          10000 (Nb iter for iter resolution )
       NSWRSY =              1 (Nb iter for rhs reconstr.   )
       NSWRGY =            100 (Nb iter for grad. reconstr. )
       IMLIGY =             -1 (Gradient limitation method  )
       IRCFLY =              1 (Conv. Diff. flow reconstr.  )
       ISCHCY =              1 (Convective scheme           )
       ISSTPY =              0 (Slope tet use               )
       IWARNY =              0 (Verbosity level             )
       NTCMXY =           1000 (Nb iter for steady convect. )

       BLENCY =    0.00000E+00 (2nd order conv. scheme prop.)
       EPSILY =    0.10000E-07 (Iterative solver precision  )
       EPSRSY =    0.10000E-04 (rhs reconstruction precision)
       EPSRGY =    0.10000E-04 (Gradient reconstr. precision)
       CLIMGY =    0.15000E+01 (Coeff. for grad. limitation )
       EXTRAY =    0.00000E+00 (Coeff. for grad. extrapolat.)
       COUMXY =    0.50000E+04 (Max CFL for convection      )
       EPSCVY =    0.10000E-07 (Precision for steady conv.  )
       YPLMXY =    0.20000E+03 (y+ max w. damping influence )


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


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

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

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


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

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

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

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

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

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

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

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

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


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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =           3000 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
nu_tilda
TempC
TurbVisc
total_pressure
         --           --

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

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 nu_tilda                      -1
         7 TempC                         -1
         9 LamVisc                       -1
        10 TurbVisc                      -1
        13 total_pressure                -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 nu_tilda                       0
         7 TempC                          0
        10 TurbVisc                    -999
        13 total_pressure              -999
         --           --                --

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


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


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

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


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


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

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


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

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [      52133 ;      52134 ] =          3

 Partitioning finished (1.74 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =              52133
    maximum value =              52134

      1 : [      52133 ;      52134 ] =          3

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

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

    minimum value =              52627
    maximum value =              53195

      1 : [      52627 ;      52740 [ =          2
      2 : [      52740 ;      52854 [ =          0
      3 : [      52854 ;      52967 [ =          0
      4 : [      52967 ;      53081 [ =          0
      5 : [      53081 ;      53195 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =                494
    maximum value =               1062

      1 : [        494 ;        607 [ =          2
      2 : [        607 ;        721 [ =          0
      3 : [        721 ;        834 [ =          0
      4 : [        834 ;        948 [ =          0
      5 : [        948 ;       1062 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =             104106
    maximum value =             104441

      1 : [     104106 ;     104173 [ =          1
      2 : [     104173 ;     104240 [ =          0
      3 : [     104240 ;     104307 [ =          1
      4 : [     104307 ;     104374 [ =          0
      5 : [     104374 ;     104441 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =             104843
    maximum value =             105086

      1 : [     104843 ;     104891 [ =          1
      2 : [     104891 ;     104940 [ =          0
      3 : [     104940 ;     104988 [ =          0
      4 : [     104988 ;     105037 [ =          1
      5 : [     105037 ;     105086 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =          6
      2 : [          3 ;          4 ] =     156394

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  2
    maximum value =                  2

      1 : [          2 ;          2 ] =          3

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

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

 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =              51373
    maximum value =              51992

      1 : [      51373 ;      51496 [ =          1
      2 : [      51496 ;      51620 [ =          0
      3 : [      51620 ;      51744 [ =          0
      4 : [      51744 ;      51868 [ =          1
      5 : [      51868 ;      51992 ] =          1

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =                982
    maximum value =               1125

      1 : [        982 ;       1010 [ =          1
      2 : [       1010 ;       1039 [ =          1
      3 : [       1039 ;       1067 [ =          0
      4 : [       1067 ;       1096 [ =          0
      5 : [       1096 ;       1125 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : -1.7763568e-018 2.0000000e-001
                       Y : -2.6645353e-018 5.0000000e-002
                       Z : 0.0000000e+000 1.0000000e-003
 Mesh
     Number of cells:          156400
     Number of interior faces: 311740
     Number of boundary faces: 314920
     Number of vertices:       314922

 Groups:
    "Inflow"
       boundary faces:          200
    "Outflow"
       boundary faces:          200
    "Solid"
       boundary faces:          180
    "Symmetry"
       boundary faces:       312800
    "Wall"
       boundary faces:         1540

 --- Information on the volumes
       Minimum control volume      = 6.2500000e-011
       Maximum control volume      = 6.2500000e-011
       Total volume for the domain = 9.7750000e-006

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

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

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

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

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

 Computing geometric quantities (0.149 s)
                                                             
       ALMAX  =    0.21464E-01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  nu_tilda          0.5258E-03  0.5258E-03
  TempC             0.2100E+02  0.2100E+02
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.6140E-03  0.6140E-03
 -----------------------------------------

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



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         200
Smooth wall               5        1720
Rough wall                6           0
Symmetry                  4      312800
Free outlet               3         200
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.20000E+00   0.12500E-03   0.50000E-03



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200         0.000000000E+00
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.00000E+00 0.00000E+00
   Dimensionless distance   yplus :  0.00000E+00 0.00000E+00
   Friction thermal sca.    tstar : -0.72375E+14 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74611E-12 0.74611E-12
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.93384E-04 Max distance =    0.24870E-01
                                                             
     (Distance calculation done in       1396 iterations)


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80220E-04      44   0.34817E-01   0.10740E+07 0.48815E+05 
c  Velocity[X]                                      0.10528E+07 
c  Velocity[Y]                                      0.21180E+05 
c  Velocity[Z]                                      0.15396E-22 
c  Pressure     0.13622E-04    1114   0.96663E-08   0.10000E+01 0.48886E+05 
c  nu_tilda     0.60587E-06      47   0.14951E+00   0.20715E-02 0.15797E+05 
c  TempC        0.14497E+02      33   0.96398E-03   0.78641E+02 0.81828E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.05125          23.156          4.5712          4.5712
v  Velocity[Y]             -21.29          21.296      0.00010336      0.00010336
v  Velocity[Z]        -3.708e-013     3.7105e-013     1.4159e-016     1.4159e-016
v  ǁVelocityǁ           0.10863          23.259          4.6249          4.6249
v  Pressure                6.7851           16632          8056.2          8056.2
v  nu_tilda            0.00018021       0.0062517       0.0005285       0.0005285
v  TempC                       21          23.314          21.002          21.002
v  TurbVisc            0.00061401      0.00061401      0.00061401      0.00061401
v  total_pressure     1.0133e+005     1.1796e+005     1.0938e+005     1.0938e+005


 TIME FOR THE TIME STEP                1:        0.10004E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421560E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16133E+02
   Friction velocity        uet   :  0.97678E-01 0.19663E+01
   Friction velocity        uk    :  0.97678E-01 0.19663E+01
   Dimensionless distance   yplus :  0.78637E+00 0.15830E+02
   Friction thermal sca.    tstar : -0.88167E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58672E+00 0.10344E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1706
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37082E-02      40   0.17406E-01   0.78300E+03 0.27398E+04 
c  Velocity[X]                                      0.58099E+03 
c  Velocity[Y]                                      0.20201E+03 
c  Velocity[Z]                                      0.10383E-22 
c  Pressure     0.69875E-05     730   0.91425E-08   0.10000E+01 0.94854E+05 
c  nu_tilda     0.14654E-05      43   0.11667E-01   0.12998E-02 0.34918E+05 
c  TempC        0.17314E+02      33   0.93198E-03   0.22718E+03 0.16594E+03 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           0.043957           19.82          4.5728          4.5728
v  Velocity[Y]            -15.609           18.47      0.00017838      0.00017838
v  Velocity[Z]       -1.5971e-013     1.7634e-013     1.2594e-016     1.2594e-016
v  ǁVelocityǁ          0.069165          19.923          4.6266          4.6266
v  Pressure               -202.75          55.661          11.922          11.922
v  nu_tilda           6.2544e-005       0.0054054      0.00052583      0.00052583
v  TempC                       21          28.409          21.005          21.005
v  TurbVisc            0.00017284       0.0073683      0.00061677      0.00061677
v  total_pressure     1.0112e+005     1.0138e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                2:        0.47690E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421565E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.13648E+02
   Friction velocity        uet   :  0.77542E-01 0.17282E+01
   Friction velocity        uk    :  0.77542E-01 0.17282E+01
   Dimensionless distance   yplus :  0.62427E+00 0.13913E+02
   Friction thermal sca.    tstar : -0.10071E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46577E+00 0.97565E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1714
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36954E-02      38   0.14611E-01   0.26584E+03 0.13289E+04 
c  Velocity[X]                                      0.16712E+03 
c  Velocity[Y]                                      0.98727E+02 
c  Velocity[Z]                                      0.11201E-23 
c  Pressure     0.40679E-05     538   0.96717E-08   0.57561E+00 0.22955E+05 
c  nu_tilda     0.14172E-05      42   0.26893E-02   0.47319E-03 0.24150E+05 
c  TempC        0.16825E+02      32   0.10637E-02   0.28332E+03 0.14440E+03 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.42226          17.231           4.573           4.573
v  Velocity[Y]            -11.959          15.581       0.0002011       0.0002011
v  Velocity[Z]        -8.278e-014     1.0043e-013      1.121e-016      1.121e-016
v  ǁVelocityǁ         0.0050476          18.379           4.627           4.627
v  Pressure               -247.53          47.447          11.539          11.539
v  nu_tilda           2.2207e-005       0.0049367      0.00052393      0.00052393
v  TempC                       21          42.628          21.009          21.009
v  TurbVisc           1.1383e-005       0.0063709      0.00061294      0.00061294
v  total_pressure     1.0108e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                3:        0.37260E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421575E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.11733E+02
   Friction velocity        uet   :  0.16012E-01 0.15394E+01
   Friction velocity        uk    :  0.16012E-01 0.15394E+01
   Dimensionless distance   yplus :  0.12890E+00 0.12394E+02
   Friction thermal sca.    tstar : -0.25960E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96178E-01 0.90842E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1717
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36517E-02      38   0.11435E-01   0.20120E+03 0.85247E+03 
c  Velocity[X]                                      0.11691E+03 
c  Velocity[Y]                                      0.84284E+02 
c  Velocity[Z]                                      0.23100E-24 
c  Pressure     0.24204E-05     423   0.91023E-08   0.37378E+00 0.72791E+04 
c  nu_tilda     0.13961E-05      41   0.81990E-03   0.21510E-03 0.14712E+05 
c  TempC        0.16570E+02      32   0.10812E-02   0.23968E+03 0.12746E+03 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.1492          16.104           4.573           4.573
v  Velocity[Y]            -9.9205          14.481      0.00019555      0.00019555
v  Velocity[Z]       -5.2324e-014     6.2321e-014     9.9624e-017     9.9624e-017
v  ǁVelocityǁ          0.017219          16.926          4.6272          4.6272
v  Pressure               -248.42          46.108          11.489          11.489
v  nu_tilda           8.3465e-006       0.0046486       0.0005225       0.0005225
v  TempC                       21          52.703          21.014          21.014
v  TurbVisc           2.1224e-007       0.0058185      0.00061051      0.00061051
v  total_pressure     1.0108e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                4:        0.29500E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421574E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.10904E+02
   Friction velocity        uet   :  0.22503E-01 0.14560E+01
   Friction velocity        uk    :  0.22503E-01 0.14560E+01
   Dimensionless distance   yplus :  0.18117E+00 0.11722E+02
   Friction thermal sca.    tstar : -0.22780E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13517E+00 0.87004E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1719
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36216E-02      37   0.78568E-02   0.16118E+03 0.70494E+03 
c  Velocity[X]                                      0.97747E+02 
c  Velocity[Y]                                      0.63431E+02 
c  Velocity[Z]                                      0.84559E-25 
c  Pressure     0.72985E-05     538   0.91554E-08   0.12091E+01 0.37836E+04 
c  nu_tilda     0.13858E-05      41   0.40115E-03   0.12306E-03 0.10319E+05 
c  TempC        0.16427E+02      32   0.10428E-02   0.19005E+03 0.11343E+03 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.5186          15.601           4.573           4.573
v  Velocity[Y]             -9.593          13.876       0.0001627       0.0001627
v  Velocity[Z]        -3.966e-014     4.0827e-014     8.8571e-017     8.8571e-017
v  ǁVelocityǁ          0.013886          16.274          4.6276          4.6276
v  Pressure               -230.35          46.443          11.776          11.776
v  nu_tilda           3.6403e-006       0.0044575      0.00052135      0.00052135
v  TempC                       21          59.023          21.019          21.019
v  TurbVisc           4.2678e-009       0.0054788      0.00060869      0.00060869
v  total_pressure     1.0109e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                5:        0.31680E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421566E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.99891E+01
   Friction velocity        uet   :  0.19027E-01 0.13625E+01
   Friction velocity        uk    :  0.19027E-01 0.13625E+01
   Dimensionless distance   yplus :  0.15318E+00 0.10969E+02
   Friction thermal sca.    tstar : -0.12850E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11429E+00 0.81844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1719
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36046E-02      37   0.73460E-02   0.12439E+03 0.60680E+03 
c  Velocity[X]                                      0.72827E+02 
c  Velocity[Y]                                      0.51562E+02 
c  Velocity[Z]                                      0.38798E-25 
c  Pressure     0.62374E-05     553   0.97706E-08   0.13040E+01 0.37235E+04 
c  nu_tilda     0.13824E-05      41   0.23392E-03   0.80230E-04 0.78587E+04 
c  TempC        0.16341E+02      32   0.93365E-03   0.15727E+03 0.10545E+03 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.7094          14.478          4.5729          4.5729
v  Velocity[Y]             -9.309          13.752      0.00013591      0.00013591
v  Velocity[Z]       -3.1431e-014     2.9493e-014     7.8782e-017     7.8782e-017
v  ǁVelocityǁ           0.01571          15.081           4.628           4.628
v  Pressure               -206.61          44.875          11.377          11.377
v  nu_tilda           2.1721e-006       0.0043249      0.00052046      0.00052046
v  TempC                       21          62.771          21.024          21.024
v  TurbVisc           1.5449e-010       0.0052536      0.00060717      0.00060717
v  total_pressure     1.0112e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                6:        0.31670E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421573E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24747E-01 0.13093E+01
   Friction velocity        uk    :  0.24747E-01 0.13093E+01
   Dimensionless distance   yplus :  0.19923E+00 0.10541E+02
   Friction thermal sca.    tstar : -0.15384E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14865E+00 0.78644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35954E-02      37   0.69968E-02   0.97304E+02 0.53990E+03 
c  Velocity[X]                                      0.56129E+02 
c  Velocity[Y]                                      0.41175E+02 
c  Velocity[Z]                                      0.21708E-25 
c  Pressure     0.56379E-05     581   0.97464E-08   0.14681E+01 0.35268E+04 
c  nu_tilda     0.13839E-05      41   0.18419E-03   0.57044E-04 0.63250E+04 
c  TempC        0.16290E+02      32   0.10188E-02   0.13252E+03 0.99601E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6782          13.807          4.5729          4.5729
v  Velocity[Y]            -9.0235          13.029      0.00011993      0.00011993
v  Velocity[Z]       -2.3676e-014     2.3461e-014     6.9835e-017     6.9835e-017
v  ǁVelocityǁ          0.011069           14.47          4.6283          4.6283
v  Pressure               -186.58          43.095          11.011          11.011
v  nu_tilda           1.7302e-006       0.0042301      0.00051959      0.00051959
v  TempC                       21          65.176          21.028          21.028
v  TurbVisc           1.9583e-011       0.0050973      0.00060589      0.00060589
v  total_pressure     1.0114e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                7:        0.32640E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421572E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.43195E-02 0.12766E+01
   Friction velocity        uk    :  0.43195E-02 0.12766E+01
   Dimensionless distance   yplus :  0.34775E-01 0.10277E+02
   Friction thermal sca.    tstar : -0.82489E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25946E-01 0.76681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35908E-02      37   0.62140E-02   0.87636E+02 0.51407E+03 
c  Velocity[X]                                      0.49164E+02 
c  Velocity[Y]                                      0.38471E+02 
c  Velocity[Z]                                      0.13302E-25 
c  Pressure     0.42410E-05     458   0.99115E-08   0.13091E+01 0.11843E+04 
c  nu_tilda     0.13891E-05      41   0.11229E-03   0.43121E-04 0.53010E+04 
c  TempC        0.16261E+02      32   0.96899E-03   0.12018E+03 0.99703E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9848          13.375          4.5729          4.5729
v  Velocity[Y]            -8.8315          12.716      0.00010295      0.00010295
v  Velocity[Z]       -2.0171e-014     2.1282e-014     6.1756e-017     6.1756e-017
v  ǁVelocityǁ         0.0077617          14.514          4.6288          4.6288
v  Pressure               -167.54          42.905          11.052          11.052
v  nu_tilda           1.5356e-006       0.0041612      0.00051898      0.00051898
v  TempC                       21          66.822          21.032          21.032
v  TurbVisc           7.8843e-012       0.0049856      0.00060476      0.00060476
v  total_pressure     1.0116e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                8:        0.28940E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421567E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.39222E-02 0.12408E+01
   Friction velocity        uk    :  0.39222E-02 0.12408E+01
   Dimensionless distance   yplus :  0.31576E-01 0.99896E+01
   Friction thermal sca.    tstar : -0.81692E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23559E-01 0.74534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35898E-02      37   0.63101E-02   0.77096E+02 0.48343E+03 
c  Velocity[X]                                      0.42759E+02 
c  Velocity[Y]                                      0.34337E+02 
c  Velocity[Z]                                      0.89227E-26 
c  Pressure     0.36748E-05     586   0.96514E-08   0.13213E+01 0.22452E+04 
c  nu_tilda     0.13971E-05      40   0.15269E-03   0.34176E-04 0.45837E+04 
c  TempC        0.16246E+02      32   0.99070E-03   0.87204E+02 0.92261E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5563          12.852          4.5729          4.5729
v  Velocity[Y]             -8.618          12.479     9.3146e-005     9.3146e-005
v  Velocity[Z]       -1.7038e-014     1.8921e-014     5.4505e-017     5.4505e-017
v  ǁVelocityǁ         0.0074401          14.055          4.6293          4.6293
v  Pressure               -151.52          41.875          10.796          10.796
v  nu_tilda           1.4104e-006       0.0041104      0.00051828      0.00051828
v  TempC                       21          68.002          21.036          21.036
v  TurbVisc           4.8924e-012       0.0049043      0.00060381      0.00060381
v  total_pressure     1.0117e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP                9:        0.32540E+01

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421572E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.91640E-02 0.12256E+01
   Friction velocity        uk    :  0.91640E-02 0.12256E+01
   Dimensionless distance   yplus :  0.73776E-01 0.98666E+01
   Friction thermal sca.    tstar : -0.38047E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55045E-01 0.73616E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35909E-02      37   0.52791E-02   0.74408E+02 0.47455E+03 
c  Velocity[X]                                      0.39263E+02 
c  Velocity[Y]                                      0.35145E+02 
c  Velocity[Z]                                      0.60873E-26 
c  Pressure     0.29512E-05     567   0.95634E-08   0.12155E+01 0.13407E+04 
c  nu_tilda     0.14071E-05      40   0.70016E-04   0.28039E-04 0.40606E+04 
c  TempC        0.16242E+02      32   0.90422E-03   0.72083E+02 0.92220E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1878          12.482          4.5729          4.5729
v  Velocity[Y]            -8.4823          12.181     8.5751e-005     8.5751e-005
v  Velocity[Z]       -1.4534e-014     1.6507e-014     4.7988e-017     4.7988e-017
v  ǁVelocityǁ          0.017764          13.952            4.63            4.63
v  Pressure               -138.44          41.159          10.659          10.659
v  nu_tilda           1.3102e-006       0.0040726      0.00051783      0.00051783
v  TempC                       21          68.871          21.039          21.039
v  TurbVisc           3.4813e-012       0.0048445      0.00060294      0.00060294
v  total_pressure     1.0119e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP               10:        0.32850E+01

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


 INSTANT    0.110000000E+02   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.33456E-01 0.11947E+01
   Friction velocity        uk    :  0.33456E-01 0.11947E+01
   Dimensionless distance   yplus :  0.26934E+00 0.96180E+01
   Friction thermal sca.    tstar : -0.57899E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20096E+00 0.71761E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35937E-02      37   0.50264E-02   0.67160E+02 0.44989E+03 
c  Velocity[X]                                      0.35843E+02 
c  Velocity[Y]                                      0.31317E+02 
c  Velocity[Z]                                      0.43903E-26 
c  Pressure     0.27265E-05     551   0.93882E-08   0.11461E+01 0.10127E+04 
c  nu_tilda     0.14186E-05      40   0.11771E-03   0.23687E-04 0.36671E+04 
c  TempC        0.16246E+02      32   0.11544E-02   0.62700E+02 0.88435E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6158           12.32          4.5729          4.5729
v  Velocity[Y]            -8.4456          12.033     8.6959e-005     8.6959e-005
v  Velocity[Z]       -1.2676e-014     1.4412e-014     4.2139e-017     4.2139e-017
v  ǁVelocityǁ          0.013479          13.785          4.6307          4.6307
v  Pressure               -128.28          41.081          10.549          10.549
v  nu_tilda           1.2263e-006       0.0040445      0.00051728      0.00051728
v  TempC                       21           69.53          21.042          21.042
v  TurbVisc           2.5921e-012          0.0048      0.00060221      0.00060221
v  total_pressure      1.012e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP               11:        0.36610E+01

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


 INSTANT    0.120000000E+02   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.25443E-01 0.11913E+01
   Friction velocity        uk    :  0.25443E-01 0.11913E+01
   Dimensionless distance   yplus :  0.20484E+00 0.95909E+01
   Friction thermal sca.    tstar : -0.12858E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15283E+00 0.71559E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35977E-02      37   0.45601E-02   0.62916E+02 0.43730E+03 
c  Velocity[X]                                      0.32887E+02 
c  Velocity[Y]                                      0.30028E+02 
c  Velocity[Z]                                      0.31981E-26 
c  Pressure     0.19314E-05     581   0.99104E-08   0.84403E+00 0.18172E+04 
c  nu_tilda     0.14313E-05      40   0.49387E-04   0.20434E-04 0.33615E+04 
c  TempC        0.16254E+02      32   0.10544E-02   0.61325E+02 0.92442E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8384          11.885          4.5729          4.5729
v  Velocity[Y]            -8.3287          11.823     8.7257e-005     8.7257e-005
v  Velocity[Z]       -1.0834e-014     1.2609e-014     3.6898e-017     3.6898e-017
v  ǁVelocityǁ          0.011935          13.664          4.6315          4.6315
v  Pressure               -119.78          40.448           10.34           10.34
v  nu_tilda           1.1542e-006       0.0040234      0.00051696      0.00051696
v  TempC                       21          70.032          21.044          21.044
v  TurbVisc           1.9894e-012       0.0047668      0.00060154      0.00060154
v  total_pressure     1.0121e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP               12:        0.41250E+01

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


 INSTANT    0.130000000E+02   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21359E-01 0.11779E+01
   Friction velocity        uk    :  0.21359E-01 0.11779E+01
   Dimensionless distance   yplus :  0.17195E+00 0.94829E+01
   Friction thermal sca.    tstar : -0.70224E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12830E+00 0.70753E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36024E-02      37   0.41358E-02   0.60595E+02 0.43145E+03 
c  Velocity[X]                                      0.31114E+02 
c  Velocity[Y]                                      0.29481E+02 
c  Velocity[Z]                                      0.23880E-26 
c  Pressure     0.14024E-05     601   0.98231E-08   0.67586E+00 0.15963E+04 
c  nu_tilda     0.14449E-05      40   0.78884E-04   0.17960E-04 0.31185E+04 
c  TempC        0.16267E+02      32   0.10754E-02   0.50616E+02 0.86098E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0859          11.676          4.5729          4.5729
v  Velocity[Y]             -8.287          11.629      8.707e-005      8.707e-005
v  Velocity[Z]       -9.3191e-015      1.113e-014     3.2176e-017     3.2176e-017
v  ǁVelocityǁ         0.0085223          13.493          4.6323          4.6323
v  Pressure               -112.15          40.008          10.147          10.147
v  nu_tilda           1.0921e-006       0.0040077      0.00051655      0.00051655
v  TempC                       21           70.42          21.046          21.046
v  TurbVisc           1.5612e-012        0.004742      0.00060098      0.00060098
v  total_pressure     1.0121e+005     1.0137e+005     1.0134e+005     1.0134e+005


 TIME FOR THE TIME STEP               13:        0.38800E+01

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


 INSTANT    0.140000000E+02   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15679E-01 0.11538E+01
   Friction velocity        uk    :  0.15679E-01 0.11538E+01
   Dimensionless distance   yplus :  0.12623E+00 0.92885E+01
   Friction thermal sca.    tstar : -0.15127E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94178E-01 0.69303E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36078E-02      37   0.46871E-02   0.56590E+02 0.41914E+03 
c  Velocity[X]                                      0.28348E+02 
c  Velocity[Y]                                      0.28242E+02 
c  Velocity[Z]                                      0.18053E-26 
c  Pressure     0.11730E-05     615   0.91140E-08   0.60073E+00 0.18851E+04 
c  nu_tilda     0.14591E-05      40   0.37992E-04   0.16004E-04 0.29204E+04 
c  TempC        0.16283E+02      32   0.11028E-02   0.52985E+02 0.90691E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2969           11.49          4.5729          4.5729
v  Velocity[Y]            -8.1753          11.438      8.834e-005      8.834e-005
v  Velocity[Z]       -8.1428e-015     9.8149e-015     2.7912e-017     2.7912e-017
v  ǁVelocityǁ         0.0037621          13.355          4.6331          4.6331
v  Pressure               -105.21           39.47          9.9304          9.9304
v  nu_tilda           1.0412e-006       0.0039961      0.00051632      0.00051632
v  TempC                       21          70.712          21.048          21.048
v  TurbVisc           1.2514e-012       0.0047235      0.00060047      0.00060047
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               14:        0.40500E+01

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


 INSTANT    0.150000000E+02   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.70881E-02 0.11479E+01
   Friction velocity        uk    :  0.70881E-02 0.11479E+01
   Dimensionless distance   yplus :  0.57064E-01 0.92410E+01
   Friction thermal sca.    tstar : -0.14002E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42576E-01 0.68948E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36137E-02      37   0.39474E-02   0.55378E+02 0.41878E+03 
c  Velocity[X]                                      0.26780E+02 
c  Velocity[Y]                                      0.28598E+02 
c  Velocity[Z]                                      0.13792E-26 
c  Pressure     0.10134E-05     602   0.93318E-08   0.52616E+00 0.24854E+04 
c  nu_tilda     0.14738E-05      40   0.44320E-04   0.14436E-04 0.27558E+04 
c  TempC        0.16302E+02      32   0.11522E-02   0.45752E+02 0.85852E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4329          11.463          4.5729          4.5729
v  Velocity[Y]            -8.1534          11.314     8.9873e-005     8.9873e-005
v  Velocity[Z]        -7.465e-015     8.4771e-015     2.4053e-017     2.4053e-017
v  ǁVelocityǁ         0.0015633          13.179           4.634           4.634
v  Pressure               -103.36          38.802          9.6482          9.6482
v  nu_tilda           1.0055e-006       0.0039877      0.00051603      0.00051603
v  TempC                       21          70.939           21.05           21.05
v  TurbVisc           1.0341e-012       0.0047098      0.00060004      0.00060004
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               15:        0.59090E+01

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


 INSTANT    0.160000000E+02   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93860E-03 0.11385E+01
   Friction velocity        uk    :  0.93860E-03 0.11385E+01
   Dimensionless distance   yplus :  0.75564E-02 0.91656E+01
   Friction thermal sca.    tstar : -0.23594E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56379E-02 0.68385E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36198E-02      37   0.43762E-02   0.52851E+02 0.41055E+03 
c  Velocity[X]                                      0.25275E+02 
c  Velocity[Y]                                      0.27576E+02 
c  Velocity[Z]                                      0.10688E-26 
c  Pressure     0.10473E-05     599   0.94271E-08   0.61776E+00 0.19140E+04 
c  nu_tilda     0.14889E-05      40   0.29718E-04   0.13147E-04 0.26164E+04 
c  TempC        0.16322E+02      32   0.91216E-03   0.49244E+02 0.90871E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6299          11.488          4.5729          4.5729
v  Velocity[Y]            -8.0919          11.221     9.1317e-005     9.1317e-005
v  Velocity[Z]       -6.9285e-015     7.4191e-015     2.0544e-017     2.0544e-017
v  ǁVelocityǁ         0.0072648          13.079          4.6348          4.6348
v  Pressure               -103.16          38.329          9.4301          9.4301
v  nu_tilda            9.775e-007       0.0039816      0.00051587      0.00051587
v  TempC                       21          71.117          21.051          21.051
v  TurbVisc            8.992e-013       0.0046998      0.00059965      0.00059965
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               16:        0.39740E+01

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


 INSTANT    0.170000000E+02   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11327E-01 0.11119E+01
   Friction velocity        uk    :  0.11327E-01 0.11119E+01
   Dimensionless distance   yplus :  0.91187E-01 0.89514E+01
   Friction thermal sca.    tstar : -0.27467E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68036E-01 0.66787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36263E-02      37   0.40516E-02   0.51484E+02 0.40682E+03 
c  Velocity[X]                                      0.23978E+02 
c  Velocity[Y]                                      0.27506E+02 
c  Velocity[Z]                                      0.82559E-27 
c  Pressure     0.93840E-06     586   0.96276E-08   0.56897E+00 0.24669E+04 
c  nu_tilda     0.15042E-05      40   0.34686E-04   0.12076E-04 0.24966E+04 
c  TempC        0.16343E+02      32   0.12325E-02   0.40923E+02 0.82907E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7999          11.491          4.5729          4.5729
v  Velocity[Y]            -8.0299           11.09     8.9933e-005     8.9933e-005
v  Velocity[Z]       -6.9285e-015     6.3945e-015     1.7344e-017     1.7344e-017
v  ǁVelocityǁ         0.0072358          12.917          4.6357          4.6357
v  Pressure               -103.13          37.679          9.1571          9.1571
v  nu_tilda           9.5294e-007       0.0039775      0.00051566      0.00051566
v  TempC                       21          71.254          21.053          21.053
v  TurbVisc           8.0323e-013       0.0046927      0.00059932      0.00059932
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               17:        0.37030E+01

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


 INSTANT    0.180000000E+02   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27843E-01 0.10798E+01
   Friction velocity        uk    :  0.27843E-01 0.10798E+01
   Dimensionless distance   yplus :  0.22415E+00 0.86928E+01
   Friction thermal sca.    tstar : -0.73051E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16724E+00 0.64858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36328E-02      37   0.36032E-02   0.49638E+02 0.40326E+03 
c  Velocity[X]                                      0.23053E+02 
c  Velocity[Y]                                      0.26585E+02 
c  Velocity[Z]                                      0.64656E-27 
c  Pressure     0.10338E-05     602   0.96862E-08   0.70669E+00 0.31174E+04 
c  nu_tilda     0.15196E-05      40   0.24064E-04   0.11165E-04 0.23920E+04 
c  TempC        0.16366E+02      32   0.11308E-02   0.47444E+02 0.90759E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8974          11.489          4.5729          4.5729
v  Velocity[Y]            -7.9612          10.872     8.9766e-005     8.9766e-005
v  Velocity[Z]       -6.9285e-015     5.6041e-015     1.4423e-017     1.4423e-017
v  ǁVelocityǁ         0.0050877          12.905          4.6366          4.6366
v  Pressure               -102.16          36.749          8.8399          8.8399
v  nu_tilda           9.3007e-007       0.0039748      0.00051555      0.00051555
v  TempC                       21          71.355          21.054          21.054
v  TurbVisc            7.255e-013       0.0046878      0.00059903      0.00059903
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               18:        0.41330E+01

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


 INSTANT    0.190000000E+02   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12202E-01 0.10695E+01
   Friction velocity        uk    :  0.12202E-01 0.10695E+01
   Dimensionless distance   yplus :  0.98233E-01 0.86099E+01
   Friction thermal sca.    tstar : -0.19506E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73292E-01 0.64240E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36395E-02      37   0.38462E-02   0.47400E+02 0.39585E+03 
c  Velocity[X]                                      0.21767E+02 
c  Velocity[Y]                                      0.25633E+02 
c  Velocity[Z]                                      0.51048E-27 
c  Pressure     0.69017E-06     586   0.93002E-08   0.45171E+00 0.19542E+04 
c  nu_tilda     0.15352E-05      40   0.28216E-04   0.10387E-04 0.22998E+04 
c  TempC        0.16390E+02      32   0.11469E-02   0.45441E+02 0.88924E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9908          11.493          4.5729          4.5729
v  Velocity[Y]            -7.8947          10.767     9.2017e-005     9.2017e-005
v  Velocity[Z]       -6.9286e-015      5.139e-015     1.1753e-017     1.1753e-017
v  ǁVelocityǁ         0.0056537          12.704          4.6375          4.6375
v  Pressure                -102.3          36.403          8.6229          8.6229
v  nu_tilda           9.1198e-007       0.0039734      0.00051542      0.00051542
v  TempC                       21          71.434          21.056          21.056
v  TurbVisc           6.5832e-013       0.0046847      0.00059879      0.00059879
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               19:        0.40550E+01

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


 INSTANT    0.200000000E+02   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.23962E-01 0.10634E+01
   Friction velocity        uk    :  0.23962E-01 0.10634E+01
   Dimensionless distance   yplus :  0.19291E+00 0.85613E+01
   Friction thermal sca.    tstar : -0.81172E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14393E+00 0.63877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36463E-02      37   0.34328E-02   0.46280E+02 0.39435E+03 
c  Velocity[X]                                      0.20786E+02 
c  Velocity[Y]                                      0.25494E+02 
c  Velocity[Z]                                      0.40227E-27 
c  Pressure     0.79583E-06     615   0.92126E-08   0.56107E+00 0.34420E+04 
c  nu_tilda     0.15508E-05      40   0.20990E-04   0.97122E-05 0.22175E+04 
c  TempC        0.16414E+02      32   0.11046E-02   0.40548E+02 0.84683E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1478          11.478          4.5729          4.5729
v  Velocity[Y]            -7.8237          10.591     9.2579e-005     9.2579e-005
v  Velocity[Z]       -6.9286e-015     5.0407e-015     9.3156e-018     9.3156e-018
v  ǁVelocityǁ         0.0066607          12.626          4.6384          4.6384
v  Pressure               -101.98          35.426          8.2903          8.2903
v  nu_tilda             8.99e-007       0.0039728      0.00051539      0.00051539
v  TempC                       21          71.493          21.057          21.057
v  TurbVisc           6.0858e-013        0.004683      0.00059858      0.00059858
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               20:        0.43890E+01

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


 INSTANT    0.210000000E+02   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14041E-01 0.10573E+01
   Friction velocity        uk    :  0.14041E-01 0.10573E+01
   Dimensionless distance   yplus :  0.11304E+00 0.85119E+01
   Friction thermal sca.    tstar : -0.22125E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84343E-01 0.63508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36531E-02      37   0.32237E-02   0.44529E+02 0.38837E+03 
c  Velocity[X]                                      0.19842E+02 
c  Velocity[Y]                                      0.24687E+02 
c  Velocity[Z]                                      0.31924E-27 
c  Pressure     0.52213E-06     601   0.96894E-08   0.35821E+00 0.22831E+04 
c  nu_tilda     0.15664E-05      40   0.25595E-04   0.91218E-05 0.21435E+04 
c  TempC        0.16439E+02      32   0.11782E-02   0.43199E+02 0.87606E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2582          11.516          4.5729          4.5729
v  Velocity[Y]            -7.7795          10.466     9.5293e-005     9.5293e-005
v  Velocity[Z]       -6.9286e-015     5.0578e-015     7.0972e-018     7.0972e-018
v  ǁVelocityǁ         0.0044595          12.576          4.6393          4.6393
v  Pressure               -102.53          35.003          8.0472          8.0472
v  nu_tilda           8.9005e-007        0.003973      0.00051533      0.00051533
v  TempC                       21          71.542          21.058          21.058
v  TurbVisc           5.7466e-013       0.0046824      0.00059842      0.00059842
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               21:        0.38470E+01

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


 INSTANT    0.220000000E+02   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.22080E-01 0.10537E+01
   Friction velocity        uk    :  0.22080E-01 0.10537E+01
   Dimensionless distance   yplus :  0.17776E+00 0.84826E+01
   Friction thermal sca.    tstar : -0.13879E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13263E+00 0.63290E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36599E-02      37   0.31541E-02   0.43050E+02 0.38311E+03 
c  Velocity[X]                                      0.18918E+02 
c  Velocity[Y]                                      0.24132E+02 
c  Velocity[Z]                                      0.25635E-27 
c  Pressure     0.51070E-06     617   0.95885E-08   0.34815E+00 0.24029E+04 
c  nu_tilda     0.15820E-05      39   0.19409E-04   0.86007E-05 0.20763E+04 
c  TempC        0.16464E+02      32   0.11645E-02   0.42676E+02 0.86282E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3186          11.528          4.5729          4.5729
v  Velocity[Y]            -7.7152          10.378     9.9146e-005     9.9146e-005
v  Velocity[Z]       -6.9286e-015     4.7424e-015     5.0827e-018     5.0827e-018
v  ǁVelocityǁ         0.0050793          12.516          4.6402          4.6402
v  Pressure               -102.44          34.494          7.8083          7.8083
v  nu_tilda           8.8382e-007       0.0039738      0.00051534      0.00051534
v  TempC                       21          71.576          21.059          21.059
v  TurbVisc           5.5211e-013       0.0046826      0.00059828      0.00059828
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               22:        0.47860E+01

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


 INSTANT    0.230000000E+02   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12985E-01 0.10463E+01
   Friction velocity        uk    :  0.12985E-01 0.10463E+01
   Dimensionless distance   yplus :  0.10454E+00 0.84237E+01
   Friction thermal sca.    tstar : -0.23024E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77996E-01 0.62850E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36668E-02      37   0.29834E-02   0.42184E+02 0.38093E+03 
c  Velocity[X]                                      0.18454E+02 
c  Velocity[Y]                                      0.23731E+02 
c  Velocity[Z]                                      0.20629E-27 
c  Pressure     0.58039E-06     634   0.98736E-08   0.42036E+00 0.31771E+04 
c  nu_tilda     0.15975E-05      39   0.25612E-04   0.81377E-05 0.20149E+04 
c  TempC        0.16490E+02      32   0.10331E-02   0.43156E+02 0.88229E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4401          11.529          4.5729          4.5729
v  Velocity[Y]            -7.6453          10.197      0.00010113      0.00010113
v  Velocity[Z]       -6.9286e-015     4.5199e-015      3.265e-018      3.265e-018
v  ǁVelocityǁ          0.004187          12.461          4.6412          4.6412
v  Pressure               -101.76          33.718          7.5134          7.5134
v  nu_tilda           8.7979e-007        0.003975      0.00051532      0.00051532
v  TempC                       21          71.596          21.061          21.061
v  TurbVisc           5.3682e-013       0.0046835      0.00059818      0.00059818
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               23:        0.55760E+01

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


 INSTANT    0.240000000E+02   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.99671E-02 0.10444E+01
   Friction velocity        uk    :  0.99671E-02 0.10444E+01
   Dimensionless distance   yplus :  0.80242E-01 0.84083E+01
   Friction thermal sca.    tstar : -0.96439E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59870E-01 0.62736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36736E-02      37   0.28841E-02   0.40635E+02 0.37503E+03 
c  Velocity[X]                                      0.17669E+02 
c  Velocity[Y]                                      0.22966E+02 
c  Velocity[Z]                                      0.16555E-27 
c  Pressure     0.49474E-06     618   0.94656E-08   0.34303E+00 0.23658E+04 
c  nu_tilda     0.16130E-05      39   0.18656E-04   0.77226E-05 0.19584E+04 
c  TempC        0.16515E+02      32   0.12254E-02   0.38576E+02 0.84060E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5312          11.529          4.5729          4.5729
v  Velocity[Y]            -7.5802          10.071      0.00010457      0.00010457
v  Velocity[Z]       -6.9286e-015     4.4983e-015     1.6254e-018     1.6254e-018
v  ǁVelocityǁ         0.0027405          12.379          4.6421          4.6421
v  Pressure               -101.86          33.215          7.2945          7.2945
v  nu_tilda           8.7798e-007       0.0039766      0.00051537      0.00051537
v  TempC                       21          71.609          21.062          21.062
v  TurbVisc            5.271e-013       0.0046849       0.0005981       0.0005981
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               24:        0.45590E+01

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


 INSTANT    0.250000000E+02   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13992E-01 0.10419E+01
   Friction velocity        uk    :  0.13992E-01 0.10419E+01
   Dimensionless distance   yplus :  0.11264E+00 0.83882E+01
   Friction thermal sca.    tstar : -0.10579E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84044E-01 0.62585E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36805E-02      37   0.28065E-02   0.39597E+02 0.37191E+03 
c  Velocity[X]                                      0.17028E+02 
c  Velocity[Y]                                      0.22569E+02 
c  Velocity[Z]                                      0.13515E-27 
c  Pressure     0.46139E-06     617   0.95250E-08   0.31363E+00 0.24077E+04 
c  nu_tilda     0.16284E-05      39   0.27920E-04   0.73493E-05 0.19062E+04 
c  TempC        0.16541E+02      32   0.12246E-02   0.39357E+02 0.85343E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5898          11.526          4.5729          4.5729
v  Velocity[Y]            -7.5183          9.9977      0.00010773      0.00010773
v  Velocity[Z]       -6.9287e-015     4.3484e-015     1.5727e-019     1.5727e-019
v  ǁVelocityǁ         0.0025953           12.33          4.6431          4.6431
v  Pressure                -102.2          32.746          7.0733          7.0733
v  nu_tilda           8.7768e-007       0.0039784      0.00051538      0.00051538
v  TempC                       21          71.613          21.063          21.063
v  TurbVisc           5.2277e-013       0.0046868      0.00059805      0.00059805
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               25:        0.42200E+01

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


 INSTANT    0.260000000E+02   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14695E-01 0.10397E+01
   Friction velocity        uk    :  0.14695E-01 0.10397E+01
   Dimensionless distance   yplus :  0.11831E+00 0.83703E+01
   Friction thermal sca.    tstar : -0.11495E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88270E-01 0.62452E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36873E-02      37   0.28017E-02   0.38737E+02 0.36839E+03 
c  Velocity[X]                                      0.16659E+02 
c  Velocity[Y]                                      0.22078E+02 
c  Velocity[Z]                                      0.10898E-27 
c  Pressure     0.44326E-06     602   0.92227E-08   0.29596E+00 0.19869E+04 
c  nu_tilda     0.16437E-05      39   0.18087E-04   0.70105E-05 0.18577E+04 
c  TempC        0.16568E+02      32   0.11799E-02   0.37597E+02 0.82475E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.624          11.557          4.5729          4.5729
v  Velocity[Y]            -7.4519          9.9421       0.0001104       0.0001104
v  Velocity[Z]       -6.9287e-015     3.9308e-015    -1.1582e-018    -1.1582e-018
v  ǁVelocityǁ         0.0019589          12.306           4.644           4.644
v  Pressure               -102.07          32.376           6.899           6.899
v  nu_tilda           8.7964e-007       0.0039806      0.00051547      0.00051547
v  TempC                       21          71.615          21.064          21.064
v  TurbVisc           5.2205e-013        0.004689      0.00059802      0.00059802
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               26:        0.33260E+01

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


 INSTANT    0.270000000E+02   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12951E-01 0.10383E+01
   Friction velocity        uk    :  0.12951E-01 0.10383E+01
   Dimensionless distance   yplus :  0.10426E+00 0.83593E+01
   Friction thermal sca.    tstar : -0.92605E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77790E-01 0.62370E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.36942E-02      37   0.25949E-02   0.37880E+02 0.36529E+03 
c  Velocity[X]                                      0.16196E+02 
c  Velocity[Y]                                      0.21684E+02 
c  Velocity[Z]                                      0.88873E-28 
c  Pressure     0.42453E-06     602   0.94842E-08   0.28899E+00 0.24782E+04 
c  nu_tilda     0.16589E-05      39   0.33785E-04   0.67032E-05 0.18125E+04 
c  TempC        0.16594E+02      32   0.91390E-03   0.38041E+02 0.83053E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7178          11.569          4.5729          4.5729
v  Velocity[Y]            -7.4022          9.8394      0.00011276      0.00011276
v  Velocity[Z]       -6.9287e-015     3.8408e-015    -2.3371e-018    -2.3371e-018
v  ǁVelocityǁ         0.0010438           12.25           4.645           4.645
v  Pressure                -101.6          31.875          6.6869          6.6869
v  nu_tilda           8.8152e-007       0.0039829       0.0005155       0.0005155
v  TempC                       21          71.613          21.065          21.065
v  TurbVisc           5.2674e-013       0.0046915      0.00059802      0.00059802
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               27:        0.32780E+01

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


 INSTANT    0.280000000E+02   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.86176E-02 0.10348E+01
   Friction velocity        uk    :  0.86176E-02 0.10348E+01
   Dimensionless distance   yplus :  0.69377E-01 0.83308E+01
   Friction thermal sca.    tstar : -0.54692E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51763E-01 0.62157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37010E-02      37   0.28968E-02   0.36978E+02 0.36133E+03 
c  Velocity[X]                                      0.15777E+02 
c  Velocity[Y]                                      0.21201E+02 
c  Velocity[Z]                                      0.72943E-28 
c  Pressure     0.40948E-06     582   0.96727E-08   0.28263E+00 0.17695E+04 
c  nu_tilda     0.16739E-05      39   0.17763E-04   0.64207E-05 0.17701E+04 
c  TempC        0.16620E+02      32   0.10564E-02   0.35897E+02 0.80396E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7705          11.557          4.5729          4.5729
v  Velocity[Y]            -7.3425          9.7957      0.00011502      0.00011502
v  Velocity[Z]       -6.9287e-015       4.06e-015    -3.3873e-018    -3.3873e-018
v  ǁVelocityǁ        0.00035775          12.205           4.646           4.646
v  Pressure                -101.6          31.556          6.5435          6.5435
v  nu_tilda            8.827e-007       0.0039855      0.00051563      0.00051563
v  TempC                       21          71.612          21.066          21.066
v  TurbVisc           5.3124e-013       0.0046943      0.00059803      0.00059803
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               28:        0.30240E+01

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


 INSTANT    0.290000000E+02   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14072E-02 0.10335E+01
   Friction velocity        uk    :  0.14072E-02 0.10335E+01
   Dimensionless distance   yplus :  0.11329E-01 0.83200E+01
   Friction thermal sca.    tstar : -0.84662E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84526E-02 0.62076E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37078E-02      37   0.26412E-02   0.36253E+02 0.35860E+03 
c  Velocity[X]                                      0.15423E+02 
c  Velocity[Y]                                      0.20829E+02 
c  Velocity[Z]                                      0.60537E-28 
c  Pressure     0.42894E-06     586   0.97807E-08   0.29506E+00 0.25858E+04 
c  nu_tilda     0.16889E-05      39   0.38376E-04   0.61624E-05 0.17303E+04 
c  TempC        0.16647E+02      32   0.14400E-02   0.35977E+02 0.80279E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7913          11.553          4.5729          4.5729
v  Velocity[Y]            -7.2784          9.7001      0.00011721      0.00011721
v  Velocity[Z]       -6.9287e-015     4.2684e-015    -4.3254e-018    -4.3254e-018
v  ǁVelocityǁ        0.00062421          12.192           4.647           4.647
v  Pressure               -101.11          31.021          6.3365          6.3365
v  nu_tilda           8.8341e-007       0.0039881      0.00051569      0.00051569
v  TempC                       21          71.608          21.067          21.067
v  TurbVisc           5.3409e-013       0.0046973      0.00059807      0.00059807
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               29:        0.25740E+01

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


 INSTANT    0.300000000E+02   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38923E-02 0.10308E+01
   Friction velocity        uk    :  0.38923E-02 0.10308E+01
   Dimensionless distance   yplus :  0.31336E-01 0.82990E+01
   Friction thermal sca.    tstar : -0.14507E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23380E-01 0.61920E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37145E-02      37   0.25362E-02   0.35597E+02 0.35560E+03 
c  Velocity[X]                                      0.15223E+02 
c  Velocity[Y]                                      0.20374E+02 
c  Velocity[Z]                                      0.49686E-28 
c  Pressure     0.44036E-06     554   0.99945E-08   0.30514E+00 0.16288E+04 
c  nu_tilda     0.17038E-05      39   0.17828E-04   0.59229E-05 0.16927E+04 
c  TempC        0.16674E+02      32   0.11543E-02   0.40699E+02 0.85506E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.847          11.539          4.5729          4.5729
v  Velocity[Y]            -7.2239          9.6815      0.00011923      0.00011923
v  Velocity[Z]       -6.9287e-015     4.4604e-015    -5.1586e-018    -5.1586e-018
v  ǁVelocityǁ         0.0014982           12.15          4.6479          4.6479
v  Pressure               -100.39          30.744          6.2151          6.2151
v  nu_tilda           8.8263e-007       0.0039909      0.00051585      0.00051585
v  TempC                       21          71.601          21.068          21.068
v  TurbVisc           5.3582e-013       0.0047004      0.00059812      0.00059812
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               30:        0.24660E+01

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


 INSTANT    0.310000000E+02   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92189E-02 0.10308E+01
   Friction velocity        uk    :  0.92189E-02 0.10308E+01
   Dimensionless distance   yplus :  0.74218E-01 0.82989E+01
   Friction thermal sca.    tstar : -0.32295E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55375E-01 0.61919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37212E-02      37   0.24817E-02   0.34695E+02 0.35185E+03 
c  Velocity[X]                                      0.14651E+02 
c  Velocity[Y]                                      0.20044E+02 
c  Velocity[Z]                                      0.40937E-28 
c  Pressure     0.35101E-06     570   0.97953E-08   0.24930E+00 0.19948E+04 
c  nu_tilda     0.17185E-05      39   0.37229E-04   0.57022E-05 0.16573E+04 
c  TempC        0.16700E+02      32   0.11431E-02   0.37962E+02 0.80728E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.898          11.565          4.5729          4.5729
v  Velocity[Y]            -7.1601          9.6064      0.00012177      0.00012177
v  Velocity[Z]       -6.9287e-015     4.5443e-015     -5.908e-018     -5.908e-018
v  ǁVelocityǁ         0.0022436          12.104          4.6489          4.6489
v  Pressure               -100.56          30.396          6.0583          6.0583
v  nu_tilda           8.8139e-007       0.0039938      0.00051593      0.00051593
v  TempC                       21          71.595          21.069          21.069
v  TurbVisc           5.3393e-013       0.0047037       0.0005982       0.0005982
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               31:        0.32650E+01

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


 INSTANT    0.320000000E+02   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12113E-01 0.10281E+01
   Friction velocity        uk    :  0.12113E-01 0.10281E+01
   Dimensionless distance   yplus :  0.97515E-01 0.82768E+01
   Friction thermal sca.    tstar : -0.80291E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72757E-01 0.61754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37279E-02      37   0.25244E-02   0.34015E+02 0.34867E+03 
c  Velocity[X]                                      0.14347E+02 
c  Velocity[Y]                                      0.19668E+02 
c  Velocity[Z]                                      0.34185E-28 
c  Pressure     0.34117E-06     538   0.99250E-08   0.24382E+00 0.12982E+04 
c  nu_tilda     0.17331E-05      39   0.17949E-04   0.54966E-05 0.16236E+04 
c  TempC        0.16727E+02      32   0.86402E-03   0.37902E+02 0.79801E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9196           11.56          4.5729          4.5729
v  Velocity[Y]            -7.1075          9.5942      0.00012388      0.00012388
v  Velocity[Z]       -6.9287e-015     4.7593e-015    -6.5766e-018    -6.5766e-018
v  ǁVelocityǁ         0.0030296          12.092          4.6499          4.6499
v  Pressure               -100.55           30.24            5.97            5.97
v  nu_tilda           8.7941e-007       0.0039967      0.00051613      0.00051613
v  TempC                       21          71.588          21.071          21.071
v  TurbVisc           5.3093e-013        0.004707      0.00059829      0.00059829
v  total_pressure     1.0122e+005     1.0136e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               32:        0.32130E+01

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


 INSTANT    0.330000000E+02   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14446E-01 0.10270E+01
   Friction velocity        uk    :  0.14446E-01 0.10270E+01
   Dimensionless distance   yplus :  0.11630E+00 0.82678E+01
   Friction thermal sca.    tstar : -0.90007E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86771E-01 0.61687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37346E-02      37   0.23901E-02   0.33313E+02 0.34547E+03 
c  Velocity[X]                                      0.14043E+02 
c  Velocity[Y]                                      0.19269E+02 
c  Velocity[Z]                                      0.29158E-28 
c  Pressure     0.38461E-06     570   0.99375E-08   0.27232E+00 0.23267E+04 
c  nu_tilda     0.17476E-05      39   0.36808E-04   0.53061E-05 0.15917E+04 
c  TempC        0.16754E+02      32   0.10366E-02   0.35127E+02 0.76426E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9142          11.562          4.5729          4.5729
v  Velocity[Y]            -7.0516          9.5177      0.00012582      0.00012582
v  Velocity[Z]       -6.9287e-015     4.4985e-015    -7.1812e-018    -7.1812e-018
v  ǁVelocityǁ         0.0038135          12.073          4.6509          4.6509
v  Pressure                -99.89          29.788          5.8001          5.8001
v  nu_tilda           8.7798e-007       0.0039997      0.00051623      0.00051623
v  TempC                       21          71.582          21.072          21.072
v  TurbVisc           5.2619e-013       0.0047105       0.0005984       0.0005984
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               33:        0.26710E+01

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


 INSTANT    0.340000000E+02   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16474E-01 0.10242E+01
   Friction velocity        uk    :  0.16474E-01 0.10242E+01
   Dimensionless distance   yplus :  0.13263E+00 0.82453E+01
   Friction thermal sca.    tstar : -0.17395E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98957E-01 0.61519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37412E-02      37   0.22515E-02   0.32625E+02 0.34204E+03 
c  Velocity[X]                                      0.13673E+02 
c  Velocity[Y]                                      0.18953E+02 
c  Velocity[Z]                                      0.24439E-28 
c  Pressure     0.31985E-06     521   0.94293E-08   0.23421E+00 0.11060E+04 
c  nu_tilda     0.17619E-05      39   0.18154E-04   0.51273E-05 0.15613E+04 
c  TempC        0.16780E+02      32   0.13978E-02   0.36767E+02 0.77765E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9652          11.543          4.5729          4.5729
v  Velocity[Y]            -6.9941          9.5047       0.0001277       0.0001277
v  Velocity[Z]       -6.9287e-015     4.5445e-015    -7.7259e-018    -7.7259e-018
v  ǁVelocityǁ         0.0026708          12.034          4.6519          4.6519
v  Pressure               -99.477          29.704          5.7348          5.7348
v  nu_tilda           8.7752e-007       0.0040027      0.00051645      0.00051645
v  TempC                       21          71.584          21.073          21.073
v  TurbVisc           5.2277e-013        0.004714      0.00059852      0.00059852
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               34:        0.28120E+01

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


 INSTANT    0.350000000E+02   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72466E-02 0.10231E+01
   Friction velocity        uk    :  0.72466E-02 0.10231E+01
   Dimensionless distance   yplus :  0.58340E-01 0.82364E+01
   Friction thermal sca.    tstar : -0.10811E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43528E-01 0.61453E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37479E-02      37   0.23391E-02   0.31906E+02 0.33859E+03 
c  Velocity[X]                                      0.13304E+02 
c  Velocity[Y]                                      0.18603E+02 
c  Velocity[Z]                                      0.20529E-28 
c  Pressure     0.30030E-06     585   0.98562E-08   0.22162E+00 0.18545E+04 
c  nu_tilda     0.17762E-05      39   0.35060E-04   0.49608E-05 0.15323E+04 
c  TempC        0.16807E+02      32   0.10775E-02   0.43371E+02 0.85088E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9918          11.515          4.5729          4.5729
v  Velocity[Y]            -6.9392           9.473      0.00012962      0.00012962
v  Velocity[Z]       -6.9287e-015     4.1933e-015    -8.2215e-018    -8.2215e-018
v  ǁVelocityǁ         0.0038014          11.979           4.653           4.653
v  Pressure               -99.229          29.405          5.6015          5.6015
v  nu_tilda           8.7756e-007       0.0040057      0.00051658      0.00051658
v  TempC                       21          71.589          21.074          21.074
v  TurbVisc           5.2167e-013       0.0047175      0.00059867      0.00059867
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               35:        0.31010E+01

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


 INSTANT    0.360000000E+02   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82926E-02 0.10204E+01
   Friction velocity        uk    :  0.82926E-02 0.10204E+01
   Dimensionless distance   yplus :  0.66761E-01 0.82147E+01
   Friction thermal sca.    tstar : -0.11798E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49811E-01 0.61291E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37545E-02      37   0.22969E-02   0.31314E+02 0.33563E+03 
c  Velocity[X]                                      0.13058E+02 
c  Velocity[Y]                                      0.18257E+02 
c  Velocity[Z]                                      0.18269E-28 
c  Pressure     0.32507E-06     566   0.91482E-08   0.24473E+00 0.16402E+04 
c  nu_tilda     0.17903E-05      39   0.18163E-04   0.48040E-05 0.15047E+04 
c  TempC        0.16834E+02      31   0.89186E-03   0.35169E+02 0.77026E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9945          11.543          4.5729          4.5729
v  Velocity[Y]            -6.8819          9.4124      0.00013131      0.00013131
v  Velocity[Z]       -6.9287e-015     4.1065e-015    -8.6702e-018    -8.6702e-018
v  ǁVelocityǁ         0.0045034          11.945           4.654           4.654
v  Pressure               -98.482          29.104          5.4989          5.4989
v  nu_tilda           8.7847e-007       0.0040087      0.00051683      0.00051683
v  TempC                       21           71.59          21.075          21.075
v  TurbVisc           5.2176e-013       0.0047211      0.00059882      0.00059882
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               36:        0.30470E+01

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


 INSTANT    0.370000000E+02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19832E-01 0.10170E+01
   Friction velocity        uk    :  0.19832E-01 0.10170E+01
   Dimensionless distance   yplus :  0.15966E+00 0.81873E+01
   Friction thermal sca.    tstar : -0.12110E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11912E+00 0.61087E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37611E-02      37   0.22096E-02   0.30681E+02 0.33248E+03 
c  Velocity[X]                                      0.12733E+02 
c  Velocity[Y]                                      0.17948E+02 
c  Velocity[Z]                                      0.15430E-28 
c  Pressure     0.28849E-06     568   0.99534E-08   0.21700E+00 0.14741E+04 
c  nu_tilda     0.18042E-05      39   0.33781E-04   0.46570E-05 0.14782E+04 
c  TempC        0.16860E+02      31   0.11087E-02   0.32303E+02 0.74643E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9894          11.531          4.5729          4.5729
v  Velocity[Y]            -6.8304          9.3952      0.00013308      0.00013308
v  Velocity[Z]       -6.9287e-015     3.6506e-015    -9.0814e-018    -9.0814e-018
v  ǁVelocityǁ         0.0051674          11.924           4.655           4.655
v  Pressure               -97.715          28.936          5.3951          5.3951
v  nu_tilda           8.7801e-007       0.0040118      0.00051699      0.00051699
v  TempC                       21          71.591          21.076          21.076
v  TurbVisc           5.2394e-013       0.0047247        0.000599        0.000599
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               37:        0.28500E+01

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


 INSTANT    0.380000000E+02   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20771E-01 0.10159E+01
   Friction velocity        uk    :  0.20771E-01 0.10159E+01
   Dimensionless distance   yplus :  0.16722E+00 0.81783E+01
   Friction thermal sca.    tstar : -0.67945E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12476E+00 0.61019E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37676E-02      37   0.21901E-02   0.30093E+02 0.32940E+03 
c  Velocity[X]                                      0.12457E+02 
c  Velocity[Y]                                      0.17637E+02 
c  Velocity[Z]                                      0.12747E-28 
c  Pressure     0.31353E-06     569   0.97955E-08   0.23410E+00 0.17213E+04 
c  nu_tilda     0.18181E-05      39   0.18093E-04   0.45187E-05 0.14528E+04 
c  TempC        0.16887E+02      31   0.10617E-02   0.34307E+02 0.76005E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0272          11.519          4.5729          4.5729
v  Velocity[Y]             -6.781          9.3289      0.00013483      0.00013483
v  Velocity[Z]       -6.9287e-015     3.4486e-015    -9.4578e-018    -9.4578e-018
v  ǁVelocityǁ         0.0056767          11.898           4.656           4.656
v  Pressure                 -97.3          28.624          5.2886          5.2886
v  nu_tilda           8.7782e-007       0.0040148      0.00051726      0.00051726
v  TempC                       21           71.59          21.077          21.077
v  TurbVisc           5.2284e-013       0.0047282      0.00059918      0.00059918
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               38:        0.30830E+01

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


 INSTANT    0.390000000E+02   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18190E-01 0.10132E+01
   Friction velocity        uk    :  0.18190E-01 0.10132E+01
   Dimensionless distance   yplus :  0.14644E+00 0.81571E+01
   Friction thermal sca.    tstar : -0.34306E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10926E+00 0.60861E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37741E-02      37   0.21733E-02   0.29568E+02 0.32661E+03 
c  Velocity[X]                                      0.12242E+02 
c  Velocity[Y]                                      0.17326E+02 
c  Velocity[Z]                                      0.11576E-28 
c  Pressure     0.27648E-06     553   0.96606E-08   0.21029E+00 0.14589E+04 
c  nu_tilda     0.18318E-05      39   0.34560E-04   0.43882E-05 0.14284E+04 
c  TempC        0.16913E+02      31   0.10023E-02   0.32175E+02 0.74377E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0388          11.492          4.5729          4.5729
v  Velocity[Y]             -6.731          9.3229      0.00013661      0.00013661
v  Velocity[Z]       -6.9287e-015     3.4438e-015    -9.8025e-018    -9.8025e-018
v  ǁVelocityǁ         0.0048339          11.857           4.657           4.657
v  Pressure               -97.082          28.471          5.1878          5.1878
v  nu_tilda           8.7635e-007       0.0040178      0.00051744      0.00051744
v  TempC                       21          71.592          21.078          21.078
v  TurbVisc           5.2239e-013       0.0047318      0.00059939      0.00059939
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               39:        0.28150E+01

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


 INSTANT    0.400000000E+02   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19516E-01 0.10125E+01
   Friction velocity        uk    :  0.19516E-01 0.10125E+01
   Dimensionless distance   yplus :  0.15712E+00 0.81513E+01
   Friction thermal sca.    tstar : -0.56248E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11723E+00 0.60818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37806E-02      37   0.20888E-02   0.28951E+02 0.32353E+03 
c  Velocity[X]                                      0.11889E+02 
c  Velocity[Y]                                      0.17062E+02 
c  Velocity[Z]                                      0.10304E-28 
c  Pressure     0.28821E-06     551   0.93314E-08   0.21950E+00 0.13684E+04 
c  nu_tilda     0.18454E-05      38   0.17832E-04   0.42651E-05 0.14050E+04 
c  TempC        0.16940E+02      31   0.98193E-03   0.33021E+02 0.75043E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0325          11.466          4.5729          4.5729
v  Velocity[Y]            -6.6797          9.3012       0.0001382       0.0001382
v  Velocity[Z]       -6.9287e-015      3.764e-015    -1.0119e-017    -1.0119e-017
v  ǁVelocityǁ         0.0036305          11.834          4.6581          4.6581
v  Pressure               -96.462          28.273          5.1078          5.1078
v  nu_tilda           8.7562e-007       0.0040208      0.00051774      0.00051774
v  TempC                       21          71.595          21.079          21.079
v  TurbVisc            5.189e-013       0.0047354      0.00059961      0.00059961
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               40:        0.27450E+01

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


 INSTANT    0.410000000E+02   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15303E-01 0.10101E+01
   Friction velocity        uk    :  0.15303E-01 0.10101E+01
   Dimensionless distance   yplus :  0.12320E+00 0.81317E+01
   Friction thermal sca.    tstar : -0.82254E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91919E-01 0.60671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37871E-02      37   0.20196E-02   0.28406E+02 0.32053E+03 
c  Velocity[X]                                      0.11668E+02 
c  Velocity[Y]                                      0.16737E+02 
c  Velocity[Z]                                      0.84896E-29 
c  Pressure     0.27889E-06     599   0.91222E-08   0.21885E+00 0.19710E+04 
c  nu_tilda     0.18589E-05      38   0.36034E-04   0.41484E-05 0.13825E+04 
c  TempC        0.16966E+02      31   0.11367E-02   0.31996E+02 0.73435E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0215          11.472          4.5729          4.5729
v  Velocity[Y]            -6.6309          9.2346      0.00014024      0.00014024
v  Velocity[Z]       -6.9287e-015     3.4979e-015    -1.0412e-017    -1.0412e-017
v  ǁVelocityǁ         0.0025083          11.811          4.6591          4.6591
v  Pressure               -96.015          27.956          4.9778          4.9778
v  nu_tilda           8.7593e-007       0.0040238      0.00051794      0.00051794
v  TempC                       21          71.597           21.08           21.08
v  TurbVisc           5.1715e-013       0.0047389      0.00059984      0.00059984
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               41:        0.28040E+01

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


 INSTANT    0.420000000E+02   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86664E-02 0.10063E+01
   Friction velocity        uk    :  0.86664E-02 0.10063E+01
   Dimensionless distance   yplus :  0.69770E-01 0.81018E+01
   Friction thermal sca.    tstar : -0.20780E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52056E-01 0.60448E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37935E-02      37   0.21279E-02   0.27875E+02 0.31777E+03 
c  Velocity[X]                                      0.11435E+02 
c  Velocity[Y]                                      0.16440E+02 
c  Velocity[Z]                                      0.90995E-29 
c  Pressure     0.25152E-06     537   0.93420E-08   0.19266E+00 0.11290E+04 
c  nu_tilda     0.18722E-05      38   0.17493E-04   0.40380E-05 0.13609E+04 
c  TempC        0.16993E+02      31   0.85392E-03   0.36058E+02 0.75990E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.047          11.466          4.5729          4.5729
v  Velocity[Y]            -6.5815          9.2263      0.00014214      0.00014214
v  Velocity[Z]       -6.9287e-015     3.7539e-015    -1.0679e-017    -1.0679e-017
v  ǁVelocityǁ         0.0018831          11.788          4.6601          4.6601
v  Pressure               -95.641          27.833          4.9197          4.9197
v  nu_tilda           8.7621e-007       0.0040268      0.00051825      0.00051825
v  TempC                       21          71.709          21.081          21.081
v  TurbVisc           5.1789e-013       0.0047424      0.00060008      0.00060008
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               42:        0.26530E+01

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


 INSTANT    0.430000000E+02   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97399E-02 0.10058E+01
   Friction velocity        uk    :  0.97399E-02 0.10058E+01
   Dimensionless distance   yplus :  0.78413E-01 0.80976E+01
   Friction thermal sca.    tstar : -0.95368E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58505E-01 0.60417E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37999E-02      36   0.20611E-02   0.27484E+02 0.31562E+03 
c  Velocity[X]                                      0.11277E+02 
c  Velocity[Y]                                      0.16208E+02 
c  Velocity[Z]                                      0.74984E-29 
c  Pressure     0.26192E-06     586   0.92589E-08   0.20379E+00 0.18887E+04 
c  nu_tilda     0.18854E-05      38   0.37060E-04   0.39330E-05 0.13400E+04 
c  TempC        0.17019E+02      31   0.10973E-02   0.31440E+02 0.71424E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0491          11.451          4.5729          4.5729
v  Velocity[Y]            -6.5353          9.1672       0.0001442       0.0001442
v  Velocity[Z]       -6.9287e-015     3.4582e-015    -1.0928e-017    -1.0928e-017
v  ǁVelocityǁ         0.0024707          11.755          4.6611          4.6611
v  Pressure               -95.005          27.534          4.7993          4.7993
v  nu_tilda           8.7628e-007       0.0040297      0.00051846      0.00051846
v  TempC                       21          73.998          21.083          21.083
v  TurbVisc           5.1855e-013       0.0047459      0.00060033      0.00060033
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               43:        0.28970E+01

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


 INSTANT    0.440000000E+02   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69939E-02 0.10034E+01
   Friction velocity        uk    :  0.69939E-02 0.10034E+01
   Dimensionless distance   yplus :  0.56306E-01 0.80781E+01
   Friction thermal sca.    tstar : -0.45927E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42011E-01 0.60272E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38062E-02      36   0.18950E-02   0.26949E+02 0.31257E+03 
c  Velocity[X]                                      0.11030E+02 
c  Velocity[Y]                                      0.15918E+02 
c  Velocity[Z]                                      0.61613E-29 
c  Pressure     0.23391E-06     505   0.95796E-08   0.18054E+00 0.10420E+04 
c  nu_tilda     0.18986E-05      38   0.17184E-04   0.38334E-05 0.13199E+04 
c  TempC        0.17046E+02      31   0.11290E-02   0.32964E+02 0.72365E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0352          11.438          4.5729          4.5729
v  Velocity[Y]            -6.4836          9.1656      0.00014655      0.00014655
v  Velocity[Z]       -6.9287e-015     3.6893e-015    -1.1157e-017    -1.1157e-017
v  ǁVelocityǁ         0.0035099           11.72          4.6622          4.6622
v  Pressure                -94.25          27.442           4.752           4.752
v  nu_tilda           8.7534e-007       0.0040326       0.0005188       0.0005188
v  TempC                       21          71.599          21.084          21.084
v  TurbVisc           5.1873e-013       0.0047494      0.00060059      0.00060059
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               44:        0.26190E+01

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


 INSTANT    0.450000000E+02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47797E-02 0.10034E+01
   Friction velocity        uk    :  0.47797E-02 0.10034E+01
   Dimensionless distance   yplus :  0.38480E-01 0.80783E+01
   Friction thermal sca.    tstar : -0.23016E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28710E-01 0.60273E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38126E-02      36   0.20469E-02   0.26413E+02 0.30967E+03 
c  Velocity[X]                                      0.10765E+02 
c  Velocity[Y]                                      0.15647E+02 
c  Velocity[Z]                                      0.58351E-29 
c  Pressure     0.23408E-06     569   0.96202E-08   0.18442E+00 0.18303E+04 
c  nu_tilda     0.19116E-05      38   0.37553E-04   0.37384E-05 0.13004E+04 
c  TempC        0.17072E+02      31   0.10138E-02   0.30987E+02 0.71464E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0258          11.408          4.5729          4.5729
v  Velocity[Y]            -6.4435           9.115      0.00014874      0.00014874
v  Velocity[Z]       -6.9287e-015     3.4123e-015    -1.1371e-017    -1.1371e-017
v  ǁVelocityǁ         0.0049915          11.699          4.6632          4.6632
v  Pressure               -93.866          27.163          4.6385          4.6385
v  nu_tilda           8.7419e-007       0.0040355      0.00051902      0.00051902
v  TempC                       21          72.898          21.085          21.085
v  TurbVisc            5.165e-013       0.0047528      0.00060086      0.00060086
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               45:        0.30470E+01

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


 INSTANT    0.460000000E+02   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15665E-01 0.10014E+01
   Friction velocity        uk    :  0.15665E-01 0.10014E+01
   Dimensionless distance   yplus :  0.12611E+00 0.80617E+01
   Friction thermal sca.    tstar : -0.82052E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94094E-01 0.60149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38189E-02      36   0.19116E-02   0.26037E+02 0.30761E+03 
c  Velocity[X]                                      0.10599E+02 
c  Velocity[Y]                                      0.15438E+02 
c  Velocity[Z]                                      0.60855E-29 
c  Pressure     0.23826E-06     488   0.98638E-08   0.18807E+00 0.96407E+03 
c  nu_tilda     0.19244E-05      38   0.16770E-04   0.36480E-05 0.12816E+04 
c  TempC        0.17098E+02      31   0.93151E-03   0.32443E+02 0.71431E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0413          11.384          4.5729          4.5729
v  Velocity[Y]            -6.3968          9.1162      0.00015066      0.00015066
v  Velocity[Z]       -6.9287e-015     3.6082e-015    -1.1568e-017    -1.1568e-017
v  ǁVelocityǁ          0.006213          11.668          4.6642          4.6642
v  Pressure               -93.354          27.097           4.601           4.601
v  nu_tilda           8.7202e-007       0.0040383      0.00051936      0.00051936
v  TempC                       21          73.949          21.086          21.086
v  TurbVisc            5.138e-013       0.0047562      0.00060114      0.00060114
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               46:        0.23740E+01

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


 INSTANT    0.470000000E+02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23849E-01 0.10011E+01
   Friction velocity        uk    :  0.23849E-01 0.10011E+01
   Dimensionless distance   yplus :  0.19200E+00 0.80599E+01
   Friction thermal sca.    tstar : -0.92940E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14325E+00 0.60136E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38251E-02      36   0.19283E-02   0.25592E+02 0.30503E+03 
c  Velocity[X]                                      0.10432E+02 
c  Velocity[Y]                                      0.15160E+02 
c  Velocity[Z]                                      0.49690E-29 
c  Pressure     0.25425E-06     554   0.97158E-08   0.19706E+00 0.16956E+04 
c  nu_tilda     0.19372E-05      38   0.37620E-04   0.35616E-05 0.12634E+04 
c  TempC        0.17124E+02      31   0.11262E-02   0.30364E+02 0.68540E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0371          11.379          4.5729          4.5729
v  Velocity[Y]            -6.3522          9.0913      0.00015309      0.00015309
v  Velocity[Z]       -6.9287e-015     3.3355e-015    -1.1751e-017    -1.1751e-017
v  ǁVelocityǁ         0.0070262          11.641          4.6652          4.6652
v  Pressure               -92.656          26.856          4.4982          4.4982
v  nu_tilda           8.6995e-007       0.0040411       0.0005196       0.0005196
v  TempC                       21          71.613          21.087          21.087
v  TurbVisc           5.0872e-013       0.0047596      0.00060143      0.00060143
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               47:        0.34120E+01

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


 INSTANT    0.480000000E+02   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11372E-01 0.99939E+00
   Friction velocity        uk    :  0.11372E-01 0.99939E+00
   Dimensionless distance   yplus :  0.91550E-01 0.80458E+01
   Friction thermal sca.    tstar : -0.17439E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68306E-01 0.60030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38314E-02      36   0.18851E-02   0.25229E+02 0.30293E+03 
c  Velocity[X]                                      0.10326E+02 
c  Velocity[Y]                                      0.14903E+02 
c  Velocity[Z]                                      0.45224E-29 
c  Pressure     0.24867E-06     522   0.98329E-08   0.19674E+00 0.12524E+04 
c  nu_tilda     0.19499E-05      38   0.16050E-04   0.34791E-05 0.12458E+04 
c  TempC        0.17150E+02      31   0.85213E-03   0.31804E+02 0.70783E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.018          11.384          4.5729          4.5729
v  Velocity[Y]            -6.3096          9.0311      0.00015527      0.00015527
v  Velocity[Z]       -6.9287e-015     3.5158e-015    -1.1919e-017    -1.1919e-017
v  ǁVelocityǁ         0.0060788          11.619          4.6662          4.6662
v  Pressure               -91.895           26.67          4.4398          4.4398
v  nu_tilda           8.7104e-007       0.0040439      0.00051996      0.00051996
v  TempC                   20.957          73.981          21.088          21.088
v  TurbVisc            5.039e-013       0.0047629      0.00060173      0.00060173
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               48:        0.26590E+01

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


 INSTANT    0.490000000E+02   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15798E-01 0.99797E+00
   Friction velocity        uk    :  0.15798E-01 0.99797E+00
   Dimensionless distance   yplus :  0.12718E+00 0.80343E+01
   Friction thermal sca.    tstar : -0.22818E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94893E-01 0.59945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38376E-02      36   0.18193E-02   0.24767E+02 0.30035E+03 
c  Velocity[X]                                      0.10069E+02 
c  Velocity[Y]                                      0.14698E+02 
c  Velocity[Z]                                      0.46313E-29 
c  Pressure     0.21835E-06     534   0.97474E-08   0.17148E+00 0.13523E+04 
c  nu_tilda     0.19624E-05      38   0.37384E-04   0.34002E-05 0.12287E+04 
c  TempC        0.17176E+02      31   0.91622E-03   0.29992E+02 0.68247E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.003          11.364          4.5729          4.5729
v  Velocity[Y]            -6.2647          9.0297      0.00015754      0.00015754
v  Velocity[Z]       -6.9287e-015     3.3638e-015    -1.2079e-017    -1.2079e-017
v  ǁVelocityǁ           0.00464           11.59          4.6673          4.6673
v  Pressure               -91.521           26.53            4.36            4.36
v  nu_tilda           8.7181e-007       0.0040467      0.00052021      0.00052021
v  TempC                   20.928          73.509          21.089          21.089
v  TurbVisc           5.0643e-013       0.0047662      0.00060204      0.00060204
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               49:        0.28210E+01

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


 INSTANT    0.500000000E+02   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13025E-01 0.99703E+00
   Friction velocity        uk    :  0.13025E-01 0.99703E+00
   Dimensionless distance   yplus :  0.10486E+00 0.80268E+01
   Friction thermal sca.    tstar : -0.55253E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78239E-01 0.59889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38437E-02      36   0.18188E-02   0.24317E+02 0.29781E+03 
c  Velocity[X]                                      0.98787E+01 
c  Velocity[Y]                                      0.14438E+02 
c  Velocity[Z]                                      0.42618E-29 
c  Pressure     0.22376E-06     505   0.99130E-08   0.17932E+00 0.12064E+04 
c  nu_tilda     0.19748E-05      38   0.15208E-04   0.33247E-05 0.12122E+04 
c  TempC        0.17202E+02      31   0.79367E-03   0.30869E+02 0.67858E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0105          11.342          4.5729          4.5729
v  Velocity[Y]            -6.2231          8.9877      0.00016006      0.00016006
v  Velocity[Z]       -6.9287e-015     3.4582e-015    -1.2229e-017    -1.2229e-017
v  ǁVelocityǁ         0.0034452          11.565          4.6683          4.6683
v  Pressure               -90.961          26.359          4.3059          4.3059
v  nu_tilda           8.7186e-007       0.0040494      0.00052058      0.00052058
v  TempC                       21          71.642           21.09           21.09
v  TurbVisc           5.0821e-013       0.0047694      0.00060235      0.00060235
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               50:        0.32220E+01

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


 INSTANT    0.510000000E+02   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24189E-02 0.99750E+00
   Friction velocity        uk    :  0.24189E-02 0.99750E+00
   Dimensionless distance   yplus :  0.19474E-01 0.80306E+01
   Friction thermal sca.    tstar : -0.72380E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14530E-01 0.59917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38499E-02      36   0.18977E-02   0.23948E+02 0.29559E+03 
c  Velocity[X]                                      0.97484E+01 
c  Velocity[Y]                                      0.14199E+02 
c  Velocity[Z]                                      0.38057E-29 
c  Pressure     0.21216E-06     522   0.93910E-08   0.16755E+00 0.12977E+04 
c  nu_tilda     0.19872E-05      38   0.36954E-04   0.32524E-05 0.11961E+04 
c  TempC        0.17228E+02      31   0.93922E-03   0.27377E+02 0.65162E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.0018          11.314          4.5729          4.5729
v  Velocity[Y]            -6.1821          8.9939      0.00016246      0.00016246
v  Velocity[Z]       -6.9287e-015     3.4401e-015    -1.2371e-017    -1.2371e-017
v  ǁVelocityǁ         0.0040587          11.544          4.6693          4.6693
v  Pressure               -90.425          26.229          4.2311          4.2311
v  nu_tilda           8.7213e-007       0.0040521      0.00052084      0.00052084
v  TempC                       21          74.552          21.092          21.092
v  TurbVisc           5.0834e-013       0.0047726      0.00060268      0.00060268
v  total_pressure     1.0123e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               51:        0.24220E+01

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


 INSTANT    0.520000000E+02   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81043E-02 0.99696E+00
   Friction velocity        uk    :  0.81043E-02 0.99696E+00
   Dimensionless distance   yplus :  0.65245E-01 0.80262E+01
   Friction thermal sca.    tstar : -0.80581E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48680E-01 0.59884E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38560E-02      36   0.18167E-02   0.23684E+02 0.29397E+03 
c  Velocity[X]                                      0.96469E+01 
c  Velocity[Y]                                      0.14037E+02 
c  Velocity[Z]                                      0.35421E-29 
c  Pressure     0.26113E-06     537   0.93456E-08   0.20330E+00 0.13931E+04 
c  nu_tilda     0.19994E-05      38   0.14263E-04   0.31829E-05 0.11806E+04 
c  TempC        0.17254E+02      31   0.12653E-02   0.28842E+02 0.65280E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9802           11.29          4.5729          4.5729
v  Velocity[Y]            -6.1418          8.9337      0.00016462      0.00016462
v  Velocity[Z]       -6.9287e-015     3.5554e-015    -1.2501e-017    -1.2501e-017
v  ǁVelocityǁ         0.0068221          11.521          4.6703          4.6703
v  Pressure               -89.825          26.007          4.1675          4.1675
v  nu_tilda             8.73e-007       0.0040547      0.00052122      0.00052122
v  TempC                       21          73.799          21.093          21.093
v  TurbVisc           5.0897e-013       0.0047758      0.00060301      0.00060301
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               52:        0.23610E+01

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


 INSTANT    0.530000000E+02   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13965E-01 0.99562E+00
   Friction velocity        uk    :  0.13965E-01 0.99562E+00
   Dimensionless distance   yplus :  0.11243E+00 0.80154E+01
   Friction thermal sca.    tstar : -0.12594E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83882E-01 0.59804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38620E-02      36   0.16022E-02   0.23244E+02 0.29136E+03 
c  Velocity[X]                                      0.94748E+01 
c  Velocity[Y]                                      0.13769E+02 
c  Velocity[Z]                                      0.41583E-29 
c  Pressure     0.22450E-06     522   0.95855E-08   0.17723E+00 0.11230E+04 
c  nu_tilda     0.20115E-05      38   0.36393E-04   0.31164E-05 0.11654E+04 
c  TempC        0.17279E+02      31   0.11584E-02   0.31528E+02 0.67911E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9651          11.283          4.5729          4.5729
v  Velocity[Y]            -6.1006          8.9456       0.0001672       0.0001672
v  Velocity[Z]       -6.9287e-015     3.4944e-015    -1.2622e-017    -1.2622e-017
v  ǁVelocityǁ          0.008066          11.494          4.6713          4.6713
v  Pressure                -89.53          25.943          4.1063          4.1063
v  nu_tilda           8.7422e-007       0.0040573      0.00052149      0.00052149
v  TempC                       21           72.46          21.094          21.094
v  TurbVisc           5.1101e-013       0.0047789      0.00060335      0.00060335
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               53:        0.23510E+01

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


 INSTANT    0.540000000E+02   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17430E-01 0.99467E+00
   Friction velocity        uk    :  0.17430E-01 0.99467E+00
   Dimensionless distance   yplus :  0.14033E+00 0.80078E+01
   Friction thermal sca.    tstar : -0.14043E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10470E+00 0.59747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38681E-02      36   0.17532E-02   0.22814E+02 0.28886E+03 
c  Velocity[X]                                      0.92626E+01 
c  Velocity[Y]                                      0.13551E+02 
c  Velocity[Z]                                      0.30051E-29 
c  Pressure     0.20254E-06     503   0.91739E-08   0.16171E+00 0.95649E+03 
c  nu_tilda     0.20235E-05      38   0.13602E-04   0.30523E-05 0.11507E+04 
c  TempC        0.17305E+02      31   0.92568E-03   0.29419E+02 0.65652E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9688          11.273          4.5729          4.5729
v  Velocity[Y]            -6.0646          8.9392      0.00016968      0.00016968
v  Velocity[Z]       -6.9287e-015     3.6508e-015    -1.2735e-017    -1.2735e-017
v  ǁVelocityǁ         0.0056269          11.475          4.6723          4.6723
v  Pressure               -88.998          25.853          4.0715          4.0715
v  nu_tilda           8.7634e-007       0.0040599      0.00052189      0.00052189
v  TempC                       21          75.114          21.095          21.095
v  TurbVisc           5.1387e-013       0.0047819      0.00060369      0.00060369
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               54:        0.33980E+01

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


 INSTANT    0.550000000E+02   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14310E-01 0.99490E+00
   Friction velocity        uk    :  0.14310E-01 0.99490E+00
   Dimensionless distance   yplus :  0.11520E+00 0.80096E+01
   Friction thermal sca.    tstar : -0.94584E+02 0.32660E+00
   Rough dim-less th. sca.  tplus :  0.85956E-01 0.59761E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38742E-02      36   0.16678E-02   0.22549E+02 0.28726E+03 
c  Velocity[X]                                      0.91559E+01 
c  Velocity[Y]                                      0.13393E+02 
c  Velocity[Z]                                      0.32701E-29 
c  Pressure     0.22808E-06     553   0.95647E-08   0.18452E+00 0.17443E+04 
c  nu_tilda     0.20354E-05      38   0.35762E-04   0.29909E-05 0.11364E+04 
c  TempC        0.17331E+02      31   0.10568E-02   0.28429E+02 0.64522E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9578          11.258          4.5729          4.5729
v  Velocity[Y]            -6.0236          8.8894       0.0001721       0.0001721
v  Velocity[Z]       -6.9287e-015     3.5506e-015    -1.2841e-017    -1.2841e-017
v  ǁVelocityǁ         0.0033266          11.447          4.6733          4.6733
v  Pressure               -88.409          25.603          3.9734          3.9734
v  nu_tilda           8.7886e-007       0.0040624      0.00052217      0.00052217
v  TempC                   20.998          74.157          21.096          21.096
v  TurbVisc           5.1887e-013        0.004785      0.00060405      0.00060405
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               55:        0.30180E+01

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


 INSTANT    0.560000000E+02   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93056E-02 0.99422E+00
   Friction velocity        uk    :  0.93056E-02 0.99422E+00
   Dimensionless distance   yplus :  0.74916E-01 0.80041E+01
   Friction thermal sca.    tstar : -0.62711E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55896E-01 0.59720E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38801E-02      36   0.17321E-02   0.22168E+02 0.28508E+03 
c  Velocity[X]                                      0.90064E+01 
c  Velocity[Y]                                      0.13162E+02 
c  Velocity[Z]                                      0.28690E-29 
c  Pressure     0.22249E-06     473   0.99762E-08   0.17627E+00 0.91672E+03 
c  nu_tilda     0.20473E-05      38   0.13187E-04   0.29318E-05 0.11225E+04 
c  TempC        0.17356E+02      31   0.10859E-02   0.34214E+02 0.69138E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9373          11.246          4.5729          4.5729
v  Velocity[Y]            -5.9897          8.8921      0.00017441      0.00017441
v  Velocity[Z]       -6.9287e-015     3.5479e-015    -1.2934e-017    -1.2934e-017
v  ǁVelocityǁ         0.0027547          11.431          4.6743          4.6743
v  Pressure               -87.918          25.543          3.9416          3.9416
v  nu_tilda           8.8125e-007       0.0040649      0.00052259      0.00052259
v  TempC                       21          73.106          21.097          21.097
v  TurbVisc           5.2486e-013        0.004788      0.00060441      0.00060441
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               56:        0.23420E+01

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


 INSTANT    0.570000000E+02   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35882E-02 0.99293E+00
   Friction velocity        uk    :  0.35882E-02 0.99293E+00
   Dimensionless distance   yplus :  0.28887E-01 0.79938E+01
   Friction thermal sca.    tstar : -0.18215E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21553E-01 0.59643E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38861E-02      36   0.17080E-02   0.21890E+02 0.28312E+03 
c  Velocity[X]                                      0.89443E+01 
c  Velocity[Y]                                      0.12945E+02 
c  Velocity[Z]                                      0.38953E-29 
c  Pressure     0.25528E-06     538   0.98201E-08   0.19831E+00 0.17785E+04 
c  nu_tilda     0.20590E-05      38   0.35176E-04   0.28748E-05 0.11090E+04 
c  TempC        0.17382E+02      31   0.86944E-03   0.31068E+02 0.65923E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9163          11.223          4.5729          4.5729
v  Velocity[Y]            -5.9477          8.8433      0.00017703      0.00017703
v  Velocity[Z]       -6.9287e-015     3.5737e-015    -1.3021e-017    -1.3021e-017
v  ǁVelocityǁ         0.0032192          11.414          4.6752          4.6752
v  Pressure               -87.469          25.282           3.843           3.843
v  nu_tilda           8.8377e-007       0.0040674      0.00052288      0.00052288
v  TempC                       21          75.572          21.099          21.099
v  TurbVisc            5.306e-013       0.0047909      0.00060479      0.00060479
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               57:        0.27090E+01

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


 INSTANT    0.580000000E+02   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18029E-01 0.99162E+00
   Friction velocity        uk    :  0.18029E-01 0.99162E+00
   Dimensionless distance   yplus :  0.14515E+00 0.79832E+01
   Friction thermal sca.    tstar : -0.13585E+03 0.16630E+01
   Rough dim-less th. sca.  tplus :  0.10830E+00 0.59564E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38921E-02      36   0.16134E-02   0.21538E+02 0.28107E+03 
c  Velocity[X]                                      0.87519E+01 
c  Velocity[Y]                                      0.12786E+02 
c  Velocity[Z]                                      0.27614E-29 
c  Pressure     0.22693E-06     441   0.97325E-08   0.18139E+00 0.81922E+03 
c  nu_tilda     0.20706E-05      38   0.12858E-04   0.28199E-05 0.10958E+04 
c  TempC        0.17407E+02      31   0.10051E-02   0.29521E+02 0.62176E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9175            11.2          4.5729          4.5729
v  Velocity[Y]            -5.9157          8.8508      0.00017948      0.00017948
v  Velocity[Z]       -6.9287e-015     3.7952e-015      -1.31e-017      -1.31e-017
v  ǁVelocityǁ         0.0048983          11.391          4.6762          4.6762
v  Pressure                -87.02          25.297          3.8268          3.8268
v  nu_tilda           8.8559e-007       0.0040698      0.00052331      0.00052331
v  TempC                       21          74.696            21.1            21.1
v  TurbVisc            5.367e-013       0.0047938      0.00060516      0.00060516
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               58:        0.23750E+01

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


 INSTANT    0.590000000E+02   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12973E-01 0.99169E+00
   Friction velocity        uk    :  0.12973E-01 0.99169E+00
   Dimensionless distance   yplus :  0.10444E+00 0.79838E+01
   Friction thermal sca.    tstar : -0.26843E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77927E-01 0.59568E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38980E-02      36   0.16435E-02   0.21134E+02 0.27862E+03 
c  Velocity[X]                                      0.85814E+01 
c  Velocity[Y]                                      0.12553E+02 
c  Velocity[Z]                                      0.26580E-29 
c  Pressure     0.22986E-06     566   0.96812E-08   0.18367E+00 0.18863E+04 
c  nu_tilda     0.20821E-05      38   0.34723E-04   0.27671E-05 0.10830E+04 
c  TempC        0.17432E+02      31   0.97282E-03   0.29466E+02 0.63693E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9046           11.18          4.5729          4.5729
v  Velocity[Y]            -5.8759          8.8136      0.00018219      0.00018219
v  Velocity[Z]       -6.9287e-015     3.6111e-015     -1.317e-017     -1.317e-017
v  ǁVelocityǁ         0.0033131          11.368          4.6772          4.6772
v  Pressure               -86.456          25.027          3.7229          3.7229
v  nu_tilda           8.8771e-007       0.0040722      0.00052361      0.00052361
v  TempC                       21          73.213          21.101          21.101
v  TurbVisc           5.4113e-013       0.0047967      0.00060555      0.00060555
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               59:        0.29760E+01

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


 INSTANT    0.600000000E+02   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65440E-02 0.99089E+00
   Friction velocity        uk    :  0.65440E-02 0.99089E+00
   Dimensionless distance   yplus :  0.52684E-01 0.79773E+01
   Friction thermal sca.    tstar : -0.85479E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39308E-01 0.59520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39039E-02      36   0.15946E-02   0.20878E+02 0.27695E+03 
c  Velocity[X]                                      0.85150E+01 
c  Velocity[Y]                                      0.12363E+02 
c  Velocity[Z]                                      0.35609E-29 
c  Pressure     0.22100E-06     409   0.92196E-08   0.17788E+00 0.79116E+03 
c  nu_tilda     0.20936E-05      38   0.12659E-04   0.27160E-05 0.10704E+04 
c  TempC        0.17457E+02      31   0.96150E-03   0.28439E+02 0.62164E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8836          11.176          4.5729          4.5729
v  Velocity[Y]             -5.845          8.8273      0.00018459      0.00018459
v  Velocity[Z]       -6.9287e-015      3.574e-015    -1.3232e-017    -1.3232e-017
v  ǁVelocityǁ          0.005309          11.344          4.6781          4.6781
v  Pressure               -85.921           25.04            3.71            3.71
v  nu_tilda           8.8615e-007       0.0040746      0.00052405      0.00052405
v  TempC                       21          75.407          21.102          21.102
v  TurbVisc           5.4632e-013       0.0047995      0.00060594      0.00060594
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               60:        0.24790E+01

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


 INSTANT    0.610000000E+02   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20151E-01 0.98957E+00
   Friction velocity        uk    :  0.20151E-01 0.98957E+00
   Dimensionless distance   yplus :  0.16223E+00 0.79667E+01
   Friction thermal sca.    tstar : -0.65350E+02 0.21908E+01
   Rough dim-less th. sca.  tplus :  0.12104E+00 0.59441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39098E-02      36   0.16902E-02   0.20606E+02 0.27521E+03 
c  Velocity[X]                                      0.83789E+01 
c  Velocity[Y]                                      0.12227E+02 
c  Velocity[Z]                                      0.27949E-29 
c  Pressure     0.22999E-06     550   0.92663E-08   0.17956E+00 0.16274E+04 
c  nu_tilda     0.21049E-05      38   0.34395E-04   0.26667E-05 0.10582E+04 
c  TempC        0.17483E+02      31   0.82596E-03   0.28642E+02 0.61746E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8612          11.166          4.5729          4.5729
v  Velocity[Y]            -5.8084          8.8105      0.00018727      0.00018727
v  Velocity[Z]       -6.9287e-015     3.5669e-015    -1.3285e-017    -1.3285e-017
v  ǁVelocityǁ         0.0066767          11.327          4.6791          4.6791
v  Pressure               -85.545          24.831          3.6201          3.6201
v  nu_tilda            8.859e-007       0.0040769      0.00052436      0.00052436
v  TempC                       21          71.659          21.103          21.103
v  TurbVisc            5.425e-013       0.0048023      0.00060635      0.00060635
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               61:        0.25850E+01

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


 INSTANT    0.620000000E+02   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21871E-01 0.98816E+00
   Friction velocity        uk    :  0.21871E-01 0.98816E+00
   Dimensionless distance   yplus :  0.17607E+00 0.79554E+01
   Friction thermal sca.    tstar : -0.10323E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13137E+00 0.59356E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39156E-02      36   0.15190E-02   0.20346E+02 0.27341E+03 
c  Velocity[X]                                      0.83169E+01 
c  Velocity[Y]                                      0.12029E+02 
c  Velocity[Z]                                      0.23091E-29 
c  Pressure     0.24770E-06     489   0.94965E-08   0.20089E+00 0.93853E+03 
c  nu_tilda     0.21162E-05      38   0.12531E-04   0.26191E-05 0.10463E+04 
c  TempC        0.17508E+02      31   0.18033E-02   0.27087E+02 0.59093E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8601          11.155          4.5729          4.5729
v  Velocity[Y]            -5.7786          8.7623      0.00019013      0.00019013
v  Velocity[Z]       -6.9287e-015     3.5795e-015    -1.3333e-017    -1.3333e-017
v  ǁVelocityǁ         0.0030292          11.303            4.68            4.68
v  Pressure               -85.014          24.732          3.5863          3.5863
v  nu_tilda           8.8336e-007       0.0040792      0.00052481      0.00052481
v  TempC                       21          74.359          21.105          21.105
v  TurbVisc           5.4189e-013        0.004805      0.00060675      0.00060675
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               62:        0.27510E+01

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


 INSTANT    0.630000000E+02   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93332E-02 0.98809E+00
   Friction velocity        uk    :  0.93332E-02 0.98809E+00
   Dimensionless distance   yplus :  0.75139E-01 0.79548E+01
   Friction thermal sca.    tstar : -0.15434E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56062E-01 0.59352E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39214E-02      36   0.15787E-02   0.19930E+02 0.27096E+03 
c  Velocity[X]                                      0.81278E+01 
c  Velocity[Y]                                      0.11802E+02 
c  Velocity[Z]                                      0.30656E-29 
c  Pressure     0.20413E-06     537   0.93959E-08   0.16160E+00 0.13529E+04 
c  nu_tilda     0.21273E-05      38   0.34085E-04   0.25731E-05 0.10347E+04 
c  TempC        0.17533E+02      32   0.11955E-02   0.35698E+02 0.69057E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8476          11.136          4.5729          4.5729
v  Velocity[Y]            -5.7452          8.7729      0.00019293      0.00019293
v  Velocity[Z]       -6.9287e-015     3.8408e-015    -1.3368e-017    -1.3368e-017
v  ǁVelocityǁ         0.0047522          11.286           4.681           4.681
v  Pressure               -84.605          24.614          3.5117          3.5117
v  nu_tilda           8.8052e-007       0.0040815      0.00052513      0.00052513
v  TempC                       21          73.289          21.106          21.106
v  TurbVisc           5.3569e-013       0.0048077      0.00060716      0.00060716
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               63:        0.28390E+01

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


 INSTANT    0.640000000E+02   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20877E-01 0.98730E+00
   Friction velocity        uk    :  0.20877E-01 0.98730E+00
   Dimensionless distance   yplus :  0.16807E+00 0.79485E+01
   Friction thermal sca.    tstar : -0.12526E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12540E+00 0.59305E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39272E-02      36   0.15789E-02   0.19667E+02 0.26920E+03 
c  Velocity[X]                                      0.80034E+01 
c  Velocity[Y]                                      0.11664E+02 
c  Velocity[Z]                                      0.26640E-29 
c  Pressure     0.22771E-06     505   0.92999E-08   0.18790E+00 0.97197E+03 
c  nu_tilda     0.21384E-05      37   0.12480E-04   0.25286E-05 0.10233E+04 
c  TempC        0.17558E+02      31   0.72648E-03   0.29939E+02 0.61385E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8265          11.118          4.5729          4.5729
v  Velocity[Y]            -5.7166          8.7397      0.00019557      0.00019557
v  Velocity[Z]       -6.9287e-015     3.5879e-015    -1.3398e-017    -1.3398e-017
v  ǁVelocityǁ         0.0061838          11.273          4.6819          4.6819
v  Pressure               -84.024          24.493          3.4767          3.4767
v  nu_tilda           8.7712e-007       0.0040837      0.00052558      0.00052558
v  TempC                       21          73.666          21.107          21.107
v  TurbVisc           5.2885e-013       0.0048104      0.00060757      0.00060757
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               64:        0.23230E+01

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


 INSTANT    0.650000000E+02   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47964E-02 0.98598E+00
   Friction velocity        uk    :  0.47964E-02 0.98598E+00
   Dimensionless distance   yplus :  0.38614E-01 0.79378E+01
   Friction thermal sca.    tstar : -0.17422E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28811E-01 0.59225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39329E-02      36   0.15576E-02   0.19380E+02 0.26735E+03 
c  Velocity[X]                                      0.79171E+01 
c  Velocity[Y]                                      0.11463E+02 
c  Velocity[Z]                                      0.21889E-29 
c  Pressure     0.19800E-06     518   0.92620E-08   0.15899E+00 0.11439E+04 
c  nu_tilda     0.21494E-05      37   0.33627E-04   0.24855E-05 0.10123E+04 
c  TempC        0.17582E+02      31   0.76265E-03   0.25400E+02 0.57392E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8006          11.092          4.5729          4.5729
v  Velocity[Y]            -5.6847          8.7515      0.00019828      0.00019828
v  Velocity[Z]       -6.9287e-015     3.5673e-015    -1.3419e-017    -1.3419e-017
v  ǁVelocityǁ         0.0034291          11.254          4.6829          4.6829
v  Pressure               -83.753           24.41          3.4155          3.4155
v  nu_tilda           8.7526e-007       0.0040859      0.00052591      0.00052591
v  TempC                       21          74.948          21.108          21.108
v  TurbVisc           5.2073e-013        0.004813        0.000608        0.000608
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               65:        0.23930E+01

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


 INSTANT    0.660000000E+02   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10714E-01 0.98435E+00
   Friction velocity        uk    :  0.10714E-01 0.98435E+00
   Dimensionless distance   yplus :  0.86259E-01 0.79247E+01
   Friction thermal sca.    tstar : -0.65326E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64359E-01 0.59127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39387E-02      36   0.15457E-02   0.19131E+02 0.26556E+03 
c  Velocity[X]                                      0.78545E+01 
c  Velocity[Y]                                      0.11277E+02 
c  Velocity[Z]                                      0.29020E-29 
c  Pressure     0.25330E-06     506   0.94844E-08   0.20117E+00 0.11963E+04 
c  nu_tilda     0.21603E-05      37   0.12440E-04   0.24438E-05 0.10014E+04 
c  TempC        0.17607E+02      31   0.10493E-02   0.25163E+02 0.56087E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7977          11.076          4.5729          4.5729
v  Velocity[Y]            -5.6582          8.7028       0.0002013       0.0002013
v  Velocity[Z]       -6.9287e-015     4.2874e-015    -1.3433e-017    -1.3433e-017
v  ǁVelocityǁ         0.0058011          11.236          4.6838          4.6838
v  Pressure               -83.258          24.234           3.368           3.368
v  nu_tilda           8.7361e-007        0.004088      0.00052637      0.00052637
v  TempC                       21          73.481           21.11           21.11
v  TurbVisc           5.1631e-013       0.0048156      0.00060842      0.00060842
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               66:        0.30050E+01

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


 INSTANT    0.670000000E+02   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11445E-01 0.98416E+00
   Friction velocity        uk    :  0.11445E-01 0.98416E+00
   Dimensionless distance   yplus :  0.92142E-01 0.79232E+01
   Friction thermal sca.    tstar : -0.59299E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68748E-01 0.59116E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39444E-02      36   0.13802E-02   0.18823E+02 0.26362E+03 
c  Velocity[X]                                      0.77016E+01 
c  Velocity[Y]                                      0.11121E+02 
c  Velocity[Z]                                      0.24193E-29 
c  Pressure     0.21684E-06     490   0.96680E-08   0.17597E+00 0.10405E+04 
c  nu_tilda     0.21712E-05      37   0.33241E-04   0.24034E-05 0.99084E+03 
c  TempC        0.17632E+02      31   0.11527E-02   0.26919E+02 0.58778E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7849          11.073          4.5729          4.5729
v  Velocity[Y]            -5.6241          8.7167      0.00020425      0.00020425
v  Velocity[Z]       -6.9287e-015     5.4086e-015    -1.3442e-017    -1.3442e-017
v  ǁVelocityǁ         0.0056531           11.22          4.6847          4.6847
v  Pressure               -82.931          24.199          3.3152          3.3152
v  nu_tilda           8.7205e-007       0.0040902      0.00052671      0.00052671
v  TempC                       21          73.865          21.111          21.111
v  TurbVisc           5.1244e-013       0.0048182      0.00060886      0.00060886
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               67:        0.25570E+01

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


 INSTANT    0.680000000E+02   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23871E-01 0.98336E+00
   Friction velocity        uk    :  0.23871E-01 0.98336E+00
   Dimensionless distance   yplus :  0.19218E+00 0.79167E+01
   Friction thermal sca.    tstar : -0.15673E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14339E+00 0.59067E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39501E-02      36   0.14887E-02   0.18477E+02 0.26140E+03 
c  Velocity[X]                                      0.75391E+01 
c  Velocity[Y]                                      0.10938E+02 
c  Velocity[Z]                                      0.21504E-29 
c  Pressure     0.19447E-06     472   0.94644E-08   0.15774E+00 0.80138E+03 
c  nu_tilda     0.21819E-05      37   0.12427E-04   0.23643E-05 0.98049E+03 
c  TempC        0.17657E+02      31   0.83037E-03   0.29320E+02 0.61063E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7646          11.067          4.5729          4.5729
v  Velocity[Y]            -5.5982          8.7181      0.00020729      0.00020729
v  Velocity[Z]       -6.9287e-015     6.2317e-015    -1.3439e-017    -1.3439e-017
v  ǁVelocityǁ         0.0029828            11.2          4.6856          4.6856
v  Pressure               -82.376           24.14          3.2942          3.2942
v  nu_tilda           8.7042e-007       0.0040923      0.00052718      0.00052718
v  TempC                       21          75.096          21.112          21.112
v  TurbVisc           5.0878e-013       0.0048207      0.00060929      0.00060929
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               68:        0.23010E+01

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


 INSTANT    0.690000000E+02   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10998E-01 0.98207E+00
   Friction velocity        uk    :  0.10998E-01 0.98207E+00
   Dimensionless distance   yplus :  0.88544E-01 0.79064E+01
   Friction thermal sca.    tstar : -0.89539E+02 0.13982E+00
   Rough dim-less th. sca.  tplus :  0.66064E-01 0.58990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39558E-02      36   0.15170E-02   0.18281E+02 0.26002E+03 
c  Velocity[X]                                      0.75080E+01 
c  Velocity[Y]                                      0.10772E+02 
c  Velocity[Z]                                      0.31041E-29 
c  Pressure     0.21280E-06     568   0.94467E-08   0.17634E+00 0.17162E+04 
c  nu_tilda     0.21926E-05      37   0.32819E-04   0.23263E-05 0.97037E+03 
c  TempC        0.17681E+02      31   0.74539E-03   0.24666E+02 0.56124E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7374          11.054          4.5729          4.5729
v  Velocity[Y]            -5.5666          8.6769      0.00021018      0.00021018
v  Velocity[Z]       -6.9287e-015     7.5441e-015     -1.343e-017     -1.343e-017
v  ǁVelocityǁ         0.0061988          11.184          4.6866          4.6866
v  Pressure               -82.036          23.919          3.2051          3.2051
v  nu_tilda           8.7024e-007       0.0040943      0.00052752      0.00052752
v  TempC                   20.998          71.759          21.114          21.114
v  TurbVisc           5.0498e-013       0.0048231      0.00060973      0.00060973
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               69:        0.35400E+01

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


 INSTANT    0.700000000E+02   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12035E-01 0.98035E+00
   Friction velocity        uk    :  0.12035E-01 0.98035E+00
   Dimensionless distance   yplus :  0.96887E-01 0.78925E+01
   Friction thermal sca.    tstar : -0.30381E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72289E-01 0.58887E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39614E-02      36   0.15342E-02   0.18045E+02 0.25835E+03 
c  Velocity[X]                                      0.73981E+01 
c  Velocity[Y]                                      0.10647E+02 
c  Velocity[Z]                                      0.24880E-29 
c  Pressure     0.20660E-06     409   0.98879E-08   0.16461E+00 0.75233E+03 
c  nu_tilda     0.22032E-05      37   0.12416E-04   0.22894E-05 0.96047E+03 
c  TempC        0.17706E+02      31   0.87537E-03   0.24520E+02 0.55226E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7318          11.042          4.5729          4.5729
v  Velocity[Y]            -5.5374          8.6782      0.00021297      0.00021297
v  Velocity[Z]       -6.9287e-015      8.549e-015    -1.3414e-017    -1.3414e-017
v  ǁVelocityǁ         0.0032618           11.17          4.6875          4.6875
v  Pressure               -81.643          23.903          3.1915          3.1915
v  nu_tilda            8.688e-007       0.0040964        0.000528        0.000528
v  TempC                   20.995           74.47          21.115          21.115
v  TurbVisc           5.0456e-013       0.0048256      0.00061017      0.00061017
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               70:        0.28510E+01

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


 INSTANT    0.710000000E+02   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37514E-02 0.98042E+00
   Friction velocity        uk    :  0.37514E-02 0.98042E+00
   Dimensionless distance   yplus :  0.30201E-01 0.78931E+01
   Friction thermal sca.    tstar : -0.39093E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22534E-01 0.58891E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39670E-02      36   0.14750E-02   0.17805E+02 0.25669E+03 
c  Velocity[X]                                      0.73359E+01 
c  Velocity[Y]                                      0.10469E+02 
c  Velocity[Z]                                      0.21348E-29 
c  Pressure     0.20999E-06     522   0.94929E-08   0.17250E+00 0.14788E+04 
c  nu_tilda     0.22137E-05      37   0.32407E-04   0.22537E-05 0.95078E+03 
c  TempC        0.17730E+02      31   0.84394E-03   0.24109E+02 0.55623E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.7186          11.023          4.5729          4.5729
v  Velocity[Y]            -5.5094          8.6454      0.00021611      0.00021611
v  Velocity[Z]       -6.9287e-015     9.3532e-015      -1.34e-017      -1.34e-017
v  ǁVelocityǁ         0.0047401          11.155          4.6884          4.6884
v  Pressure               -81.222          23.724          3.1152          3.1152
v  nu_tilda            8.677e-007       0.0040984      0.00052835      0.00052835
v  TempC                       21           73.06          21.116          21.116
v  TurbVisc           5.0125e-013        0.004828      0.00061063      0.00061063
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               71:        0.25830E+01

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


 INSTANT    0.720000000E+02   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14245E-01 0.97924E+00
   Friction velocity        uk    :  0.14245E-01 0.97924E+00
   Dimensionless distance   yplus :  0.11469E+00 0.78835E+01
   Friction thermal sca.    tstar : -0.84533E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85568E-01 0.58820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39726E-02      36   0.14555E-02   0.17489E+02 0.25461E+03 
c  Velocity[X]                                      0.72136E+01 
c  Velocity[Y]                                      0.10276E+02 
c  Velocity[Z]                                      0.31118E-29 
c  Pressure     0.18701E-06     362   0.98885E-08   0.15252E+00 0.73863E+03 
c  nu_tilda     0.22241E-05      37   0.12412E-04   0.22189E-05 0.94129E+03 
c  TempC        0.17755E+02      31   0.95774E-03   0.25436E+02 0.54882E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6991          11.002          4.5729          4.5729
v  Velocity[Y]            -5.4796          8.6625       0.0002192       0.0002192
v  Velocity[Z]       -6.9287e-015     1.0167e-014    -1.3378e-017    -1.3378e-017
v  ǁVelocityǁ         0.0051406          11.136          4.6893          4.6893
v  Pressure               -80.765          23.741          3.1081          3.1081
v  nu_tilda           8.6444e-007       0.0041004      0.00052883      0.00052883
v  TempC                       21          74.286          21.118          21.118
v  TurbVisc           4.9871e-013       0.0048303      0.00061108      0.00061108
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               72:        0.22980E+01

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


 INSTANT    0.730000000E+02   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22621E-01 0.97992E+00
   Friction velocity        uk    :  0.22621E-01 0.97992E+00
   Dimensionless distance   yplus :  0.18211E+00 0.78890E+01
   Friction thermal sca.    tstar : -0.76440E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13588E+00 0.58861E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39782E-02      36   0.14079E-02   0.17238E+02 0.25283E+03 
c  Velocity[X]                                      0.70689E+01 
c  Velocity[Y]                                      0.10169E+02 
c  Velocity[Z]                                      0.22907E-29 
c  Pressure     0.20656E-06     506   0.95148E-08   0.17295E+00 0.14201E+04 
c  nu_tilda     0.22345E-05      37   0.31976E-04   0.21852E-05 0.93201E+03 
c  TempC        0.17779E+02      31   0.93598E-03   0.25354E+02 0.56094E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.674          10.981          4.5729          4.5729
v  Velocity[Y]            -5.4535           8.624      0.00022228      0.00022228
v  Velocity[Z]       -6.9287e-015     1.0594e-014    -1.3355e-017    -1.3355e-017
v  ǁVelocityǁ         0.0037087          11.117          4.6902          4.6902
v  Pressure               -80.344           23.57          3.0354          3.0354
v  nu_tilda           8.6329e-007       0.0041023      0.00052919      0.00052919
v  TempC                       21          74.518          21.119          21.119
v  TurbVisc           4.9125e-013       0.0048327      0.00061155      0.00061155
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               73:        0.23730E+01

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


 INSTANT    0.740000000E+02   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57706E-02 0.97797E+00
   Friction velocity        uk    :  0.57706E-02 0.97797E+00
   Dimensionless distance   yplus :  0.46457E-01 0.78733E+01
   Friction thermal sca.    tstar : -0.83129E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34662E-01 0.58744E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39837E-02      36   0.13075E-02   0.16935E+02 0.25077E+03 
c  Velocity[X]                                      0.69758E+01 
c  Velocity[Y]                                      0.99594E+01 
c  Velocity[Z]                                      0.22545E-29 
c  Pressure     0.16356E-06     409   0.94335E-08   0.13340E+00 0.74072E+03 
c  nu_tilda     0.22448E-05      37   0.12412E-04   0.21524E-05 0.92291E+03 
c  TempC        0.17803E+02      31   0.80603E-03   0.24077E+02 0.54523E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6625          10.974          4.5729          4.5729
v  Velocity[Y]            -5.4234          8.6384      0.00022552      0.00022552
v  Velocity[Z]       -6.9287e-015     1.0854e-014    -1.3328e-017    -1.3328e-017
v  ǁVelocityǁ         0.0067646          11.097           4.691           4.691
v  Pressure               -80.006          23.569          3.0231          3.0231
v  nu_tilda            8.629e-007       0.0041042      0.00052968      0.00052968
v  TempC                       21          73.269           21.12           21.12
v  TurbVisc           4.8865e-013        0.004835      0.00061201      0.00061201
v  total_pressure     1.0124e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               74:        0.20510E+01

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


 INSTANT    0.750000000E+02   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27361E-01 0.97839E+00
   Friction velocity        uk    :  0.27361E-01 0.97839E+00
   Dimensionless distance   yplus :  0.22027E+00 0.78767E+01
   Friction thermal sca.    tstar : -0.12601E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16435E+00 0.58769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39893E-02      36   0.14671E-02   0.16694E+02 0.24899E+03 
c  Velocity[X]                                      0.68914E+01 
c  Velocity[Y]                                      0.98028E+01 
c  Velocity[Z]                                      0.27294E-29 
c  Pressure     0.20350E-06     522   0.99714E-08   0.16457E+00 0.13433E+04 
c  nu_tilda     0.22550E-05      37   0.31553E-04   0.21205E-05 0.91400E+03 
c  TempC        0.17827E+02      31   0.10607E-02   0.22703E+02 0.52291E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6508          10.968          4.5729          4.5729
v  Velocity[Y]            -5.3981          8.6321      0.00022853      0.00022853
v  Velocity[Z]       -6.9287e-015     1.1059e-014    -1.3293e-017    -1.3293e-017
v  ǁVelocityǁ         0.0031979          11.078          4.6919          4.6919
v  Pressure                -79.64          23.426          2.9539          2.9539
v  nu_tilda           8.6374e-007       0.0041061      0.00053006      0.00053006
v  TempC                       21           74.06          21.122          21.122
v  TurbVisc           4.8776e-013       0.0048373      0.00061249      0.00061249
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               75:        0.24070E+01

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


 INSTANT    0.760000000E+02   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86477E-02 0.97728E+00
   Friction velocity        uk    :  0.86477E-02 0.97728E+00
   Dimensionless distance   yplus :  0.69620E-01 0.78678E+01
   Friction thermal sca.    tstar : -0.10431E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51944E-01 0.58703E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39948E-02      36   0.13548E-02   0.16507E+02 0.24764E+03 
c  Velocity[X]                                      0.68197E+01 
c  Velocity[Y]                                      0.96870E+01 
c  Velocity[Z]                                      0.24751E-29 
c  Pressure     0.20790E-06     458   0.96985E-08   0.17417E+00 0.85820E+03 
c  nu_tilda     0.22651E-05      37   0.12410E-04   0.20895E-05 0.90526E+03 
c  TempC        0.17851E+02      31   0.79302E-03   0.24310E+02 0.53899E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6322          10.959          4.5729          4.5729
v  Velocity[Y]            -5.3717          8.5958      0.00023186      0.00023186
v  Velocity[Z]       -6.9287e-015     1.0473e-014    -1.3248e-017    -1.3248e-017
v  ǁVelocityǁ          0.007399           11.06          4.6928          4.6928
v  Pressure               -79.164          23.342          2.9275          2.9275
v  nu_tilda           8.6406e-007        0.004108      0.00053055      0.00053055
v  TempC                       21          74.144          21.123          21.123
v  TurbVisc           4.8966e-013       0.0048395      0.00061296      0.00061296
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               76:        0.24120E+01

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


 INSTANT    0.770000000E+02   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20619E-01 0.97534E+00
   Friction velocity        uk    :  0.20619E-01 0.97534E+00
   Dimensionless distance   yplus :  0.16600E+00 0.78521E+01
   Friction thermal sca.    tstar : -0.77417E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12385E+00 0.58586E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40003E-02      36   0.13649E-02   0.16235E+02 0.24568E+03 
c  Velocity[X]                                      0.67171E+01 
c  Velocity[Y]                                      0.95180E+01 
c  Velocity[Z]                                      0.24619E-29 
c  Pressure     0.19644E-06     520   0.97823E-08   0.15888E+00 0.12033E+04 
c  nu_tilda     0.22752E-05      37   0.31152E-04   0.20593E-05 0.89670E+03 
c  TempC        0.17875E+02      31   0.76144E-03   0.19692E+02 0.50060E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6086          10.944          4.5729          4.5729
v  Velocity[Y]            -5.3456          8.6027      0.00023533      0.00023533
v  Velocity[Z]       -6.9287e-015      1.039e-014    -1.3202e-017    -1.3202e-017
v  ǁVelocityǁ         0.0031412          11.049          4.6937          4.6937
v  Pressure                -78.76          23.238          2.8654          2.8654
v  nu_tilda           8.6595e-007       0.0041099      0.00053093      0.00053093
v  TempC                       21          73.706          21.124          21.124
v  TurbVisc           4.9039e-013       0.0048417      0.00061345      0.00061345
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               77:        0.27200E+01

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


 INSTANT    0.780000000E+02   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56878E-02 0.97603E+00
   Friction velocity        uk    :  0.56878E-02 0.97603E+00
   Dimensionless distance   yplus :  0.45790E-01 0.78577E+01
   Friction thermal sca.    tstar : -0.71423E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34165E-01 0.58627E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40057E-02      36   0.13962E-02   0.16002E+02 0.24397E+03 
c  Velocity[X]                                      0.66535E+01 
c  Velocity[Y]                                      0.93484E+01 
c  Velocity[Z]                                      0.28210E-29 
c  Pressure     0.16940E-06     488   0.95694E-08   0.14135E+00 0.89771E+03 
c  nu_tilda     0.22852E-05      37   0.12435E-04   0.20299E-05 0.88831E+03 
c  TempC        0.17899E+02      31   0.11953E-02   0.21667E+02 0.51867E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5902          10.933          4.5729          4.5729
v  Velocity[Y]            -5.3207          8.5695      0.00023848      0.00023848
v  Velocity[Z]       -6.9287e-015      1.054e-014    -1.3145e-017    -1.3145e-017
v  ǁVelocityǁ         0.0066074          11.039          4.6945          4.6945
v  Pressure               -78.369          23.142          2.8358          2.8358
v  nu_tilda           8.6953e-007       0.0041117      0.00053143      0.00053143
v  TempC                   20.988           73.83          21.126          21.126
v  TurbVisc           4.9469e-013       0.0048439      0.00061393      0.00061393
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               78:        0.26280E+01

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


 INSTANT    0.790000000E+02   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63252E-02 0.97494E+00
   Friction velocity        uk    :  0.63252E-02 0.97494E+00
   Dimensionless distance   yplus :  0.50922E-01 0.78489E+01
   Friction thermal sca.    tstar : -0.14733E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37994E-01 0.58562E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40112E-02      36   0.13191E-02   0.15774E+02 0.24233E+03 
c  Velocity[X]                                      0.65271E+01 
c  Velocity[Y]                                      0.92465E+01 
c  Velocity[Z]                                      0.28094E-29 
c  Pressure     0.18829E-06     506   0.99203E-08   0.15572E+00 0.95005E+03 
c  nu_tilda     0.22951E-05      37   0.30749E-04   0.20013E-05 0.88008E+03 
c  TempC        0.17923E+02      31   0.94244E-03   0.25077E+02 0.57898E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5797          10.914          4.5729          4.5729
v  Velocity[Y]            -5.2972          8.5864      0.00024149      0.00024149
v  Velocity[Z]       -6.9287e-015     1.0591e-014    -1.3076e-017    -1.3076e-017
v  ǁVelocityǁ         0.0032085          11.023          4.6954          4.6954
v  Pressure               -78.062            23.1          2.7891          2.7891
v  nu_tilda           8.7453e-007       0.0041135      0.00053182      0.00053182
v  TempC                       21          73.494          21.127          21.127
v  TurbVisc           5.0294e-013        0.004846      0.00061442      0.00061442
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               79:        0.29970E+01

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


 INSTANT    0.800000000E+02   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11653E-01 0.97573E+00
   Friction velocity        uk    :  0.11653E-01 0.97573E+00
   Dimensionless distance   yplus :  0.93815E-01 0.78553E+01
   Friction thermal sca.    tstar : -0.10545E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69996E-01 0.58609E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40166E-02      36   0.13601E-02   0.15471E+02 0.24026E+03 
c  Velocity[X]                                      0.64125E+01 
c  Velocity[Y]                                      0.90588E+01 
c  Velocity[Z]                                      0.25406E-29 
c  Pressure     0.15349E-06     505   0.90696E-08   0.12856E+00 0.10407E+04 
c  nu_tilda     0.23049E-05      37   0.12457E-04   0.19734E-05 0.87200E+03 
c  TempC        0.17947E+02      31   0.74761E-03   0.22601E+02 0.53146E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5619          10.896          4.5729          4.5729
v  Velocity[Y]            -5.2744          8.5526      0.00024499      0.00024499
v  Velocity[Z]       -6.9287e-015     1.0541e-014    -1.3011e-017    -1.3011e-017
v  ǁVelocityǁ         0.0058528          11.008          4.6962          4.6962
v  Pressure               -77.647          22.976           2.751           2.751
v  nu_tilda           8.7999e-007       0.0041152      0.00053233      0.00053233
v  TempC                       21          73.492          21.129          21.129
v  TurbVisc           5.1459e-013       0.0048481      0.00061491      0.00061491
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               80:        0.23290E+01

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


 INSTANT    0.810000000E+02   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74330E-02 0.97408E+00
   Friction velocity        uk    :  0.74330E-02 0.97408E+00
   Dimensionless distance   yplus :  0.59841E-01 0.78420E+01
   Friction thermal sca.    tstar : -0.53150E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44648E-01 0.58510E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40220E-02      36   0.12856E-02   0.15288E+02 0.23876E+03 
c  Velocity[X]                                      0.63812E+01 
c  Velocity[Y]                                      0.89070E+01 
c  Velocity[Z]                                      0.26610E-29 
c  Pressure     0.17166E-06     521   0.93101E-08   0.14346E+00 0.99237E+03 
c  nu_tilda     0.23147E-05      37   0.30347E-04   0.19463E-05 0.86408E+03 
c  TempC        0.17971E+02      31   0.86396E-03   0.20632E+02 0.49149E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5397          10.878          4.5729          4.5729
v  Velocity[Y]            -5.2524          8.5719      0.00024859      0.00024859
v  Velocity[Z]       -7.5507e-015     1.0569e-014    -1.2927e-017    -1.2927e-017
v  ǁVelocityǁ         0.0033124          10.989          4.6971          4.6971
v  Pressure               -77.323          22.925          2.7015          2.7015
v  nu_tilda           8.8543e-007        0.004117      0.00053272      0.00053272
v  TempC                       21          73.732           21.13           21.13
v  TurbVisc           5.2756e-013       0.0048502      0.00061541      0.00061541
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               81:        0.27840E+01

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


 INSTANT    0.820000000E+02   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13177E-01 0.97442E+00
   Friction velocity        uk    :  0.13177E-01 0.97442E+00
   Dimensionless distance   yplus :  0.10608E+00 0.78447E+01
   Friction thermal sca.    tstar : -0.10230E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79149E-01 0.58530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40274E-02      36   0.13943E-02   0.15084E+02 0.23722E+03 
c  Velocity[X]                                      0.62693E+01 
c  Velocity[Y]                                      0.88151E+01 
c  Velocity[Z]                                      0.27459E-29 
c  Pressure     0.18708E-06     457   0.97930E-08   0.15288E+00 0.84822E+03 
c  nu_tilda     0.23245E-05      37   0.12519E-04   0.19198E-05 0.85630E+03 
c  TempC        0.17995E+02      31   0.92922E-03   0.20514E+02 0.50311E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5165          10.863          4.5729          4.5729
v  Velocity[Y]            -5.2285          8.5562      0.00025174      0.00025174
v  Velocity[Z]       -8.3634e-015     1.0466e-014    -1.2833e-017    -1.2833e-017
v  ǁVelocityǁ         0.0056299          10.971          4.6979          4.6979
v  Pressure               -76.923           22.84          2.6749          2.6749
v  nu_tilda           8.9149e-007       0.0041187      0.00053323      0.00053323
v  TempC                       21          73.509          21.131          21.131
v  TurbVisc           5.4072e-013       0.0048522      0.00061591      0.00061591
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               82:        0.26050E+01

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


 INSTANT    0.830000000E+02   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24847E-01 0.97349E+00
   Friction velocity        uk    :  0.24847E-01 0.97349E+00
   Dimensionless distance   yplus :  0.20004E+00 0.78373E+01
   Friction thermal sca.    tstar : -0.68634E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14925E+00 0.58475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40327E-02      36   0.13015E-02   0.14915E+02 0.23583E+03 
c  Velocity[X]                                      0.62530E+01 
c  Velocity[Y]                                      0.86623E+01 
c  Velocity[Z]                                      0.29366E-29 
c  Pressure     0.20076E-06     521   0.97436E-08   0.16870E+00 0.13897E+04 
c  nu_tilda     0.23341E-05      37   0.29964E-04   0.18940E-05 0.84867E+03 
c  TempC        0.18018E+02      31   0.69928E-03   0.20082E+02 0.50503E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5066          10.862          4.5729          4.5729
v  Velocity[Y]            -5.2028          8.5241      0.00025536      0.00025536
v  Velocity[Z]        -9.145e-015     1.0281e-014    -1.2734e-017    -1.2734e-017
v  ǁVelocityǁ         0.0031134          10.955          4.6987          4.6987
v  Pressure               -76.622          22.685          2.6056          2.6056
v  nu_tilda           8.9681e-007       0.0041204      0.00053362      0.00053362
v  TempC                       21          74.055          21.133          21.133
v  TurbVisc           5.5569e-013       0.0048543      0.00061642      0.00061642
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               83:        0.31330E+01

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


 INSTANT    0.840000000E+02   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10543E-01 0.97195E+00
   Friction velocity        uk    :  0.10543E-01 0.97195E+00
   Dimensionless distance   yplus :  0.84879E-01 0.78249E+01
   Friction thermal sca.    tstar : -0.50632E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63329E-01 0.58382E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40380E-02      36   0.12894E-02   0.14615E+02 0.23375E+03 
c  Velocity[X]                                      0.61241E+01 
c  Velocity[Y]                                      0.84909E+01 
c  Velocity[Z]                                      0.31262E-29 
c  Pressure     0.15888E-06     408   0.97889E-08   0.13264E+00 0.71320E+03 
c  nu_tilda     0.23437E-05      37   0.12576E-04   0.18688E-05 0.84117E+03 
c  TempC        0.18042E+02      31   0.10939E-02   0.20100E+02 0.47535E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4897          10.851          4.5729          4.5729
v  Velocity[Y]            -5.1807          8.5368      0.00025897      0.00025897
v  Velocity[Z]       -9.7531e-015     1.0048e-014    -1.2626e-017    -1.2626e-017
v  ǁVelocityǁ         0.0036531          10.938          4.6995          4.6995
v  Pressure               -76.315          22.683          2.5929          2.5929
v  nu_tilda           9.0231e-007        0.004122      0.00053414      0.00053414
v  TempC                       21          74.451          21.134          21.134
v  TurbVisc           5.6908e-013       0.0048563      0.00061692      0.00061692
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               84:        0.33200E+01

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


 INSTANT    0.850000000E+02   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13504E-01 0.97247E+00
   Friction velocity        uk    :  0.13504E-01 0.97247E+00
   Dimensionless distance   yplus :  0.10872E+00 0.78291E+01
   Friction thermal sca.    tstar : -0.10828E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81114E-01 0.58414E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40434E-02      36   0.12544E-02   0.14389E+02 0.23204E+03 
c  Velocity[X]                                      0.60112E+01 
c  Velocity[Y]                                      0.83776E+01 
c  Velocity[Z]                                      0.31287E-29 
c  Pressure     0.17727E-06     520   0.99790E-08   0.15158E+00 0.14616E+04 
c  nu_tilda     0.23532E-05      37   0.29600E-04   0.18443E-05 0.83382E+03 
c  TempC        0.18065E+02      31   0.81356E-03   0.21565E+02 0.51035E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4688           10.84          4.5729          4.5729
v  Velocity[Y]            -5.1558           8.499      0.00026248      0.00026248
v  Velocity[Z]       -1.0101e-014      9.743e-015    -1.2507e-017    -1.2507e-017
v  ǁVelocityǁ         0.0029164          10.926          4.7004          4.7004
v  Pressure               -75.957          22.513           2.521           2.521
v  nu_tilda           9.0642e-007       0.0041237      0.00053454      0.00053454
v  TempC                       21          73.368          21.135          21.135
v  TurbVisc           5.8316e-013       0.0048582      0.00061744      0.00061744
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               85:        0.33850E+01

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


 INSTANT    0.860000000E+02   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79336E-02 0.97089E+00
   Friction velocity        uk    :  0.79336E-02 0.97089E+00
   Dimensionless distance   yplus :  0.63871E-01 0.78163E+01
   Friction thermal sca.    tstar : -0.10663E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47655E-01 0.58318E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40486E-02      36   0.12555E-02   0.14165E+02 0.23028E+03 
c  Velocity[X]                                      0.59358E+01 
c  Velocity[Y]                                      0.82287E+01 
c  Velocity[Z]                                      0.30706E-29 
c  Pressure     0.17393E-06     344   0.99345E-08   0.14626E+00 0.69362E+03 
c  nu_tilda     0.23627E-05      37   0.12627E-04   0.18203E-05 0.82659E+03 
c  TempC        0.18089E+02      31   0.71375E-03   0.19957E+02 0.48545E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4445          10.826          4.5729          4.5729
v  Velocity[Y]            -5.1354           8.519      0.00026609      0.00026609
v  Velocity[Z]       -1.0349e-014     9.5025e-015    -1.2383e-017    -1.2383e-017
v  ǁVelocityǁ         0.0058017          10.914          4.7012          4.7012
v  Pressure               -75.576          22.542          2.5177          2.5177
v  nu_tilda           9.0912e-007       0.0041253      0.00053507      0.00053507
v  TempC                       21           73.73          21.137          21.137
v  TurbVisc           5.9386e-013       0.0048602      0.00061795      0.00061795
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               86:        0.27230E+01

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


 INSTANT    0.870000000E+02   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23062E-01 0.97195E+00
   Friction velocity        uk    :  0.23062E-01 0.97195E+00
   Dimensionless distance   yplus :  0.18567E+00 0.78249E+01
   Friction thermal sca.    tstar : -0.13169E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13853E+00 0.58382E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40539E-02      36   0.13594E-02   0.14001E+02 0.22886E+03 
c  Velocity[X]                                      0.59153E+01 
c  Velocity[Y]                                      0.80861E+01 
c  Velocity[Z]                                      0.30483E-29 
c  Pressure     0.21246E-06     537   0.92624E-08   0.17685E+00 0.18418E+04 
c  nu_tilda     0.23721E-05      37   0.29241E-04   0.17969E-05 0.81949E+03 
c  TempC        0.18112E+02      31   0.99205E-03   0.18579E+02 0.46396E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4322          10.813          4.5729          4.5729
v  Velocity[Y]            -5.1124          8.4827      0.00026999      0.00026999
v  Velocity[Z]       -9.8765e-015     9.2466e-015    -1.2255e-017    -1.2255e-017
v  ǁVelocityǁ          0.002837          10.902           4.702           4.702
v  Pressure                -75.26          22.306          2.4305          2.4305
v  nu_tilda           9.1098e-007       0.0041269      0.00053547      0.00053547
v  TempC                       21           72.17          21.138          21.138
v  TurbVisc           6.0098e-013       0.0048621      0.00061847      0.00061847
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               87:        0.34170E+01

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


 INSTANT    0.880000000E+02   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52914E-02 0.97104E+00
   Friction velocity        uk    :  0.52914E-02 0.97104E+00
   Dimensionless distance   yplus :  0.42599E-01 0.78176E+01
   Friction thermal sca.    tstar : -0.16337E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31784E-01 0.58328E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40591E-02      36   0.11332E-02   0.13805E+02 0.22740E+03 
c  Velocity[X]                                      0.58242E+01 
c  Velocity[Y]                                      0.79812E+01 
c  Velocity[Z]                                      0.42268E-29 
c  Pressure     0.19369E-06     425   0.98927E-08   0.16396E+00 0.79384E+03 
c  nu_tilda     0.23815E-05      37   0.12683E-04   0.17740E-05 0.81251E+03 
c  TempC        0.18136E+02      31   0.88209E-03   0.22003E+02 0.51277E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4153          10.794          4.5729          4.5729
v  Velocity[Y]            -5.0913           8.503       0.0002735       0.0002735
v  Velocity[Z]        -9.794e-015     9.9166e-015    -1.2129e-017    -1.2129e-017
v  ǁVelocityǁ         0.0061729          10.888          4.7028          4.7028
v  Pressure               -74.969          22.384          2.4383          2.4383
v  nu_tilda            9.132e-007       0.0041285        0.000536        0.000536
v  TempC                       21          74.294           21.14           21.14
v  TurbVisc           6.0591e-013        0.004864      0.00061899      0.00061899
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               88:        0.29460E+01

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


 INSTANT    0.890000000E+02   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69508E-02 0.97174E+00
   Friction velocity        uk    :  0.69508E-02 0.97174E+00
   Dimensionless distance   yplus :  0.55959E-01 0.78232E+01
   Friction thermal sca.    tstar : -0.93858E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41752E-01 0.58369E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40644E-02      36   0.11776E-02   0.13507E+02 0.22523E+03 
c  Velocity[X]                                      0.56719E+01 
c  Velocity[Y]                                      0.78354E+01 
c  Velocity[Z]                                      0.32465E-29 
c  Pressure     0.14809E-06     520   0.98191E-08   0.12565E+00 0.13240E+04 
c  nu_tilda     0.23907E-05      37   0.28889E-04   0.17517E-05 0.80565E+03 
c  TempC        0.18159E+02      31   0.63665E-03   0.20773E+02 0.48992E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3955           10.78          4.5729          4.5729
v  Velocity[Y]            -5.0714          8.5061      0.00027745      0.00027745
v  Velocity[Z]       -9.7254e-015     8.5605e-015    -1.1984e-017    -1.1984e-017
v  ǁVelocityǁ          0.002812          10.873          4.7036          4.7036
v  Pressure               -74.676          22.252          2.3729          2.3729
v  nu_tilda           9.1589e-007         0.00413      0.00053641      0.00053641
v  TempC                       21          72.048          21.141          21.141
v  TurbVisc           6.1182e-013       0.0048658      0.00061952      0.00061952
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               89:        0.33220E+01

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


 INSTANT    0.900000000E+02   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36632E-02 0.97070E+00
   Friction velocity        uk    :  0.36632E-02 0.97070E+00
   Dimensionless distance   yplus :  0.29491E-01 0.78148E+01
   Friction thermal sca.    tstar : -0.22186E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22004E-01 0.58307E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40696E-02      36   0.12353E-02   0.13355E+02 0.22386E+03 
c  Velocity[X]                                      0.56404E+01 
c  Velocity[Y]                                      0.77149E+01 
c  Velocity[Z]                                      0.37742E-29 
c  Pressure     0.18163E-06     486   0.91341E-08   0.15837E+00 0.89176E+03 
c  nu_tilda     0.24000E-05      37   0.12737E-04   0.17299E-05 0.79891E+03 
c  TempC        0.18182E+02      31   0.10059E-02   0.17036E+02 0.43858E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3722          10.762          4.5729          4.5729
v  Velocity[Y]             -5.051          8.4656      0.00028128      0.00028128
v  Velocity[Z]       -9.7916e-015     8.3039e-015    -1.1842e-017    -1.1842e-017
v  ǁVelocityǁ         0.0068824          10.858          4.7043          4.7043
v  Pressure               -74.283          22.149          2.3447          2.3447
v  nu_tilda           9.1865e-007       0.0041316      0.00053694      0.00053694
v  TempC                       21          73.694          21.142          21.142
v  TurbVisc           6.1908e-013       0.0048677      0.00062004      0.00062004
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               90:        0.34140E+01

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


 INSTANT    0.910000000E+02   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20065E-01 0.96841E+00
   Friction velocity        uk    :  0.20065E-01 0.96841E+00
   Dimensionless distance   yplus :  0.16154E+00 0.77964E+01
   Friction thermal sca.    tstar : -0.17908E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12052E+00 0.58170E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40748E-02      36   0.12917E-02   0.13226E+02 0.22273E+03 
c  Velocity[X]                                      0.55934E+01 
c  Velocity[Y]                                      0.76326E+01 
c  Velocity[Z]                                      0.31305E-29 
c  Pressure     0.17445E-06     506   0.94187E-08   0.14680E+00 0.10941E+04 
c  nu_tilda     0.24091E-05      37   0.28544E-04   0.17085E-05 0.79229E+03 
c  TempC        0.18205E+02      31   0.91891E-03   0.17781E+02 0.46616E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.355          10.757          4.5729          4.5729
v  Velocity[Y]            -5.0301          8.4812      0.00028501      0.00028501
v  Velocity[Z]       -9.7888e-015     8.2095e-015    -1.1694e-017    -1.1694e-017
v  ǁVelocityǁ         0.0029047          10.843          4.7051          4.7051
v  Pressure               -73.972          22.072          2.2904          2.2904
v  nu_tilda           9.2082e-007       0.0041331      0.00053736      0.00053736
v  TempC                       21          73.211          21.144          21.144
v  TurbVisc           6.2656e-013       0.0048695      0.00062058      0.00062058
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               91:        0.36640E+01

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


 INSTANT    0.920000000E+02   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11122E-01 0.96924E+00
   Friction velocity        uk    :  0.11122E-01 0.96924E+00
   Dimensionless distance   yplus :  0.89542E-01 0.78030E+01
   Friction thermal sca.    tstar : -0.16013E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66809E-01 0.58219E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40799E-02      36   0.11952E-02   0.13036E+02 0.22120E+03 
c  Velocity[X]                                      0.55385E+01 
c  Velocity[Y]                                      0.74976E+01 
c  Velocity[Z]                                      0.40059E-29 
c  Pressure     0.19981E-06     502   0.92441E-08   0.16816E+00 0.95015E+03 
c  nu_tilda     0.24182E-05      37   0.12786E-04   0.16877E-05 0.78577E+03 
c  TempC        0.18228E+02      30   0.85832E-03   0.18599E+02 0.45752E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3392           10.75          4.5729          4.5729
v  Velocity[Y]            -5.0074          8.4405      0.00028915      0.00028915
v  Velocity[Z]       -9.6492e-015      9.123e-015    -1.1556e-017    -1.1556e-017
v  ǁVelocityǁ         0.0058749          10.828          4.7059          4.7059
v  Pressure               -73.623          21.957          2.2594          2.2594
v  nu_tilda            9.231e-007       0.0041346       0.0005379       0.0005379
v  TempC                       21          73.875          21.145          21.145
v  TurbVisc           6.3252e-013       0.0048712      0.00062111      0.00062111
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               92:        0.30620E+01

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


 INSTANT    0.930000000E+02   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25725E-01 0.96812E+00
   Friction velocity        uk    :  0.25725E-01 0.96812E+00
   Dimensionless distance   yplus :  0.20710E+00 0.77940E+01
   Friction thermal sca.    tstar : -0.10302E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15452E+00 0.58152E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40851E-02      36   0.12303E-02   0.12780E+02 0.21919E+03 
c  Velocity[X]                                      0.54330E+01 
c  Velocity[Y]                                      0.73467E+01 
c  Velocity[Z]                                      0.45229E-29 
c  Pressure     0.17327E-06     501   0.98424E-08   0.14848E+00 0.87378E+03 
c  nu_tilda     0.24273E-05      37   0.28202E-04   0.16673E-05 0.77936E+03 
c  TempC        0.18251E+02      31   0.10156E-02   0.18933E+02 0.47003E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3203          10.742          4.5729          4.5729
v  Velocity[Y]            -4.9874           8.464      0.00029297      0.00029297
v  Velocity[Z]       -9.6193e-015     7.7034e-015    -1.1394e-017    -1.1394e-017
v  ǁVelocityǁ         0.0031314          10.812          4.7066          4.7066
v  Pressure               -73.408          21.943          2.2183          2.2183
v  nu_tilda           9.2613e-007        0.004136      0.00053832      0.00053832
v  TempC                       21          72.062          21.147          21.147
v  TurbVisc           6.3879e-013        0.004873      0.00062165      0.00062165
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               93:        0.32770E+01

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


 INSTANT    0.940000000E+02   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15262E-01 0.96893E+00
   Friction velocity        uk    :  0.15262E-01 0.96893E+00
   Dimensionless distance   yplus :  0.12287E+00 0.78005E+01
   Friction thermal sca.    tstar : -0.89386E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91673E-01 0.58201E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40902E-02      36   0.12342E-02   0.12606E+02 0.21781E+03 
c  Velocity[X]                                      0.53350E+01 
c  Velocity[Y]                                      0.72714E+01 
c  Velocity[Z]                                      0.35892E-29 
c  Pressure     0.17527E-06     474   0.96139E-08   0.15142E+00 0.91858E+03 
c  nu_tilda     0.24363E-05      37   0.12846E-04   0.16473E-05 0.77306E+03 
c  TempC        0.18274E+02      30   0.83185E-03   0.20795E+02 0.49837E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.298          10.731          4.5729          4.5729
v  Velocity[Y]            -4.9664           8.435      0.00029694      0.00029694
v  Velocity[Z]       -9.5014e-015     7.4841e-015    -1.1239e-017    -1.1239e-017
v  ǁVelocityǁ         0.0050529          10.805          4.7074          4.7074
v  Pressure               -73.035          21.832          2.1889          2.1889
v  nu_tilda           9.3031e-007       0.0041375      0.00053886      0.00053886
v  TempC                       21           73.19          21.148          21.148
v  TurbVisc           6.4724e-013       0.0048747      0.00062219      0.00062219
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               94:        0.26980E+01

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


 INSTANT    0.950000000E+02   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21749E-01 0.96784E+00
   Friction velocity        uk    :  0.21749E-01 0.96784E+00
   Dimensionless distance   yplus :  0.17509E+00 0.77917E+01
   Friction thermal sca.    tstar : -0.76561E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13064E+00 0.58135E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40953E-02      36   0.11217E-02   0.12450E+02 0.21636E+03 
c  Velocity[X]                                      0.53325E+01 
c  Velocity[Y]                                      0.71173E+01 
c  Velocity[Z]                                      0.32504E-29 
c  Pressure     0.16568E-06     521   0.92941E-08   0.14153E+00 0.10308E+04 
c  nu_tilda     0.24452E-05      37   0.27863E-04   0.16278E-05 0.76685E+03 
c  TempC        0.18297E+02      30   0.91403E-03   0.19642E+02 0.47085E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2748          10.719          4.5729          4.5729
v  Velocity[Y]            -4.9455          8.4594      0.00030091      0.00030091
v  Velocity[Z]       -9.3629e-015     7.4541e-015    -1.1078e-017    -1.1078e-017
v  ǁVelocityǁ         0.0043341          10.792          4.7081          4.7081
v  Pressure               -72.778          21.776          2.1381          2.1381
v  nu_tilda           9.3489e-007       0.0041389      0.00053929      0.00053929
v  TempC                       21          73.272          21.149          21.149
v  TurbVisc             6.59e-013       0.0048764      0.00062274      0.00062274
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               95:        0.31760E+01

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


 INSTANT    0.960000000E+02   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20765E-01 0.96851E+00
   Friction velocity        uk    :  0.20765E-01 0.96851E+00
   Dimensionless distance   yplus :  0.16717E+00 0.77971E+01
   Friction thermal sca.    tstar : -0.20432E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12473E+00 0.58175E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41004E-02      36   0.11906E-02   0.12245E+02 0.21467E+03 
c  Velocity[X]                                      0.52589E+01 
c  Velocity[Y]                                      0.69864E+01 
c  Velocity[Z]                                      0.53504E-29 
c  Pressure     0.18411E-06     473   0.96871E-08   0.15544E+00 0.76293E+03 
c  nu_tilda     0.24541E-05      37   0.12879E-04   0.16087E-05 0.76075E+03 
c  TempC        0.18320E+02      30   0.95629E-03   0.19111E+02 0.46891E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2621          10.705          4.5729          4.5729
v  Velocity[Y]            -4.9277          8.4488      0.00030511      0.00030511
v  Velocity[Z]       -9.2247e-015     8.3974e-015    -1.0912e-017    -1.0912e-017
v  ǁVelocityǁ         0.0035671           10.78          4.7089          4.7089
v  Pressure               -72.399          21.709          2.1171          2.1171
v  nu_tilda           9.3927e-007       0.0041403      0.00053984      0.00053984
v  TempC                       21          72.953          21.151          21.151
v  TurbVisc           6.7207e-013       0.0048781      0.00062329      0.00062329
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               96:        0.30500E+01

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


 INSTANT    0.970000000E+02   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17692E-01 0.96752E+00
   Friction velocity        uk    :  0.17692E-01 0.96752E+00
   Dimensionless distance   yplus :  0.14243E+00 0.77892E+01
   Friction thermal sca.    tstar : -0.91333E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10627E+00 0.58116E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41054E-02      36   0.11559E-02   0.12048E+02 0.21305E+03 
c  Velocity[X]                                      0.51412E+01 
c  Velocity[Y]                                      0.69067E+01 
c  Velocity[Z]                                      0.42057E-29 
c  Pressure     0.15510E-06     538   0.94225E-08   0.13581E+00 0.13945E+04 
c  nu_tilda     0.24629E-05      37   0.27540E-04   0.15900E-05 0.75475E+03 
c  TempC        0.18343E+02      30   0.70038E-03   0.18490E+02 0.46567E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2436          10.691          4.5729          4.5729
v  Velocity[Y]            -4.9088          8.4119      0.00030897      0.00030897
v  Velocity[Z]       -9.0662e-015     7.4794e-015    -1.0738e-017    -1.0738e-017
v  ǁVelocityǁ         0.0068494          10.768          4.7096          4.7096
v  Pressure               -72.147          21.561          2.0507          2.0507
v  nu_tilda           9.4319e-007       0.0041417      0.00054027      0.00054027
v  TempC                       21          72.637          21.152          21.152
v  TurbVisc           6.8476e-013       0.0048798      0.00062384      0.00062384
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               97:        0.29560E+01

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


 INSTANT    0.980000000E+02   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11147E-01 0.96552E+00
   Friction velocity        uk    :  0.11147E-01 0.96552E+00
   Dimensionless distance   yplus :  0.89741E-01 0.77731E+01
   Friction thermal sca.    tstar : -0.35465E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66957E-01 0.57996E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41105E-02      36   0.11555E-02   0.11848E+02 0.21148E+03 
c  Velocity[X]                                      0.50476E+01 
c  Velocity[Y]                                      0.68001E+01 
c  Velocity[Z]                                      0.37523E-29 
c  Pressure     0.14423E-06     409   0.94208E-08   0.12421E+00 0.64761E+03 
c  nu_tilda     0.24717E-05      36   0.12885E-04   0.15716E-05 0.74883E+03 
c  TempC        0.18366E+02      31   0.62300E-03   0.16080E+02 0.41943E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2225          10.675          4.5729          4.5729
v  Velocity[Y]            -4.8896          8.4265      0.00031336      0.00031336
v  Velocity[Z]       -8.9536e-015     7.9021e-015    -1.0566e-017    -1.0566e-017
v  ǁVelocityǁ         0.0026069          10.754          4.7103          4.7103
v  Pressure               -71.877          21.572          2.0429          2.0429
v  nu_tilda           9.4649e-007       0.0041431      0.00054082      0.00054082
v  TempC                       21          72.545          21.154          21.154
v  TurbVisc           6.9624e-013       0.0048814      0.00062439      0.00062439
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               98:        0.27340E+01

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


 INSTANT    0.990000000E+02   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42087E-02 0.96605E+00
   Friction velocity        uk    :  0.42087E-02 0.96605E+00
   Dimensionless distance   yplus :  0.33883E-01 0.77774E+01
   Friction thermal sca.    tstar : -0.88655E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25281E-01 0.58028E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41155E-02      36   0.12407E-02   0.11706E+02 0.21007E+03 
c  Velocity[X]                                      0.50458E+01 
c  Velocity[Y]                                      0.66606E+01 
c  Velocity[Z]                                      0.41899E-29 
c  Pressure     0.18870E-06     553   0.96047E-08   0.16219E+00 0.16185E+04 
c  nu_tilda     0.24804E-05      36   0.27222E-04   0.15537E-05 0.74301E+03 
c  TempC        0.18388E+02      30   0.14188E-02   0.17754E+02 0.43161E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.198          10.661          4.5729          4.5729
v  Velocity[Y]            -4.8689          8.3946      0.00031756      0.00031756
v  Velocity[Z]       -8.8654e-015     8.3065e-015    -1.0391e-017    -1.0391e-017
v  ǁVelocityǁ         0.0029447          10.739          4.7111          4.7111
v  Pressure               -71.572           21.38          1.9683          1.9683
v  nu_tilda           9.4976e-007       0.0041445      0.00054126      0.00054126
v  TempC                       21          74.157          21.155          21.155
v  TurbVisc           7.0603e-013       0.0048831      0.00062495      0.00062495
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP               99:        0.36440E+01

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


 INSTANT    0.100000000E+03   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18259E-01 0.96495E+00
   Friction velocity        uk    :  0.18259E-01 0.96495E+00
   Dimensionless distance   yplus :  0.14700E+00 0.77685E+01
   Friction thermal sca.    tstar : -0.65574E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10968E+00 0.57962E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41205E-02      36   0.11523E-02   0.11556E+02 0.20879E+03 
c  Velocity[X]                                      0.49704E+01 
c  Velocity[Y]                                      0.65853E+01 
c  Velocity[Z]                                      0.48031E-29 
c  Pressure     0.18069E-06     424   0.94934E-08   0.15575E+00 0.71272E+03 
c  nu_tilda     0.24891E-05      36   0.12872E-04   0.15361E-05 0.73728E+03 
c  TempC        0.18411E+02      31   0.10522E-02   0.24781E+02 0.53164E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1816           10.65          4.5729          4.5729
v  Velocity[Y]            -4.8501          8.4161      0.00032188      0.00032188
v  Velocity[Z]       -8.8152e-015     8.6313e-015     -1.022e-017     -1.022e-017
v  ǁVelocityǁ         0.0022608          10.726          4.7118          4.7118
v  Pressure                -71.26          21.442          1.9736          1.9736
v  nu_tilda           9.5215e-007       0.0041458      0.00054181      0.00054181
v  TempC                       21          72.066          21.156          21.156
v  TurbVisc           7.1584e-013       0.0048847      0.00062551      0.00062551
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              100:        0.30810E+01

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


 INSTANT    0.101000000E+03   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16223E-01 0.96575E+00
   Friction velocity        uk    :  0.16223E-01 0.96575E+00
   Dimensionless distance   yplus :  0.13061E+00 0.77750E+01
   Friction thermal sca.    tstar : -0.11788E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97447E-01 0.58010E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41255E-02      35   0.11372E-02   0.11362E+02 0.20704E+03 
c  Velocity[X]                                      0.49030E+01 
c  Velocity[Y]                                      0.64591E+01 
c  Velocity[Z]                                      0.47062E-29 
c  Pressure     0.18500E-06     537   0.94654E-08   0.15722E+00 0.17876E+04 
c  nu_tilda     0.24977E-05      36   0.26922E-04   0.15189E-05 0.73164E+03 
c  TempC        0.18433E+02      30   0.89180E-03   0.18225E+02 0.46248E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1655          10.646          4.5729          4.5729
v  Velocity[Y]            -4.8316          8.3787      0.00032638      0.00032638
v  Velocity[Z]       -8.7908e-015     9.0191e-015    -1.0036e-017    -1.0036e-017
v  ǁVelocityǁ         0.0030176          10.712          4.7125          4.7125
v  Pressure               -70.971          21.223          1.8928          1.8928
v  nu_tilda           9.5369e-007       0.0041471      0.00054225      0.00054225
v  TempC                       21          72.924          21.158          21.158
v  TurbVisc           7.2308e-013       0.0048862      0.00062608      0.00062608
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              101:        0.30460E+01

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


 INSTANT    0.102000000E+03   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89446E-02 0.96490E+00
   Friction velocity        uk    :  0.89446E-02 0.96490E+00
   Dimensionless distance   yplus :  0.72010E-01 0.77681E+01
   Friction thermal sca.    tstar : -0.59667E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53727E-01 0.57959E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41304E-02      35   0.11181E-02   0.11198E+02 0.20556E+03 
c  Velocity[X]                                      0.48557E+01 
c  Velocity[Y]                                      0.63426E+01 
c  Velocity[Z]                                      0.38756E-29 
c  Pressure     0.15257E-06     393   0.98553E-08   0.13099E+00 0.67642E+03 
c  nu_tilda     0.25063E-05      36   0.12833E-04   0.15020E-05 0.72608E+03 
c  TempC        0.18456E+02      30   0.82065E-03   0.17889E+02 0.44967E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.145          10.636          4.5729          4.5729
v  Velocity[Y]            -4.8143           8.404      0.00033075      0.00033075
v  Velocity[Z]       -8.8168e-015     9.3673e-015    -9.8605e-018    -9.8605e-018
v  ǁVelocityǁ         0.0052466          10.696          4.7132          4.7132
v  Pressure               -70.733          21.273          1.8952          1.8952
v  nu_tilda           9.5476e-007       0.0041484      0.00054281      0.00054281
v  TempC                       21          72.575          21.159          21.159
v  TurbVisc           7.2776e-013       0.0048878      0.00062664      0.00062664
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              102:        0.20800E+01

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


 INSTANT    0.103000000E+03   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15714E-01 0.96592E+00
   Friction velocity        uk    :  0.15714E-01 0.96592E+00
   Dimensionless distance   yplus :  0.12651E+00 0.77763E+01
   Friction thermal sca.    tstar : -0.91796E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94392E-01 0.58020E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41354E-02      35   0.11546E-02   0.11001E+02 0.20400E+03 
c  Velocity[X]                                      0.47245E+01 
c  Velocity[Y]                                      0.62769E+01 
c  Velocity[Z]                                      0.38709E-29 
c  Pressure     0.14661E-06     553   0.92104E-08   0.12664E+00 0.12154E+04 
c  nu_tilda     0.25148E-05      36   0.26662E-04   0.14854E-05 0.72061E+03 
c  TempC        0.18478E+02      30   0.94367E-03   0.16446E+02 0.43904E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1221          10.629          4.5729          4.5729
v  Velocity[Y]            -4.7955          8.4066      0.00033512      0.00033512
v  Velocity[Z]       -9.2663e-015     9.6993e-015    -9.6776e-018    -9.6776e-018
v  ǁVelocityǁ         0.0060684          10.689          4.7138          4.7138
v  Pressure               -70.499          21.165          1.8371          1.8371
v  nu_tilda           9.5578e-007       0.0041497      0.00054326      0.00054326
v  TempC                       21          72.749           21.16           21.16
v  TurbVisc           7.3104e-013       0.0048893      0.00062721      0.00062721
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              103:        0.24270E+01

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


 INSTANT    0.104000000E+03   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14555E-01 0.96500E+00
   Friction velocity        uk    :  0.14555E-01 0.96500E+00
   Dimensionless distance   yplus :  0.11718E+00 0.77689E+01
   Friction thermal sca.    tstar : -0.27544E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87429E-01 0.57965E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41403E-02      35   0.11029E-02   0.10855E+02 0.20263E+03 
c  Velocity[X]                                      0.46860E+01 
c  Velocity[Y]                                      0.61688E+01 
c  Velocity[Z]                                      0.59610E-29 
c  Pressure     0.15575E-06     489   0.93276E-08   0.13736E+00 0.89355E+03 
c  nu_tilda     0.25232E-05      36   0.12742E-04   0.14692E-05 0.71522E+03 
c  TempC        0.18501E+02      30   0.79316E-03   0.18047E+02 0.44550E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1001          10.618          4.5729          4.5729
v  Velocity[Y]            -4.7752          8.3679      0.00033958      0.00033958
v  Velocity[Z]        -9.669e-015     9.9789e-015    -9.5019e-018    -9.5019e-018
v  ǁVelocityǁ         0.0029833          10.679          4.7145          4.7145
v  Pressure               -70.176          21.064          1.8093          1.8093
v  nu_tilda           9.5661e-007        0.004151      0.00054382      0.00054382
v  TempC                       21          73.616          21.162          21.162
v  TurbVisc           7.3418e-013       0.0048909      0.00062778      0.00062778
v  total_pressure     1.0125e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              104:        0.22860E+01

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


 INSTANT    0.105000000E+03   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13281E-01 0.96291E+00
   Friction velocity        uk    :  0.13281E-01 0.96291E+00
   Dimensionless distance   yplus :  0.10692E+00 0.77521E+01
   Friction thermal sca.    tstar : -0.17003E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79776E-01 0.57839E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41452E-02      35   0.12021E-02   0.10673E+02 0.20100E+03 
c  Velocity[X]                                      0.46393E+01 
c  Velocity[Y]                                      0.60333E+01 
c  Velocity[Z]                                      0.48159E-29 
c  Pressure     0.16673E-06     490   0.99299E-08   0.14392E+00 0.92694E+03 
c  nu_tilda     0.25317E-05      36   0.26403E-04   0.14533E-05 0.70990E+03 
c  TempC        0.18523E+02      30   0.66446E-03   0.16699E+02 0.43865E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.086          10.607          4.5729          4.5729
v  Velocity[Y]            -4.7577          8.3863      0.00034449      0.00034449
v  Velocity[Z]       -1.0011e-014     1.0239e-014    -9.3317e-018    -9.3317e-018
v  ǁVelocityǁ         0.0034731          10.668          4.7152          4.7152
v  Pressure               -69.928          21.016          1.7648          1.7648
v  nu_tilda           9.5601e-007       0.0041523      0.00054427      0.00054427
v  TempC                       21          72.496          21.163          21.163
v  TurbVisc           7.3671e-013       0.0048924      0.00062836      0.00062836
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              105:        0.26430E+01

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


 INSTANT    0.106000000E+03   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14294E-01 0.96361E+00
   Friction velocity        uk    :  0.14294E-01 0.96361E+00
   Dimensionless distance   yplus :  0.11508E+00 0.77577E+01
   Friction thermal sca.    tstar : -0.78337E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85859E-01 0.57881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41501E-02      35   0.10821E-02   0.10611E+02 0.20010E+03 
c  Velocity[X]                                      0.46371E+01 
c  Velocity[Y]                                      0.59734E+01 
c  Velocity[Z]                                      0.38224E-29 
c  Pressure     0.17961E-06     520   0.99989E-08   0.15309E+00 0.11010E+04 
c  nu_tilda     0.25400E-05      36   0.12682E-04   0.14377E-05 0.70467E+03 
c  TempC        0.18545E+02      30   0.10187E-02   0.15437E+02 0.40449E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0659          10.594          4.5729          4.5729
v  Velocity[Y]            -4.7389          8.3465      0.00034873      0.00034873
v  Velocity[Z]        -9.653e-015     1.0459e-014    -9.1583e-018    -9.1583e-018
v  ǁVelocityǁ         0.0056615          10.656          4.7159          4.7159
v  Pressure               -69.599          20.871          1.7283          1.7283
v  nu_tilda           9.5427e-007       0.0041535      0.00054483      0.00054483
v  TempC                       21          72.566          21.164          21.164
v  TurbVisc           7.3487e-013       0.0048938      0.00062893      0.00062893
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              106:        0.24010E+01

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


 INSTANT    0.107000000E+03   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22567E-01 0.96269E+00
   Friction velocity        uk    :  0.22567E-01 0.96269E+00
   Dimensionless distance   yplus :  0.18168E+00 0.77503E+01
   Friction thermal sca.    tstar : -0.10169E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13555E+00 0.57826E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41550E-02      35   0.99654E-03   0.10370E+02 0.19808E+03 
c  Velocity[X]                                      0.45206E+01 
c  Velocity[Y]                                      0.58494E+01 
c  Velocity[Z]                                      0.44769E-29 
c  Pressure     0.15435E-06     506   0.94042E-08   0.13392E+00 0.76046E+03 
c  nu_tilda     0.25483E-05      36   0.26140E-04   0.14224E-05 0.69951E+03 
c  TempC        0.18567E+02      30   0.90557E-03   0.20511E+02 0.48024E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0436          10.581          4.5729          4.5729
v  Velocity[Y]            -4.7234            8.37      0.00035383      0.00035383
v  Velocity[Z]       -9.6818e-015     1.0598e-014    -8.9942e-018    -8.9942e-018
v  ǁVelocityǁ         0.0061458          10.645          4.7165          4.7165
v  Pressure               -69.423          20.879          1.6947          1.6947
v  nu_tilda           9.5258e-007       0.0041547      0.00054529      0.00054529
v  TempC                       21          73.372          21.166          21.166
v  TurbVisc           7.2956e-013       0.0048953      0.00062951      0.00062951
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              107:        0.28530E+01

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


 INSTANT    0.108000000E+03   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13720E-02 0.96352E+00
   Friction velocity        uk    :  0.13720E-02 0.96352E+00
   Dimensionless distance   yplus :  0.11045E-01 0.77570E+01
   Friction thermal sca.    tstar : -0.71622E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82411E-02 0.57876E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41598E-02      35   0.11563E-02   0.10165E+02 0.19634E+03 
c  Velocity[X]                                      0.44276E+01 
c  Velocity[Y]                                      0.57370E+01 
c  Velocity[Z]                                      0.55456E-29 
c  Pressure     0.13843E-06     474   0.96096E-08   0.12084E+00 0.91936E+03 
c  nu_tilda     0.25566E-05      36   0.12680E-04   0.14073E-05 0.69442E+03 
c  TempC        0.18589E+02      30   0.89499E-03   0.17403E+02 0.44866E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0176          10.567          4.5729          4.5729
v  Velocity[Y]            -4.7049          8.3445      0.00035836      0.00035836
v  Velocity[Z]       -9.7351e-015     1.0735e-014    -8.8344e-018    -8.8344e-018
v  ǁVelocityǁ         0.0034734          10.632          4.7172          4.7172
v  Pressure               -69.119          20.769          1.6662          1.6662
v  nu_tilda           9.5108e-007       0.0041559      0.00054586      0.00054586
v  TempC                       21          73.265          21.167          21.167
v  TurbVisc           7.2439e-013       0.0048967      0.00063009      0.00063009
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              108:        0.24340E+01

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


 INSTANT    0.109000000E+03   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17010E-01 0.96252E+00
   Friction velocity        uk    :  0.17010E-01 0.96252E+00
   Dimensionless distance   yplus :  0.13694E+00 0.77489E+01
   Friction thermal sca.    tstar : -0.91965E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+00 0.57816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41647E-02      35   0.10515E-02   0.10076E+02 0.19532E+03 
c  Velocity[X]                                      0.44093E+01 
c  Velocity[Y]                                      0.56663E+01 
c  Velocity[Z]                                      0.50496E-29 
c  Pressure     0.18092E-06     505   0.96835E-08   0.15634E+00 0.81256E+03 
c  nu_tilda     0.25648E-05      36   0.25874E-04   0.13926E-05 0.68941E+03 
c  TempC        0.18611E+02      30   0.90836E-03   0.15882E+02 0.43166E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0041          10.554          4.5729          4.5729
v  Velocity[Y]            -4.6856          8.3667      0.00036311      0.00036311
v  Velocity[Z]       -9.9386e-015     1.0854e-014     -8.678e-018     -8.678e-018
v  ǁVelocityǁ          0.003015          10.618          4.7178          4.7178
v  Pressure               -68.902          20.752          1.6282          1.6282
v  nu_tilda           9.4943e-007       0.0041571      0.00054631      0.00054631
v  TempC                       21          72.337          21.169          21.169
v  TurbVisc           7.1985e-013       0.0048982      0.00063068      0.00063068
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              109:        0.23830E+01

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


 INSTANT    0.110000000E+03   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62016E-02 0.96315E+00
   Friction velocity        uk    :  0.62016E-02 0.96315E+00
   Dimensionless distance   yplus :  0.49927E-01 0.77540E+01
   Friction thermal sca.    tstar : -0.26242E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37251E-01 0.57854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41695E-02      35   0.10727E-02   0.99119E+01 0.19381E+03 
c  Velocity[X]                                      0.43339E+01 
c  Velocity[Y]                                      0.55780E+01 
c  Velocity[Z]                                      0.43449E-29 
c  Pressure     0.16863E-06     474   0.97074E-08   0.14417E+00 0.81497E+03 
c  nu_tilda     0.25730E-05      36   0.12727E-04   0.13781E-05 0.68446E+03 
c  TempC        0.18633E+02      30   0.85588E-03   0.17409E+02 0.43325E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9864          10.543          4.5729          4.5729
v  Velocity[Y]            -4.6685           8.358      0.00036804      0.00036804
v  Velocity[Z]       -9.9758e-015      1.094e-014    -8.5129e-018    -8.5129e-018
v  ǁVelocityǁ         0.0041414          10.606          4.7184          4.7184
v  Pressure               -68.583          20.671          1.6042          1.6042
v  nu_tilda           9.4891e-007       0.0041583      0.00054689      0.00054689
v  TempC                       21           73.27           21.17           21.17
v  TurbVisc           7.1487e-013       0.0048996      0.00063126      0.00063126
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              110:        0.25320E+01

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


 INSTANT    0.111000000E+03   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10942E-01 0.96228E+00
   Friction velocity        uk    :  0.10942E-01 0.96228E+00
   Dimensionless distance   yplus :  0.88090E-01 0.77470E+01
   Friction thermal sca.    tstar : -0.17090E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65725E-01 0.57801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41743E-02      35   0.11337E-02   0.98047E+01 0.19259E+03 
c  Velocity[X]                                      0.43415E+01 
c  Velocity[Y]                                      0.54633E+01 
c  Velocity[Z]                                      0.38211E-29 
c  Pressure     0.16891E-06     522   0.97494E-08   0.14758E+00 0.13631E+04 
c  nu_tilda     0.25811E-05      36   0.25605E-04   0.13639E-05 0.67959E+03 
c  TempC        0.18655E+02      30   0.89922E-03   0.18326E+02 0.43342E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9642          10.538          4.5729          4.5729
v  Velocity[Y]            -4.6512          8.3249      0.00037317      0.00037317
v  Velocity[Z]       -1.0023e-014        1.1e-014     -8.361e-018     -8.361e-018
v  ǁVelocityǁ         0.0058535          10.593          4.7191          4.7191
v  Pressure               -68.324          20.526          1.5421          1.5421
v  nu_tilda           9.4942e-007       0.0041594      0.00054735      0.00054735
v  TempC                       21          71.971          21.171          21.171
v  TurbVisc           7.1329e-013       0.0049009      0.00063185      0.00063185
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              111:        0.27510E+01

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


 INSTANT    0.112000000E+03   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21283E-01 0.96053E+00
   Friction velocity        uk    :  0.21283E-01 0.96053E+00
   Dimensionless distance   yplus :  0.17135E+00 0.77329E+01
   Friction thermal sca.    tstar : -0.78606E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12784E+00 0.57696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41790E-02      35   0.10090E-02   0.96465E+01 0.19121E+03 
c  Velocity[X]                                      0.42451E+01 
c  Velocity[Y]                                      0.54014E+01 
c  Velocity[Z]                                      0.59957E-29 
c  Pressure     0.14330E-06     409   0.95209E-08   0.12375E+00 0.63233E+03 
c  nu_tilda     0.25892E-05      36   0.12800E-04   0.13500E-05 0.67478E+03 
c  TempC        0.18677E+02      30   0.83186E-03   0.15870E+02 0.42335E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9405          10.529          4.5729          4.5729
v  Velocity[Y]            -4.6348           8.338      0.00037784      0.00037784
v  Velocity[Z]       -1.0194e-014     1.1031e-014    -8.2063e-018    -8.2063e-018
v  ǁVelocityǁ         0.0058482          10.578          4.7197          4.7197
v  Pressure               -68.082          20.573          1.5456          1.5456
v  nu_tilda           9.4898e-007       0.0041606      0.00054793      0.00054793
v  TempC                       21          72.263          21.173          21.173
v  TurbVisc           7.1484e-013       0.0049023      0.00063244      0.00063244
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              112:        0.28110E+01

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


 INSTANT    0.113000000E+03   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25701E-01 0.96116E+00
   Friction velocity        uk    :  0.25701E-01 0.96116E+00
   Dimensionless distance   yplus :  0.20691E+00 0.77380E+01
   Friction thermal sca.    tstar : -0.13348E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15438E+00 0.57734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41838E-02      35   0.10611E-02   0.94459E+01 0.18935E+03 
c  Velocity[X]                                      0.41546E+01 
c  Velocity[Y]                                      0.52913E+01 
c  Velocity[Z]                                      0.52399E-29 
c  Pressure     0.16340E-06     536   0.99784E-08   0.14340E+00 0.14499E+04 
c  nu_tilda     0.25973E-05      36   0.25337E-04   0.13363E-05 0.67004E+03 
c  TempC        0.18699E+02      30   0.88536E-03   0.14263E+02 0.41002E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9195          10.522          4.5729          4.5729
v  Velocity[Y]            -4.6173          8.3069      0.00038314      0.00038314
v  Velocity[Z]       -1.0355e-014     1.1036e-014    -8.0515e-018    -8.0515e-018
v  ǁVelocityǁ         0.0048026          10.572          4.7203          4.7203
v  Pressure               -67.824          20.409          1.4808          1.4808
v  nu_tilda           9.4755e-007       0.0041617      0.00054839      0.00054839
v  TempC                       21          73.614          21.174          21.174
v  TurbVisc            7.135e-013       0.0049037      0.00063304      0.00063304
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              113:        0.29920E+01

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


 INSTANT    0.114000000E+03   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19899E-01 0.95993E+00
   Friction velocity        uk    :  0.19899E-01 0.95993E+00
   Dimensionless distance   yplus :  0.16020E+00 0.77281E+01
   Friction thermal sca.    tstar : -0.18108E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11952E+00 0.57660E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41886E-02      35   0.11421E-02   0.93469E+01 0.18817E+03 
c  Velocity[X]                                      0.41583E+01 
c  Velocity[Y]                                      0.51885E+01 
c  Velocity[Z]                                      0.45224E-29 
c  Pressure     0.13693E-06     342   0.94696E-08   0.11932E+00 0.59230E+03 
c  nu_tilda     0.26053E-05      36   0.12910E-04   0.13228E-05 0.66536E+03 
c  TempC        0.18721E+02      30   0.60068E-03   0.16903E+02 0.42388E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9038          10.512          4.5729          4.5729
v  Velocity[Y]             -4.599          8.3321       0.0003882       0.0003882
v  Velocity[Z]       -1.0508e-014     1.1011e-014    -7.8956e-018    -7.8956e-018
v  ǁVelocityǁ         0.0026334          10.562          4.7209          4.7209
v  Pressure               -67.567          20.438          1.4796          1.4796
v  nu_tilda            9.467e-007       0.0041628      0.00054897      0.00054897
v  TempC                       21          71.964          21.175          21.175
v  TurbVisc           7.0922e-013        0.004905      0.00063364      0.00063364
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              114:        0.25910E+01

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


 INSTANT    0.115000000E+03   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11258E-01 0.96080E+00
   Friction velocity        uk    :  0.11258E-01 0.96080E+00
   Dimensionless distance   yplus :  0.90636E-01 0.77351E+01
   Friction thermal sca.    tstar : -0.96213E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67625E-01 0.57713E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41933E-02      35   0.10807E-02   0.92534E+01 0.18712E+03 
c  Velocity[X]                                      0.41048E+01 
c  Velocity[Y]                                      0.51486E+01 
c  Velocity[Z]                                      0.50782E-29 
c  Pressure     0.17708E-06     521   0.93920E-08   0.15228E+00 0.15918E+04 
c  nu_tilda     0.26132E-05      36   0.25069E-04   0.13095E-05 0.66074E+03 
c  TempC        0.18743E+02      30   0.76008E-03   0.14318E+02 0.38028E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8837          10.502          4.5729          4.5729
v  Velocity[Y]            -4.5815          8.2931      0.00039362      0.00039362
v  Velocity[Z]       -1.0628e-014     1.1002e-014    -7.7509e-018    -7.7509e-018
v  ǁVelocityǁ         0.0028358          10.552          4.7215          4.7215
v  Pressure               -67.289          20.254          1.4099          1.4099
v  nu_tilda           9.4561e-007       0.0041639      0.00054944      0.00054944
v  TempC                       21          72.051          21.177          21.177
v  TurbVisc           7.0668e-013       0.0049063      0.00063424      0.00063424
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              115:        0.31930E+01

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


 INSTANT    0.116000000E+03   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58296E-02 0.95994E+00
   Friction velocity        uk    :  0.58296E-02 0.95994E+00
   Dimensionless distance   yplus :  0.46932E-01 0.77282E+01
   Friction thermal sca.    tstar : -0.46332E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35017E-01 0.57661E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41980E-02      35   0.93259E-03   0.90527E+01 0.18535E+03 
c  Velocity[X]                                      0.40107E+01 
c  Velocity[Y]                                      0.50420E+01 
c  Velocity[Z]                                      0.60944E-29 
c  Pressure     0.14118E-06     424   0.99679E-08   0.12310E+00 0.70651E+03 
c  nu_tilda     0.26211E-05      36   0.13024E-04   0.12966E-05 0.65619E+03 
c  TempC        0.18764E+02      30   0.81563E-03   0.13944E+02 0.39642E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8607          10.491          4.5729          4.5729
v  Velocity[Y]            -4.5646          8.3189      0.00039862      0.00039862
v  Velocity[Z]       -1.0738e-014     1.0901e-014    -7.6077e-018    -7.6077e-018
v  ǁVelocityǁ         0.0039339          10.542          4.7221          4.7221
v  Pressure               -67.024          20.329          1.4194          1.4194
v  nu_tilda           9.4424e-007        0.004165      0.00055003      0.00055003
v  TempC                       21          73.162          21.178          21.178
v  TurbVisc           7.0341e-013       0.0049076      0.00063484      0.00063484
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              116:        0.23350E+01

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


 INSTANT    0.117000000E+03   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19735E-01 0.96095E+00
   Friction velocity        uk    :  0.19735E-01 0.96095E+00
   Dimensionless distance   yplus :  0.15888E+00 0.77363E+01
   Friction thermal sca.    tstar : -0.88943E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11854E+00 0.57721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42027E-02      35   0.11498E-02   0.88870E+01 0.18380E+03 
c  Velocity[X]                                      0.39567E+01 
c  Velocity[Y]                                      0.49302E+01 
c  Velocity[Z]                                      0.56917E-29 
c  Pressure     0.15341E-06     506   0.96157E-08   0.13396E+00 0.11869E+04 
c  nu_tilda     0.26290E-05      36   0.24809E-04   0.12838E-05 0.65170E+03 
c  TempC        0.18786E+02      30   0.66970E-03   0.15608E+02 0.42165E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8351          10.479          4.5729          4.5729
v  Velocity[Y]            -4.5487          8.3187      0.00040412      0.00040412
v  Velocity[Z]       -1.0814e-014     1.0767e-014    -7.4613e-018    -7.4613e-018
v  ǁVelocityǁ          0.005555          10.531          4.7227          4.7227
v  Pressure               -66.811          20.219          1.3646          1.3646
v  nu_tilda           9.4312e-007       0.0041661       0.0005505       0.0005505
v  TempC                   20.987          72.412          21.179          21.179
v  TurbVisc           6.9937e-013       0.0049089      0.00063545      0.00063545
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              117:        0.27990E+01

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


 INSTANT    0.118000000E+03   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24461E-01 0.95993E+00
   Friction velocity        uk    :  0.24461E-01 0.95993E+00
   Dimensionless distance   yplus :  0.19693E+00 0.77281E+01
   Friction thermal sca.    tstar : -0.14465E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14693E+00 0.57660E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42074E-02      35   0.96955E-03   0.88869E+01 0.18331E+03 
c  Velocity[X]                                      0.39933E+01 
c  Velocity[Y]                                      0.48935E+01 
c  Velocity[Z]                                      0.50626E-29 
c  Pressure     0.17088E-06     458   0.96383E-08   0.14996E+00 0.77641E+03 
c  nu_tilda     0.26368E-05      36   0.13113E-04   0.12712E-05 0.64727E+03 
c  TempC        0.18808E+02      30   0.88543E-03   0.13415E+02 0.37809E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8207          10.466          4.5729          4.5729
v  Velocity[Y]            -4.5316          8.2859      0.00040946      0.00040946
v  Velocity[Z]       -1.0858e-014     1.0655e-014    -7.3179e-018    -7.3179e-018
v  ǁVelocityǁ         0.0070527           10.52          4.7232          4.7232
v  Pressure               -66.514          20.134          1.3432          1.3432
v  nu_tilda           9.4287e-007       0.0041672      0.00055109      0.00055109
v  TempC                       21          72.479           21.18           21.18
v  TurbVisc           6.9603e-013       0.0049102      0.00063605      0.00063605
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              118:        0.29770E+01

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


 INSTANT    0.119000000E+03   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22335E-01 0.95812E+00
   Friction velocity        uk    :  0.22335E-01 0.95812E+00
   Dimensionless distance   yplus :  0.17982E+00 0.77135E+01
   Friction thermal sca.    tstar : -0.67320E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13416E+00 0.57552E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42120E-02      35   0.91623E-03   0.86293E+01 0.18101E+03 
c  Velocity[X]                                      0.38603E+01 
c  Velocity[Y]                                      0.47690E+01 
c  Velocity[Z]                                      0.44401E-29 
c  Pressure     0.14170E-06     504   0.99102E-08   0.12396E+00 0.84298E+03 
c  nu_tilda     0.26446E-05      36   0.24557E-04   0.12589E-05 0.64289E+03 
c  TempC        0.18829E+02      30   0.82593E-03   0.15982E+02 0.41638E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8022          10.455          4.5729          4.5729
v  Velocity[Y]            -4.5145          8.3036      0.00041502      0.00041502
v  Velocity[Z]       -1.0884e-014     1.0475e-014    -7.1764e-018    -7.1764e-018
v  ǁVelocityǁ         0.0058333          10.508          4.7238          4.7238
v  Pressure               -66.304          20.097          1.3031          1.3031
v  nu_tilda           9.4137e-007       0.0041682      0.00055156      0.00055156
v  TempC                       21          73.344          21.182          21.182
v  TurbVisc           6.9531e-013       0.0049114      0.00063666      0.00063666
v  total_pressure     1.0126e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              119:        0.24120E+01

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


 INSTANT    0.120000000E+03   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25412E-01 0.95885E+00
   Friction velocity        uk    :  0.25412E-01 0.95885E+00
   Dimensionless distance   yplus :  0.20458E+00 0.77194E+01
   Friction thermal sca.    tstar : -0.61024E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15264E+00 0.57595E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42167E-02      35   0.11430E-02   0.84918E+01 0.17956E+03 
c  Velocity[X]                                      0.38194E+01 
c  Velocity[Y]                                      0.46723E+01 
c  Velocity[Z]                                      0.68208E-29 
c  Pressure     0.16554E-06     489   0.91537E-08   0.14417E+00 0.86621E+03 
c  nu_tilda     0.26523E-05      36   0.13246E-04   0.12467E-05 0.63857E+03 
c  TempC        0.18851E+02      30   0.95021E-03   0.15572E+02 0.40992E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7802          10.441          4.5729          4.5729
v  Velocity[Y]            -4.4979          8.2673      0.00042086      0.00042086
v  Velocity[Z]         -1.09e-014     1.0311e-014    -7.0356e-018    -7.0356e-018
v  ǁVelocityǁ         0.0044505          10.495          4.7244          4.7244
v  Pressure               -65.964          19.987          1.2785          1.2785
v  nu_tilda           9.3983e-007       0.0041693      0.00055215      0.00055215
v  TempC                       21          72.138          21.183          21.183
v  TurbVisc           6.9089e-013       0.0049127      0.00063727      0.00063727
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              120:        0.25700E+01

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


 INSTANT    0.121000000E+03   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21363E-01 0.95785E+00
   Friction velocity        uk    :  0.21363E-01 0.95785E+00
   Dimensionless distance   yplus :  0.17199E+00 0.77113E+01
   Friction thermal sca.    tstar : -0.86445E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12832E+00 0.57535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42213E-02      35   0.99580E-03   0.84483E+01 0.17886E+03 
c  Velocity[X]                                      0.38253E+01 
c  Velocity[Y]                                      0.46230E+01 
c  Velocity[Z]                                      0.62401E-29 
c  Pressure     0.15718E-06     489   0.96948E-08   0.13695E+00 0.72999E+03 
c  nu_tilda     0.26600E-05      36   0.24317E-04   0.12348E-05 0.63431E+03 
c  TempC        0.18872E+02      30   0.89203E-03   0.14972E+02 0.42402E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.755          10.432          4.5729          4.5729
v  Velocity[Y]            -4.4824          8.2895      0.00042628      0.00042628
v  Velocity[Z]       -1.0895e-014      1.009e-014    -6.8916e-018    -6.8916e-018
v  ǁVelocityǁ         0.0034306          10.484          4.7249          4.7249
v  Pressure                -65.76          19.984          1.2449          1.2449
v  nu_tilda           9.3797e-007       0.0041703      0.00055263      0.00055263
v  TempC                       21          71.934          21.184          21.184
v  TurbVisc           6.8639e-013       0.0049139      0.00063789      0.00063789
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              121:        0.23370E+01

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


 INSTANT    0.122000000E+03   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24789E-02 0.95879E+00
   Friction velocity        uk    :  0.24789E-02 0.95879E+00
   Dimensionless distance   yplus :  0.19957E-01 0.77189E+01
   Friction thermal sca.    tstar : -0.22454E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14890E-01 0.57592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42259E-02      35   0.95608E-03   0.82504E+01 0.17698E+03 
c  Velocity[X]                                      0.37276E+01 
c  Velocity[Y]                                      0.45228E+01 
c  Velocity[Z]                                      0.45297E-29 
c  Pressure     0.15719E-06     458   0.97834E-08   0.13749E+00 0.69245E+03 
c  nu_tilda     0.26677E-05      36   0.13355E-04   0.12231E-05 0.63010E+03 
c  TempC        0.18893E+02      30   0.83924E-03   0.14663E+02 0.40624E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7361          10.426          4.5729          4.5729
v  Velocity[Y]             -4.465          8.2632       0.0004322       0.0004322
v  Velocity[Z]       -1.0841e-014     9.8888e-015    -6.7529e-018    -6.7529e-018
v  ǁVelocityǁ         0.0025851          10.471          4.7255          4.7255
v  Pressure               -65.467          19.912          1.2283          1.2283
v  nu_tilda           9.3644e-007       0.0041713      0.00055322      0.00055322
v  TempC                       21          73.045          21.186          21.186
v  TurbVisc           6.8097e-013       0.0049151       0.0006385       0.0006385
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              122:        0.25660E+01

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


 INSTANT    0.123000000E+03   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73781E-02 0.95775E+00
   Friction velocity        uk    :  0.73781E-02 0.95775E+00
   Dimensionless distance   yplus :  0.59399E-01 0.77105E+01
   Friction thermal sca.    tstar : -0.10345E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44318E-01 0.57529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42305E-02      35   0.98721E-03   0.81047E+01 0.17545E+03 
c  Velocity[X]                                      0.36678E+01 
c  Velocity[Y]                                      0.44370E+01 
c  Velocity[Z]                                      0.47378E-29 
c  Pressure     0.13871E-06     488   0.96003E-08   0.12195E+00 0.70263E+03 
c  nu_tilda     0.26753E-05      36   0.24079E-04   0.12115E-05 0.62594E+03 
c  TempC        0.18915E+02      30   0.80727E-03   0.14851E+02 0.40522E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7195          10.419          4.5729          4.5729
v  Velocity[Y]            -4.4493          8.2888      0.00043799      0.00043799
v  Velocity[Z]       -1.0773e-014     9.6373e-015    -6.6084e-018    -6.6084e-018
v  ǁVelocityǁ         0.0029396          10.458           4.726           4.726
v  Pressure               -65.274          19.912          1.1959          1.1959
v  nu_tilda            9.331e-007       0.0041723      0.00055371      0.00055371
v  TempC                       21          72.724          21.187          21.187
v  TurbVisc           6.7653e-013       0.0049163      0.00063912      0.00063912
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              123:        0.34030E+01

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


 INSTANT    0.124000000E+03   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11783E-01 0.95834E+00
   Friction velocity        uk    :  0.11783E-01 0.95834E+00
   Dimensionless distance   yplus :  0.94861E-01 0.77153E+01
   Friction thermal sca.    tstar : -0.64119E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70777E-01 0.57565E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42351E-02      35   0.10663E-02   0.80284E+01 0.17449E+03 
c  Velocity[X]                                      0.36333E+01 
c  Velocity[Y]                                      0.43951E+01 
c  Velocity[Z]                                      0.65950E-29 
c  Pressure     0.18096E-06     456   0.98700E-08   0.15677E+00 0.63333E+03 
c  nu_tilda     0.26829E-05      36   0.13468E-04   0.12002E-05 0.62184E+03 
c  TempC        0.18936E+02      30   0.87900E-03   0.13537E+02 0.39547E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6992           10.41          4.5729          4.5729
v  Velocity[Y]            -4.4332          8.2776      0.00044388      0.00044388
v  Velocity[Z]       -1.0704e-014     9.6004e-015    -6.4644e-018    -6.4644e-018
v  ǁVelocityǁ         0.0037336           10.45          4.7266          4.7266
v  Pressure               -64.975          19.855          1.1819          1.1819
v  nu_tilda           9.2926e-007       0.0041733       0.0005543       0.0005543
v  TempC                       21          72.548          21.188          21.188
v  TurbVisc           6.6693e-013       0.0049175      0.00063973      0.00063973
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              124:        0.32400E+01

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


 INSTANT    0.125000000E+03   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14946E-01 0.95736E+00
   Friction velocity        uk    :  0.14946E-01 0.95736E+00
   Dimensionless distance   yplus :  0.12032E+00 0.77074E+01
   Friction thermal sca.    tstar : -0.57699E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89775E-01 0.57506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42397E-02      35   0.98173E-03   0.79756E+01 0.17369E+03 
c  Velocity[X]                                      0.36597E+01 
c  Velocity[Y]                                      0.43159E+01 
c  Velocity[Z]                                      0.60905E-29 
c  Pressure     0.16016E-06     537   0.93881E-08   0.14181E+00 0.12447E+04 
c  nu_tilda     0.26904E-05      36   0.23850E-04   0.11889E-05 0.61778E+03 
c  TempC        0.18957E+02      30   0.80389E-03   0.14052E+02 0.39955E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6758          10.402          4.5729          4.5729
v  Velocity[Y]            -4.4167          8.2445      0.00044967      0.00044967
v  Velocity[Z]        -1.061e-014     9.6272e-015    -6.3275e-018    -6.3275e-018
v  ǁVelocityǁ         0.0044417          10.442          4.7271          4.7271
v  Pressure               -64.713          19.724          1.1261          1.1261
v  nu_tilda           9.2613e-007       0.0041743      0.00055479      0.00055479
v  TempC                       21          72.674           21.19           21.19
v  TurbVisc           6.5602e-013       0.0049186      0.00064036      0.00064036
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              125:        0.30220E+01

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


 INSTANT    0.126000000E+03   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13254E-01 0.95559E+00
   Friction velocity        uk    :  0.13254E-01 0.95559E+00
   Dimensionless distance   yplus :  0.10670E+00 0.76931E+01
   Friction thermal sca.    tstar : -0.15961E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79613E-01 0.57399E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42442E-02      35   0.99255E-03   0.77774E+01 0.17177E+03 
c  Velocity[X]                                      0.35743E+01 
c  Velocity[Y]                                      0.42030E+01 
c  Velocity[Z]                                      0.52895E-29 
c  Pressure     0.15943E-06     472   0.99577E-08   0.13938E+00 0.67883E+03 
c  nu_tilda     0.26979E-05      36   0.13547E-04   0.11780E-05 0.61378E+03 
c  TempC        0.18978E+02      30   0.79791E-03   0.14052E+02 0.39708E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6513          10.392          4.5729          4.5729
v  Velocity[Y]            -4.4007           8.261      0.00045585      0.00045585
v  Velocity[Z]       -1.0488e-014     9.7579e-015    -6.1879e-018    -6.1879e-018
v  ǁVelocityǁ         0.0028381          10.433          4.7277          4.7277
v  Pressure               -64.444          19.789          1.1379          1.1379
v  nu_tilda           9.2339e-007       0.0041752      0.00055539      0.00055539
v  TempC                       21          72.759          21.191          21.191
v  TurbVisc           6.4722e-013       0.0049198      0.00064098      0.00064098
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              126:        0.38580E+01

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


 INSTANT    0.127000000E+03   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84358E-02 0.95627E+00
   Friction velocity        uk    :  0.84358E-02 0.95627E+00
   Dimensionless distance   yplus :  0.67914E-01 0.76986E+01
   Friction thermal sca.    tstar : -0.72045E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50671E-01 0.57440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42488E-02      35   0.92911E-03   0.76566E+01 0.17044E+03 
c  Velocity[X]                                      0.35004E+01 
c  Velocity[Y]                                      0.41562E+01 
c  Velocity[Z]                                      0.52269E-29 
c  Pressure     0.15056E-06     538   0.95085E-08   0.13517E+00 0.13749E+04 
c  nu_tilda     0.27053E-05      36   0.23627E-04   0.11671E-05 0.60983E+03 
c  TempC        0.18999E+02      30   0.84856E-03   0.13626E+02 0.39257E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.636          10.382          4.5729          4.5729
v  Velocity[Y]            -4.3845          8.2281      0.00046191      0.00046191
v  Velocity[Z]       -1.0371e-014     9.7845e-015     -6.047e-018     -6.047e-018
v  ǁVelocityǁ         0.0020452          10.424          4.7282          4.7282
v  Pressure               -64.227           19.64          1.0773          1.0773
v  nu_tilda           9.2023e-007       0.0041762      0.00055588      0.00055588
v  TempC                       21          72.944          21.192          21.192
v  TurbVisc            6.396e-013       0.0049209      0.00064161      0.00064161
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              127:        0.43720E+01

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


 INSTANT    0.128000000E+03   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80197E-02 0.95486E+00
   Friction velocity        uk    :  0.80197E-02 0.95486E+00
   Dimensionless distance   yplus :  0.64564E-01 0.76873E+01
   Friction thermal sca.    tstar : -0.11192E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48172E-01 0.57356E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42533E-02      35   0.95904E-03   0.75146E+01 0.16889E+03 
c  Velocity[X]                                      0.34519E+01 
c  Velocity[Y]                                      0.40628E+01 
c  Velocity[Z]                                      0.62123E-29 
c  Pressure     0.14076E-06     424   0.94842E-08   0.12292E+00 0.58754E+03 
c  nu_tilda     0.27128E-05      36   0.13643E-04   0.11565E-05 0.60592E+03 
c  TempC        0.19021E+02      30   0.88302E-03   0.13146E+02 0.39141E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6173           10.37          4.5729          4.5729
v  Velocity[Y]            -4.3686          8.2501      0.00046852      0.00046852
v  Velocity[Z]       -1.0235e-014     9.7769e-015    -5.9165e-018    -5.9165e-018
v  ǁVelocityǁ         0.0013233          10.414          4.7287          4.7287
v  Pressure               -63.978          19.688          1.0837          1.0837
v  nu_tilda           9.1666e-007       0.0041771      0.00055648      0.00055648
v  TempC                       21          72.833          21.193          21.193
v  TurbVisc           6.3088e-013        0.004922      0.00064223      0.00064223
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              128:        0.42090E+01

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


 INSTANT    0.129000000E+03   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68540E-02 0.95586E+00
   Friction velocity        uk    :  0.68540E-02 0.95586E+00
   Dimensionless distance   yplus :  0.55179E-01 0.76953E+01
   Friction thermal sca.    tstar : -0.13626E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41170E-01 0.57416E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42578E-02      35   0.10456E-02   0.74611E+01 0.16794E+03 
c  Velocity[X]                                      0.34781E+01 
c  Velocity[Y]                                      0.39830E+01 
c  Velocity[Z]                                      0.57987E-29 
c  Pressure     0.20169E-06     550   0.96614E-08   0.17484E+00 0.14890E+04 
c  nu_tilda     0.27201E-05      36   0.23413E-04   0.11459E-05 0.60206E+03 
c  TempC        0.19042E+02      30   0.82234E-03   0.14980E+02 0.39847E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5955          10.359          4.5729          4.5729
v  Velocity[Y]            -4.3531          8.2156      0.00047475      0.00047475
v  Velocity[Z]       -1.0062e-014     9.7564e-015    -5.7805e-018    -5.7805e-018
v  ǁVelocityǁ         0.0010015          10.403          4.7292          4.7292
v  Pressure               -63.715          19.514          1.0204          1.0204
v  nu_tilda           9.1287e-007        0.004178      0.00055697      0.00055697
v  TempC                       21          72.108          21.195          21.195
v  TurbVisc           6.2116e-013       0.0049231      0.00064286      0.00064286
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              129:        0.49970E+01

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


 INSTANT    0.130000000E+03   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73226E-02 0.95520E+00
   Friction velocity        uk    :  0.73226E-02 0.95520E+00
   Dimensionless distance   yplus :  0.58952E-01 0.76900E+01
   Friction thermal sca.    tstar : -0.13692E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43985E-01 0.57376E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42623E-02      35   0.84797E-03   0.73499E+01 0.16680E+03 
c  Velocity[X]                                      0.34146E+01 
c  Velocity[Y]                                      0.39353E+01 
c  Velocity[Z]                                      0.59065E-29 
c  Pressure     0.17291E-06     488   0.98674E-08   0.15242E+00 0.88780E+03 
c  nu_tilda     0.27275E-05      36   0.13702E-04   0.11356E-05 0.59825E+03 
c  TempC        0.19063E+02      30   0.78571E-03   0.13633E+02 0.39429E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5711          10.347          4.5729          4.5729
v  Velocity[Y]            -4.3364           8.239      0.00048129      0.00048129
v  Velocity[Z]       -9.9454e-015     9.7789e-015    -5.6458e-018    -5.6458e-018
v  ǁVelocityǁ         0.0013839          10.392          4.7297          4.7297
v  Pressure               -63.464          19.628          1.0408          1.0408
v  nu_tilda           9.0873e-007        0.004179      0.00055757      0.00055757
v  TempC                       21          72.193          21.196          21.196
v  TurbVisc           6.1093e-013       0.0049242      0.00064349      0.00064349
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              130:        0.44920E+01

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


 INSTANT    0.131000000E+03   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26217E-02 0.95614E+00
   Friction velocity        uk    :  0.26217E-02 0.95614E+00
   Dimensionless distance   yplus :  0.21106E-01 0.76976E+01
   Friction thermal sca.    tstar : -0.20600E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15748E-01 0.57432E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42668E-02      35   0.93228E-03   0.71745E+01 0.16507E+03 
c  Velocity[X]                                      0.33082E+01 
c  Velocity[Y]                                      0.38663E+01 
c  Velocity[Z]                                      0.51544E-29 
c  Pressure     0.13772E-06     536   0.99283E-08   0.12150E+00 0.10857E+04 
c  nu_tilda     0.27348E-05      36   0.23203E-04   0.11254E-05 0.59448E+03 
c  TempC        0.19083E+02      30   0.80700E-03   0.12755E+02 0.37664E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.553          10.336          4.5729          4.5729
v  Velocity[Y]            -4.3207          8.2453      0.00048781      0.00048781
v  Velocity[Z]        -9.755e-015       9.82e-015    -5.5174e-018    -5.5174e-018
v  ǁVelocityǁ         0.0028546           10.38          4.7302          4.7302
v  Pressure               -63.233          19.528          0.9908          0.9908
v  nu_tilda            9.037e-007       0.0041799      0.00055807      0.00055807
v  TempC                       21          72.109          21.197          21.197
v  TurbVisc           5.9993e-013       0.0049253      0.00064413      0.00064413
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              131:        0.44180E+01

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


 INSTANT    0.132000000E+03   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14683E-01 0.95524E+00
   Friction velocity        uk    :  0.14683E-01 0.95524E+00
   Dimensionless distance   yplus :  0.11821E+00 0.76903E+01
   Friction thermal sca.    tstar : -0.68381E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88196E-01 0.57379E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42712E-02      35   0.10105E-02   0.70901E+01 0.16386E+03 
c  Velocity[X]                                      0.33174E+01 
c  Velocity[Y]                                      0.37727E+01 
c  Velocity[Z]                                      0.45735E-29 
c  Pressure     0.17080E-06     486   0.94022E-08   0.15283E+00 0.71115E+03 
c  nu_tilda     0.27421E-05      36   0.13732E-04   0.11154E-05 0.59076E+03 
c  TempC        0.19104E+02      30   0.78135E-03   0.13184E+02 0.38187E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5355          10.324          4.5729          4.5729
v  Velocity[Y]            -4.3061          8.2029      0.00049487      0.00049487
v  Velocity[Z]       -9.5341e-015     9.8261e-015    -5.3916e-018    -5.3916e-018
v  ǁVelocityǁ         0.0028539          10.367          4.7307          4.7307
v  Pressure               -62.941          19.438         0.97356         0.97356
v  nu_tilda           8.9822e-007       0.0041808      0.00055868      0.00055868
v  TempC                       21          72.486          21.198          21.198
v  TurbVisc           5.8677e-013       0.0049264      0.00064476      0.00064476
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              132:        0.40310E+01

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


 INSTANT    0.133000000E+03   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11039E-01 0.95335E+00
   Friction velocity        uk    :  0.11039E-01 0.95335E+00
   Dimensionless distance   yplus :  0.88875E-01 0.76751E+01
   Friction thermal sca.    tstar : -0.63059E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66311E-01 0.57265E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42757E-02      35   0.95017E-03   0.70472E+01 0.16316E+03 
c  Velocity[X]                                      0.33021E+01 
c  Velocity[Y]                                      0.37451E+01 
c  Velocity[Z]                                      0.65316E-29 
c  Pressure     0.17086E-06     490   0.98279E-08   0.14953E+00 0.62634E+03 
c  nu_tilda     0.27493E-05      36   0.23003E-04   0.11055E-05 0.58708E+03 
c  TempC        0.19125E+02      30   0.79960E-03   0.12811E+02 0.37529E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5155          10.316          4.5729          4.5729
v  Velocity[Y]            -4.2899          8.2197      0.00050137      0.00050137
v  Velocity[Z]       -9.3712e-015     9.9614e-015     -5.265e-018     -5.265e-018
v  ǁVelocityǁ         0.0025728          10.357          4.7312          4.7312
v  Pressure               -62.739          19.435         0.94497         0.94497
v  nu_tilda           8.9235e-007       0.0041816      0.00055918      0.00055918
v  TempC                       21          72.145            21.2            21.2
v  TurbVisc           5.7265e-013       0.0049274       0.0006454       0.0006454
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              133:        0.37280E+01

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


 INSTANT    0.134000000E+03   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10141E-01 0.95428E+00
   Friction velocity        uk    :  0.10141E-01 0.95428E+00
   Dimensionless distance   yplus :  0.81642E-01 0.76826E+01
   Friction thermal sca.    tstar : -0.84670E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60914E-01 0.57321E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42801E-02      35   0.87288E-03   0.69034E+01 0.16157E+03 
c  Velocity[X]                                      0.32637E+01 
c  Velocity[Y]                                      0.36397E+01 
c  Velocity[Z]                                      0.58950E-29 
c  Pressure     0.18947E-06     425   0.92049E-08   0.16946E+00 0.52576E+03 
c  nu_tilda     0.27565E-05      36   0.13785E-04   0.10958E-05 0.58345E+03 
c  TempC        0.19146E+02      30   0.78121E-03   0.13226E+02 0.38493E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.493          10.309          4.5729          4.5729
v  Velocity[Y]            -4.2744          8.1948       0.0005083       0.0005083
v  Velocity[Z]       -9.1734e-015     1.0085e-014    -5.1477e-018    -5.1477e-018
v  ǁVelocityǁ         0.0022363          10.345          4.7317          4.7317
v  Pressure               -62.426           19.39         0.93769         0.93769
v  nu_tilda           8.8682e-007       0.0041825      0.00055978      0.00055978
v  TempC                       21          72.221          21.201          21.201
v  TurbVisc           5.5784e-013       0.0049285      0.00064604      0.00064604
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              134:        0.33220E+01

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


 INSTANT    0.135000000E+03   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41871E-02 0.95304E+00
   Friction velocity        uk    :  0.41871E-02 0.95304E+00
   Dimensionless distance   yplus :  0.33709E-01 0.76726E+01
   Friction thermal sca.    tstar : -0.33506E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25151E-01 0.57246E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42846E-02      35   0.98035E-03   0.67477E+01 0.15988E+03 
c  Velocity[X]                                      0.31929E+01 
c  Velocity[Y]                                      0.35548E+01 
c  Velocity[Z]                                      0.45077E-29 
c  Pressure     0.13322E-06     489   0.96241E-08   0.11723E+00 0.60448E+03 
c  nu_tilda     0.27636E-05      36   0.22802E-04   0.10861E-05 0.57985E+03 
c  TempC        0.19167E+02      30   0.81292E-03   0.12657E+02 0.37564E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4702          10.302          4.5729          4.5729
v  Velocity[Y]            -4.2594          8.2169      0.00051529      0.00051529
v  Velocity[Z]       -8.9668e-015     1.0302e-014    -5.0329e-018    -5.0329e-018
v  ǁVelocityǁ         0.0026122          10.334          4.7322          4.7322
v  Pressure               -62.209          19.401         0.91027         0.91027
v  nu_tilda           8.8156e-007       0.0041834      0.00056029      0.00056029
v  TempC                       21           72.25          21.202          21.202
v  TurbVisc           5.4414e-013       0.0049295      0.00064668      0.00064668
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              135:        0.36830E+01

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


 INSTANT    0.136000000E+03   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11740E-01 0.95375E+00
   Friction velocity        uk    :  0.11740E-01 0.95375E+00
   Dimensionless distance   yplus :  0.94518E-01 0.76784E+01
   Friction thermal sca.    tstar : -0.89202E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70521E-01 0.57289E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42890E-02      35   0.98929E-03   0.66919E+01 0.15901E+03 
c  Velocity[X]                                      0.31744E+01 
c  Velocity[Y]                                      0.35175E+01 
c  Velocity[Z]                                      0.56510E-29 
c  Pressure     0.17623E-06     488   0.97163E-08   0.15568E+00 0.68492E+03 
c  nu_tilda     0.27708E-05      36   0.13798E-04   0.10767E-05 0.57630E+03 
c  TempC        0.19187E+02      30   0.76582E-03   0.12578E+02 0.37128E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4542          10.294          4.5729          4.5729
v  Velocity[Y]            -4.2437          8.1762      0.00052269      0.00052269
v  Velocity[Z]       -8.8129e-015     1.0751e-014     -4.917e-018     -4.917e-018
v  ǁVelocityǁ         0.0028186          10.326          4.7327          4.7327
v  Pressure                -61.88          19.313          0.8945          0.8945
v  nu_tilda           8.7611e-007       0.0041842       0.0005609       0.0005609
v  TempC                       21          72.335          21.203          21.203
v  TurbVisc           5.3134e-013       0.0049305      0.00064732      0.00064732
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              136:        0.36260E+01

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


 INSTANT    0.137000000E+03   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11164E-01 0.95260E+00
   Friction velocity        uk    :  0.11164E-01 0.95260E+00
   Dimensionless distance   yplus :  0.89879E-01 0.76691E+01
   Friction thermal sca.    tstar : -0.69745E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67060E-01 0.57220E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42934E-02      35   0.80609E-03   0.66564E+01 0.15828E+03 
c  Velocity[X]                                      0.32037E+01 
c  Velocity[Y]                                      0.34527E+01 
c  Velocity[Z]                                      0.49364E-29 
c  Pressure     0.16916E-06     474   0.98701E-08   0.14950E+00 0.55790E+03 
c  nu_tilda     0.27779E-05      36   0.22610E-04   0.10673E-05 0.57279E+03 
c  TempC        0.19208E+02      30   0.90275E-03   0.11896E+02 0.36420E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4357          10.284          4.5729          4.5729
v  Velocity[Y]            -4.2287          8.2019      0.00052971      0.00052971
v  Velocity[Z]       -8.7258e-015     1.1173e-014    -4.8067e-018    -4.8067e-018
v  ǁVelocityǁ         0.0035765          10.318          4.7332          4.7332
v  Pressure               -61.687          19.355         0.87565         0.87565
v  nu_tilda           8.7051e-007       0.0041851       0.0005614       0.0005614
v  TempC                       21          72.368          21.204          21.204
v  TurbVisc           5.1833e-013       0.0049315      0.00064797      0.00064797
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              137:        0.35330E+01

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


 INSTANT    0.138000000E+03   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17622E-01 0.95355E+00
   Friction velocity        uk    :  0.17622E-01 0.95355E+00
   Dimensionless distance   yplus :  0.14187E+00 0.76767E+01
   Friction thermal sca.    tstar : -0.11745E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10585E+00 0.57277E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42978E-02      35   0.93085E-03   0.64649E+01 0.15635E+03 
c  Velocity[X]                                      0.31035E+01 
c  Velocity[Y]                                      0.33614E+01 
c  Velocity[Z]                                      0.56502E-29 
c  Pressure     0.15467E-06     393   0.93610E-08   0.13757E+00 0.47672E+03 
c  nu_tilda     0.27849E-05      36   0.13856E-04   0.10582E-05 0.56931E+03 
c  TempC        0.19229E+02      30   0.76561E-03   0.13476E+02 0.38556E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.415          10.276          4.5729          4.5729
v  Velocity[Y]            -4.2139          8.2001      0.00053726      0.00053726
v  Velocity[Z]       -8.6261e-015     1.1548e-014    -4.6908e-018    -4.6908e-018
v  ǁVelocityǁ         0.0043977          10.309          4.7337          4.7337
v  Pressure                 -61.4          19.361         0.87951         0.87951
v  nu_tilda           8.6437e-007       0.0041859      0.00056202      0.00056202
v  TempC                       21          72.452          21.206          21.206
v  TurbVisc            5.052e-013       0.0049325      0.00064862      0.00064862
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              138:        0.32030E+01

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


 INSTANT    0.139000000E+03   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18445E-01 0.95241E+00
   Friction velocity        uk    :  0.18445E-01 0.95241E+00
   Dimensionless distance   yplus :  0.14850E+00 0.76675E+01
   Friction thermal sca.    tstar : -0.13824E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11079E+00 0.57208E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43022E-02      35   0.85010E-03   0.64133E+01 0.15551E+03 
c  Velocity[X]                                      0.30801E+01 
c  Velocity[Y]                                      0.33332E+01 
c  Velocity[Z]                                      0.66498E-29 
c  Pressure     0.15349E-06     505   0.93857E-08   0.13831E+00 0.11268E+04 
c  nu_tilda     0.27919E-05      36   0.22415E-04   0.10491E-05 0.56588E+03 
c  TempC        0.19249E+02      30   0.79789E-03   0.12783E+02 0.37266E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3915          10.266          4.5729          4.5729
v  Velocity[Y]            -4.1984          8.1676      0.00054442      0.00054442
v  Velocity[Z]       -8.6436e-015     1.2011e-014    -4.5794e-018    -4.5794e-018
v  ǁVelocityǁ         0.0047651            10.3          4.7342          4.7342
v  Pressure               -61.163          19.248         0.82894         0.82894
v  nu_tilda           8.5925e-007       0.0041867      0.00056252      0.00056252
v  TempC                       21          72.539          21.207          21.207
v  TurbVisc           4.9109e-013       0.0049335      0.00064927      0.00064927
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              139:        0.46840E+01

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


 INSTANT    0.140000000E+03   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14044E-01 0.95037E+00
   Friction velocity        uk    :  0.14044E-01 0.95037E+00
   Dimensionless distance   yplus :  0.11306E+00 0.76511E+01
   Friction thermal sca.    tstar : -0.74164E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84358E-01 0.57086E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43065E-02      35   0.90221E-03   0.62896E+01 0.15393E+03 
c  Velocity[X]                                      0.30461E+01 
c  Velocity[Y]                                      0.32435E+01 
c  Velocity[Z]                                      0.51859E-29 
c  Pressure     0.17912E-06     425   0.95063E-08   0.15599E+00 0.55625E+03 
c  nu_tilda     0.27989E-05      36   0.13871E-04   0.10402E-05 0.56248E+03 
c  TempC        0.19270E+02      30   0.83930E-03   0.12550E+02 0.37178E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3741          10.256          4.5729          4.5729
v  Velocity[Y]            -4.1831          8.1788      0.00055241      0.00055241
v  Velocity[Z]       -8.7166e-015     1.2361e-014    -4.4625e-018    -4.4625e-018
v  ǁVelocityǁ         0.0049822           10.29          4.7347          4.7347
v  Pressure               -60.859          19.276         0.83893         0.83893
v  nu_tilda           8.5515e-007       0.0041876      0.00056314      0.00056314
v  TempC                       21          72.418          21.208          21.208
v  TurbVisc           4.7957e-013       0.0049345      0.00064991      0.00064991
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              140:        0.48820E+01

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


 INSTANT    0.141000000E+03   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14479E-01 0.95134E+00
   Friction velocity        uk    :  0.14479E-01 0.95134E+00
   Dimensionless distance   yplus :  0.11657E+00 0.76590E+01
   Friction thermal sca.    tstar : -0.10595E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86972E-01 0.57144E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43109E-02      35   0.99341E-03   0.62518E+01 0.15322E+03 
c  Velocity[X]                                      0.30762E+01 
c  Velocity[Y]                                      0.31756E+01 
c  Velocity[Z]                                      0.47881E-29 
c  Pressure     0.16507E-06     517   0.93418E-08   0.14859E+00 0.10322E+04 
c  nu_tilda     0.28059E-05      36   0.22231E-04   0.10313E-05 0.55913E+03 
c  TempC        0.19290E+02      30   0.67928E-03   0.12639E+02 0.37165E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3566          10.245          4.5729          4.5729
v  Velocity[Y]            -4.1685          8.1549      0.00055997      0.00055997
v  Velocity[Z]       -8.7749e-015     1.1446e-014    -4.3492e-018    -4.3492e-018
v  ǁVelocityǁ         0.0043232           10.28          4.7352          4.7352
v  Pressure               -60.597          19.176         0.79221         0.79221
v  nu_tilda           8.5068e-007       0.0041884      0.00056365      0.00056365
v  TempC                       21          72.404          21.209          21.209
v  TurbVisc           4.7048e-013       0.0049354      0.00065057      0.00065057
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              141:        0.38880E+01

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


 INSTANT    0.142000000E+03   TIME STEP NUMBER             142
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76446E-02 0.95029E+00
   Friction velocity        uk    :  0.76446E-02 0.95029E+00
   Dimensionless distance   yplus :  0.61545E-01 0.76505E+01
   Friction thermal sca.    tstar : -0.16921E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45919E-01 0.57081E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43153E-02      35   0.90142E-03   0.61619E+01 0.15221E+03 
c  Velocity[X]                                      0.30132E+01 
c  Velocity[Y]                                      0.31486E+01 
c  Velocity[Z]                                      0.56209E-29 
c  Pressure     0.14696E-06     458   0.94240E-08   0.13005E+00 0.85068E+03 
c  nu_tilda     0.28128E-05      36   0.13926E-04   0.10227E-05 0.55581E+03 
c  TempC        0.19311E+02      30   0.61910E-03   0.10833E+02 0.35191E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3372          10.234          4.5729          4.5729
v  Velocity[Y]            -4.1534           8.173      0.00056786      0.00056786
v  Velocity[Z]       -8.8585e-015     1.1438e-014    -4.2252e-018    -4.2252e-018
v  ǁVelocityǁ         0.0016523          10.269          4.7356          4.7356
v  Pressure               -60.345          19.275         0.81339         0.81339
v  nu_tilda           8.4583e-007       0.0041892      0.00056427      0.00056427
v  TempC                   20.968          72.399           21.21           21.21
v  TurbVisc           4.6072e-013       0.0049364      0.00065122      0.00065122
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              142:        0.35140E+01

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


 INSTANT    0.143000000E+03   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93704E-02 0.95099E+00
   Friction velocity        uk    :  0.93704E-02 0.95099E+00
   Dimensionless distance   yplus :  0.75438E-01 0.76561E+01
   Friction thermal sca.    tstar : -0.83672E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56285E-01 0.57123E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43196E-02      35   0.91270E-03   0.60242E+01 0.15058E+03 
c  Velocity[X]                                      0.29499E+01 
c  Velocity[Y]                                      0.30742E+01 
c  Velocity[Z]                                      0.50695E-29 
c  Pressure     0.17443E-06     506   0.99604E-08   0.15678E+00 0.97303E+03 
c  nu_tilda     0.28197E-05      36   0.22045E-04   0.10141E-05 0.55252E+03 
c  TempC        0.19331E+02      30   0.80403E-03   0.97084E+01 0.32421E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3157          10.223          4.5729          4.5729
v  Velocity[Y]            -4.1385          8.1399      0.00057595      0.00057595
v  Velocity[Z]       -8.8758e-015     1.1523e-014    -4.1043e-018    -4.1043e-018
v  ǁVelocityǁ         0.0011486          10.259          4.7361          4.7361
v  Pressure               -60.089          19.177          0.7697          0.7697
v  nu_tilda           8.4131e-007       0.0041899      0.00056478      0.00056478
v  TempC                   20.998          72.444          21.212          21.212
v  TurbVisc           4.5029e-013       0.0049373      0.00065188      0.00065188
v  total_pressure     1.0126e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              143:        0.37660E+01

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


 INSTANT    0.144000000E+03   TIME STEP NUMBER             144
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59123E-02 0.94953E+00
   Friction velocity        uk    :  0.59123E-02 0.94953E+00
   Dimensionless distance   yplus :  0.47598E-01 0.76444E+01
   Friction thermal sca.    tstar : -0.10272E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35514E-01 0.57036E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43239E-02      35   0.89139E-03   0.59602E+01 0.14952E+03 
c  Velocity[X]                                      0.29662E+01 
c  Velocity[Y]                                      0.29940E+01 
c  Velocity[Z]                                      0.47700E-29 
c  Pressure     0.13902E-06     488   0.96254E-08   0.12344E+00 0.70626E+03 
c  nu_tilda     0.28265E-05      36   0.13938E-04   0.10057E-05 0.54927E+03 
c  TempC        0.19351E+02      30   0.75706E-03   0.12433E+02 0.37179E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2948          10.212          4.5729          4.5729
v  Velocity[Y]            -4.1241          8.1643       0.0005839       0.0005839
v  Velocity[Z]       -8.8727e-015     1.1628e-014    -3.9896e-018    -3.9896e-018
v  ǁVelocityǁ         0.0066059          10.249          4.7366          4.7366
v  Pressure                -59.83          19.249         0.78536         0.78536
v  nu_tilda           8.3674e-007       0.0041907       0.0005654       0.0005654
v  TempC                   20.998          72.564          21.213          21.213
v  TurbVisc           4.4075e-013       0.0049383      0.00065253      0.00065253
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              144:        0.36240E+01

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


 INSTANT    0.145000000E+03   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19504E-01 0.95021E+00
   Friction velocity        uk    :  0.19504E-01 0.95021E+00
   Dimensionless distance   yplus :  0.15702E+00 0.76499E+01
   Friction thermal sca.    tstar : -0.13823E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11716E+00 0.57077E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43283E-02      35   0.85928E-03   0.59132E+01 0.14878E+03 
c  Velocity[X]                                      0.29396E+01 
c  Velocity[Y]                                      0.29736E+01 
c  Velocity[Z]                                      0.53132E-29 
c  Pressure     0.18650E-06     536   0.99014E-08   0.16161E+00 0.84698E+03 
c  nu_tilda     0.28334E-05      36   0.21866E-04   0.99729E-06 0.54606E+03 
c  TempC        0.19372E+02      30   0.78314E-03   0.12320E+02 0.36332E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2787          10.201          4.5729          4.5729
v  Velocity[Y]            -4.1099          8.1543       0.0005925       0.0005925
v  Velocity[Z]       -8.8957e-015     1.1746e-014    -3.8588e-018    -3.8588e-018
v  ǁVelocityǁ          0.006721          10.238          4.7371          4.7371
v  Pressure               -59.578          19.173         0.74575         0.74575
v  nu_tilda           8.3145e-007       0.0041915      0.00056592      0.00056592
v  TempC                       21           72.52          21.214          21.214
v  TurbVisc           4.3125e-013       0.0049392      0.00065319      0.00065319
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              145:        0.38780E+01

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


 INSTANT    0.146000000E+03   TIME STEP NUMBER             146
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56787E-02 0.94931E+00
   Friction velocity        uk    :  0.56787E-02 0.94931E+00
   Dimensionless distance   yplus :  0.45718E-01 0.76426E+01
   Friction thermal sca.    tstar : -0.64268E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34110E-01 0.57023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43326E-02      34   0.76014E-03   0.57729E+01 0.14712E+03 
c  Velocity[X]                                      0.28937E+01 
c  Velocity[Y]                                      0.28792E+01 
c  Velocity[Z]                                      0.52323E-29 
c  Pressure     0.15591E-06     298   0.98611E-08   0.13956E+00 0.42590E+03 
c  nu_tilda     0.28401E-05      35   0.13987E-04   0.98912E-06 0.54288E+03 
c  TempC        0.19392E+02      29   0.79402E-03   0.11793E+02 0.36007E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2601          10.193          4.5729          4.5729
v  Velocity[Y]            -4.0949          8.1206       0.0006006       0.0006006
v  Velocity[Z]       -8.8553e-015     1.1854e-014    -3.7428e-018    -3.7428e-018
v  ǁVelocityǁ          0.006364          10.226          4.7375          4.7375
v  Pressure               -59.258          19.152         0.74658         0.74658
v  nu_tilda            8.262e-007       0.0041922      0.00056654      0.00056654
v  TempC                       21          72.494          21.215          21.215
v  TurbVisc           4.2045e-013       0.0049401      0.00065385      0.00065385
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              146:        0.28940E+01

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


 INSTANT    0.147000000E+03   TIME STEP NUMBER             147
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87301E-02 0.94739E+00
   Friction velocity        uk    :  0.87301E-02 0.94739E+00
   Dimensionless distance   yplus :  0.70283E-01 0.76272E+01
   Friction thermal sca.    tstar : -0.62611E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52439E-01 0.56907E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43369E-02      34   0.94018E-03   0.56439E+01 0.14563E+03 
c  Velocity[X]                                      0.28365E+01 
c  Velocity[Y]                                      0.28074E+01 
c  Velocity[Z]                                      0.43944E-29 
c  Pressure     0.14894E-06     474   0.97256E-08   0.13143E+00 0.51490E+03 
c  nu_tilda     0.28469E-05      35   0.21688E-04   0.98094E-06 0.53973E+03 
c  TempC        0.19412E+02      30   0.79065E-03   0.11253E+02 0.34132E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.24          10.187          4.5729          4.5729
v  Velocity[Y]            -4.0812          8.1368      0.00060903      0.00060903
v  Velocity[Z]       -8.8304e-015     1.1972e-014    -3.6243e-018    -3.6243e-018
v  ǁVelocityǁ         0.0062344          10.215           4.738           4.738
v  Pressure               -59.037          19.172         0.72533         0.72533
v  nu_tilda           8.2167e-007        0.004193      0.00056706      0.00056706
v  TempC                       21          72.587          21.216          21.216
v  TurbVisc           4.0994e-013        0.004941      0.00065452      0.00065452
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              147:        0.39820E+01

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


 INSTANT    0.148000000E+03   TIME STEP NUMBER             148
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25231E-01 0.94790E+00
   Friction velocity        uk    :  0.25231E-01 0.94790E+00
   Dimensionless distance   yplus :  0.20313E+00 0.76313E+01
   Friction thermal sca.    tstar : -0.13312E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15156E+00 0.56938E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43412E-02      34   0.95205E-03   0.56807E+01 0.14550E+03 
c  Velocity[X]                                      0.28938E+01 
c  Velocity[Y]                                      0.27869E+01 
c  Velocity[Z]                                      0.44282E-29 
c  Pressure     0.19121E-06     469   0.96369E-08   0.16901E+00 0.59484E+03 
c  nu_tilda     0.28536E-05      35   0.13983E-04   0.97299E-06 0.53662E+03 
c  TempC        0.19432E+02      30   0.76581E-03   0.11363E+02 0.35075E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2171          10.178          4.5729          4.5729
v  Velocity[Y]            -4.0669           8.097      0.00061755      0.00061755
v  Velocity[Z]       -8.7538e-015     1.2077e-014    -3.5026e-018    -3.5026e-018
v  ǁVelocityǁ         0.0061689          10.205          4.7385          4.7385
v  Pressure               -58.721          19.087         0.71411         0.71411
v  nu_tilda           8.1773e-007       0.0041937      0.00056768      0.00056768
v  TempC                       21           72.62          21.218          21.218
v  TurbVisc             4.01e-013       0.0049419      0.00065518      0.00065518
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              148:        0.35290E+01

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


 INSTANT    0.149000000E+03   TIME STEP NUMBER             149
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48545E-02 0.94685E+00
   Friction velocity        uk    :  0.48545E-02 0.94685E+00
   Dimensionless distance   yplus :  0.39082E-01 0.76228E+01
   Friction thermal sca.    tstar : -0.13289E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29160E-01 0.56875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43455E-02      34   0.79720E-03   0.55478E+01 0.14399E+03 
c  Velocity[X]                                      0.28378E+01 
c  Velocity[Y]                                      0.27099E+01 
c  Velocity[Z]                                      0.50289E-29 
c  Pressure     0.13647E-06     442   0.98133E-08   0.11923E+00 0.54654E+03 
c  nu_tilda     0.28603E-05      35   0.21516E-04   0.96504E-06 0.53354E+03 
c  TempC        0.19453E+02      29   0.74419E-03   0.12091E+02 0.36689E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2009          10.171          4.5729          4.5729
v  Velocity[Y]            -4.0525          8.1189      0.00062629      0.00062629
v  Velocity[Z]       -8.7001e-015     1.2109e-014    -3.3891e-018    -3.3891e-018
v  ǁVelocityǁ         0.0059348          10.197           4.739           4.739
v  Pressure               -58.513          19.148         0.69959         0.69959
v  nu_tilda           8.1351e-007       0.0041945       0.0005682       0.0005682
v  TempC                   20.995          72.694          21.219          21.219
v  TurbVisc           3.9338e-013       0.0049427      0.00065585      0.00065585
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              149:        0.33810E+01

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


 INSTANT    0.150000000E+03   TIME STEP NUMBER             150
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92931E-02 0.94796E+00
   Friction velocity        uk    :  0.92931E-02 0.94796E+00
   Dimensionless distance   yplus :  0.74816E-01 0.76318E+01
   Friction thermal sca.    tstar : -0.72862E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55821E-01 0.56941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43498E-02      34   0.87010E-03   0.54317E+01 0.14256E+03 
c  Velocity[X]                                      0.27837E+01 
c  Velocity[Y]                                      0.26480E+01 
c  Velocity[Z]                                      0.50401E-29 
c  Pressure     0.16992E-06     330   0.92716E-08   0.15171E+00 0.42068E+03 
c  nu_tilda     0.28670E-05      35   0.14044E-04   0.95730E-06 0.53049E+03 
c  TempC        0.19473E+02      29   0.84643E-03   0.11068E+02 0.34992E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1831          10.162          4.5729          4.5729
v  Velocity[Y]            -4.0389           8.095       0.0006354       0.0006354
v  Velocity[Z]       -8.6556e-015     1.2231e-014    -3.2736e-018    -3.2736e-018
v  ǁVelocityǁ         0.0056791          10.188          4.7394          4.7394
v  Pressure               -58.187          19.111         0.69917         0.69917
v  nu_tilda           8.0932e-007       0.0041952      0.00056883      0.00056883
v  TempC                   20.984          72.707           21.22           21.22
v  TurbVisc           3.8531e-013       0.0049436      0.00065651      0.00065651
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              150:        0.29950E+01

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


 INSTANT    0.151000000E+03   TIME STEP NUMBER             151
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20209E-01 0.94694E+00
   Friction velocity        uk    :  0.20209E-01 0.94694E+00
   Dimensionless distance   yplus :  0.16270E+00 0.76235E+01
   Friction thermal sca.    tstar : -0.67245E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12139E+00 0.56880E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43540E-02      34   0.86820E-03   0.53836E+01 0.14181E+03 
c  Velocity[X]                                      0.27554E+01 
c  Velocity[Y]                                      0.26282E+01 
c  Velocity[Z]                                      0.53394E-29 
c  Pressure     0.16147E-06     472   0.99225E-08   0.14003E+00 0.50094E+03 
c  nu_tilda     0.28736E-05      35   0.21344E-04   0.94954E-06 0.52747E+03 
c  TempC        0.19493E+02      29   0.75310E-03   0.14319E+02 0.38062E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1636          10.153          4.5729          4.5729
v  Velocity[Y]            -4.0248          8.1162      0.00064413      0.00064413
v  Velocity[Z]       -8.6126e-015     1.2279e-014    -3.1627e-018    -3.1627e-018
v  ǁVelocityǁ         0.0055811           10.18          4.7399          4.7399
v  Pressure               -57.961          19.145          0.6808          0.6808
v  nu_tilda           8.0589e-007       0.0041959      0.00056936      0.00056936
v  TempC                       21          72.785          21.221          21.221
v  TurbVisc           3.7743e-013       0.0049445      0.00065718      0.00065718
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              151:        0.35670E+01

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


 INSTANT    0.152000000E+03   TIME STEP NUMBER             152
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18262E-01 0.94772E+00
   Friction velocity        uk    :  0.18262E-01 0.94772E+00
   Dimensionless distance   yplus :  0.14702E+00 0.76298E+01
   Friction thermal sca.    tstar : -0.59532E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10969E+00 0.56927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43583E-02      34   0.77818E-03   0.53586E+01 0.14116E+03 
c  Velocity[X]                                      0.27842E+01 
c  Velocity[Y]                                      0.25743E+01 
c  Velocity[Z]                                      0.40742E-29 
c  Pressure     0.20771E-06     344   0.95485E-08   0.17638E+00 0.41096E+03 
c  nu_tilda     0.28802E-05      35   0.14049E-04   0.94200E-06 0.52449E+03 
c  TempC        0.19513E+02      29   0.65432E-03   0.10933E+02 0.34390E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1425          10.144          4.5729          4.5729
v  Velocity[Y]             -4.011          8.1084      0.00065316      0.00065316
v  Velocity[Z]       -8.5573e-015     1.2277e-014    -3.0519e-018    -3.0519e-018
v  ǁVelocityǁ          0.005256          10.171          4.7404          4.7404
v  Pressure               -57.639           19.13         0.68377         0.68377
v  nu_tilda           8.0277e-007       0.0041966      0.00056998      0.00056998
v  TempC                       21          72.815          21.222          21.222
v  TurbVisc           3.7109e-013       0.0049453      0.00065785      0.00065785
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              152:        0.30680E+01

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


 INSTANT    0.153000000E+03   TIME STEP NUMBER             153
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24663E-01 0.94694E+00
   Friction velocity        uk    :  0.24663E-01 0.94694E+00
   Dimensionless distance   yplus :  0.19856E+00 0.76235E+01
   Friction thermal sca.    tstar : -0.59347E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14815E+00 0.56880E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43626E-02      34   0.85300E-03   0.52434E+01 0.13967E+03 
c  Velocity[X]                                      0.27457E+01 
c  Velocity[Y]                                      0.24977E+01 
c  Velocity[Z]                                      0.55865E-29 
c  Pressure     0.18507E-06     489   0.95577E-08   0.16344E+00 0.67264E+03 
c  nu_tilda     0.28868E-05      35   0.21176E-04   0.93445E-06 0.52154E+03 
c  TempC        0.19533E+02      30   0.83658E-03   0.96472E+01 0.31604E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1212          10.134          4.5729          4.5729
v  Velocity[Y]            -3.9972          8.0759      0.00066244      0.00066244
v  Velocity[Z]       -8.4836e-015      1.229e-014    -2.9463e-018    -2.9463e-018
v  ǁVelocityǁ         0.0056389          10.162          4.7409          4.7409
v  Pressure               -57.389          19.077         0.65149         0.65149
v  nu_tilda           7.9964e-007       0.0041973      0.00057051      0.00057051
v  TempC                       21          72.906          21.224          21.224
v  TurbVisc           3.6537e-013       0.0049461      0.00065852      0.00065852
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              153:        0.35790E+01

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


 INSTANT    0.154000000E+03   TIME STEP NUMBER             154
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10433E-01 0.94482E+00
   Friction velocity        uk    :  0.10433E-01 0.94482E+00
   Dimensionless distance   yplus :  0.83992E-01 0.76064E+01
   Friction thermal sca.    tstar : -0.74096E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62668E-01 0.56752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43668E-02      34   0.89089E-03   0.51743E+01 0.13885E+03 
c  Velocity[X]                                      0.26860E+01 
c  Velocity[Y]                                      0.24883E+01 
c  Velocity[Z]                                      0.47458E-29 
c  Pressure     0.14018E-06     490   0.95619E-08   0.12198E+00 0.77308E+03 
c  nu_tilda     0.28933E-05      35   0.14123E-04   0.92711E-06 0.51862E+03 
c  TempC        0.19553E+02      30   0.83298E-03   0.13061E+02 0.35840E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1046          10.124          4.5729          4.5729
v  Velocity[Y]            -3.9835          8.0908      0.00067142      0.00067142
v  Velocity[Z]        -8.403e-015     1.2349e-014    -2.8434e-018    -2.8434e-018
v  ǁVelocityǁ         0.0050852          10.153          4.7413          4.7413
v  Pressure               -57.119          19.151         0.67129         0.67129
v  nu_tilda           7.9768e-007        0.004198      0.00057114      0.00057114
v  TempC                       21          72.955          21.225          21.225
v  TurbVisc           3.5971e-013        0.004947      0.00065919      0.00065919
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              154:        0.35340E+01

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


 INSTANT    0.155000000E+03   TIME STEP NUMBER             155
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66242E-02 0.94554E+00
   Friction velocity        uk    :  0.66242E-02 0.94554E+00
   Dimensionless distance   yplus :  0.53329E-01 0.76122E+01
   Friction thermal sca.    tstar : -0.13706E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39790E-01 0.56796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43710E-02      34   0.76129E-03   0.51278E+01 0.13789E+03 
c  Velocity[X]                                      0.27203E+01 
c  Velocity[Y]                                      0.24074E+01 
c  Velocity[Z]                                      0.39801E-29 
c  Pressure     0.17573E-06     554   0.92562E-08   0.15118E+00 0.10192E+04 
c  nu_tilda     0.28998E-05      35   0.21009E-04   0.91974E-06 0.51572E+03 
c  TempC        0.19573E+02      29   0.71750E-03   0.13128E+02 0.38034E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0853          10.114          4.5729          4.5729
v  Velocity[Y]            -3.9694          8.0545      0.00068123      0.00068123
v  Velocity[Z]       -8.3158e-015     1.2449e-014      -2.74e-018      -2.74e-018
v  ǁVelocityǁ         0.0057849          10.143          4.7418          4.7418
v  Pressure               -56.836          19.035         0.62638         0.62638
v  nu_tilda           7.9764e-007       0.0041987      0.00057167      0.00057167
v  TempC                   20.986          72.936          21.226          21.226
v  TurbVisc            3.562e-013       0.0049478      0.00065987      0.00065987
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              155:        0.39150E+01

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


 INSTANT    0.156000000E+03   TIME STEP NUMBER             156
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23265E-02 0.94411E+00
   Friction velocity        uk    :  0.23265E-02 0.94411E+00
   Dimensionless distance   yplus :  0.18730E-01 0.76007E+01
   Friction thermal sca.    tstar : -0.12937E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13974E-01 0.56710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43753E-02      34   0.83246E-03   0.50150E+01 0.13653E+03 
c  Velocity[X]                                      0.26689E+01 
c  Velocity[Y]                                      0.23461E+01 
c  Velocity[Z]                                      0.42084E-29 
c  Pressure     0.15350E-06     520   0.98816E-08   0.13187E+00 0.11069E+04 
c  nu_tilda     0.29063E-05      35   0.14122E-04   0.91258E-06 0.51286E+03 
c  TempC        0.19593E+02      29   0.70018E-03   0.11164E+02 0.34258E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0647          10.104          4.5729          4.5729
v  Velocity[Y]            -3.9556          8.0744      0.00069045      0.00069045
v  Velocity[Z]       -8.2187e-015      1.256e-014    -2.6415e-018    -2.6415e-018
v  ǁVelocityǁ         0.0051986          10.133          4.7423          4.7423
v  Pressure               -56.553          19.167         0.65807         0.65807
v  nu_tilda           7.9936e-007       0.0041994       0.0005723       0.0005723
v  TempC                       21           72.98          21.227          21.227
v  TurbVisc           3.5611e-013       0.0049486      0.00066054      0.00066054
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              156:        0.37250E+01

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


 INSTANT    0.157000000E+03   TIME STEP NUMBER             157
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88507E-02 0.94518E+00
   Friction velocity        uk    :  0.88507E-02 0.94518E+00
   Dimensionless distance   yplus :  0.71254E-01 0.76093E+01
   Friction thermal sca.    tstar : -0.76852E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53164E-01 0.56774E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43795E-02      34   0.90860E-03   0.49794E+01 0.13588E+03 
c  Velocity[X]                                      0.26522E+01 
c  Velocity[Y]                                      0.23271E+01 
c  Velocity[Z]                                      0.48209E-29 
c  Pressure     0.17245E-06     537   0.97382E-08   0.14961E+00 0.83362E+03 
c  nu_tilda     0.29128E-05      35   0.20849E-04   0.90541E-06 0.51002E+03 
c  TempC        0.19612E+02      29   0.75399E-03   0.13165E+02 0.35414E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0455          10.093          4.5729          4.5729
v  Velocity[Y]            -3.9422          8.0494      0.00070013      0.00070013
v  Velocity[Z]        -8.106e-015     1.2706e-014    -2.5444e-018    -2.5444e-018
v  ǁVelocityǁ         0.0057942          10.122          4.7428          4.7428
v  Pressure               -56.281          19.082         0.61891         0.61891
v  nu_tilda           8.0313e-007       0.0042001      0.00057284      0.00057284
v  TempC                       21          72.967          21.228          21.228
v  TurbVisc           3.5921e-013       0.0049494      0.00066122      0.00066122
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              157:        0.41050E+01

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


 INSTANT    0.158000000E+03   TIME STEP NUMBER             158
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11981E-01 0.94403E+00
   Friction velocity        uk    :  0.11981E-01 0.94403E+00
   Dimensionless distance   yplus :  0.96453E-01 0.76001E+01
   Friction thermal sca.    tstar : -0.57467E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71964E-01 0.56705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43837E-02      34   0.77904E-03   0.49313E+01 0.13516E+03 
c  Velocity[X]                                      0.26492E+01 
c  Velocity[Y]                                      0.22821E+01 
c  Velocity[Z]                                      0.40625E-29 
c  Pressure     0.17000E-06     521   0.95110E-08   0.14452E+00 0.10287E+04 
c  nu_tilda     0.29192E-05      35   0.14157E-04   0.89843E-06 0.50721E+03 
c  TempC        0.19632E+02      30   0.62097E-03   0.12497E+02 0.34878E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0286          10.082          4.5729          4.5729
v  Velocity[Y]            -3.9287          8.0715      0.00071007      0.00071007
v  Velocity[Z]       -7.9845e-015      1.281e-014     -2.451e-018     -2.451e-018
v  ǁVelocityǁ         0.0053267          10.111          4.7433          4.7433
v  Pressure               -55.992          19.192         0.64893         0.64893
v  nu_tilda           8.0755e-007       0.0042007      0.00057347      0.00057347
v  TempC                       21          72.932          21.229          21.229
v  TurbVisc           3.6603e-013       0.0049502       0.0006619       0.0006619
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              158:        0.41800E+01

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


 INSTANT    0.159000000E+03   TIME STEP NUMBER             159
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10689E-01 0.94468E+00
   Friction velocity        uk    :  0.10689E-01 0.94468E+00
   Dimensionless distance   yplus :  0.86054E-01 0.76053E+01
   Friction thermal sca.    tstar : -0.53021E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64206E-01 0.56744E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43880E-02      34   0.87597E-03   0.48943E+01 0.13431E+03 
c  Velocity[X]                                      0.26684E+01 
c  Velocity[Y]                                      0.22258E+01 
c  Velocity[Z]                                      0.36499E-29 
c  Pressure     0.20797E-06     489   0.94218E-08   0.17250E+00 0.65033E+03 
c  nu_tilda     0.29256E-05      35   0.20688E-04   0.89143E-06 0.50443E+03 
c  TempC        0.19652E+02      30   0.75919E-03   0.10810E+02 0.31716E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0168          10.071          4.5729          4.5729
v  Velocity[Y]            -3.9157           8.065       0.0007199       0.0007199
v  Velocity[Z]       -7.8488e-015     1.2988e-014    -2.3583e-018    -2.3583e-018
v  ǁVelocityǁ         0.0058617          10.101          4.7438          4.7438
v  Pressure               -55.743          19.138         0.61651         0.61651
v  nu_tilda           8.1174e-007       0.0042014        0.000574        0.000574
v  TempC                       21          72.461           21.23           21.23
v  TurbVisc           3.7414e-013        0.004951      0.00066259      0.00066259
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              159:        0.35770E+01

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


 INSTANT    0.160000000E+03   TIME STEP NUMBER             160
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47986E-02 0.94370E+00
   Friction velocity        uk    :  0.47986E-02 0.94370E+00
   Dimensionless distance   yplus :  0.38632E-01 0.75974E+01
   Friction thermal sca.    tstar : -0.10106E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28824E-01 0.56685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43922E-02      34   0.75998E-03   0.48372E+01 0.13353E+03 
c  Velocity[X]                                      0.26258E+01 
c  Velocity[Y]                                      0.22115E+01 
c  Velocity[Z]                                      0.36753E-29 
c  Pressure     0.17462E-06     442   0.97887E-08   0.14926E+00 0.52639E+03 
c  nu_tilda     0.29319E-05      35   0.14132E-04   0.88462E-06 0.50168E+03 
c  TempC        0.19672E+02      30   0.63344E-03   0.12126E+02 0.33220E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0025          10.063          4.5729          4.5729
v  Velocity[Y]            -3.9023          8.0262      0.00073013      0.00073013
v  Velocity[Z]       -7.7015e-015      1.302e-014    -2.2659e-018    -2.2659e-018
v  ǁVelocityǁ          0.005553           10.09          4.7443          4.7443
v  Pressure               -55.422          19.154          0.6291          0.6291
v  nu_tilda           8.1549e-007        0.004202      0.00057464      0.00057464
v  TempC                   20.999          72.459          21.232          21.232
v  TurbVisc           3.8197e-013       0.0049518      0.00066327      0.00066327
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              160:        0.34630E+01

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


 INSTANT    0.161000000E+03   TIME STEP NUMBER             161
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14901E-01 0.94142E+00
   Friction velocity        uk    :  0.14901E-01 0.94142E+00
   Dimensionless distance   yplus :  0.11996E+00 0.75791E+01
   Friction thermal sca.    tstar : -0.71793E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89505E-01 0.56549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43964E-02      34   0.80557E-03   0.47356E+01 0.13225E+03 
c  Velocity[X]                                      0.25899E+01 
c  Velocity[Y]                                      0.21456E+01 
c  Velocity[Z]                                      0.43645E-29 
c  Pressure     0.15417E-06     440   0.98101E-08   0.12918E+00 0.55259E+03 
c  nu_tilda     0.29383E-05      35   0.20537E-04   0.87781E-06 0.49896E+03 
c  TempC        0.19692E+02      29   0.81319E-03   0.13141E+02 0.34507E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9874          10.056          4.5729          4.5729
v  Velocity[Y]            -3.8897          8.0423      0.00074022      0.00074022
v  Velocity[Z]       -7.5504e-015     1.2748e-014    -2.1758e-018    -2.1758e-018
v  ǁVelocityǁ        0.00053022          10.079          4.7448          4.7448
v  Pressure               -55.163          19.206          0.6197          0.6197
v  nu_tilda             8.17e-007       0.0042027      0.00057518      0.00057518
v  TempC                       21          72.689          21.233          21.233
v  TurbVisc           3.8908e-013       0.0049525      0.00066395      0.00066395
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              161:        0.33740E+01

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


 INSTANT    0.162000000E+03   TIME STEP NUMBER             162
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60898E-03 0.94184E+00
   Friction velocity        uk    :  0.60898E-03 0.94184E+00
   Dimensionless distance   yplus :  0.49027E-02 0.75825E+01
   Friction thermal sca.    tstar : -0.83781E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36580E-02 0.56574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44006E-02      34   0.83903E-03   0.47251E+01 0.13166E+03 
c  Velocity[X]                                      0.26203E+01 
c  Velocity[Y]                                      0.21048E+01 
c  Velocity[Z]                                      0.40586E-29 
c  Pressure     0.17648E-06     394   0.99228E-08   0.14681E+00 0.42657E+03 
c  nu_tilda     0.29446E-05      35   0.14171E-04   0.87118E-06 0.49626E+03 
c  TempC        0.19711E+02      29   0.69050E-03   0.13828E+02 0.37610E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9708          10.049          4.5729          4.5729
v  Velocity[Y]            -3.8761          8.0027      0.00075051      0.00075051
v  Velocity[Z]       -7.3915e-015       1.27e-014    -2.0964e-018    -2.0964e-018
v  ǁVelocityǁ         0.0031962           10.07          4.7453          4.7453
v  Pressure               -54.818          19.141         0.61626         0.61626
v  nu_tilda           8.1756e-007       0.0042033      0.00057582      0.00057582
v  TempC                       21          72.674          21.234          21.234
v  TurbVisc           3.9198e-013       0.0049533      0.00066463      0.00066463
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              162:        0.32890E+01

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


 INSTANT    0.163000000E+03   TIME STEP NUMBER             163
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13232E-01 0.94059E+00
   Friction velocity        uk    :  0.13232E-01 0.94059E+00
   Dimensionless distance   yplus :  0.10653E+00 0.75724E+01
   Friction thermal sca.    tstar : -0.20595E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79481E-01 0.56498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44048E-02      34   0.85558E-03   0.46841E+01 0.13109E+03 
c  Velocity[X]                                      0.25819E+01 
c  Velocity[Y]                                      0.21022E+01 
c  Velocity[Z]                                      0.37237E-29 
c  Pressure     0.17716E-06     410   0.93660E-08   0.14621E+00 0.60333E+03 
c  nu_tilda     0.29509E-05      35   0.20382E-04   0.86452E-06 0.49359E+03 
c  TempC        0.19731E+02      29   0.76285E-03   0.13269E+02 0.34225E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9539           10.04          4.5729          4.5729
v  Velocity[Y]            -3.8632          8.0217      0.00076097      0.00076097
v  Velocity[Z]       -7.2443e-015     1.3159e-014     -2.005e-018     -2.005e-018
v  ǁVelocityǁ         0.0037254          10.062          4.7458          4.7458
v  Pressure               -54.604          19.224         0.60919         0.60919
v  nu_tilda           8.1634e-007       0.0042039      0.00057636      0.00057636
v  TempC                       21          72.738          21.235          21.235
v  TurbVisc           3.9304e-013        0.004954      0.00066532      0.00066532
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              163:        0.31590E+01

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


 INSTANT    0.164000000E+03   TIME STEP NUMBER             164
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17901E-01 0.94152E+00
   Friction velocity        uk    :  0.17901E-01 0.94152E+00
   Dimensionless distance   yplus :  0.14411E+00 0.75799E+01
   Friction thermal sca.    tstar : -0.16945E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10752E+00 0.56555E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44090E-02      34   0.78923E-03   0.46673E+01 0.13059E+03 
c  Velocity[X]                                      0.26122E+01 
c  Velocity[Y]                                      0.20551E+01 
c  Velocity[Z]                                      0.38412E-29 
c  Pressure     0.18432E-06     438   0.96542E-08   0.15704E+00 0.43938E+03 
c  nu_tilda     0.29571E-05      35   0.14177E-04   0.85806E-06 0.49095E+03 
c  TempC        0.19751E+02      29   0.84935E-03   0.14307E+02 0.36590E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9414          10.032          4.5729          4.5729
v  Velocity[Y]            -3.8506          7.9956      0.00077106      0.00077106
v  Velocity[Z]       -7.1215e-015     1.3284e-014    -1.9256e-018    -1.9256e-018
v  ǁVelocityǁ         0.0038545          10.054          4.7463          4.7463
v  Pressure               -54.278          19.215         0.61801         0.61801
v  nu_tilda           8.1279e-007       0.0042046        0.000577        0.000577
v  TempC                       21          72.874          21.236          21.236
v  TurbVisc           3.9071e-013       0.0049548      0.00066601      0.00066601
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              164:        0.28980E+01

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


 INSTANT    0.165000000E+03   TIME STEP NUMBER             165
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15777E-01 0.94031E+00
   Friction velocity        uk    :  0.15777E-01 0.94031E+00
   Dimensionless distance   yplus :  0.12701E+00 0.75701E+01
   Friction thermal sca.    tstar : -0.11559E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94767E-01 0.56481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44132E-02      34   0.79558E-03   0.45497E+01 0.12920E+03 
c  Velocity[X]                                      0.25543E+01 
c  Velocity[Y]                                      0.19954E+01 
c  Velocity[Z]                                      0.41558E-29 
c  Pressure     0.17918E-06     409   0.93770E-08   0.14693E+00 0.62391E+03 
c  nu_tilda     0.29633E-05      35   0.20236E-04   0.85157E-06 0.48832E+03 
c  TempC        0.19770E+02      30   0.70913E-03   0.14759E+02 0.37460E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9273          10.023          4.5729          4.5729
v  Velocity[Y]            -3.8378          8.0179      0.00078196      0.00078196
v  Velocity[Z]       -6.9923e-015     1.3431e-014    -1.8489e-018    -1.8489e-018
v  ǁVelocityǁ         0.0068743          10.046          4.7468          4.7468
v  Pressure               -54.011          19.282         0.61274         0.61274
v  nu_tilda           8.0689e-007       0.0042052      0.00057754      0.00057754
v  TempC                       21           72.35          21.237          21.237
v  TurbVisc           3.8395e-013       0.0049555       0.0006667       0.0006667
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              165:        0.28460E+01

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


 INSTANT    0.166000000E+03   TIME STEP NUMBER             166
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28487E-01 0.94099E+00
   Friction velocity        uk    :  0.28487E-01 0.94099E+00
   Dimensionless distance   yplus :  0.22934E+00 0.75756E+01
   Friction thermal sca.    tstar : -0.73638E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17111E+00 0.56523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44174E-02      34   0.82327E-03   0.45792E+01 0.12913E+03 
c  Velocity[X]                                      0.25812E+01 
c  Velocity[Y]                                      0.19980E+01 
c  Velocity[Z]                                      0.35241E-29 
c  Pressure     0.19970E-06     441   0.98296E-08   0.15935E+00 0.56360E+03 
c  nu_tilda     0.29695E-05      35   0.14210E-04   0.84527E-06 0.48573E+03 
c  TempC        0.19790E+02      30   0.63144E-03   0.14472E+02 0.34546E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9116          10.014          4.5729          4.5729
v  Velocity[Y]            -3.8254          8.0054      0.00079254      0.00079254
v  Velocity[Z]       -6.9287e-015     1.3034e-014    -1.7815e-018    -1.7815e-018
v  ǁVelocityǁ          0.002895          10.037          4.7473          4.7473
v  Pressure               -53.673          19.304         0.62711         0.62711
v  nu_tilda           7.9914e-007       0.0042058      0.00057818      0.00057818
v  TempC                       21           72.33          21.238          21.238
v  TurbVisc           3.7293e-013       0.0049562      0.00066739      0.00066739
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              166:        0.28950E+01

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


 INSTANT    0.167000000E+03   TIME STEP NUMBER             167
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12111E-01 0.94006E+00
   Friction velocity        uk    :  0.12111E-01 0.94006E+00
   Dimensionless distance   yplus :  0.97503E-01 0.75681E+01
   Friction thermal sca.    tstar : -0.55569E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72748E-01 0.56467E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44216E-02      34   0.73904E-03   0.45337E+01 0.12842E+03 
c  Velocity[X]                                      0.25890E+01 
c  Velocity[Y]                                      0.19446E+01 
c  Velocity[Z]                                      0.37863E-29 
c  Pressure     0.17866E-06     489   0.92505E-08   0.14589E+00 0.65967E+03 
c  nu_tilda     0.29757E-05      35   0.20086E-04   0.83894E-06 0.48316E+03 
c  TempC        0.19809E+02      29   0.95354E-03   0.14065E+02 0.33592E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8949          10.005          4.5729          4.5729
v  Velocity[Y]            -3.8129          7.9719      0.00080405      0.00080405
v  Velocity[Z]       -6.9287e-015     1.3362e-014     -1.715e-018     -1.715e-018
v  ǁVelocityǁ         0.0057192          10.027          4.7478          4.7478
v  Pressure               -53.431          19.239         0.59366         0.59366
v  nu_tilda           7.9105e-007       0.0042064      0.00057873      0.00057873
v  TempC                       21          72.612          21.239          21.239
v  TurbVisc           3.5881e-013       0.0049569      0.00066809      0.00066809
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              167:        0.26940E+01

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


 INSTANT    0.168000000E+03   TIME STEP NUMBER             168
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25679E-01 0.93793E+00
   Friction velocity        uk    :  0.25679E-01 0.93793E+00
   Dimensionless distance   yplus :  0.20674E+00 0.75509E+01
   Friction thermal sca.    tstar : -0.60880E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15425E+00 0.56338E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44258E-02      34   0.90975E-03   0.44537E+01 0.12742E+03 
c  Velocity[X]                                      0.25461E+01 
c  Velocity[Y]                                      0.19076E+01 
c  Velocity[Z]                                      0.36875E-29 
c  Pressure     0.14682E-06     504   0.94269E-08   0.11954E+00 0.11709E+04 
c  nu_tilda     0.29819E-05      35   0.14230E-04   0.83280E-06 0.48062E+03 
c  TempC        0.19829E+02      30   0.90359E-03   0.17136E+02 0.40536E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8772          9.9949          4.5729          4.5729
v  Velocity[Y]            -3.8005          7.9857      0.00081464      0.00081464
v  Velocity[Z]       -6.9287e-015     1.3427e-014    -1.6497e-018    -1.6497e-018
v  ǁVelocityǁ          0.005435          10.018          4.7484          4.7484
v  Pressure               -53.107          19.363         0.62885         0.62885
v  nu_tilda           7.8251e-007        0.004207      0.00057937      0.00057937
v  TempC                       21          73.034           21.24           21.24
v  TurbVisc           3.4449e-013       0.0049577      0.00066878      0.00066878
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              168:        0.24340E+01

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


 INSTANT    0.169000000E+03   TIME STEP NUMBER             169
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21507E-01 0.93826E+00
   Friction velocity        uk    :  0.21507E-01 0.93826E+00
   Dimensionless distance   yplus :  0.17315E+00 0.75537E+01
   Friction thermal sca.    tstar : -0.85301E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12919E+00 0.56359E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44299E-02      34   0.85498E-03   0.45214E+01 0.12782E+03 
c  Velocity[X]                                      0.26054E+01 
c  Velocity[Y]                                      0.19160E+01 
c  Velocity[Z]                                      0.35157E-29 
c  Pressure     0.20392E-06     489   0.98040E-08   0.16347E+00 0.76285E+03 
c  nu_tilda     0.29880E-05      35   0.19942E-04   0.82664E-06 0.47810E+03 
c  TempC        0.19848E+02      30   0.68835E-03   0.17041E+02 0.39097E+02 
-----------------------------------------------------------------------------
  
  

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

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8632          9.9848          4.5729          4.5729
v  Velocity[Y]            -3.7879           7.946      0.00082581      0.00082581
v  Velocity[Z]       -6.9287e-015     1.3556e-014    -1.5816e-018    -1.5816e-018
v  ǁVelocityǁ         0.0011403          10.009          4.7489          4.7489
v  Pressure               -52.795           19.26         0.59365         0.59365
v  nu_tilda           7.7359e-007       0.0042076      0.00057992      0.00057992
v  TempC                       21          72.507          21.241          21.241
v  TurbVisc           3.2985e-013       0.0049584      0.00066948      0.00066948
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              169:        0.34980E+01

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


 INSTANT    0.170000000E+03   TIME STEP NUMBER             170
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10285E-01 0.93704E+00
   Friction velocity        uk    :  0.10285E-01 0.93704E+00
   Dimensionless distance   yplus :  0.82802E-01 0.75438E+01
   Friction thermal sca.    tstar : -0.15405E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61779E-01 0.56285E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44341E-02      34   0.75769E-03   0.44507E+01 0.12699E+03 
c  Velocity[X]                                      0.25680E+01 
c  Velocity[Y]                                      0.18828E+01 
c  Velocity[Z]                                      0.36412E-29 
c  Pressure     0.16621E-06     521   0.97475E-08   0.13181E+00 0.16261E+04 
c  nu_tilda     0.29941E-05      35   0.14232E-04   0.82065E-06 0.47561E+03 
c  TempC        0.19868E+02      30   0.62564E-03   0.14836E+02 0.34921E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8485          9.9741          4.5729          4.5729
v  Velocity[Y]            -3.7753          7.9651      0.00083677      0.00083677
v  Velocity[Z]       -6.9287e-015     1.3065e-014    -1.5363e-018    -1.5363e-018
v  ǁVelocityǁ         0.0017018          9.9994          4.7495          4.7495
v  Pressure               -52.449           19.45         0.64314         0.64314
v  nu_tilda           7.6475e-007       0.0042082      0.00058056      0.00058056
v  TempC                       21          72.515          21.241          21.241
v  TurbVisc           3.1507e-013        0.004959      0.00067017      0.00067017
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              170:        0.39760E+01

===============================================================


 INSTANT    0.171000000E+03   TIME STEP NUMBER             171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26174E-02 0.93798E+00
   Friction velocity        uk    :  0.26174E-02 0.93798E+00
   Dimensionless distance   yplus :  0.21072E-01 0.75513E+01
   Friction thermal sca.    tstar : -0.16972E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15722E-01 0.56341E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44383E-02      34   0.86183E-03   0.43749E+01 0.12591E+03 
c  Velocity[X]                                      0.25398E+01 
c  Velocity[Y]                                      0.18351E+01 
c  Velocity[Z]                                      0.35805E-29 
c  Pressure     0.19428E-06     522   0.96096E-08   0.15533E+00 0.95708E+03 
c  nu_tilda     0.30001E-05      35   0.19804E-04   0.81463E-06 0.47313E+03 
c  TempC        0.19887E+02      30   0.55757E-03   0.15133E+02 0.34558E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8318          9.9644          4.5729          4.5729
v  Velocity[Y]            -3.7634          7.9359      0.00084827      0.00084827
v  Velocity[Z]       -6.9287e-015     1.3451e-014    -1.4871e-018    -1.4871e-018
v  ǁVelocityǁ         0.0021859          9.9895            4.75            4.75
v  Pressure               -52.237          19.338         0.59835         0.59835
v  nu_tilda           7.5653e-007       0.0042087      0.00058111      0.00058111
v  TempC                       21          72.858          21.242          21.242
v  TurbVisc           3.0092e-013       0.0049597      0.00067087      0.00067087
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              171:        0.38070E+01

===============================================================


 INSTANT    0.172000000E+03   TIME STEP NUMBER             172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16419E-01 0.93664E+00
   Friction velocity        uk    :  0.16419E-01 0.93664E+00
   Dimensionless distance   yplus :  0.13218E+00 0.75406E+01
   Friction thermal sca.    tstar : -0.77048E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98622E-01 0.56261E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44425E-02      34   0.77339E-03   0.43964E+01 0.12599E+03 
c  Velocity[X]                                      0.25489E+01 
c  Velocity[Y]                                      0.18475E+01 
c  Velocity[Z]                                      0.33670E-29 
c  Pressure     0.15924E-06     518   0.98057E-08   0.12594E+00 0.13224E+04 
c  nu_tilda     0.30062E-05      35   0.14233E-04   0.80879E-06 0.47069E+03 
c  TempC        0.19907E+02      30   0.69829E-03   0.15196E+02 0.33854E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8141          9.9532          4.5729          4.5729
v  Velocity[Y]            -3.7513          7.9557      0.00085957      0.00085957
v  Velocity[Z]       -6.9287e-015     1.3342e-014     -1.453e-018     -1.453e-018
v  ǁVelocityǁ         0.0033522          9.9791          4.7506          4.7506
v  Pressure               -51.912          19.487          0.6381          0.6381
v  nu_tilda           7.4948e-007       0.0042093      0.00058176      0.00058176
v  TempC                       21           73.03          21.243          21.243
v  TurbVisc           2.8818e-013       0.0049604      0.00067157      0.00067157
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              172:        0.36920E+01

===============================================================


 INSTANT    0.173000000E+03   TIME STEP NUMBER             173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18638E-01 0.93745E+00
   Friction velocity        uk    :  0.18638E-01 0.93745E+00
   Dimensionless distance   yplus :  0.15005E+00 0.75471E+01
   Friction thermal sca.    tstar : -0.89331E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11196E+00 0.56310E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44467E-02      34   0.78786E-03   0.43725E+01 0.12542E+03 
c  Velocity[X]                                      0.25747E+01 
c  Velocity[Y]                                      0.17978E+01 
c  Velocity[Z]                                      0.33743E-29 
c  Pressure     0.20474E-06     489   0.94219E-08   0.15656E+00 0.47162E+03 
c  nu_tilda     0.30122E-05      35   0.19667E-04   0.80292E-06 0.46826E+03 
c  TempC        0.19926E+02      30   0.83914E-03   0.16474E+02 0.36707E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7959          9.9427          4.5729          4.5729
v  Velocity[Y]            -3.7391          7.9501      0.00087206      0.00087206
v  Velocity[Z]       -6.9287e-015     1.3508e-014    -1.4103e-018    -1.4103e-018
v  ǁVelocityǁ         0.0027402          9.9694          4.7511          4.7511
v  Pressure               -51.605          19.452         0.61547         0.61547
v  nu_tilda           7.4393e-007       0.0042099      0.00058231      0.00058231
v  TempC                       21          72.817          21.244          21.244
v  TurbVisc            2.776e-013       0.0049611      0.00067228      0.00067228
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              173:        0.35500E+01

===============================================================


 INSTANT    0.174000000E+03   TIME STEP NUMBER             174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55740E-02 0.93654E+00
   Friction velocity        uk    :  0.55740E-02 0.93654E+00
   Dimensionless distance   yplus :  0.44874E-01 0.75398E+01
   Friction thermal sca.    tstar : -0.18349E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33481E-01 0.56255E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44508E-02      34   0.78060E-03   0.43357E+01 0.12492E+03 
c  Velocity[X]                                      0.25597E+01 
c  Velocity[Y]                                      0.17760E+01 
c  Velocity[Z]                                      0.32364E-29 
c  Pressure     0.17736E-06     505   0.95873E-08   0.13933E+00 0.10307E+04 
c  nu_tilda     0.30182E-05      35   0.14215E-04   0.79723E-06 0.46586E+03 
c  TempC        0.19946E+02      30   0.68878E-03   0.20329E+02 0.41510E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7769          9.9329          4.5729          4.5729
v  Velocity[Y]             -3.727          7.9161      0.00088312      0.00088312
v  Velocity[Z]       -6.9287e-015     1.3046e-014    -1.3845e-018    -1.3845e-018
v  ǁVelocityǁ         0.0021955           9.959          4.7517          4.7517
v  Pressure               -51.192          19.522         0.64773         0.64773
v  nu_tilda           7.4028e-007       0.0042104      0.00058296      0.00058296
v  TempC                       21          72.858          21.244          21.244
v  TurbVisc           2.6946e-013       0.0049617      0.00067298      0.00067298
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              174:        0.36160E+01

===============================================================


 INSTANT    0.175000000E+03   TIME STEP NUMBER             175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70062E-02 0.93458E+00
   Friction velocity        uk    :  0.70062E-02 0.93458E+00
   Dimensionless distance   yplus :  0.56404E-01 0.75240E+01
   Friction thermal sca.    tstar : -0.12646E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42084E-01 0.56137E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44550E-02      34   0.91006E-03   0.43123E+01 0.12461E+03 
c  Velocity[X]                                      0.25270E+01 
c  Velocity[Y]                                      0.17852E+01 
c  Velocity[Z]                                      0.32071E-29 
c  Pressure     0.15519E-06     488   0.97174E-08   0.11959E+00 0.51703E+03 
c  nu_tilda     0.30241E-05      35   0.19531E-04   0.79150E-06 0.46348E+03 
c  TempC        0.19965E+02      30   0.82951E-03   0.16514E+02 0.36357E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7613          9.9255          4.5729          4.5729
v  Velocity[Y]            -3.7155          7.9319      0.00089508      0.00089508
v  Velocity[Z]       -6.9287e-015      1.328e-014    -1.3735e-018    -1.3735e-018
v  ǁVelocityǁ         0.0020394          9.9482          4.7522          4.7522
v  Pressure               -51.016          19.512         0.61879         0.61879
v  nu_tilda           7.3822e-007        0.004211      0.00058352      0.00058352
v  TempC                       21          72.894          21.245          21.245
v  TurbVisc           2.6421e-013       0.0049624      0.00067368      0.00067368
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              175:        0.35620E+01

===============================================================


 INSTANT    0.176000000E+03   TIME STEP NUMBER             176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78369E-02 0.93497E+00
   Friction velocity        uk    :  0.78369E-02 0.93497E+00
   Dimensionless distance   yplus :  0.63092E-01 0.75271E+01
   Friction thermal sca.    tstar : -0.79573E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47074E-01 0.56161E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44592E-02      34   0.84127E-03   0.43780E+01 0.12501E+03 
c  Velocity[X]                                      0.26047E+01 
c  Velocity[Y]                                      0.17734E+01 
c  Velocity[Z]                                      0.36303E-29 
c  Pressure     0.17836E-06     456   0.95354E-08   0.13768E+00 0.61139E+03 
c  nu_tilda     0.30301E-05      35   0.14200E-04   0.78596E-06 0.46113E+03 
c  TempC        0.19984E+02      30   0.10495E-02   0.17881E+02 0.39717E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7431          9.9182          4.5729          4.5729
v  Velocity[Y]            -3.7038          7.8917      0.00090737      0.00090737
v  Velocity[Z]       -6.9287e-015     1.2974e-014    -1.3555e-018    -1.3555e-018
v  ǁVelocityǁ         0.0017706          9.9378          4.7528          4.7528
v  Pressure                -50.62          19.509         0.63652         0.63652
v  nu_tilda           7.3868e-007       0.0042115      0.00058417      0.00058417
v  TempC                       21          72.896          21.245          21.245
v  TurbVisc           2.6129e-013       0.0049631      0.00067439      0.00067439
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              176:        0.33510E+01

===============================================================


 INSTANT    0.177000000E+03   TIME STEP NUMBER             177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20289E-02 0.93351E+00
   Friction velocity        uk    :  0.20289E-02 0.93351E+00
   Dimensionless distance   yplus :  0.16334E-01 0.75154E+01
   Friction thermal sca.    tstar : -0.86304E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12187E-01 0.56073E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44634E-02      34   0.82457E-03   0.43040E+01 0.12424E+03 
c  Velocity[X]                                      0.25771E+01 
c  Velocity[Y]                                      0.17268E+01 
c  Velocity[Z]                                      0.33671E-29 
c  Pressure     0.19951E-06     442   0.97788E-08   0.14930E+00 0.91777E+03 
c  nu_tilda     0.30360E-05      35   0.19401E-04   0.78039E-06 0.45879E+03 
c  TempC        0.20004E+02      30   0.72959E-03   0.24934E+02 0.48568E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7243          9.9098          4.5729          4.5729
v  Velocity[Y]            -3.6923          7.9112      0.00091916      0.00091916
v  Velocity[Z]       -6.9287e-015     1.3138e-014    -1.3282e-018    -1.3282e-018
v  ǁVelocityǁ         0.0020817          9.9289          4.7534          4.7534
v  Pressure               -50.347          19.623         0.64275         0.64275
v  nu_tilda           7.4146e-007       0.0042121      0.00058473      0.00058473
v  TempC                       21          72.977          21.246          21.246
v  TurbVisc           2.6193e-013       0.0049637       0.0006751       0.0006751
v  total_pressure     1.0127e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              177:        0.38100E+01

===============================================================


 INSTANT    0.178000000E+03   TIME STEP NUMBER             178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10411E-01 0.93428E+00
   Friction velocity        uk    :  0.10411E-01 0.93428E+00
   Dimensionless distance   yplus :  0.83818E-01 0.75216E+01
   Friction thermal sca.    tstar : -0.16996E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62538E-01 0.56120E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44675E-02      34   0.80075E-03   0.43055E+01 0.12414E+03 
c  Velocity[X]                                      0.25568E+01 
c  Velocity[Y]                                      0.17487E+01 
c  Velocity[Z]                                      0.34879E-29 
c  Pressure     0.20687E-06     486   0.92648E-08   0.15662E+00 0.10456E+04 
c  nu_tilda     0.30419E-05      35   0.14202E-04   0.77500E-06 0.45648E+03 
c  TempC        0.20023E+02      30   0.80876E-03   0.20182E+02 0.39281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7045           9.902          4.5729          4.5729
v  Velocity[Y]            -3.6806          7.8821      0.00093093      0.00093093
v  Velocity[Z]       -6.9287e-015     1.2559e-014      -1.34e-018      -1.34e-018
v  ǁVelocityǁ         0.0022815          9.9213           4.754           4.754
v  Pressure               -49.926          19.689         0.67546         0.67546
v  nu_tilda           7.4553e-007       0.0042126      0.00058538      0.00058538
v  TempC                       21          73.055          21.247          21.247
v  TurbVisc            2.659e-013       0.0049643      0.00067581      0.00067581
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              178:        0.36240E+01

===============================================================


 INSTANT    0.179000000E+03   TIME STEP NUMBER             179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13925E-01 0.93280E+00
   Friction velocity        uk    :  0.13925E-01 0.93280E+00
   Dimensionless distance   yplus :  0.11210E+00 0.75096E+01
   Friction thermal sca.    tstar : -0.12244E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83641E-01 0.56030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44717E-02      34   0.76120E-03   0.42868E+01 0.12379E+03 
c  Velocity[X]                                      0.25725E+01 
c  Velocity[Y]                                      0.17142E+01 
c  Velocity[Z]                                      0.38204E-29 
c  Pressure     0.16389E-06     506   0.99104E-08   0.12313E+00 0.56402E+03 
c  nu_tilda     0.30478E-05      35   0.19271E-04   0.76957E-06 0.45419E+03 
c  TempC        0.20042E+02      30   0.69580E-03   0.20586E+02 0.39795E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6826          9.8931          4.5729          4.5729
v  Velocity[Y]            -3.6695          7.9031      0.00094351      0.00094351
v  Velocity[Z]       -6.9287e-015     1.3336e-014    -1.3223e-018    -1.3223e-018
v  ǁVelocityǁ          0.003132          9.9136          4.7546          4.7546
v  Pressure               -49.791          19.675         0.64306         0.64306
v  nu_tilda            7.513e-007       0.0042131      0.00058594      0.00058594
v  TempC                       21          73.024          21.247          21.247
v  TurbVisc           2.7179e-013        0.004965      0.00067652      0.00067652
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              179:        0.35220E+01

===============================================================


 INSTANT    0.180000000E+03   TIME STEP NUMBER             180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17674E-01 0.93326E+00
   Friction velocity        uk    :  0.17674E-01 0.93326E+00
   Dimensionless distance   yplus :  0.14229E+00 0.75134E+01
   Friction thermal sca.    tstar : -0.78703E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10617E+00 0.56058E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44759E-02      34   0.81690E-03   0.43286E+01 0.12407E+03 
c  Velocity[X]                                      0.26085E+01 
c  Velocity[Y]                                      0.17201E+01 
c  Velocity[Z]                                      0.32380E-29 
c  Pressure     0.20753E-06     485   0.93200E-08   0.15146E+00 0.14752E+04 
c  nu_tilda     0.30536E-05      35   0.14169E-04   0.76432E-06 0.45192E+03 
c  TempC        0.20062E+02      30   0.72155E-03   0.20576E+02 0.41130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6606          9.8842          4.5729          4.5729
v  Velocity[Y]            -3.6581          7.8899      0.00095567      0.00095567
v  Velocity[Z]       -6.9287e-015     1.2456e-014    -1.3439e-018    -1.3439e-018
v  ǁVelocityǁ          0.003491          9.9052          4.7552          4.7552
v  Pressure               -49.307          19.792         0.68988         0.68988
v  nu_tilda           7.5819e-007       0.0042137       0.0005866       0.0005866
v  TempC                       21          73.032          21.248          21.248
v  TurbVisc            2.803e-013       0.0049656      0.00067723      0.00067723
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              180:        0.34180E+01

===============================================================


 INSTANT    0.181000000E+03   TIME STEP NUMBER             181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18113E-01 0.93205E+00
   Friction velocity        uk    :  0.18113E-01 0.93205E+00
   Dimensionless distance   yplus :  0.14582E+00 0.75036E+01
   Friction thermal sca.    tstar : -0.59292E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10880E+00 0.55985E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44801E-02      34   0.74283E-03   0.43224E+01 0.12398E+03 
c  Velocity[X]                                      0.26208E+01 
c  Velocity[Y]                                      0.17016E+01 
c  Velocity[Z]                                      0.31810E-29 
c  Pressure     0.18152E-06     489   0.91385E-08   0.13371E+00 0.66917E+03 
c  nu_tilda     0.30594E-05      35   0.19144E-04   0.75903E-06 0.44967E+03 
c  TempC        0.20081E+02      30   0.56813E-03   0.17934E+02 0.37440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6379          9.8746          4.5729          4.5729
v  Velocity[Y]            -3.6468          7.8539       0.0009691       0.0009691
v  Velocity[Z]       -6.9287e-015     1.2903e-014    -1.3453e-018    -1.3453e-018
v  ǁVelocityǁ         0.0047158          9.8966          4.7558          4.7558
v  Pressure               -49.064          19.718         0.65497         0.65497
v  nu_tilda           7.6501e-007       0.0042142      0.00058716      0.00058716
v  TempC                       21          72.918          21.248          21.248
v  TurbVisc           2.9072e-013       0.0049662      0.00067795      0.00067795
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              181:        0.33930E+01

===============================================================


 INSTANT    0.182000000E+03   TIME STEP NUMBER             182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15904E-01 0.92970E+00
   Friction velocity        uk    :  0.15904E-01 0.92970E+00
   Dimensionless distance   yplus :  0.12804E+00 0.74847E+01
   Friction thermal sca.    tstar : -0.54121E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95530E-01 0.55844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44843E-02      34   0.89621E-03   0.42903E+01 0.12360E+03 
c  Velocity[X]                                      0.25972E+01 
c  Velocity[Y]                                      0.16931E+01 
c  Velocity[Z]                                      0.30463E-29 
c  Pressure     0.13910E-06     488   0.98259E-08   0.10295E+00 0.14089E+04 
c  nu_tilda     0.30652E-05      35   0.14160E-04   0.75390E-06 0.44745E+03 
c  TempC        0.20100E+02      30   0.10110E-02   0.17182E+02 0.36488E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.617          9.8658          4.5729          4.5729
v  Velocity[Y]            -3.6356           7.867      0.00098187      0.00098187
v  Velocity[Z]       -6.9287e-015     1.2811e-014    -1.3793e-018    -1.3793e-018
v  ǁVelocityǁ         0.0051191          9.8878          4.7564          4.7564
v  Pressure               -48.686          19.858         0.69837         0.69837
v  nu_tilda           7.7097e-007       0.0042147      0.00058782      0.00058782
v  TempC                       21          72.875          21.249          21.249
v  TurbVisc           3.0132e-013       0.0049668      0.00067866      0.00067866
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              182:        0.33110E+01

===============================================================


 INSTANT    0.183000000E+03   TIME STEP NUMBER             183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87741E-02 0.93025E+00
   Friction velocity        uk    :  0.87741E-02 0.93025E+00
   Dimensionless distance   yplus :  0.70637E-01 0.74891E+01
   Friction thermal sca.    tstar : -0.63035E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52703E-01 0.55877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44885E-02      34   0.87514E-03   0.43813E+01 0.12447E+03 
c  Velocity[X]                                      0.26638E+01 
c  Velocity[Y]                                      0.17175E+01 
c  Velocity[Z]                                      0.29924E-29 
c  Pressure     0.19394E-06     473   0.91446E-08   0.13967E+00 0.87570E+03 
c  nu_tilda     0.30710E-05      35   0.19027E-04   0.74874E-06 0.44524E+03 
c  TempC        0.20119E+02      30   0.70815E-03   0.23233E+02 0.42774E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5939          9.8558          4.5729          4.5729
v  Velocity[Y]            -3.6245          7.8268      0.00099478      0.00099478
v  Velocity[Z]       -6.9287e-015     1.3014e-014    -1.3994e-018    -1.3994e-018
v  ǁVelocityǁ          0.006683          9.8786           4.757           4.757
v  Pressure               -48.428          19.732         0.65643         0.65643
v  nu_tilda            7.751e-007       0.0042152      0.00058839      0.00058839
v  TempC                       21          72.883          21.249          21.249
v  TurbVisc           3.1083e-013       0.0049674      0.00067938      0.00067938
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              183:        0.33530E+01

===============================================================


 INSTANT    0.184000000E+03   TIME STEP NUMBER             184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81493E-02 0.92897E+00
   Friction velocity        uk    :  0.81493E-02 0.92897E+00
   Dimensionless distance   yplus :  0.65608E-01 0.74789E+01
   Friction thermal sca.    tstar : -0.77785E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48951E-01 0.55801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44926E-02      34   0.79596E-03   0.43585E+01 0.12433E+03 
c  Velocity[X]                                      0.26547E+01 
c  Velocity[Y]                                      0.17038E+01 
c  Velocity[Z]                                      0.30310E-29 
c  Pressure     0.16591E-06     490   0.97539E-08   0.11997E+00 0.18134E+04 
c  nu_tilda     0.30767E-05      35   0.14123E-04   0.74375E-06 0.44306E+03 
c  TempC        0.20138E+02      30   0.60351E-03   0.18804E+02 0.38253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5699          9.8458          4.5729          4.5729
v  Velocity[Y]            -3.6138          7.8453       0.0010078       0.0010078
v  Velocity[Z]       -6.9287e-015     1.2701e-014    -1.4413e-018    -1.4413e-018
v  ǁVelocityǁ         0.0069876          9.8692          4.7576          4.7576
v  Pressure               -48.064          19.935         0.71255         0.71255
v  nu_tilda           7.7769e-007       0.0042157      0.00058905      0.00058905
v  TempC                       21          72.882           21.25           21.25
v  TurbVisc           3.1754e-013        0.004968       0.0006801       0.0006801
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              184:        0.38750E+01

===============================================================


 INSTANT    0.185000000E+03   TIME STEP NUMBER             185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95986E-02 0.92980E+00
   Friction velocity        uk    :  0.95986E-02 0.92980E+00
   Dimensionless distance   yplus :  0.77276E-01 0.74855E+01
   Friction thermal sca.    tstar : -0.10537E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57656E-01 0.55851E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44968E-02      34   0.86756E-03   0.43266E+01 0.12392E+03 
c  Velocity[X]                                      0.26414E+01 
c  Velocity[Y]                                      0.16852E+01 
c  Velocity[Z]                                      0.32563E-29 
c  Pressure     0.21536E-06     456   0.98645E-08   0.15485E+00 0.47814E+03 
c  nu_tilda     0.30824E-05      35   0.18905E-04   0.73873E-06 0.44089E+03 
c  TempC        0.20157E+02      30   0.86855E-03   0.17999E+02 0.37070E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5444           9.836          4.5729          4.5729
v  Velocity[Y]             -3.603          7.8201       0.0010208       0.0010208
v  Velocity[Z]       -6.9287e-015     1.3026e-014    -1.4793e-018    -1.4793e-018
v  ǁVelocityǁ         0.0057769          9.8596          4.7583          4.7583
v  Pressure               -47.758          19.886         0.68928         0.68928
v  nu_tilda           7.7762e-007       0.0042162      0.00058961      0.00058961
v  TempC                   20.986          72.965           21.25           21.25
v  TurbVisc           3.2181e-013       0.0049686      0.00068082      0.00068082
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              185:        0.39660E+01

===============================================================


 INSTANT    0.186000000E+03   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10024E-01 0.92835E+00
   Friction velocity        uk    :  0.10024E-01 0.92835E+00
   Dimensionless distance   yplus :  0.80700E-01 0.74739E+01
   Friction thermal sca.    tstar : -0.52906E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60211E-01 0.55763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45010E-02      34   0.80953E-03   0.43708E+01 0.12444E+03 
c  Velocity[X]                                      0.26527E+01 
c  Velocity[Y]                                      0.17181E+01 
c  Velocity[Z]                                      0.32079E-29 
c  Pressure     0.17370E-06     489   0.99044E-08   0.12465E+00 0.11641E+04 
c  nu_tilda     0.30881E-05      35   0.14092E-04   0.73389E-06 0.43875E+03 
c  TempC        0.20177E+02      30   0.85681E-03   0.18517E+02 0.39200E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5171          9.8252          4.5729          4.5729
v  Velocity[Y]             -3.592          7.8357       0.0010342       0.0010342
v  Velocity[Z]       -6.9287e-015     1.2709e-014    -1.5484e-018    -1.5484e-018
v  ǁVelocityǁ         0.0022691          9.8501          4.7589          4.7589
v  Pressure                -47.43          20.011         0.72324         0.72324
v  nu_tilda           7.7481e-007       0.0042167      0.00059028      0.00059028
v  TempC                       21          72.865          21.251          21.251
v  TurbVisc           3.2169e-013       0.0049692      0.00068154      0.00068154
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              186:        0.36720E+01

===============================================================


 INSTANT    0.187000000E+03   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48003E-02 0.92871E+00
   Friction velocity        uk    :  0.48003E-02 0.92871E+00
   Dimensionless distance   yplus :  0.38645E-01 0.74767E+01
   Friction thermal sca.    tstar : -0.56431E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28834E-01 0.55785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45052E-02      34   0.87077E-03   0.44063E+01 0.12464E+03 
c  Velocity[X]                                      0.27119E+01 
c  Velocity[Y]                                      0.16944E+01 
c  Velocity[Z]                                      0.25257E-29 
c  Pressure     0.21322E-06     456   0.95440E-08   0.14621E+00 0.46868E+03 
c  nu_tilda     0.30938E-05      35   0.18786E-04   0.72901E-06 0.43663E+03 
c  TempC        0.20196E+02      30   0.86127E-03   0.20115E+02 0.40743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4889          9.8149          4.5729          4.5729
v  Velocity[Y]            -3.5813          7.8257       0.0010483       0.0010483
v  Velocity[Z]       -6.9287e-015     1.2851e-014    -1.5933e-018    -1.5933e-018
v  ǁVelocityǁ         0.0038815          9.8406          4.7595          4.7595
v  Pressure               -47.144           19.97          0.6994          0.6994
v  nu_tilda           7.7034e-007       0.0042172      0.00059085      0.00059085
v  TempC                       21          72.846          21.251          21.251
v  TurbVisc           3.1707e-013       0.0049698      0.00068227      0.00068227
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              187:        0.34250E+01

===============================================================


 INSTANT    0.188000000E+03   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20417E-01 0.92757E+00
   Friction velocity        uk    :  0.20417E-01 0.92757E+00
   Dimensionless distance   yplus :  0.16437E+00 0.74676E+01
   Friction thermal sca.    tstar : -0.10502E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12264E+00 0.55717E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45094E-02      34   0.80829E-03   0.44101E+01 0.12470E+03 
c  Velocity[X]                                      0.27131E+01 
c  Velocity[Y]                                      0.16970E+01 
c  Velocity[Z]                                      0.32154E-29 
c  Pressure     0.18396E-06     489   0.96034E-08   0.12985E+00 0.11012E+04 
c  nu_tilda     0.30995E-05      35   0.14074E-04   0.72430E-06 0.43453E+03 
c  TempC        0.20215E+02      30   0.99230E-03   0.20454E+02 0.43351E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4593          9.8039          4.5729          4.5729
v  Velocity[Y]             -3.571           7.787       0.0010617       0.0010617
v  Velocity[Z]       -6.9287e-015     1.2733e-014    -1.6522e-018    -1.6522e-018
v  ǁVelocityǁ         0.0028138          9.8305          4.7602          4.7602
v  Pressure               -46.712          20.043         0.73473         0.73473
v  nu_tilda           7.6472e-007       0.0042176      0.00059151      0.00059151
v  TempC                       21           72.99          21.252          21.252
v  TurbVisc           3.0981e-013       0.0049703      0.00068299      0.00068299
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              188:        0.36280E+01

===============================================================


 INSTANT    0.189000000E+03   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12843E-01 0.92523E+00
   Friction velocity        uk    :  0.12843E-01 0.92523E+00
   Dimensionless distance   yplus :  0.10339E+00 0.74487E+01
   Friction thermal sca.    tstar : -0.71694E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77144E-01 0.55576E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45136E-02      34   0.86541E-03   0.44021E+01 0.12487E+03 
c  Velocity[X]                                      0.26837E+01 
c  Velocity[Y]                                      0.17184E+01 
c  Velocity[Z]                                      0.27241E-29 
c  Pressure     0.15508E-06     457   0.93350E-08   0.10674E+00 0.45693E+03 
c  nu_tilda     0.31051E-05      35   0.18670E-04   0.71954E-06 0.43245E+03 
c  TempC        0.20234E+02      30   0.88495E-03   0.24152E+02 0.48107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4285          9.7955          4.5729          4.5729
v  Velocity[Y]            -3.5606          7.8001        0.001075        0.001075
v  Velocity[Z]       -6.9287e-015     1.2993e-014     -1.727e-018     -1.727e-018
v  ǁVelocityǁ         0.0022234          9.8204          4.7608          4.7608
v  Pressure               -46.515          20.048         0.71135         0.71135
v  nu_tilda           7.5812e-007       0.0042181      0.00059208      0.00059208
v  TempC                       21          72.827          21.252          21.252
v  TurbVisc           3.0087e-013       0.0049709      0.00068372      0.00068372
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              189:        0.34530E+01

===============================================================


 INSTANT    0.190000000E+03   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83820E-02 0.92576E+00
   Friction velocity        uk    :  0.83820E-02 0.92576E+00
   Dimensionless distance   yplus :  0.67481E-01 0.74530E+01
   Friction thermal sca.    tstar : -0.60781E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50348E-01 0.55608E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45178E-02      34   0.82889E-03   0.44625E+01 0.12561E+03 
c  Velocity[X]                                      0.27390E+01 
c  Velocity[Y]                                      0.17235E+01 
c  Velocity[Z]                                      0.25603E-29 
c  Pressure     0.17933E-06     377   0.97648E-08   0.12265E+00 0.39359E+03 
c  nu_tilda     0.31107E-05      35   0.14027E-04   0.71493E-06 0.43038E+03 
c  TempC        0.20253E+02      30   0.81737E-03   0.20231E+02 0.43473E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.395          9.7884          4.5729          4.5729
v  Velocity[Y]            -3.5502          7.7604       0.0010898       0.0010898
v  Velocity[Z]       -6.9287e-015     1.3315e-014     -1.795e-018     -1.795e-018
v  ǁVelocityǁ         0.0017745          9.8101          4.7615          4.7615
v  Pressure               -46.145          19.995         0.71708         0.71708
v  nu_tilda           7.5109e-007       0.0042186      0.00059275      0.00059275
v  TempC                       21          72.824          21.253          21.253
v  TurbVisc           2.9062e-013       0.0049715      0.00068444      0.00068444
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              190:        0.32110E+01

===============================================================


 INSTANT    0.191000000E+03   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71590E-02 0.92451E+00
   Friction velocity        uk    :  0.71590E-02 0.92451E+00
   Dimensionless distance   yplus :  0.57635E-01 0.74429E+01
   Friction thermal sca.    tstar : -0.51074E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43002E-01 0.55533E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45220E-02      34   0.84700E-03   0.44535E+01 0.12551E+03 
c  Velocity[X]                                      0.27443E+01 
c  Velocity[Y]                                      0.17092E+01 
c  Velocity[Z]                                      0.36938E-29 
c  Pressure     0.17418E-06     457   0.97519E-08   0.11843E+00 0.13368E+04 
c  nu_tilda     0.31163E-05      35   0.18561E-04   0.71028E-06 0.42834E+03 
c  TempC        0.20272E+02      30   0.66542E-03   0.18045E+02 0.39884E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3636          9.7799          4.5729          4.5729
v  Velocity[Y]            -3.5398          7.7801       0.0011033       0.0011033
v  Velocity[Z]       -6.9287e-015     1.2455e-014    -1.8749e-018    -1.8749e-018
v  ǁVelocityǁ         0.0023105          9.7991          4.7621          4.7621
v  Pressure               -45.812          20.152         0.73548         0.73548
v  nu_tilda            7.438e-007       0.0042191      0.00059333      0.00059333
v  TempC                       21          72.804          21.253          21.253
v  TurbVisc           2.7998e-013        0.004972      0.00068518      0.00068518
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              191:        0.34530E+01

===============================================================


 INSTANT    0.192000000E+03   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12783E-01 0.92526E+00
   Friction velocity        uk    :  0.12783E-01 0.92526E+00
   Dimensionless distance   yplus :  0.10291E+00 0.74490E+01
   Friction thermal sca.    tstar : -0.51173E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76785E-01 0.55578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45262E-02      34   0.80744E-03   0.45004E+01 0.12611E+03 
c  Velocity[X]                                      0.27549E+01 
c  Velocity[Y]                                      0.17454E+01 
c  Velocity[Z]                                      0.24539E-29 
c  Pressure     0.20753E-06     440   0.94497E-08   0.13875E+00 0.47597E+03 
c  nu_tilda     0.31219E-05      35   0.13993E-04   0.70580E-06 0.42632E+03 
c  TempC        0.20291E+02      30   0.86091E-03   0.16521E+02 0.36877E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3293          9.7719          4.5729          4.5729
v  Velocity[Y]            -3.5296          7.7501       0.0011178       0.0011178
v  Velocity[Z]       -6.9287e-015     1.2564e-014    -1.9597e-018    -1.9597e-018
v  ǁVelocityǁ         0.0030597          9.7914          4.7628          4.7628
v  Pressure               -45.465          20.137         0.74693         0.74693
v  nu_tilda           7.3662e-007       0.0042195        0.000594        0.000594
v  TempC                       21          72.818          21.254          21.254
v  TurbVisc           2.6928e-013       0.0049726      0.00068591      0.00068591
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              192:        0.34370E+01

===============================================================


 INSTANT    0.193000000E+03   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15651E-01 0.92378E+00
   Friction velocity        uk    :  0.15651E-01 0.92378E+00
   Dimensionless distance   yplus :  0.12600E+00 0.74370E+01
   Friction thermal sca.    tstar : -0.58698E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94010E-01 0.55489E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45304E-02      34   0.83082E-03   0.45294E+01 0.12660E+03 
c  Velocity[X]                                      0.27860E+01 
c  Velocity[Y]                                      0.17434E+01 
c  Velocity[Z]                                      0.23957E-29 
c  Pressure     0.19588E-06     453   0.99080E-08   0.12786E+00 0.44487E+03 
c  nu_tilda     0.31274E-05      35   0.18464E-04   0.70128E-06 0.42431E+03 
c  TempC        0.20310E+02      30   0.96037E-03   0.20219E+02 0.43575E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2931           9.763          4.5729          4.5729
v  Velocity[Y]            -3.5194          7.7703       0.0011321       0.0011321
v  Velocity[Z]       -6.9287e-015     1.2732e-014    -2.0515e-018    -2.0515e-018
v  ǁVelocityǁ         0.0041777          9.7835          4.7634          4.7634
v  Pressure               -45.262           20.14         0.72554         0.72554
v  nu_tilda           7.3115e-007         0.00422      0.00059457      0.00059457
v  TempC                       21          72.806          21.254          21.254
v  TurbVisc           2.5902e-013       0.0049731      0.00068664      0.00068664
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              193:        0.34370E+01

===============================================================


 INSTANT    0.194000000E+03   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21659E-01 0.92441E+00
   Friction velocity        uk    :  0.21659E-01 0.92441E+00
   Dimensionless distance   yplus :  0.17437E+00 0.74421E+01
   Friction thermal sca.    tstar : -0.69797E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13010E+00 0.55527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45346E-02      34   0.87886E-03   0.46024E+01 0.12724E+03 
c  Velocity[X]                                      0.28497E+01 
c  Velocity[Y]                                      0.17527E+01 
c  Velocity[Z]                                      0.33262E-29 
c  Pressure     0.21099E-06     473   0.92870E-08   0.13614E+00 0.12728E+04 
c  nu_tilda     0.31329E-05      35   0.13949E-04   0.69690E-06 0.42232E+03 
c  TempC        0.20329E+02      30   0.10760E-02   0.18078E+02 0.42884E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2554          9.7539          4.5729          4.5729
v  Velocity[Y]            -3.5093          7.7561       0.0011468       0.0011468
v  Velocity[Z]       -6.9287e-015     1.2362e-014    -2.1449e-018    -2.1449e-018
v  ǁVelocityǁ         0.0050128          9.7745          4.7641          4.7641
v  Pressure               -44.836          20.243         0.76463         0.76463
v  nu_tilda           7.2773e-007       0.0042204      0.00059525      0.00059525
v  TempC                       21          73.138          21.255          21.255
v  TurbVisc           2.5142e-013       0.0049737      0.00068737      0.00068737
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              194:        0.36800E+01

===============================================================


 INSTANT    0.195000000E+03   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24333E-01 0.92297E+00
   Friction velocity        uk    :  0.24333E-01 0.92297E+00
   Dimensionless distance   yplus :  0.19590E+00 0.74306E+01
   Friction thermal sca.    tstar : -0.86735E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14616E+00 0.55440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45388E-02      34   0.76388E-03   0.46239E+01 0.12766E+03 
c  Velocity[X]                                      0.28743E+01 
c  Velocity[Y]                                      0.17496E+01 
c  Velocity[Z]                                      0.26087E-29 
c  Pressure     0.18769E-06     489   0.96004E-08   0.11961E+00 0.85299E+03 
c  nu_tilda     0.31384E-05      35   0.18352E-04   0.69249E-06 0.42035E+03 
c  TempC        0.20348E+02      30   0.95196E-03   0.22277E+02 0.45778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2158          9.7447          4.5729          4.5729
v  Velocity[Y]            -3.4993            7.72       0.0011614       0.0011614
v  Velocity[Z]       -6.9287e-015     1.2071e-014    -2.2488e-018    -2.2488e-018
v  ǁVelocityǁ         0.0068092          9.7658          4.7648          4.7648
v  Pressure               -44.586          20.126         0.72183         0.72183
v  nu_tilda           7.2635e-007       0.0042209      0.00059583      0.00059583
v  TempC                       21          72.944          21.255          21.255
v  TurbVisc           2.4674e-013       0.0049742      0.00068811      0.00068811
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              195:        0.42720E+01

===============================================================


 INSTANT    0.196000000E+03   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11642E-01 0.92068E+00
   Friction velocity        uk    :  0.11642E-01 0.92068E+00
   Dimensionless distance   yplus :  0.93726E-01 0.74121E+01
   Friction thermal sca.    tstar : -0.14894E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69930E-01 0.55303E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45429E-02      34   0.86788E-03   0.46071E+01 0.12778E+03 
c  Velocity[X]                                      0.28404E+01 
c  Velocity[Y]                                      0.17667E+01 
c  Velocity[Z]                                      0.21584E-29 
c  Pressure     0.20102E-06     505   0.97938E-08   0.12758E+00 0.13605E+04 
c  nu_tilda     0.31439E-05      35   0.13875E-04   0.68821E-06 0.41840E+03 
c  TempC        0.20367E+02      30   0.86494E-03   0.17779E+02 0.42271E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2374          9.7346          4.5729          4.5729
v  Velocity[Y]            -3.4893          7.7324        0.001176        0.001176
v  Velocity[Z]       -6.9287e-015     1.2295e-014    -2.3549e-018    -2.3549e-018
v  ǁVelocityǁ         0.0062289          9.7567          4.7654          4.7654
v  Pressure               -44.244          20.263         0.76426         0.76426
v  nu_tilda           7.2709e-007       0.0042213       0.0005965       0.0005965
v  TempC                       21          72.992          21.256          21.256
v  TurbVisc           2.4488e-013       0.0049747      0.00068885      0.00068885
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              196:        0.41930E+01

===============================================================


 INSTANT    0.197000000E+03   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13151E-01 0.92118E+00
   Friction velocity        uk    :  0.13151E-01 0.92118E+00
   Dimensionless distance   yplus :  0.10587E+00 0.74161E+01
   Friction thermal sca.    tstar : -0.16302E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78993E-01 0.55332E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45472E-02      34   0.88616E-03   0.46876E+01 0.12859E+03 
c  Velocity[X]                                      0.28875E+01 
c  Velocity[Y]                                      0.18001E+01 
c  Velocity[Z]                                      0.34212E-29 
c  Pressure     0.21184E-06     488   0.97773E-08   0.13411E+00 0.64725E+03 
c  nu_tilda     0.31493E-05      35   0.18234E-04   0.68390E-06 0.41647E+03 
c  TempC        0.20385E+02      30   0.87507E-03   0.16727E+02 0.38508E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2586          9.7244          4.5729          4.5729
v  Velocity[Y]            -3.4793           7.692       0.0011906       0.0011906
v  Velocity[Z]       -6.9287e-015     1.2734e-014    -2.4736e-018    -2.4736e-018
v  ǁVelocityǁ         0.0046044          9.7476          4.7661          4.7661
v  Pressure               -43.895          20.168           0.732           0.732
v  nu_tilda           7.3051e-007       0.0042218      0.00059708      0.00059708
v  TempC                   20.998          73.099          21.256          21.256
v  TurbVisc           2.4588e-013       0.0049752      0.00068959      0.00068959
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              197:        0.38060E+01

===============================================================


 INSTANT    0.198000000E+03   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12973E-01 0.91969E+00
   Friction velocity        uk    :  0.12973E-01 0.91969E+00
   Dimensionless distance   yplus :  0.10444E+00 0.74041E+01
   Friction thermal sca.    tstar : -0.95213E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77924E-01 0.55243E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45513E-02      34   0.87434E-03   0.47111E+01 0.12899E+03 
c  Velocity[X]                                      0.29096E+01 
c  Velocity[Y]                                      0.18015E+01 
c  Velocity[Z]                                      0.26086E-29 
c  Pressure     0.18288E-06     457   0.97839E-08   0.11135E+00 0.84918E+03 
c  nu_tilda     0.31548E-05      35   0.13818E-04   0.67976E-06 0.41456E+03 
c  TempC        0.20404E+02      30   0.85089E-03   0.17343E+02 0.42060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2807          9.7146          4.5729          4.5729
v  Velocity[Y]            -3.4695          7.7089       0.0012059       0.0012059
v  Velocity[Z]       -6.9287e-015     1.2349e-014    -2.5892e-018    -2.5892e-018
v  ǁVelocityǁ         0.0026227          9.7382          4.7668          4.7668
v  Pressure               -43.648          20.257         0.75531         0.75531
v  nu_tilda           7.3557e-007       0.0042222      0.00059776      0.00059776
v  TempC                       21          73.262          21.257          21.257
v  TurbVisc           2.5053e-013       0.0049758      0.00069033      0.00069033
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              198:        0.36580E+01

===============================================================


 INSTANT    0.199000000E+03   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20254E-01 0.92050E+00
   Friction velocity        uk    :  0.20254E-01 0.92050E+00
   Dimensionless distance   yplus :  0.16306E+00 0.74107E+01
   Friction thermal sca.    tstar : -0.99453E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12166E+00 0.55292E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45555E-02      34   0.86400E-03   0.48968E+01 0.13080E+03 
c  Velocity[X]                                      0.29783E+01 
c  Velocity[Y]                                      0.19185E+01 
c  Velocity[Z]                                      0.21164E-29 
c  Pressure     0.23459E-06     474   0.92624E-08   0.14484E+00 0.76318E+03 
c  nu_tilda     0.31602E-05      35   0.18135E-04   0.67553E-06 0.41266E+03 
c  TempC        0.20423E+02      30   0.96462E-03   0.15828E+02 0.40613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3022          9.7033          4.5729          4.5729
v  Velocity[Y]            -3.4601          7.6812       0.0012207       0.0012207
v  Velocity[Z]       -6.9287e-015     1.2443e-014     -2.709e-018     -2.709e-018
v  ǁVelocityǁ         0.0023075          9.7283          4.7674          4.7674
v  Pressure                -43.37           20.14         0.71671         0.71671
v  nu_tilda            7.412e-007       0.0042226      0.00059834      0.00059834
v  TempC                       21          73.342          21.258          21.258
v  TurbVisc           2.5756e-013       0.0049763      0.00069107      0.00069107
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              199:        0.37640E+01

===============================================================


 INSTANT    0.200000000E+03   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13390E-01 0.91902E+00
   Friction velocity        uk    :  0.13390E-01 0.91902E+00
   Dimensionless distance   yplus :  0.10780E+00 0.73987E+01
   Friction thermal sca.    tstar : -0.14614E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80428E-01 0.55203E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45597E-02      34   0.78736E-03   0.48390E+01 0.13030E+03 
c  Velocity[X]                                      0.29903E+01 
c  Velocity[Y]                                      0.18487E+01 
c  Velocity[Z]                                      0.41197E-29 
c  Pressure     0.18438E-06     488   0.99706E-08   0.11088E+00 0.19797E+04 
c  nu_tilda     0.31656E-05      35   0.13749E-04   0.67149E-06 0.41078E+03 
c  TempC        0.20442E+02      30   0.95508E-03   0.15609E+02 0.38328E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3245          9.6926          4.5729          4.5729
v  Velocity[Y]            -3.4506            7.69       0.0012359       0.0012359
v  Velocity[Z]       -6.9287e-015     1.3526e-014    -2.8398e-018    -2.8398e-018
v  ǁVelocityǁ         0.0017316          9.7183          4.7681          4.7681
v  Pressure               -42.934          20.337         0.77887         0.77887
v  nu_tilda           7.4602e-007        0.004223      0.00059902      0.00059902
v  TempC                       21          73.409          21.258          21.258
v  TurbVisc           2.6553e-013       0.0049768      0.00069181      0.00069181
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              200:        0.37770E+01

===============================================================


 INSTANT    0.201000000E+03   TIME STEP NUMBER             201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63851E-02 0.91979E+00
   Friction velocity        uk    :  0.63851E-02 0.91979E+00
   Dimensionless distance   yplus :  0.51404E-01 0.74049E+01
   Friction thermal sca.    tstar : -0.48087E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38353E-01 0.55249E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45639E-02      34   0.81072E-03   0.47814E+01 0.13034E+03 
c  Velocity[X]                                      0.29408E+01 
c  Velocity[Y]                                      0.18406E+01 
c  Velocity[Z]                                      0.36512E-29 
c  Pressure     0.16961E-06     489   0.98965E-08   0.10315E+00 0.10039E+04 
c  nu_tilda     0.31710E-05      35   0.18033E-04   0.66738E-06 0.40892E+03 
c  TempC        0.20461E+02      30   0.98001E-03   0.16266E+02 0.38872E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3471          9.6812          4.5729          4.5729
v  Velocity[Y]            -3.4414          7.6855       0.0012502       0.0012502
v  Velocity[Z]       -6.9287e-015     1.1697e-014     -2.984e-018     -2.984e-018
v  ǁVelocityǁ         0.0020726          9.7078          4.7688          4.7688
v  Pressure               -43.648          20.228         0.72702         0.72702
v  nu_tilda           7.4991e-007       0.0042235      0.00059961      0.00059961
v  TempC                       21          72.361          21.259          21.259
v  TurbVisc            2.725e-013       0.0049773      0.00069256      0.00069256
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              201:        0.37550E+01

===============================================================


 INSTANT    0.202000000E+03   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11083E-01 0.91825E+00
   Friction velocity        uk    :  0.11083E-01 0.91825E+00
   Dimensionless distance   yplus :  0.89228E-01 0.73925E+01
   Friction thermal sca.    tstar : -0.12880E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66574E-01 0.55157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45681E-02      34   0.87241E-03   0.48561E+01 0.13130E+03 
c  Velocity[X]                                      0.30066E+01 
c  Velocity[Y]                                      0.18495E+01 
c  Velocity[Z]                                      0.26475E-29 
c  Pressure     0.18364E-06     297   0.95536E-08   0.11162E+00 0.38317E+03 
c  nu_tilda     0.31763E-05      35   0.13703E-04   0.66343E-06 0.40707E+03 
c  TempC        0.20479E+02      30   0.98198E-03   0.17637E+02 0.42819E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3699          9.6706          4.5729          4.5729
v  Velocity[Y]            -3.4318          7.6507       0.0012646       0.0012646
v  Velocity[Z]       -6.9287e-015     1.2705e-014     -3.117e-018     -3.117e-018
v  ǁVelocityǁ         0.0030806          9.6977          4.7694          4.7694
v  Pressure               -44.182          20.146         0.72558         0.72558
v  nu_tilda           7.5314e-007       0.0042239      0.00060029      0.00060029
v  TempC                       21          72.422          21.259          21.259
v  TurbVisc           2.7823e-013       0.0049778      0.00069331      0.00069331
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              202:        0.31690E+01

===============================================================


 INSTANT    0.203000000E+03   TIME STEP NUMBER             203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18091E-01 0.91615E+00
   Friction velocity        uk    :  0.18091E-01 0.91615E+00
   Dimensionless distance   yplus :  0.14565E+00 0.73756E+01
   Friction thermal sca.    tstar : -0.95347E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10867E+00 0.55030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45723E-02      34   0.89725E-03   0.49150E+01 0.13200E+03 
c  Velocity[X]                                      0.30584E+01 
c  Velocity[Y]                                      0.18566E+01 
c  Velocity[Z]                                      0.27532E-29 
c  Pressure     0.25383E-06     426   0.96931E-08   0.14921E+00 0.12273E+04 
c  nu_tilda     0.31816E-05      35   0.17943E-04   0.65942E-06 0.40524E+03 
c  TempC        0.20498E+02      30   0.80590E-03   0.15613E+02 0.41703E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3921          9.6629          4.5729          4.5729
v  Velocity[Y]            -3.4224          7.6682       0.0012806       0.0012806
v  Velocity[Z]       -6.9287e-015     1.2905e-014    -3.2741e-018    -3.2741e-018
v  ǁVelocityǁ          0.004272          9.6872          4.7701          4.7701
v  Pressure               -44.736          20.266         0.74134         0.74134
v  nu_tilda            7.548e-007       0.0042243      0.00060088      0.00060088
v  TempC                       21          72.828           21.26           21.26
v  TurbVisc           2.8305e-013       0.0049783      0.00069406      0.00069406
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              203:        0.34660E+01

===============================================================


 INSTANT    0.204000000E+03   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22008E-01 0.91680E+00
   Friction velocity        uk    :  0.22008E-01 0.91680E+00
   Dimensionless distance   yplus :  0.17718E+00 0.73809E+01
   Friction thermal sca.    tstar : -0.80890E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13220E+00 0.55070E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45765E-02      34   0.78776E-03   0.49829E+01 0.13283E+03 
c  Velocity[X]                                      0.30742E+01 
c  Velocity[Y]                                      0.19087E+01 
c  Velocity[Z]                                      0.36348E-29 
c  Pressure     0.22175E-06     394   0.99981E-08   0.13404E+00 0.45175E+03 
c  nu_tilda     0.31869E-05      35   0.13635E-04   0.65561E-06 0.40344E+03 
c  TempC        0.20517E+02      30   0.70738E-03   0.14470E+02 0.38983E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4134          9.6547          4.5729          4.5729
v  Velocity[Y]            -3.4132          7.6273       0.0012946       0.0012946
v  Velocity[Z]       -6.9287e-015     1.3151e-014    -3.4238e-018    -3.4238e-018
v  ǁVelocityǁ         0.0057314          9.6763          4.7708          4.7708
v  Pressure               -45.167           20.17         0.73061         0.73061
v  nu_tilda           7.5474e-007       0.0042247      0.00060156      0.00060156
v  TempC                       21          73.148          21.261          21.261
v  TurbVisc           2.8556e-013       0.0049788       0.0006948       0.0006948
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              204:        0.34030E+01

===============================================================


 INSTANT    0.205000000E+03   TIME STEP NUMBER             205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18199E-01 0.91506E+00
   Friction velocity        uk    :  0.18199E-01 0.91506E+00
   Dimensionless distance   yplus :  0.14652E+00 0.73669E+01
   Friction thermal sca.    tstar : -0.79205E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10932E+00 0.54965E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45807E-02      34   0.85416E-03   0.49744E+01 0.13314E+03 
c  Velocity[X]                                      0.30661E+01 
c  Velocity[Y]                                      0.19083E+01 
c  Velocity[Z]                                      0.32239E-29 
c  Pressure     0.21167E-06     440   0.99050E-08   0.12692E+00 0.46451E+03 
c  nu_tilda     0.31922E-05      35   0.17849E-04   0.65170E-06 0.40164E+03 
c  TempC        0.20535E+02      29   0.91313E-03   0.13012E+02 0.35219E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4348          9.6455          4.5729          4.5729
v  Velocity[Y]            -3.4044          7.6462       0.0013096       0.0013096
v  Velocity[Z]       -6.9287e-015     1.1945e-014    -3.5894e-018    -3.5894e-018
v  ǁVelocityǁ         0.0067021          9.6662          4.7715          4.7715
v  Pressure               -45.583          20.161          0.7046          0.7046
v  nu_tilda           7.5319e-007       0.0042251      0.00060215      0.00060215
v  TempC                       21            73.3          21.261          21.261
v  TurbVisc           2.8546e-013       0.0049792      0.00069556      0.00069556
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              205:        0.37090E+01

===============================================================


 INSTANT    0.206000000E+03   TIME STEP NUMBER             206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27521E-01 0.91564E+00
   Friction velocity        uk    :  0.27521E-01 0.91564E+00
   Dimensionless distance   yplus :  0.22156E+00 0.73715E+01
   Friction thermal sca.    tstar : -0.96585E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16531E+00 0.55000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45849E-02      34   0.93182E-03   0.50169E+01 0.13376E+03 
c  Velocity[X]                                      0.31109E+01 
c  Velocity[Y]                                      0.19060E+01 
c  Velocity[Z]                                      0.30403E-29 
c  Pressure     0.25373E-06     504   0.98561E-08   0.15136E+00 0.17389E+04 
c  nu_tilda     0.31975E-05      35   0.13597E-04   0.64799E-06 0.39987E+03 
c  TempC        0.20554E+02      29   0.10309E-02   0.16370E+02 0.42404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4573           9.636          4.5729          4.5729
v  Velocity[Y]            -3.3955          7.6473       0.0013254       0.0013254
v  Velocity[Z]       -6.9287e-015     1.3029e-014    -3.7581e-018    -3.7581e-018
v  ǁVelocityǁ          0.004278          9.6576          4.7721          4.7721
v  Pressure               -45.838          20.307         0.76034         0.76034
v  nu_tilda           7.5063e-007       0.0042255      0.00060284      0.00060284
v  TempC                       21          73.425          21.262          21.262
v  TurbVisc           2.8313e-013       0.0049797       0.0006963       0.0006963
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              206:        0.37180E+01

===============================================================


 INSTANT    0.207000000E+03   TIME STEP NUMBER             207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21173E-01 0.91433E+00
   Friction velocity        uk    :  0.21173E-01 0.91433E+00
   Dimensionless distance   yplus :  0.17046E+00 0.73610E+01
   Friction thermal sca.    tstar : -0.16158E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12718E+00 0.54921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45891E-02      34   0.84847E-03   0.51307E+01 0.13505E+03 
c  Velocity[X]                                      0.31691E+01 
c  Velocity[Y]                                      0.19616E+01 
c  Velocity[Z]                                      0.28502E-29 
c  Pressure     0.23082E-06     490   0.96459E-08   0.13845E+00 0.14695E+04 
c  nu_tilda     0.32028E-05      35   0.17750E-04   0.64426E-06 0.39811E+03 
c  TempC        0.20573E+02      30   0.67322E-03   0.17306E+02 0.44337E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4788          9.6264          4.5729          4.5729
v  Velocity[Y]            -3.3866          7.6042       0.0013404       0.0013404
v  Velocity[Z]       -6.9287e-015     1.2358e-014    -3.9392e-018    -3.9392e-018
v  ǁVelocityǁ         0.0034854          9.6489          4.7728          4.7728
v  Pressure               -46.132          20.089         0.69445         0.69445
v  nu_tilda           7.4705e-007       0.0042259      0.00060343      0.00060343
v  TempC                       21          73.493          21.262          21.262
v  TurbVisc            2.793e-013       0.0049802      0.00069706      0.00069706
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              207:        0.39710E+01

===============================================================


 INSTANT    0.208000000E+03   TIME STEP NUMBER             208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13744E-01 0.91216E+00
   Friction velocity        uk    :  0.13744E-01 0.91216E+00
   Dimensionless distance   yplus :  0.11065E+00 0.73435E+01
   Friction thermal sca.    tstar : -0.19427E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82554E-01 0.54791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45933E-02      34   0.80614E-03   0.51034E+01 0.13516E+03 
c  Velocity[X]                                      0.31401E+01 
c  Velocity[Y]                                      0.19634E+01 
c  Velocity[Z]                                      0.40846E-29 
c  Pressure     0.25157E-06     457   0.98534E-08   0.15304E+00 0.11089E+04 
c  nu_tilda     0.32080E-05      35   0.13534E-04   0.64067E-06 0.39637E+03 
c  TempC        0.20591E+02      30   0.10502E-02   0.98360E+01 0.32495E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4998          9.6166          4.5729          4.5729
v  Velocity[Y]            -3.3779          7.6132       0.0013557       0.0013557
v  Velocity[Z]       -6.9287e-015     1.3402e-014    -4.1127e-018    -4.1127e-018
v  ǁVelocityǁ         0.0026099          9.6396          4.7735          4.7735
v  Pressure               -46.479          20.203         0.72551         0.72551
v  nu_tilda           7.4271e-007       0.0042263      0.00060411      0.00060411
v  TempC                       21          73.455          21.263          21.263
v  TurbVisc           2.7401e-013       0.0049806      0.00069781      0.00069781
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              208:        0.37410E+01

===============================================================


 INSTANT    0.209000000E+03   TIME STEP NUMBER             209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16056E-01 0.91265E+00
   Friction velocity        uk    :  0.16056E-01 0.91265E+00
   Dimensionless distance   yplus :  0.12926E+00 0.73475E+01
   Friction thermal sca.    tstar : -0.10068E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96443E-01 0.54820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45975E-02      34   0.85702E-03   0.51643E+01 0.13591E+03 
c  Velocity[X]                                      0.31882E+01 
c  Velocity[Y]                                      0.19761E+01 
c  Velocity[Z]                                      0.37511E-29 
c  Pressure     0.30840E-06     457   0.94989E-08   0.18627E+00 0.62837E+03 
c  nu_tilda     0.32132E-05      35   0.17666E-04   0.63703E-06 0.39465E+03 
c  TempC        0.20610E+02      30   0.88266E-03   0.16488E+02 0.40701E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5222          9.6059          4.5729          4.5729
v  Velocity[Y]            -3.3691          7.5847       0.0013721       0.0013721
v  Velocity[Z]       -7.9498e-015     1.2366e-014    -4.3037e-018    -4.3037e-018
v  ǁVelocityǁ         0.0017472          9.6302          4.7742          4.7742
v  Pressure               -46.508          20.096         0.69562         0.69562
v  nu_tilda            7.376e-007       0.0042267      0.00060471      0.00060471
v  TempC                       21           73.48          21.264          21.264
v  TurbVisc            2.677e-013       0.0049811      0.00069857      0.00069857
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              209:        0.38930E+01

===============================================================


 INSTANT    0.210000000E+03   TIME STEP NUMBER             210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17250E-02 0.91118E+00
   Friction velocity        uk    :  0.17250E-02 0.91118E+00
   Dimensionless distance   yplus :  0.13887E-01 0.73356E+01
   Friction thermal sca.    tstar : -0.79730E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10361E-01 0.54732E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46016E-02      34   0.94721E-03   0.52439E+01 0.13702E+03 
c  Velocity[X]                                      0.32234E+01 
c  Velocity[Y]                                      0.20206E+01 
c  Velocity[Z]                                      0.33377E-29 
c  Pressure     0.42541E-06     441   0.99027E-08   0.26009E+00 0.67988E+03 
c  nu_tilda     0.32184E-05      35   0.13453E-04   0.63356E-06 0.39295E+03 
c  TempC        0.20628E+02      30   0.80125E-03   0.12863E+02 0.36093E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.543           9.595          4.5729          4.5729
v  Velocity[Y]            -3.3605           7.593       0.0013873       0.0013873
v  Velocity[Z]       -1.2877e-014     1.2718e-014    -4.5026e-018    -4.5026e-018
v  ǁVelocityǁ         0.0020447          9.6203          4.7748          4.7748
v  Pressure               -46.574          20.134         0.71244         0.71244
v  nu_tilda            7.328e-007       0.0042271      0.00060539      0.00060539
v  TempC                       21          73.498          21.264          21.264
v  TurbVisc            2.604e-013       0.0049816      0.00069932      0.00069932
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              210:        0.35250E+01

===============================================================


 INSTANT    0.211000000E+03   TIME STEP NUMBER             211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36822E-02 0.91224E+00
   Friction velocity        uk    :  0.36822E-02 0.91224E+00
   Dimensionless distance   yplus :  0.29644E-01 0.73442E+01
   Friction thermal sca.    tstar : -0.41553E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22118E-01 0.54796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46058E-02      34   0.87860E-03   0.53324E+01 0.13796E+03 
c  Velocity[X]                                      0.32847E+01 
c  Velocity[Y]                                      0.20477E+01 
c  Velocity[Z]                                      0.30440E-29 
c  Pressure     0.42832E-06     329   0.99283E-08   0.26905E+00 0.70089E+03 
c  nu_tilda     0.32235E-05      35   0.17585E-04   0.63006E-06 0.39126E+03 
c  TempC        0.20647E+02      30   0.98485E-03   0.11633E+02 0.35290E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5641          9.5839          4.5729          4.5729
v  Velocity[Y]            -3.3519          7.5969        0.001403        0.001403
v  Velocity[Z]       -1.7251e-014     1.3278e-014     -4.709e-018     -4.709e-018
v  ǁVelocityǁ         0.0032845          9.6102          4.7755          4.7755
v  Pressure               -46.338           20.17         0.70771         0.70771
v  nu_tilda           7.2957e-007       0.0042275      0.00060599      0.00060599
v  TempC                       21          73.422          21.265          21.265
v  TurbVisc           2.5369e-013        0.004982      0.00070008      0.00070008
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              211:        0.32140E+01

===============================================================


 INSTANT    0.212000000E+03   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15694E-01 0.91106E+00
   Friction velocity        uk    :  0.15694E-01 0.91106E+00
   Dimensionless distance   yplus :  0.12635E+00 0.73346E+01
   Friction thermal sca.    tstar : -0.58109E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94269E-01 0.54724E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46100E-02      34   0.80593E-03   0.53642E+01 0.13855E+03 
c  Velocity[X]                                      0.33067E+01 
c  Velocity[Y]                                      0.20576E+01 
c  Velocity[Z]                                      0.34358E-29 
c  Pressure     0.35328E-06     456   0.95179E-08   0.22807E+00 0.77388E+03 
c  nu_tilda     0.32287E-05      34   0.13384E-04   0.62663E-06 0.38959E+03 
c  TempC        0.20665E+02      30   0.73875E-03   0.16777E+02 0.40364E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5853          9.5724          4.5729          4.5729
v  Velocity[Y]            -3.3439          7.5607       0.0014166       0.0014166
v  Velocity[Z]       -2.0665e-014     1.3863e-014    -4.9083e-018    -4.9083e-018
v  ǁVelocityǁ         0.0039835          9.5999          4.7762          4.7762
v  Pressure               -46.465          20.018         0.68439         0.68439
v  nu_tilda           7.2762e-007       0.0042278      0.00060668      0.00060668
v  TempC                       21          73.468          21.265          21.265
v  TurbVisc           2.4924e-013       0.0049825      0.00070083      0.00070083
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              212:        0.40570E+01

===============================================================


 INSTANT    0.213000000E+03   TIME STEP NUMBER             213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21873E-01 0.90862E+00
   Friction velocity        uk    :  0.21873E-01 0.90862E+00
   Dimensionless distance   yplus :  0.17610E+00 0.73150E+01
   Friction thermal sca.    tstar : -0.51184E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13139E+00 0.54578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46142E-02      34   0.86799E-03   0.53661E+01 0.13904E+03 
c  Velocity[X]                                      0.32780E+01 
c  Velocity[Y]                                      0.20881E+01 
c  Velocity[Z]                                      0.35867E-29 
c  Pressure     0.29382E-06     346   0.97714E-08   0.18262E+00 0.89184E+03 
c  nu_tilda     0.32338E-05      34   0.17498E-04   0.62316E-06 0.38793E+03 
c  TempC        0.20684E+02      29   0.92259E-03   0.11784E+02 0.34386E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6073           9.561          4.5729          4.5729
v  Velocity[Y]            -3.3356          7.5618       0.0014306       0.0014306
v  Velocity[Z]       -2.2373e-014     1.4159e-014     -5.092e-018     -5.092e-018
v  ǁVelocityǁ         0.0047391          9.5892          4.7769          4.7769
v  Pressure               -46.665          20.076         0.68507         0.68507
v  nu_tilda           7.2715e-007       0.0042282      0.00060728      0.00060728
v  TempC                       21          73.477          21.266          21.266
v  TurbVisc            2.466e-013       0.0049829       0.0007016       0.0007016
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              213:        0.33190E+01

===============================================================


 INSTANT    0.214000000E+03   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12662E-01 0.90867E+00
   Friction velocity        uk    :  0.12662E-01 0.90867E+00
   Dimensionless distance   yplus :  0.10193E+00 0.73154E+01
   Friction thermal sca.    tstar : -0.50069E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76055E-01 0.54581E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46184E-02      34   0.86759E-03   0.54232E+01 0.13980E+03 
c  Velocity[X]                                      0.33147E+01 
c  Velocity[Y]                                      0.21085E+01 
c  Velocity[Z]                                      0.38313E-29 
c  Pressure     0.30041E-06     453   0.94757E-08   0.19070E+00 0.87436E+03 
c  nu_tilda     0.32389E-05      34   0.13290E-04   0.61983E-06 0.38629E+03 
c  TempC        0.20702E+02      30   0.97506E-03   0.12715E+02 0.37467E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6289          9.5498          4.5729          4.5729
v  Velocity[Y]            -3.3275          7.5203       0.0014465       0.0014465
v  Velocity[Z]       -2.1501e-014     1.4042e-014    -5.2732e-018    -5.2732e-018
v  ǁVelocityǁ         0.0055198          9.5783          4.7776          4.7776
v  Pressure               -46.454          20.081         0.71213         0.71213
v  nu_tilda           7.2805e-007       0.0042286      0.00060796      0.00060796
v  TempC                       21          73.411          21.266          21.266
v  TurbVisc           2.4596e-013       0.0049834      0.00070235      0.00070235
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              214:        0.35540E+01

===============================================================


 INSTANT    0.215000000E+03   TIME STEP NUMBER             215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21185E-01 0.90723E+00
   Friction velocity        uk    :  0.21185E-01 0.90723E+00
   Dimensionless distance   yplus :  0.17055E+00 0.73038E+01
   Friction thermal sca.    tstar : -0.62487E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12725E+00 0.54495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46226E-02      34   0.87761E-03   0.54939E+01 0.14075E+03 
c  Velocity[X]                                      0.33691E+01 
c  Velocity[Y]                                      0.21248E+01 
c  Velocity[Z]                                      0.26625E-29 
c  Pressure     0.33040E-06     442   0.98966E-08   0.21100E+00 0.46397E+03 
c  nu_tilda     0.32440E-05      34   0.17416E-04   0.61649E-06 0.38466E+03 
c  TempC        0.20720E+02      30   0.12256E-02   0.15738E+02 0.40317E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6503           9.541          4.5729          4.5729
v  Velocity[Y]            -3.3195          7.5413       0.0014619       0.0014619
v  Velocity[Z]       -2.0742e-014     1.4099e-014    -5.4292e-018    -5.4292e-018
v  ǁVelocityǁ         0.0012212          9.5676          4.7782          4.7782
v  Pressure               -46.488          20.066          0.6891          0.6891
v  nu_tilda            7.294e-007       0.0042289      0.00060856      0.00060856
v  TempC                       21          73.396          21.267          21.267
v  TurbVisc           2.4717e-013       0.0049838      0.00070311      0.00070311
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              215:        0.39460E+01

===============================================================


 INSTANT    0.216000000E+03   TIME STEP NUMBER             216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33369E-02 0.90806E+00
   Friction velocity        uk    :  0.33369E-02 0.90806E+00
   Dimensionless distance   yplus :  0.26864E-01 0.73105E+01
   Friction thermal sca.    tstar : -0.66617E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20044E-01 0.54544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46267E-02      34   0.88788E-03   0.55661E+01 0.14188E+03 
c  Velocity[X]                                      0.34112E+01 
c  Velocity[Y]                                      0.21549E+01 
c  Velocity[Z]                                      0.26140E-29 
c  Pressure     0.22923E-06     376   0.94858E-08   0.14717E+00 0.45311E+03 
c  nu_tilda     0.32491E-05      34   0.13203E-04   0.61326E-06 0.38305E+03 
c  TempC        0.20739E+02      30   0.96922E-03   0.22416E+02 0.48193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.671          9.5322          4.5729          4.5729
v  Velocity[Y]            -3.3116          7.5011       0.0014796       0.0014796
v  Velocity[Z]       -1.7946e-014     1.3804e-014    -5.5865e-018    -5.5865e-018
v  ǁVelocityǁ         0.0024832          9.5566          4.7789          4.7789
v  Pressure                 -46.4           19.97         0.68361         0.68361
v  nu_tilda           7.3138e-007       0.0042293      0.00060925      0.00060925
v  TempC                       21          73.391          21.268          21.268
v  TurbVisc           2.4901e-013       0.0049842      0.00070387      0.00070387
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              216:        0.38850E+01

===============================================================


 INSTANT    0.217000000E+03   TIME STEP NUMBER             217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11423E-01 0.90707E+00
   Friction velocity        uk    :  0.11423E-01 0.90707E+00
   Dimensionless distance   yplus :  0.91961E-01 0.73026E+01
   Friction thermal sca.    tstar : -0.65100E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68613E-01 0.54485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46309E-02      34   0.76695E-03   0.56167E+01 0.14270E+03 
c  Velocity[X]                                      0.34436E+01 
c  Velocity[Y]                                      0.21731E+01 
c  Velocity[Z]                                      0.28743E-29 
c  Pressure     0.23039E-06     438   0.93783E-08   0.15095E+00 0.55088E+03 
c  nu_tilda     0.32542E-05      34   0.17346E-04   0.61002E-06 0.38145E+03 
c  TempC        0.20757E+02      30   0.83523E-03   0.19308E+02 0.44532E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6934          9.5223          4.5729          4.5729
v  Velocity[Y]            -3.3037          7.5228       0.0014968       0.0014968
v  Velocity[Z]       -1.7298e-014     1.4219e-014     -5.735e-018     -5.735e-018
v  ǁVelocityǁ         0.0019404          9.5447          4.7796          4.7796
v  Pressure               -46.386          19.987         0.66754         0.66754
v  nu_tilda           7.3314e-007       0.0042297      0.00060985      0.00060985
v  TempC                       21          73.321          21.268          21.268
v  TurbVisc           2.5173e-013       0.0049846      0.00070464      0.00070464
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              217:        0.43440E+01

===============================================================


 INSTANT    0.218000000E+03   TIME STEP NUMBER             218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10545E-01 0.90785E+00
   Friction velocity        uk    :  0.10545E-01 0.90785E+00
   Dimensionless distance   yplus :  0.84896E-01 0.73088E+01
   Friction thermal sca.    tstar : -0.75275E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63342E-01 0.54532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46351E-02      34   0.82150E-03   0.56106E+01 0.14304E+03 
c  Velocity[X]                                      0.34184E+01 
c  Velocity[Y]                                      0.21923E+01 
c  Velocity[Z]                                      0.20337E-29 
c  Pressure     0.23775E-06     458   0.99731E-08   0.15922E+00 0.88747E+03 
c  nu_tilda     0.32592E-05      34   0.13099E-04   0.60690E-06 0.37988E+03 
c  TempC        0.20775E+02      29   0.96588E-03   0.14094E+02 0.38885E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.715          9.5123          4.5729          4.5729
v  Velocity[Y]             -3.296          7.5204       0.0015135       0.0015135
v  Velocity[Z]       -1.6542e-014     1.4002e-014    -5.8817e-018    -5.8817e-018
v  ǁVelocityǁ         0.0010823          9.5358          4.7803          4.7803
v  Pressure               -46.118          20.021         0.69384         0.69384
v  nu_tilda           7.3441e-007         0.00423      0.00061055      0.00061055
v  TempC                       21          73.352          21.269          21.269
v  TurbVisc           2.5417e-013       0.0049851       0.0007054       0.0007054
v  total_pressure     1.0128e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              218:        0.38850E+01

===============================================================


 INSTANT    0.219000000E+03   TIME STEP NUMBER             219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79051E-02 0.90671E+00
   Friction velocity        uk    :  0.79051E-02 0.90671E+00
   Dimensionless distance   yplus :  0.63641E-01 0.72997E+01
   Friction thermal sca.    tstar : -0.11929E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47484E-01 0.54464E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46393E-02      34   0.80263E-03   0.56975E+01 0.14401E+03 
c  Velocity[X]                                      0.34677E+01 
c  Velocity[Y]                                      0.22298E+01 
c  Velocity[Z]                                      0.20234E-29 
c  Pressure     0.28673E-06     505   0.94117E-08   0.19633E+00 0.11537E+04 
c  nu_tilda     0.32642E-05      34   0.17263E-04   0.60378E-06 0.37831E+03 
c  TempC        0.20794E+02      29   0.84161E-03   0.16557E+02 0.42216E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7357          9.5019          4.5729          4.5729
v  Velocity[Y]            -3.2884          7.4791       0.0015308       0.0015308
v  Velocity[Z]       -1.6171e-014     1.4191e-014    -6.0256e-018    -6.0256e-018
v  ǁVelocityǁ         0.0032434           9.526           4.781           4.781
v  Pressure               -45.919          19.827         0.63844         0.63844
v  nu_tilda           7.3481e-007       0.0042304      0.00061115      0.00061115
v  TempC                       21          73.391          21.269          21.269
v  TurbVisc           2.5593e-013       0.0049855      0.00070617      0.00070617
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              219:        0.38210E+01

===============================================================


 INSTANT    0.220000000E+03   TIME STEP NUMBER             220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18511E-01 0.90465E+00
   Friction velocity        uk    :  0.18511E-01 0.90465E+00
   Dimensionless distance   yplus :  0.14903E+00 0.72830E+01
   Friction thermal sca.    tstar : -0.10885E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11119E+00 0.54340E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46435E-02      34   0.84278E-03   0.57197E+01 0.14466E+03 
c  Velocity[X]                                      0.34804E+01 
c  Velocity[Y]                                      0.22393E+01 
c  Velocity[Z]                                      0.19247E-29 
c  Pressure     0.25237E-06     473   0.99442E-08   0.17351E+00 0.12634E+04 
c  nu_tilda     0.32692E-05      34   0.13018E-04   0.60075E-06 0.37677E+03 
c  TempC        0.20812E+02      29   0.84417E-03   0.17010E+02 0.42610E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7566          9.4909          4.5729          4.5729
v  Velocity[Y]            -3.2812          7.4895        0.001548        0.001548
v  Velocity[Z]       -1.5753e-014     1.4124e-014    -6.1724e-018    -6.1724e-018
v  ǁVelocityǁ         0.0041039          9.5161          4.7817          4.7817
v  Pressure               -45.751          19.933         0.67717         0.67717
v  nu_tilda           7.3443e-007       0.0042307      0.00061184      0.00061184
v  TempC                       21          73.325           21.27           21.27
v  TurbVisc           2.5649e-013       0.0049859      0.00070693      0.00070693
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              220:        0.36840E+01

===============================================================


 INSTANT    0.221000000E+03   TIME STEP NUMBER             221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21785E-01 0.90523E+00
   Friction velocity        uk    :  0.21785E-01 0.90523E+00
   Dimensionless distance   yplus :  0.17539E+00 0.72877E+01
   Friction thermal sca.    tstar : -0.16943E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13086E+00 0.54374E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46477E-02      34   0.84283E-03   0.57981E+01 0.14572E+03 
c  Velocity[X]                                      0.35064E+01 
c  Velocity[Y]                                      0.22917E+01 
c  Velocity[Z]                                      0.22915E-29 
c  Pressure     0.23803E-06     489   0.99302E-08   0.16915E+00 0.89136E+03 
c  nu_tilda     0.32742E-05      34   0.17181E-04   0.59772E-06 0.37523E+03 
c  TempC        0.20830E+02      29   0.79272E-03   0.16465E+02 0.41227E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7781          9.4796          4.5729          4.5729
v  Velocity[Y]            -3.2738          7.4604        0.001565        0.001565
v  Velocity[Z]       -1.5447e-014     1.4243e-014    -6.3056e-018    -6.3056e-018
v  ǁVelocityǁ         0.0059834          9.5056          4.7824          4.7824
v  Pressure               -45.718          19.785         0.63179         0.63179
v  nu_tilda           7.3358e-007        0.004231      0.00061244      0.00061244
v  TempC                       21           73.31          21.271          21.271
v  TurbVisc           2.5595e-013       0.0049863       0.0007077       0.0007077
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              221:        0.37860E+01

===============================================================


 INSTANT    0.222000000E+03   TIME STEP NUMBER             222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10455E-01 0.90356E+00
   Friction velocity        uk    :  0.10455E-01 0.90356E+00
   Dimensionless distance   yplus :  0.84172E-01 0.72743E+01
   Friction thermal sca.    tstar : -0.30134E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62802E-01 0.54274E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46518E-02      34   0.92394E-03   0.58643E+01 0.14655E+03 
c  Velocity[X]                                      0.35606E+01 
c  Velocity[Y]                                      0.23037E+01 
c  Velocity[Z]                                      0.18539E-29 
c  Pressure     0.21356E-06     457   0.99297E-08   0.15297E+00 0.84652E+03 
c  nu_tilda     0.32792E-05      34   0.12923E-04   0.59477E-06 0.37372E+03 
c  TempC        0.20849E+02      29   0.65470E-03   0.16551E+02 0.41779E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7992          9.4683          4.5729          4.5729
v  Velocity[Y]            -3.2667          7.4754       0.0015829       0.0015829
v  Velocity[Z]       -1.4781e-014     1.4334e-014    -6.4385e-018    -6.4385e-018
v  ǁVelocityǁ         0.0063148           9.495           4.783           4.783
v  Pressure               -45.671           19.84         0.65372         0.65372
v  nu_tilda           7.3212e-007       0.0042314      0.00061314      0.00061314
v  TempC                       21          73.286          21.271          21.271
v  TurbVisc           2.5478e-013       0.0049867      0.00070846      0.00070846
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              222:        0.36520E+01

===============================================================


 INSTANT    0.223000000E+03   TIME STEP NUMBER             223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15290E-01 0.90399E+00
   Friction velocity        uk    :  0.15290E-01 0.90399E+00
   Dimensionless distance   yplus :  0.12309E+00 0.72778E+01
   Friction thermal sca.    tstar : -0.13110E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91840E-01 0.54300E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46560E-02      34   0.81297E-03   0.60130E+01 0.14797E+03 
c  Velocity[X]                                      0.36463E+01 
c  Velocity[Y]                                      0.23667E+01 
c  Velocity[Z]                                      0.18643E-29 
c  Pressure     0.26351E-06     490   0.98772E-08   0.19070E+00 0.10724E+04 
c  nu_tilda     0.32841E-05      34   0.17093E-04   0.59184E-06 0.37222E+03 
c  TempC        0.20867E+02      29   0.82485E-03   0.10366E+02 0.33391E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8212          9.4558          4.5729          4.5729
v  Velocity[Y]            -3.2597           7.438       0.0016008       0.0016008
v  Velocity[Z]       -1.4545e-014     1.4584e-014    -6.5524e-018    -6.5524e-018
v  ǁVelocityǁ         0.0041638          9.4837          4.7837          4.7837
v  Pressure                 -45.6          19.648         0.60156         0.60156
v  nu_tilda            7.301e-007       0.0042317      0.00061374      0.00061374
v  TempC                       21          73.273          21.272          21.272
v  TurbVisc           2.5276e-013       0.0049871      0.00070923      0.00070923
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              223:        0.39060E+01

===============================================================


 INSTANT    0.224000000E+03   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21271E-01 0.90259E+00
   Friction velocity        uk    :  0.21271E-01 0.90259E+00
   Dimensionless distance   yplus :  0.17125E+00 0.72665E+01
   Friction thermal sca.    tstar : -0.10444E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12777E+00 0.54216E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46602E-02      34   0.65581E-03   0.59726E+01 0.14820E+03 
c  Velocity[X]                                      0.36121E+01 
c  Velocity[Y]                                      0.23605E+01 
c  Velocity[Z]                                      0.35486E-29 
c  Pressure     0.21630E-06     489   0.97449E-08   0.16072E+00 0.12005E+04 
c  nu_tilda     0.32890E-05      34   0.12836E-04   0.58900E-06 0.37073E+03 
c  TempC        0.20885E+02      29   0.87682E-03   0.14420E+02 0.40162E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8424          9.4434          4.5729          4.5729
v  Velocity[Y]            -3.2529           7.452       0.0016186       0.0016186
v  Velocity[Z]       -1.4127e-014     1.7002e-014     -6.659e-018     -6.659e-018
v  ǁVelocityǁ         0.0032711          9.4722          4.7844          4.7844
v  Pressure               -45.522          19.767          0.6369          0.6369
v  nu_tilda           7.2825e-007       0.0042321      0.00061444      0.00061444
v  TempC                       21          73.238          21.272          21.272
v  TurbVisc           2.4998e-013       0.0049875      0.00070999      0.00070999
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              224:        0.41100E+01

===============================================================


 INSTANT    0.225000000E+03   TIME STEP NUMBER             225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18912E-01 0.90296E+00
   Friction velocity        uk    :  0.18912E-01 0.90296E+00
   Dimensionless distance   yplus :  0.15225E+00 0.72694E+01
   Friction thermal sca.    tstar : -0.80162E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11360E+00 0.54238E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46644E-02      34   0.85558E-03   0.59963E+01 0.14877E+03 
c  Velocity[X]                                      0.36033E+01 
c  Velocity[Y]                                      0.23930E+01 
c  Velocity[Z]                                      0.25652E-29 
c  Pressure     0.23261E-06     490   0.94340E-08   0.17568E+00 0.84892E+03 
c  nu_tilda     0.32940E-05      34   0.17009E-04   0.58619E-06 0.36926E+03 
c  TempC        0.20903E+02      29   0.88692E-03   0.19182E+02 0.44832E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8623          9.4333          4.5729          4.5729
v  Velocity[Y]            -3.2461          7.4556       0.0016368       0.0016368
v  Velocity[Z]        -1.358e-014     1.5802e-014    -6.7558e-018    -6.7558e-018
v  ǁVelocityǁ         0.0019767          9.4606          4.7851          4.7851
v  Pressure               -45.418          19.629         0.59174         0.59174
v  nu_tilda           7.2745e-007       0.0042324      0.00061504      0.00061504
v  TempC                       21          73.186          21.273          21.273
v  TurbVisc           2.4744e-013       0.0049879      0.00071076      0.00071076
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              225:        0.40230E+01

===============================================================


 INSTANT    0.226000000E+03   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11187E-01 0.90185E+00
   Friction velocity        uk    :  0.11187E-01 0.90185E+00
   Dimensionless distance   yplus :  0.90065E-01 0.72605E+01
   Friction thermal sca.    tstar : -0.74557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67199E-01 0.54172E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46685E-02      35   0.82389E-03   0.63324E+01 0.15165E+03 
c  Velocity[X]                                      0.37198E+01 
c  Velocity[Y]                                      0.26126E+01 
c  Velocity[Z]                                      0.27637E-29 
c  Pressure     0.27295E-06     377   0.96507E-08   0.21205E+00 0.43974E+03 
c  nu_tilda     0.32988E-05      34   0.12776E-04   0.58347E-06 0.36781E+03 
c  TempC        0.20921E+02      29   0.82971E-03   0.15936E+02 0.42920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8836           9.424          4.5729          4.5729
v  Velocity[Y]            -3.2396          7.4044       0.0016552       0.0016552
v  Velocity[Z]        -1.312e-014     1.7786e-014    -6.8433e-018    -6.8433e-018
v  ǁVelocityǁ         0.0017332          9.4487          4.7858          4.7858
v  Pressure                -45.09          19.548         0.59658         0.59658
v  nu_tilda           7.2718e-007       0.0042327      0.00061574      0.00061574
v  TempC                       21          73.177          21.274          21.274
v  TurbVisc           2.4637e-013       0.0049883      0.00071153      0.00071153
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              226:        0.35550E+01

===============================================================


 INSTANT    0.227000000E+03   TIME STEP NUMBER             227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76376E-02 0.89972E+00
   Friction velocity        uk    :  0.76376E-02 0.89972E+00
   Dimensionless distance   yplus :  0.61488E-01 0.72433E+01
   Friction thermal sca.    tstar : -0.66378E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45877E-01 0.54043E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46727E-02      35   0.80248E-03   0.61956E+01 0.15118E+03 
c  Velocity[X]                                      0.36949E+01 
c  Velocity[Y]                                      0.25008E+01 
c  Velocity[Z]                                      0.30186E-29 
c  Pressure     0.25332E-06     458   0.97818E-08   0.19601E+00 0.51248E+03 
c  nu_tilda     0.33037E-05      34   0.16927E-04   0.58077E-06 0.36637E+03 
c  TempC        0.20939E+02      29   0.95079E-03   0.16167E+02 0.42204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9039           9.414          4.5729          4.5729
v  Velocity[Y]            -3.2331          7.4174       0.0016743       0.0016743
v  Velocity[Z]       -1.2525e-014      1.598e-014    -6.9357e-018    -6.9357e-018
v  ǁVelocityǁ         0.0029395           9.436          4.7864          4.7864
v  Pressure               -44.834           19.52         0.57032         0.57032
v  nu_tilda           7.2658e-007        0.004233      0.00061634      0.00061634
v  TempC                       21          73.202          21.274          21.274
v  TurbVisc             2.46e-013       0.0049887       0.0007123       0.0007123
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              227:        0.37430E+01

===============================================================


 INSTANT    0.228000000E+03   TIME STEP NUMBER             228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38159E-02 0.90032E+00
   Friction velocity        uk    :  0.38159E-02 0.90032E+00
   Dimensionless distance   yplus :  0.30721E-01 0.72482E+01
   Friction thermal sca.    tstar : -0.77800E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22921E-01 0.54080E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46769E-02      35   0.86715E-03   0.62288E+01 0.15178E+03 
c  Velocity[X]                                      0.37258E+01 
c  Velocity[Y]                                      0.25030E+01 
c  Velocity[Z]                                      0.27542E-29 
c  Pressure     0.25474E-06     362   0.97429E-08   0.20170E+00 0.45400E+03 
c  nu_tilda     0.33086E-05      34   0.12704E-04   0.57812E-06 0.36494E+03 
c  TempC        0.20957E+02      29   0.90230E-03   0.17175E+02 0.44040E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9242          9.4031          4.5729          4.5729
v  Velocity[Y]            -3.2268          7.3897       0.0016931       0.0016931
v  Velocity[Z]       -1.1948e-014     1.7656e-014    -7.0261e-018    -7.0261e-018
v  ǁVelocityǁ         0.0045073          9.4249          4.7871          4.7871
v  Pressure               -44.486          19.443         0.57488         0.57488
v  nu_tilda           7.2665e-007       0.0042334      0.00061704      0.00061704
v  TempC                       21          73.162          21.275          21.275
v  TurbVisc           2.4519e-013       0.0049891      0.00071307      0.00071307
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              228:        0.33440E+01

===============================================================


 INSTANT    0.229000000E+03   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11563E-01 0.89885E+00
   Friction velocity        uk    :  0.11563E-01 0.89885E+00
   Dimensionless distance   yplus :  0.93093E-01 0.72363E+01
   Friction thermal sca.    tstar : -0.10646E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69458E-01 0.53991E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46810E-02      35   0.82088E-03   0.63017E+01 0.15278E+03 
c  Velocity[X]                                      0.37727E+01 
c  Velocity[Y]                                      0.25290E+01 
c  Velocity[Z]                                      0.26000E-29 
c  Pressure     0.26806E-06     457   0.91904E-08   0.21019E+00 0.54072E+03 
c  nu_tilda     0.33134E-05      34   0.16858E-04   0.57545E-06 0.36353E+03 
c  TempC        0.20975E+02      29   0.80358E-03   0.18713E+02 0.45057E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9449          9.3919          4.5729          4.5729
v  Velocity[Y]            -3.2207          7.4022       0.0017128       0.0017128
v  Velocity[Z]       -1.1454e-014     1.6062e-014    -7.1273e-018    -7.1273e-018
v  ǁVelocityǁ         0.0048796          9.4145          4.7878          4.7878
v  Pressure               -44.492          19.389         0.54403         0.54403
v  nu_tilda           7.2663e-007       0.0042337      0.00061765      0.00061765
v  TempC                       21          73.155          21.275          21.275
v  TurbVisc           2.4529e-013       0.0049894      0.00071384      0.00071384
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              229:        0.38960E+01

===============================================================


 INSTANT    0.230000000E+03   TIME STEP NUMBER             230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14875E-01 0.89930E+00
   Friction velocity        uk    :  0.14875E-01 0.89930E+00
   Dimensionless distance   yplus :  0.11975E+00 0.72400E+01
   Friction thermal sca.    tstar : -0.10674E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89348E-01 0.54018E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46852E-02      35   0.79030E-03   0.63977E+01 0.15355E+03 
c  Velocity[X]                                      0.38313E+01 
c  Velocity[Y]                                      0.25664E+01 
c  Velocity[Z]                                      0.44353E-29 
c  Pressure     0.36701E-06     490   0.97023E-08   0.30654E+00 0.11434E+04 
c  nu_tilda     0.33182E-05      34   0.12639E-04   0.57289E-06 0.36213E+03 
c  TempC        0.20994E+02      29   0.10081E-02   0.14474E+02 0.41058E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9647          9.3804          4.5729          4.5729
v  Velocity[Y]             -3.215          7.3704       0.0017306       0.0017306
v  Velocity[Z]         -1.05e-014     1.7596e-014    -7.2395e-018    -7.2395e-018
v  ǁVelocityǁ         0.0045016          9.4038          4.7884          4.7884
v  Pressure               -43.813          19.422         0.58201         0.58201
v  nu_tilda           7.2678e-007        0.004234      0.00061834      0.00061834
v  TempC                       21          73.128          21.276          21.276
v  TurbVisc           2.4526e-013       0.0049898      0.00071461      0.00071461
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              230:        0.40240E+01

===============================================================


 INSTANT    0.231000000E+03   TIME STEP NUMBER             231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18184E-01 0.89739E+00
   Friction velocity        uk    :  0.18184E-01 0.89739E+00
   Dimensionless distance   yplus :  0.14639E+00 0.72246E+01
   Friction thermal sca.    tstar : -0.57272E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10922E+00 0.53904E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46894E-02      35   0.79066E-03   0.63985E+01 0.15423E+03 
c  Velocity[X]                                      0.38163E+01 
c  Velocity[Y]                                      0.25822E+01 
c  Velocity[Z]                                      0.43477E-29 
c  Pressure     0.29170E-06     489   0.97640E-08   0.24516E+00 0.65286E+03 
c  nu_tilda     0.33230E-05      34   0.16773E-04   0.57033E-06 0.36075E+03 
c  TempC        0.21012E+02      29   0.10227E-02   0.21984E+02 0.47550E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9842          9.3686          4.5729          4.5729
v  Velocity[Y]            -3.2097          7.3877       0.0017505       0.0017505
v  Velocity[Z]       -9.1449e-015     1.7114e-014    -7.3594e-018    -7.3594e-018
v  ǁVelocityǁ         0.0040527          9.3926          4.7891          4.7891
v  Pressure               -43.587          19.358         0.54276         0.54276
v  nu_tilda           7.2684e-007       0.0042343      0.00061895      0.00061895
v  TempC                       21          73.095          21.276          21.276
v  TurbVisc           2.4546e-013       0.0049902      0.00071539      0.00071539
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              231:        0.35650E+01

===============================================================


 INSTANT    0.232000000E+03   TIME STEP NUMBER             232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88122E-02 0.89736E+00
   Friction velocity        uk    :  0.88122E-02 0.89736E+00
   Dimensionless distance   yplus :  0.70945E-01 0.72244E+01
   Friction thermal sca.    tstar : -0.16033E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52933E-01 0.53902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46935E-02      35   0.84074E-03   0.65061E+01 0.15547E+03 
c  Velocity[X]                                      0.38731E+01 
c  Velocity[Y]                                      0.26330E+01 
c  Velocity[Z]                                      0.24081E-29 
c  Pressure     0.31223E-06     409   0.97147E-08   0.26054E+00 0.44159E+03 
c  nu_tilda     0.33278E-05      34   0.12587E-04   0.56778E-06 0.35937E+03 
c  TempC        0.21030E+02      29   0.87746E-03   0.20170E+02 0.45451E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.004           9.356          4.5729          4.5729
v  Velocity[Y]            -3.2044          7.3705       0.0017705       0.0017705
v  Velocity[Z]       -8.1254e-015     1.7398e-014    -7.5057e-018    -7.5057e-018
v  ǁVelocityǁ         0.0031627          9.3808          4.7898          4.7898
v  Pressure               -42.986          19.304         0.55025         0.55025
v  nu_tilda           7.2688e-007       0.0042346      0.00061965      0.00061965
v  TempC                       21          73.087          21.277          21.277
v  TurbVisc           2.4554e-013       0.0049906      0.00071616      0.00071616
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              232:        0.31630E+01

===============================================================


 INSTANT    0.233000000E+03   TIME STEP NUMBER             233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16225E-01 0.89604E+00
   Friction velocity        uk    :  0.16225E-01 0.89604E+00
   Dimensionless distance   yplus :  0.13062E+00 0.72137E+01
   Friction thermal sca.    tstar : -0.15953E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97457E-01 0.53823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46977E-02      35   0.79648E-03   0.65170E+01 0.15612E+03 
c  Velocity[X]                                      0.38640E+01 
c  Velocity[Y]                                      0.26530E+01 
c  Velocity[Z]                                      0.39588E-29 
c  Pressure     0.33846E-06     506   0.95537E-08   0.28892E+00 0.86988E+03 
c  nu_tilda     0.33326E-05      34   0.16712E-04   0.56528E-06 0.35801E+03 
c  TempC        0.21048E+02      30   0.87076E-03   0.17885E+02 0.44860E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0246          9.3432          4.5729          4.5729
v  Velocity[Y]            -3.1993          7.3375       0.0017914       0.0017914
v  Velocity[Z]        -8.412e-015     1.7653e-014    -7.6574e-018    -7.6574e-018
v  ǁVelocityǁ          0.001839          9.3686          4.7905          4.7905
v  Pressure               -42.635          19.155         0.50456         0.50456
v  nu_tilda           7.2659e-007       0.0042349      0.00062026      0.00062026
v  TempC                       21          73.131          21.278          21.278
v  TurbVisc            2.456e-013       0.0049909      0.00071693      0.00071693
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              233:        0.28890E+01

===============================================================


 INSTANT    0.234000000E+03   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56434E-02 0.89415E+00
   Friction velocity        uk    :  0.56434E-02 0.89415E+00
   Dimensionless distance   yplus :  0.45433E-01 0.71985E+01
   Friction thermal sca.    tstar : -0.58074E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33898E-01 0.53709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47019E-02      35   0.87688E-03   0.65487E+01 0.15670E+03 
c  Velocity[X]                                      0.38563E+01 
c  Velocity[Y]                                      0.26924E+01 
c  Velocity[Z]                                      0.33938E-29 
c  Pressure     0.38015E-06     506   0.93824E-08   0.31722E+00 0.14439E+04 
c  nu_tilda     0.33374E-05      34   0.12549E-04   0.56287E-06 0.35667E+03 
c  TempC        0.21065E+02      30   0.80558E-03   0.19161E+02 0.46403E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0454          9.3339          4.5729          4.5729
v  Velocity[Y]            -3.1945          7.3505        0.001812        0.001812
v  Velocity[Z]       -7.0349e-015     1.7716e-014    -7.8215e-018    -7.8215e-018
v  ǁVelocityǁ         0.0016111          9.3563          4.7911          4.7911
v  Pressure               -42.243          19.263         0.55161         0.55161
v  nu_tilda           7.2625e-007       0.0042352      0.00062096      0.00062096
v  TempC                       21          73.132          21.278          21.278
v  TurbVisc            2.452e-013       0.0049913       0.0007177       0.0007177
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              234:        0.29930E+01

===============================================================


 INSTANT    0.235000000E+03   TIME STEP NUMBER             235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78024E-02 0.89466E+00
   Friction velocity        uk    :  0.78024E-02 0.89466E+00
   Dimensionless distance   yplus :  0.62815E-01 0.72026E+01
   Friction thermal sca.    tstar : -0.61146E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46867E-01 0.53739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47060E-02      35   0.86228E-03   0.66759E+01 0.15801E+03 
c  Velocity[X]                                      0.39476E+01 
c  Velocity[Y]                                      0.27282E+01 
c  Velocity[Z]                                      0.26387E-29 
c  Pressure     0.31868E-06     552   0.93892E-08   0.26240E+00 0.15229E+04 
c  nu_tilda     0.33421E-05      34   0.16639E-04   0.56050E-06 0.35534E+03 
c  TempC        0.21083E+02      30   0.90074E-03   0.18162E+02 0.43608E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0637          9.3242          4.5729          4.5729
v  Velocity[Y]            -3.1899          7.3102       0.0018335       0.0018335
v  Velocity[Z]       -6.9287e-015     1.7581e-014    -7.9662e-018    -7.9662e-018
v  ǁVelocityǁ         0.0025804          9.3436          4.7918          4.7918
v  Pressure               -42.305          19.016         0.48022         0.48022
v  nu_tilda           7.2552e-007       0.0042355      0.00062157      0.00062157
v  TempC                       21          73.116          21.279          21.279
v  TurbVisc           2.4475e-013       0.0049916      0.00071848      0.00071848
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              235:        0.31120E+01

===============================================================


 INSTANT    0.236000000E+03   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10433E-01 0.89322E+00
   Friction velocity        uk    :  0.10433E-01 0.89322E+00
   Dimensionless distance   yplus :  0.83991E-01 0.71910E+01
   Friction thermal sca.    tstar : -0.65055E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62667E-01 0.53653E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47102E-02      35   0.82894E-03   0.66774E+01 0.15853E+03 
c  Velocity[X]                                      0.39522E+01 
c  Velocity[Y]                                      0.27253E+01 
c  Velocity[Z]                                      0.35319E-29 
c  Pressure     0.29272E-06     522   0.98490E-08   0.24113E+00 0.15282E+04 
c  nu_tilda     0.33468E-05      34   0.12503E-04   0.55825E-06 0.35403E+03 
c  TempC        0.21101E+02      30   0.85120E-03   0.18671E+02 0.43255E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0839          9.3141          4.5729          4.5729
v  Velocity[Y]            -3.1855          7.3251        0.001855        0.001855
v  Velocity[Z]       -6.9287e-015     1.6058e-014    -8.1251e-018    -8.1251e-018
v  ǁVelocityǁ         0.0023038          9.3311          4.7925          4.7925
v  Pressure               -42.071          19.148         0.52916         0.52916
v  nu_tilda           7.2507e-007       0.0042358      0.00062226      0.00062226
v  TempC                       21          73.096          21.279          21.279
v  TurbVisc           2.4376e-013        0.004992      0.00071925      0.00071925
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              236:        0.30750E+01

===============================================================


 INSTANT    0.237000000E+03   TIME STEP NUMBER             237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12303E-01 0.89388E+00
   Friction velocity        uk    :  0.12303E-01 0.89388E+00
   Dimensionless distance   yplus :  0.99048E-01 0.71964E+01
   Friction thermal sca.    tstar : -0.68067E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73901E-01 0.53693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47144E-02      35   0.82633E-03   0.67135E+01 0.15918E+03 
c  Velocity[X]                                      0.39423E+01 
c  Velocity[Y]                                      0.27712E+01 
c  Velocity[Z]                                      0.34443E-29 
c  Pressure     0.24211E-06     489   0.92342E-08   0.19971E+00 0.61051E+03 
c  nu_tilda     0.33515E-05      34   0.16582E-04   0.55600E-06 0.35274E+03 
c  TempC        0.21119E+02      30   0.97716E-03   0.18670E+02 0.45625E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.103          9.3039          4.5729          4.5729
v  Velocity[Y]            -3.1818          7.3304        0.001877        0.001877
v  Velocity[Z]       -6.9287e-015     1.5502e-014    -8.2857e-018    -8.2857e-018
v  ǁVelocityǁ         0.0021904          9.3207          4.7932          4.7932
v  Pressure               -41.961          19.059         0.49573         0.49573
v  nu_tilda           7.2511e-007       0.0042361      0.00062287      0.00062287
v  TempC                       21          73.146           21.28           21.28
v  TurbVisc           2.4316e-013       0.0049923      0.00072003      0.00072003
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              237:        0.23800E+01

===============================================================


 INSTANT    0.238000000E+03   TIME STEP NUMBER             238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12148E-01 0.89276E+00
   Friction velocity        uk    :  0.12148E-01 0.89276E+00
   Dimensionless distance   yplus :  0.97802E-01 0.71873E+01
   Friction thermal sca.    tstar : -0.70489E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72972E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47186E-02      35   0.79960E-03   0.67906E+01 0.16018E+03 
c  Velocity[X]                                      0.39887E+01 
c  Velocity[Y]                                      0.28019E+01 
c  Velocity[Z]                                      0.24189E-29 
c  Pressure     0.22086E-06     409   0.95241E-08   0.18497E+00 0.50955E+03 
c  nu_tilda     0.33562E-05      34   0.12476E-04   0.55378E-06 0.35146E+03 
c  TempC        0.21137E+02      30   0.95528E-03   0.21673E+02 0.48406E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1232          9.2932          4.5729          4.5729
v  Velocity[Y]            -3.1786          7.2823       0.0018991       0.0018991
v  Velocity[Z]       -6.9287e-015      1.526e-014    -8.4277e-018    -8.4277e-018
v  ǁVelocityǁ         0.0018931            9.31          4.7939          4.7939
v  Pressure               -41.827          18.924         0.48841         0.48841
v  nu_tilda           7.2511e-007       0.0042364      0.00062357      0.00062357
v  TempC                       21           73.14           21.28           21.28
v  TurbVisc           2.4321e-013       0.0049927       0.0007208       0.0007208
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              238:        0.22090E+01

===============================================================


 INSTANT    0.239000000E+03   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11235E-01 0.89070E+00
   Friction velocity        uk    :  0.11235E-01 0.89070E+00
   Dimensionless distance   yplus :  0.90450E-01 0.71708E+01
   Friction thermal sca.    tstar : -0.11133E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67486E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47227E-02      35   0.83055E-03   0.68150E+01 0.16080E+03 
c  Velocity[X]                                      0.39868E+01 
c  Velocity[Y]                                      0.28282E+01 
c  Velocity[Z]                                      0.29181E-29 
c  Pressure     0.17886E-06     456   0.97673E-08   0.15013E+00 0.60777E+03 
c  nu_tilda     0.33609E-05      34   0.16515E-04   0.55155E-06 0.35018E+03 
c  TempC        0.21155E+02      30   0.78203E-03   0.23019E+02 0.49338E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1409          9.2821          4.5729          4.5729
v  Velocity[Y]            -3.1755          7.2954       0.0019214       0.0019214
v  Velocity[Z]       -6.9287e-015     1.4898e-014    -8.5585e-018    -8.5585e-018
v  ǁVelocityǁ         0.0015631           9.299          4.7946          4.7946
v  Pressure               -41.787          18.931         0.47249         0.47249
v  nu_tilda            7.256e-007       0.0042367      0.00062418      0.00062418
v  TempC                       21          73.093          21.281          21.281
v  TurbVisc           2.4321e-013        0.004993      0.00072158      0.00072158
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              239:        0.28820E+01

===============================================================


 INSTANT    0.240000000E+03   TIME STEP NUMBER             240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99583E-02 0.89111E+00
   Friction velocity        uk    :  0.99583E-02 0.89111E+00
   Dimensionless distance   yplus :  0.80171E-01 0.71740E+01
   Friction thermal sca.    tstar : -0.83459E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59817E-01 0.53526E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47269E-02      35   0.83833E-03   0.68715E+01 0.16150E+03 
c  Velocity[X]                                      0.40180E+01 
c  Velocity[Y]                                      0.28535E+01 
c  Velocity[Z]                                      0.24168E-29 
c  Pressure     0.23049E-06     405   0.99772E-08   0.19438E+00 0.47982E+03 
c  nu_tilda     0.33655E-05      34   0.12444E-04   0.54928E-06 0.34891E+03 
c  TempC        0.21173E+02      30   0.89914E-03   0.17174E+02 0.44242E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1605          9.2708          4.5729          4.5729
v  Velocity[Y]            -3.1732          7.2656       0.0019432       0.0019432
v  Velocity[Z]       -6.9287e-015     1.4782e-014    -8.7032e-018    -8.7032e-018
v  ǁVelocityǁ          0.001216          9.2875          4.7953          4.7953
v  Pressure               -41.516          18.864         0.48092         0.48092
v  nu_tilda           7.2675e-007        0.004237      0.00062488      0.00062488
v  TempC                       21          73.131          21.281          21.281
v  TurbVisc           2.4387e-013       0.0049934      0.00072235      0.00072235
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              240:        0.26430E+01

===============================================================


 INSTANT    0.241000000E+03   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86869E-02 0.88959E+00
   Friction velocity        uk    :  0.86869E-02 0.88959E+00
   Dimensionless distance   yplus :  0.69935E-01 0.71618E+01
   Friction thermal sca.    tstar : -0.94824E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52180E-01 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47311E-02      35   0.84366E-03   0.69074E+01 0.16226E+03 
c  Velocity[X]                                      0.40321E+01 
c  Velocity[Y]                                      0.28753E+01 
c  Velocity[Z]                                      0.18285E-29 
c  Pressure     0.23530E-06     470   0.92494E-08   0.20384E+00 0.58142E+03 
c  nu_tilda     0.33702E-05      34   0.16460E-04   0.54705E-06 0.34765E+03 
c  TempC        0.21191E+02      30   0.10204E-02   0.20846E+02 0.47948E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1792          9.2621          4.5729          4.5729
v  Velocity[Y]            -3.1717          7.2806       0.0019652       0.0019652
v  Velocity[Z]       -6.9287e-015     1.4504e-014    -8.8299e-018    -8.8299e-018
v  ǁVelocityǁ        0.00080435          9.2758           4.796           4.796
v  Pressure               -41.302          18.854         0.46045         0.46045
v  nu_tilda           7.2838e-007       0.0042373       0.0006255       0.0006255
v  TempC                       21          73.124          21.282          21.282
v  TurbVisc           2.4542e-013       0.0049937      0.00072313      0.00072313
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              241:        0.26900E+01

===============================================================


 INSTANT    0.242000000E+03   TIME STEP NUMBER             242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65640E-02 0.88989E+00
   Friction velocity        uk    :  0.65640E-02 0.88989E+00
   Dimensionless distance   yplus :  0.52845E-01 0.71642E+01
   Friction thermal sca.    tstar : -0.11499E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39428E-01 0.53453E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47353E-02      35   0.82665E-03   0.69938E+01 0.16306E+03 
c  Velocity[X]                                      0.40950E+01 
c  Velocity[Y]                                      0.28988E+01 
c  Velocity[Z]                                      0.19042E-29 
c  Pressure     0.21394E-06     360   0.99615E-08   0.18012E+00 0.46911E+03 
c  nu_tilda     0.33748E-05      34   0.12418E-04   0.54487E-06 0.34640E+03 
c  TempC        0.21208E+02      30   0.94929E-03   0.21025E+02 0.48168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.198           9.255          4.5729          4.5729
v  Velocity[Y]            -3.1762          7.2362       0.0019885       0.0019885
v  Velocity[Z]       -6.9287e-015     1.4148e-014    -8.9563e-018    -8.9563e-018
v  ǁVelocityǁ        0.00075156           9.264          4.7966          4.7966
v  Pressure               -40.985          18.729         0.45632         0.45632
v  nu_tilda           7.3034e-007       0.0042375       0.0006262       0.0006262
v  TempC                       21          73.091          21.282          21.282
v  TurbVisc           2.4763e-013        0.004994       0.0007239       0.0007239
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              242:        0.23590E+01

===============================================================


 INSTANT    0.243000000E+03   TIME STEP NUMBER             243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64812E-02 0.88836E+00
   Friction velocity        uk    :  0.64812E-02 0.88836E+00
   Dimensionless distance   yplus :  0.52178E-01 0.71519E+01
   Friction thermal sca.    tstar : -0.12044E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38931E-01 0.53361E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47395E-02      35   0.72169E-03   0.70078E+01 0.16351E+03 
c  Velocity[X]                                      0.40689E+01 
c  Velocity[Y]                                      0.29389E+01 
c  Velocity[Z]                                      0.16925E-29 
c  Pressure     0.26038E-06     409   0.91065E-08   0.22675E+00 0.92704E+03 
c  nu_tilda     0.33794E-05      34   0.16402E-04   0.54276E-06 0.34518E+03 
c  TempC        0.21226E+02      30   0.89381E-03   0.22422E+02 0.49422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2167          9.2481          4.5729          4.5729
v  Velocity[Y]            -3.1872           7.254       0.0020101       0.0020101
v  Velocity[Z]       -6.9287e-015     1.3651e-014    -9.0733e-018    -9.0733e-018
v  ǁVelocityǁ         0.0001959          9.2546          4.7973          4.7973
v  Pressure               -40.655          18.795         0.45801         0.45801
v  nu_tilda           7.3085e-007       0.0042378      0.00062681      0.00062681
v  TempC                       21          73.114          21.283          21.283
v  TurbVisc            2.503e-013       0.0049944      0.00072468      0.00072468
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              243:        0.23640E+01

===============================================================


 INSTANT    0.244000000E+03   TIME STEP NUMBER             244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37164E-02 0.88915E+00
   Friction velocity        uk    :  0.37164E-02 0.88915E+00
   Dimensionless distance   yplus :  0.29920E-01 0.71583E+01
   Friction thermal sca.    tstar : -0.24675E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22323E-01 0.53409E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47437E-02      35   0.86822E-03   0.70305E+01 0.16422E+03 
c  Velocity[X]                                      0.40642E+01 
c  Velocity[Y]                                      0.29663E+01 
c  Velocity[Z]                                      0.19737E-29 
c  Pressure     0.17710E-06     358   0.91473E-08   0.15364E+00 0.40498E+03 
c  nu_tilda     0.33840E-05      34   0.12395E-04   0.54075E-06 0.34396E+03 
c  TempC        0.21244E+02      30   0.80294E-03   0.20520E+02 0.47641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2351          9.2409          4.5729          4.5729
v  Velocity[Y]             -3.201          7.2541       0.0020336       0.0020336
v  Velocity[Z]       -6.9287e-015     1.4192e-014    -9.1835e-018    -9.1835e-018
v  ǁVelocityǁ        0.00060031          9.2463           4.798           4.798
v  Pressure               -40.444           18.73         0.45479         0.45479
v  nu_tilda           7.3098e-007       0.0042381      0.00062751      0.00062751
v  TempC                       21           73.15          21.283          21.283
v  TurbVisc             2.51e-013       0.0049947      0.00072546      0.00072546
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              244:        0.27560E+01

===============================================================


 INSTANT    0.245000000E+03   TIME STEP NUMBER             245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63633E-02 0.88804E+00
   Friction velocity        uk    :  0.63633E-02 0.88804E+00
   Dimensionless distance   yplus :  0.51229E-01 0.71493E+01
   Friction thermal sca.    tstar : -0.17414E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38223E-01 0.53342E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47479E-02      35   0.80287E-03   0.71358E+01 0.16516E+03 
c  Velocity[X]                                      0.41390E+01 
c  Velocity[Y]                                      0.29967E+01 
c  Velocity[Z]                                      0.24377E-29 
c  Pressure     0.20073E-06     505   0.98903E-08   0.17178E+00 0.86013E+03 
c  nu_tilda     0.33886E-05      34   0.16344E-04   0.53876E-06 0.34277E+03 
c  TempC        0.21262E+02      30   0.84054E-03   0.17787E+02 0.44694E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2536           9.234          4.5729          4.5729
v  Velocity[Y]             -3.217          7.2145       0.0020568       0.0020568
v  Velocity[Z]       -6.9287e-015     1.2671e-014    -9.2906e-018    -9.2906e-018
v  ǁVelocityǁ         0.0010315           9.238          4.7987          4.7987
v  Pressure               -40.107          18.562         0.41131         0.41131
v  nu_tilda           7.3149e-007       0.0042384      0.00062812      0.00062812
v  TempC                       21          73.119          21.284          21.284
v  TurbVisc           2.5119e-013        0.004995      0.00072624      0.00072624
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              245:        0.25480E+01

===============================================================


 INSTANT    0.246000000E+03   TIME STEP NUMBER             246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92677E-02 0.88621E+00
   Friction velocity        uk    :  0.92677E-02 0.88621E+00
   Dimensionless distance   yplus :  0.74612E-01 0.71346E+01
   Friction thermal sca.    tstar : -0.12001E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55669E-01 0.53232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47521E-02      35   0.84793E-03   0.71176E+01 0.16551E+03 
c  Velocity[X]                                      0.41136E+01 
c  Velocity[Y]                                      0.30040E+01 
c  Velocity[Z]                                      0.16505E-29 
c  Pressure     0.20306E-06     474   0.94286E-08   0.17671E+00 0.98070E+03 
c  nu_tilda     0.33931E-05      34   0.12399E-04   0.53681E-06 0.34158E+03 
c  TempC        0.21279E+02      30   0.78283E-03   0.18673E+02 0.46076E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2696          9.2276          4.5729          4.5729
v  Velocity[Y]            -3.2356          7.2236       0.0020788       0.0020788
v  Velocity[Z]       -6.9287e-015     1.2231e-014    -9.3811e-018    -9.3811e-018
v  ǁVelocityǁ         0.0017756          9.2299          4.7994          4.7994
v  Pressure               -39.712          18.635         0.43972         0.43972
v  nu_tilda           7.3131e-007       0.0042386      0.00062882      0.00062882
v  TempC                       21          73.163          21.284          21.284
v  TurbVisc           2.5189e-013       0.0049953      0.00072701      0.00072701
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              246:        0.28240E+01

===============================================================


 INSTANT    0.247000000E+03   TIME STEP NUMBER             247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84611E-02 0.88674E+00
   Friction velocity        uk    :  0.84611E-02 0.88674E+00
   Dimensionless distance   yplus :  0.68118E-01 0.71389E+01
   Friction thermal sca.    tstar : -0.98894E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50824E-01 0.53264E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47563E-02      35   0.83598E-03   0.71960E+01 0.16639E+03 
c  Velocity[X]                                      0.41604E+01 
c  Velocity[Y]                                      0.30356E+01 
c  Velocity[Z]                                      0.16308E-29 
c  Pressure     0.22729E-06     472   0.96100E-08   0.20245E+00 0.89952E+03 
c  nu_tilda     0.33977E-05      34   0.16292E-04   0.53479E-06 0.34040E+03 
c  TempC        0.21297E+02      30   0.80762E-03   0.17115E+02 0.44268E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2877          9.2215          4.5729          4.5729
v  Velocity[Y]            -3.2561          7.1978       0.0021016       0.0021016
v  Velocity[Z]       -6.9287e-015      1.186e-014     -9.459e-018     -9.459e-018
v  ǁVelocityǁ         0.0021977          9.2225          4.8001          4.8001
v  Pressure               -39.373          18.477         0.39311         0.39311
v  nu_tilda           7.3117e-007       0.0042389      0.00062943      0.00062943
v  TempC                       21          73.168          21.285          21.285
v  TurbVisc           2.5164e-013       0.0049957      0.00072779      0.00072779
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              247:        0.25900E+01

===============================================================


 INSTANT    0.248000000E+03   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13578E-01 0.88522E+00
   Friction velocity        uk    :  0.13578E-01 0.88522E+00
   Dimensionless distance   yplus :  0.10931E+00 0.71266E+01
   Friction thermal sca.    tstar : -0.21184E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81560E-01 0.53172E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47605E-02      35   0.80996E-03   0.71959E+01 0.16680E+03 
c  Velocity[X]                                      0.41625E+01 
c  Velocity[Y]                                      0.30334E+01 
c  Velocity[Z]                                      0.11656E-29 
c  Pressure     0.20528E-06     473   0.99031E-08   0.17977E+00 0.73476E+03 
c  nu_tilda     0.34022E-05      34   0.12370E-04   0.53277E-06 0.33922E+03 
c  TempC        0.21315E+02      30   0.81792E-03   0.17996E+02 0.45869E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.306          9.2167          4.5729          4.5729
v  Velocity[Y]            -3.2778          7.2047       0.0021245       0.0021245
v  Velocity[Z]       -6.9287e-015     1.1513e-014    -9.5326e-018    -9.5326e-018
v  ǁVelocityǁ         0.0028404          9.2169          4.8008          4.8008
v  Pressure               -39.009          18.509         0.41393         0.41393
v  nu_tilda           7.3049e-007       0.0042392      0.00063013      0.00063013
v  TempC                       21           73.16          21.285          21.285
v  TurbVisc           2.5144e-013        0.004996      0.00072857      0.00072857
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              248:        0.25370E+01

===============================================================


 INSTANT    0.249000000E+03   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15319E-01 0.88589E+00
   Friction velocity        uk    :  0.15319E-01 0.88589E+00
   Dimensionless distance   yplus :  0.12333E+00 0.71320E+01
   Friction thermal sca.    tstar : -0.14299E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92015E-01 0.53213E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47647E-02      35   0.79571E-03   0.72353E+01 0.16740E+03 
c  Velocity[X]                                      0.41493E+01 
c  Velocity[Y]                                      0.30860E+01 
c  Velocity[Z]                                      0.14722E-29 
c  Pressure     0.20270E-06     488   0.94842E-08   0.18095E+00 0.64900E+03 
c  nu_tilda     0.34067E-05      34   0.16233E-04   0.53076E-06 0.33805E+03 
c  TempC        0.21332E+02      30   0.77545E-03   0.21238E+02 0.48732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3212          9.2156          4.5729          4.5729
v  Velocity[Y]            -3.3006          7.2027       0.0021479       0.0021479
v  Velocity[Z]       -6.9287e-015     1.1093e-014    -9.6036e-018    -9.6036e-018
v  ǁVelocityǁ         0.0027672          9.2157          4.8016          4.8016
v  Pressure               -38.711           18.43         0.37653         0.37653
v  nu_tilda           7.2984e-007       0.0042394      0.00063074      0.00063074
v  TempC                       21          73.169          21.286          21.286
v  TurbVisc           2.5051e-013       0.0049963      0.00072935      0.00072935
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              249:        0.26420E+01

===============================================================


 INSTANT    0.250000000E+03   TIME STEP NUMBER             250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16380E-01 0.88470E+00
   Friction velocity        uk    :  0.16380E-01 0.88470E+00
   Dimensionless distance   yplus :  0.13187E+00 0.71224E+01
   Friction thermal sca.    tstar : -0.92091E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98389E-01 0.53141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47689E-02      35   0.75856E-03   0.72576E+01 0.16795E+03 
c  Velocity[X]                                      0.41641E+01 
c  Velocity[Y]                                      0.30934E+01 
c  Velocity[Z]                                      0.15702E-29 
c  Pressure     0.16648E-06     377   0.95737E-08   0.15225E+00 0.47082E+03 
c  nu_tilda     0.34112E-05      34   0.12361E-04   0.52882E-06 0.33690E+03 
c  TempC        0.21350E+02      30   0.83168E-03   0.19086E+02 0.46330E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3391           9.215          4.5729          4.5729
v  Velocity[Y]            -3.3243          7.1689       0.0021717       0.0021717
v  Velocity[Z]       -6.9287e-015     1.0745e-014    -9.6608e-018    -9.6608e-018
v  ǁVelocityǁ         0.0015351          9.2154          4.8023          4.8023
v  Pressure               -38.292          18.314         0.37119         0.37119
v  nu_tilda           7.3034e-007       0.0042397      0.00063144      0.00063144
v  TempC                       21          73.164          21.286          21.286
v  TurbVisc           2.4962e-013       0.0049966      0.00073012      0.00073012
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              250:        0.22820E+01

===============================================================


 INSTANT    0.251000000E+03   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65871E-02 0.88284E+00
   Friction velocity        uk    :  0.65871E-02 0.88284E+00
   Dimensionless distance   yplus :  0.53030E-01 0.71075E+01
   Friction thermal sca.    tstar : -0.65746E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39567E-01 0.53030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47730E-02      35   0.81776E-03   0.72870E+01 0.16835E+03 
c  Velocity[X]                                      0.41726E+01 
c  Velocity[Y]                                      0.31144E+01 
c  Velocity[Z]                                      0.18160E-29 
c  Pressure     0.19650E-06     473   0.98486E-08   0.17532E+00 0.59856E+03 
c  nu_tilda     0.34157E-05      34   0.16175E-04   0.52694E-06 0.33576E+03 
c  TempC        0.21367E+02      30   0.78894E-03   0.19995E+02 0.46606E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3559          9.2149          4.5729          4.5729
v  Velocity[Y]            -3.3485          7.1773       0.0021955       0.0021955
v  Velocity[Z]       -6.9287e-015     1.0308e-014    -9.7122e-018    -9.7122e-018
v  ǁVelocityǁ         0.0019081          9.2158           4.803           4.803
v  Pressure               -38.318          18.316         0.35228         0.35228
v  nu_tilda           7.2935e-007       0.0042399      0.00063206      0.00063206
v  TempC                       21          73.131          21.287          21.287
v  TurbVisc           2.5031e-013       0.0049969       0.0007309       0.0007309
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              251:        0.25850E+01

===============================================================


 INSTANT    0.252000000E+03   TIME STEP NUMBER             252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11141E-01 0.88335E+00
   Friction velocity        uk    :  0.11141E-01 0.88335E+00
   Dimensionless distance   yplus :  0.89690E-01 0.71116E+01
   Friction thermal sca.    tstar : -0.20702E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66919E-01 0.53060E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47773E-02      35   0.81132E-03   0.73322E+01 0.16906E+03 
c  Velocity[X]                                      0.41867E+01 
c  Velocity[Y]                                      0.31455E+01 
c  Velocity[Z]                                      0.11680E-29 
c  Pressure     0.17748E-06     265   0.98001E-08   0.16297E+00 0.40819E+03 
c  nu_tilda     0.34202E-05      34   0.12353E-04   0.52510E-06 0.33463E+03 
c  TempC        0.21385E+02      30   0.77401E-03   0.19231E+02 0.46358E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3706          9.2154          4.5729          4.5729
v  Velocity[Y]            -3.3731          7.1435       0.0022191       0.0022191
v  Velocity[Z]       -6.9287e-015     9.9398e-015    -9.7652e-018    -9.7652e-018
v  ǁVelocityǁ         0.0030237          9.2168          4.8037          4.8037
v  Pressure               -38.443          18.224         0.35118         0.35118
v  nu_tilda           7.2806e-007       0.0042402      0.00063276      0.00063276
v  TempC                       21          73.128          21.287          21.287
v  TurbVisc           2.4895e-013       0.0049972      0.00073168      0.00073168
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              252:        0.21180E+01

===============================================================


 INSTANT    0.253000000E+03   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18120E-01 0.88224E+00
   Friction velocity        uk    :  0.18120E-01 0.88224E+00
   Dimensionless distance   yplus :  0.14588E+00 0.71027E+01
   Friction thermal sca.    tstar : -0.59571E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10884E+00 0.52994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47815E-02      35   0.81276E-03   0.73522E+01 0.16957E+03 
c  Velocity[X]                                      0.41837E+01 
c  Velocity[Y]                                      0.31684E+01 
c  Velocity[Z]                                      0.12835E-29 
c  Pressure     0.19429E-06     456   0.99516E-08   0.18009E+00 0.58521E+03 
c  nu_tilda     0.34246E-05      34   0.16119E-04   0.52330E-06 0.33352E+03 
c  TempC        0.21402E+02      30   0.70306E-03   0.19505E+02 0.46999E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3871          9.2163          4.5729          4.5729
v  Velocity[Y]            -3.3982          7.1632       0.0022434       0.0022434
v  Velocity[Z]       -6.9287e-015     9.5965e-015    -9.8068e-018    -9.8068e-018
v  ǁVelocityǁ         0.0035563          9.2185          4.8044          4.8044
v  Pressure               -38.648          18.241         0.33289         0.33289
v  nu_tilda           7.2623e-007       0.0042405      0.00063337      0.00063337
v  TempC                       21          73.179          21.288          21.288
v  TurbVisc           2.4719e-013       0.0049975      0.00073246      0.00073246
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              253:        0.30630E+01

===============================================================


 INSTANT    0.254000000E+03   TIME STEP NUMBER             254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15178E-01 0.88282E+00
   Friction velocity        uk    :  0.15178E-01 0.88282E+00
   Dimensionless distance   yplus :  0.12219E+00 0.71073E+01
   Friction thermal sca.    tstar : -0.62938E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91168E-01 0.53028E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47857E-02      35   0.82185E-03   0.74068E+01 0.17020E+03 
c  Velocity[X]                                      0.42220E+01 
c  Velocity[Y]                                      0.31849E+01 
c  Velocity[Z]                                      0.11885E-29 
c  Pressure     0.17852E-06     361   0.91495E-08   0.16352E+00 0.38811E+03 
c  nu_tilda     0.34291E-05      34   0.12333E-04   0.52147E-06 0.33241E+03 
c  TempC        0.21420E+02      30   0.72556E-03   0.17580E+02 0.44523E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4031          9.2177          4.5729          4.5729
v  Velocity[Y]            -3.4232          7.1526       0.0022677       0.0022677
v  Velocity[Z]       -6.9287e-015     9.2315e-015    -9.8483e-018    -9.8483e-018
v  ǁVelocityǁ         0.0025246          9.2207          4.8051          4.8051
v  Pressure                -38.78          18.196         0.33343         0.33343
v  nu_tilda           7.2426e-007       0.0042407      0.00063407      0.00063407
v  TempC                       21           73.16          21.288          21.288
v  TurbVisc           2.4471e-013       0.0049978      0.00073324      0.00073324
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              254:        0.22900E+01

===============================================================


 INSTANT    0.255000000E+03   TIME STEP NUMBER             255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10480E-01 0.88184E+00
   Friction velocity        uk    :  0.10480E-01 0.88184E+00
   Dimensionless distance   yplus :  0.84369E-01 0.70994E+01
   Friction thermal sca.    tstar : -0.69750E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62949E-01 0.52970E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47899E-02      35   0.76101E-03   0.74439E+01 0.17078E+03 
c  Velocity[X]                                      0.42412E+01 
c  Velocity[Y]                                      0.32026E+01 
c  Velocity[Z]                                      0.10059E-29 
c  Pressure     0.15733E-06     520   0.97597E-08   0.14820E+00 0.96147E+03 
c  nu_tilda     0.34335E-05      34   0.16075E-04   0.51957E-06 0.33130E+03 
c  TempC        0.21437E+02      30   0.72665E-03   0.19146E+02 0.44510E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4168          9.2194          4.5729          4.5729
v  Velocity[Y]            -3.4486          7.1209       0.0022929       0.0022929
v  Velocity[Z]       -6.9287e-015     8.9492e-015    -9.8867e-018    -9.8867e-018
v  ǁVelocityǁ         0.0015567          9.2236          4.8058          4.8058
v  Pressure               -38.975          18.032         0.28393         0.28393
v  nu_tilda           7.2331e-007       0.0042409      0.00063468      0.00063468
v  TempC                       21          73.134          21.289          21.289
v  TurbVisc           2.4207e-013       0.0049981      0.00073402      0.00073402
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              255:        0.26940E+01

===============================================================


 INSTANT    0.256000000E+03   TIME STEP NUMBER             256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78530E-02 0.88038E+00
   Friction velocity        uk    :  0.78530E-02 0.88038E+00
   Dimensionless distance   yplus :  0.63222E-01 0.70877E+01
   Friction thermal sca.    tstar : -0.14149E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47171E-01 0.52882E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47941E-02      35   0.82461E-03   0.74278E+01 0.17096E+03 
c  Velocity[X]                                      0.42099E+01 
c  Velocity[Y]                                      0.32180E+01 
c  Velocity[Z]                                      0.12995E-29 
c  Pressure     0.16406E-06     473   0.99261E-08   0.15178E+00 0.86641E+03 
c  nu_tilda     0.34379E-05      34   0.12336E-04   0.51774E-06 0.33020E+03 
c  TempC        0.21455E+02      30   0.70263E-03   0.17616E+02 0.44521E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4322          9.2214          4.5729          4.5729
v  Velocity[Y]            -3.4736          7.1357       0.0023173       0.0023173
v  Velocity[Z]       -6.9287e-015     8.6059e-015    -9.9224e-018    -9.9224e-018
v  ǁVelocityǁ         0.0019701          9.2269          4.8065          4.8065
v  Pressure               -39.128          18.114         0.30891         0.30891
v  nu_tilda           7.2285e-007       0.0042412      0.00063538      0.00063538
v  TempC                       21          73.147          21.289          21.289
v  TurbVisc            2.408e-013       0.0049984      0.00073479      0.00073479
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              256:        0.25430E+01

===============================================================


 INSTANT    0.257000000E+03   TIME STEP NUMBER             257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15267E-01 0.88122E+00
   Friction velocity        uk    :  0.15267E-01 0.88122E+00
   Dimensionless distance   yplus :  0.12291E+00 0.70944E+01
   Friction thermal sca.    tstar : -0.11704E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91702E-01 0.52932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47983E-02      35   0.81756E-03   0.74806E+01 0.17153E+03 
c  Velocity[X]                                      0.42294E+01 
c  Velocity[Y]                                      0.32512E+01 
c  Velocity[Z]                                      0.23922E-29 
c  Pressure     0.16871E-06     505   0.97204E-08   0.15882E+00 0.99433E+03 
c  nu_tilda     0.34423E-05      34   0.16023E-04   0.51593E-06 0.32911E+03 
c  TempC        0.21472E+02      30   0.77662E-03   0.18665E+02 0.45012E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4456          9.2238          4.5729          4.5729
v  Velocity[Y]             -3.499          7.1044       0.0023429       0.0023429
v  Velocity[Z]       -6.9287e-015      8.321e-015    -9.9626e-018    -9.9626e-018
v  ǁVelocityǁ         0.0029356          9.2307          4.8072          4.8072
v  Pressure                -39.32          17.954         0.25763         0.25763
v  nu_tilda           7.2212e-007       0.0042414        0.000636        0.000636
v  TempC                       21          73.166           21.29           21.29
v  TurbVisc           2.4019e-013       0.0049987      0.00073558      0.00073558
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              257:        0.26550E+01

===============================================================


 INSTANT    0.258000000E+03   TIME STEP NUMBER             258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19062E-01 0.88023E+00
   Friction velocity        uk    :  0.19062E-01 0.88023E+00
   Dimensionless distance   yplus :  0.15346E+00 0.70864E+01
   Friction thermal sca.    tstar : -0.65358E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11450E+00 0.52873E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48025E-02      35   0.80522E-03   0.74937E+01 0.17203E+03 
c  Velocity[X]                                      0.42281E+01 
c  Velocity[Y]                                      0.32656E+01 
c  Velocity[Z]                                      0.12524E-29 
c  Pressure     0.17915E-06     488   0.98225E-08   0.16658E+00 0.78407E+03 
c  nu_tilda     0.34467E-05      34   0.12333E-04   0.51417E-06 0.32804E+03 
c  TempC        0.21490E+02      30   0.70909E-03   0.19260E+02 0.46381E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4593          9.2264          4.5729          4.5729
v  Velocity[Y]            -3.5244          7.1218       0.0023673       0.0023673
v  Velocity[Z]       -6.9287e-015     8.0744e-015    -9.9812e-018    -9.9812e-018
v  ǁVelocityǁ         0.0028961          9.2347           4.808           4.808
v  Pressure               -39.465          18.026         0.27964         0.27964
v  nu_tilda           7.2158e-007       0.0042417       0.0006367       0.0006367
v  TempC                       21          73.194           21.29           21.29
v  TurbVisc           2.3923e-013        0.004999      0.00073635      0.00073635
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              258:        0.26110E+01

===============================================================


 INSTANT    0.259000000E+03   TIME STEP NUMBER             259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91983E-02 0.88129E+00
   Friction velocity        uk    :  0.91983E-02 0.88129E+00
   Dimensionless distance   yplus :  0.74053E-01 0.70950E+01
   Friction thermal sca.    tstar : -0.61385E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55252E-01 0.52937E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48067E-02      35   0.80014E-03   0.74960E+01 0.17234E+03 
c  Velocity[X]                                      0.42077E+01 
c  Velocity[Y]                                      0.32883E+01 
c  Velocity[Z]                                      0.11578E-29 
c  Pressure     0.16188E-06     489   0.96482E-08   0.15406E+00 0.58289E+03 
c  nu_tilda     0.34510E-05      34   0.15976E-04   0.51244E-06 0.32698E+03 
c  TempC        0.21507E+02      30   0.53062E-03   0.19517E+02 0.46135E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.473          9.2292          4.5729          4.5729
v  Velocity[Y]            -3.5496          7.1302       0.0023932       0.0023932
v  Velocity[Z]       -6.9287e-015     7.8215e-015    -9.9961e-018    -9.9961e-018
v  ǁVelocityǁ         0.0020221           9.239          4.8087          4.8087
v  Pressure               -39.658          17.973         0.24615         0.24615
v  nu_tilda           7.1969e-007       0.0042419      0.00063731      0.00063731
v  TempC                       21          73.194          21.291          21.291
v  TurbVisc           2.3851e-013       0.0049992      0.00073713      0.00073713
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              259:        0.26270E+01

===============================================================


 INSTANT    0.260000000E+03   TIME STEP NUMBER             260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12201E-01 0.88028E+00
   Friction velocity        uk    :  0.12201E-01 0.88028E+00
   Dimensionless distance   yplus :  0.98229E-01 0.70868E+01
   Friction thermal sca.    tstar : -0.67016E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73290E-01 0.52876E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48109E-02      35   0.80252E-03   0.75724E+01 0.17307E+03 
c  Velocity[X]                                      0.42576E+01 
c  Velocity[Y]                                      0.33148E+01 
c  Velocity[Z]                                      0.11164E-29 
c  Pressure     0.16191E-06     458   0.99994E-08   0.15362E+00 0.64428E+03 
c  nu_tilda     0.34554E-05      34   0.12328E-04   0.51078E-06 0.32593E+03 
c  TempC        0.21524E+02      30   0.73484E-03   0.16067E+02 0.41918E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4856          9.2328          4.5729          4.5729
v  Velocity[Y]            -3.5748          7.0825       0.0024182       0.0024182
v  Velocity[Z]       -6.9287e-015     7.6131e-015    -1.0018e-017    -1.0018e-017
v  ǁVelocityǁ         0.0015698          9.2434          4.8094          4.8094
v  Pressure               -39.786          17.854         0.23088         0.23088
v  nu_tilda           7.1849e-007       0.0042421      0.00063801      0.00063801
v  TempC                       21          73.212          21.291          21.291
v  TurbVisc           2.3603e-013       0.0049995      0.00073791      0.00073791
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              260:        0.25300E+01

===============================================================


 INSTANT    0.261000000E+03   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81365E-02 0.87864E+00
   Friction velocity        uk    :  0.81365E-02 0.87864E+00
   Dimensionless distance   yplus :  0.65504E-01 0.70737E+01
   Friction thermal sca.    tstar : -0.83205E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48874E-01 0.52778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48151E-02      35   0.78708E-03   0.75793E+01 0.17341E+03 
c  Velocity[X]                                      0.42471E+01 
c  Velocity[Y]                                      0.33322E+01 
c  Velocity[Z]                                      0.12147E-29 
c  Pressure     0.14038E-06     442   0.97128E-08   0.13188E+00 0.56416E+03 
c  nu_tilda     0.34597E-05      34   0.15931E-04   0.50904E-06 0.32488E+03 
c  TempC        0.21541E+02      30   0.71887E-03   0.17025E+02 0.43711E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4988          9.2376          4.5729          4.5729
v  Velocity[Y]            -3.5996          7.1036       0.0024446       0.0024446
v  Velocity[Z]       -6.9287e-015     7.3647e-015    -1.0041e-017    -1.0041e-017
v  ǁVelocityǁ         0.0022905           9.248          4.8101          4.8101
v  Pressure               -39.983          17.903         0.21264         0.21264
v  nu_tilda           7.1665e-007       0.0042424      0.00063862      0.00063862
v  TempC                       21          73.227          21.292          21.292
v  TurbVisc           2.3445e-013       0.0049998      0.00073869      0.00073869
v  total_pressure     1.0129e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              261:        0.24410E+01

===============================================================


 INSTANT    0.262000000E+03   TIME STEP NUMBER             262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14178E-01 0.87991E+00
   Friction velocity        uk    :  0.14178E-01 0.87991E+00
   Dimensionless distance   yplus :  0.11414E+00 0.70839E+01
   Friction thermal sca.    tstar : -0.20290E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85160E-01 0.52854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48193E-02      35   0.81065E-03   0.75924E+01 0.17374E+03 
c  Velocity[X]                                      0.42375E+01 
c  Velocity[Y]                                      0.33549E+01 
c  Velocity[Z]                                      0.15944E-29 
c  Pressure     0.15409E-06     330   0.95865E-08   0.14785E+00 0.39883E+03 
c  nu_tilda     0.34640E-05      34   0.12319E-04   0.50733E-06 0.32384E+03 
c  TempC        0.21559E+02      30   0.70269E-03   0.21069E+02 0.46869E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5125           9.243          4.5729          4.5729
v  Velocity[Y]            -3.6244          7.0774         0.00247         0.00247
v  Velocity[Z]       -6.9287e-015     7.1711e-015    -1.0074e-017    -1.0074e-017
v  ǁVelocityǁ         0.0032522           9.253          4.8109          4.8109
v  Pressure               -40.122          17.883         0.20975         0.20975
v  nu_tilda           7.1463e-007       0.0042426      0.00063932      0.00063932
v  TempC                       21          73.239          21.292          21.292
v  TurbVisc           2.3206e-013       0.0050001      0.00073946      0.00073946
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              262:        0.21630E+01

===============================================================


 INSTANT    0.263000000E+03   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32820E-02 0.87887E+00
   Friction velocity        uk    :  0.32820E-02 0.87887E+00
   Dimensionless distance   yplus :  0.26422E-01 0.70755E+01
   Friction thermal sca.    tstar : -0.77335E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19714E-01 0.52791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48235E-02      35   0.76027E-03   0.76143E+01 0.17412E+03 
c  Velocity[X]                                      0.42392E+01 
c  Velocity[Y]                                      0.33751E+01 
c  Velocity[Z]                                      0.15131E-29 
c  Pressure     0.15759E-06     489   0.93278E-08   0.14689E+00 0.52612E+03 
c  nu_tilda     0.34684E-05      34   0.15884E-04   0.50564E-06 0.32281E+03 
c  TempC        0.21576E+02      30   0.83247E-03   0.19496E+02 0.46831E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5248          9.2491          4.5729          4.5729
v  Velocity[Y]            -3.6495          7.0968       0.0024971       0.0024971
v  Velocity[Z]       -6.9287e-015     6.9813e-015    -1.0103e-017    -1.0103e-017
v  ǁVelocityǁ          0.004345           9.258          4.8116          4.8116
v  Pressure               -40.316          17.884         0.18095         0.18095
v  nu_tilda           7.1228e-007       0.0042428      0.00063994      0.00063994
v  TempC                       21          73.222          21.293          21.293
v  TurbVisc           2.2945e-013       0.0050003      0.00074025      0.00074025
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              263:        0.26460E+01

===============================================================


 INSTANT    0.264000000E+03   TIME STEP NUMBER             264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19951E-01 0.88027E+00
   Friction velocity        uk    :  0.19951E-01 0.88027E+00
   Dimensionless distance   yplus :  0.16062E+00 0.70868E+01
   Friction thermal sca.    tstar : -0.88503E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11984E+00 0.52875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48277E-02      35   0.80086E-03   0.76035E+01 0.17432E+03 
c  Velocity[X]                                      0.42151E+01 
c  Velocity[Y]                                      0.33883E+01 
c  Velocity[Z]                                      0.12427E-29 
c  Pressure     0.12445E-06     472   0.96840E-08   0.11866E+00 0.59584E+03 
c  nu_tilda     0.34726E-05      34   0.12332E-04   0.50399E-06 0.32179E+03 
c  TempC        0.21593E+02      30   0.63371E-03   0.20814E+02 0.48888E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5358          9.2543          4.5729          4.5729
v  Velocity[Y]             -3.674          7.1019       0.0025228       0.0025228
v  Velocity[Z]       -6.9287e-015     6.7928e-015    -1.0133e-017    -1.0133e-017
v  ǁVelocityǁ         0.0044961          9.2642          4.8123          4.8123
v  Pressure               -40.455           17.95         0.19683         0.19683
v  nu_tilda           7.0896e-007       0.0042431      0.00064063      0.00064063
v  TempC                       21          73.236          21.293          21.293
v  TurbVisc           2.2645e-013       0.0050006      0.00074102      0.00074102
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              264:        0.28680E+01

===============================================================


 INSTANT    0.265000000E+03   TIME STEP NUMBER             265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15823E-01 0.87959E+00
   Friction velocity        uk    :  0.15823E-01 0.87959E+00
   Dimensionless distance   yplus :  0.12739E+00 0.70813E+01
   Friction thermal sca.    tstar : -0.93121E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95045E-01 0.52834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48319E-02      35   0.79787E-03   0.76694E+01 0.17498E+03 
c  Velocity[X]                                      0.42481E+01 
c  Velocity[Y]                                      0.34212E+01 
c  Velocity[Z]                                      0.13859E-29 
c  Pressure     0.15373E-06     489   0.97602E-08   0.14895E+00 0.10516E+04 
c  nu_tilda     0.34769E-05      34   0.15841E-04   0.50233E-06 0.32077E+03 
c  TempC        0.21610E+02      30   0.66738E-03   0.18804E+02 0.45244E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5477          9.2595          4.5729          4.5729
v  Velocity[Y]            -3.6985          7.0723       0.0025502       0.0025502
v  Velocity[Z]       -6.9287e-015     6.5964e-015    -1.0173e-017    -1.0173e-017
v  ǁVelocityǁ         0.0022954          9.2707          4.8131          4.8131
v  Pressure               -40.636          17.832         0.14259         0.14259
v  nu_tilda           7.0469e-007       0.0042433      0.00064125      0.00064125
v  TempC                       21          73.221          21.294          21.294
v  TurbVisc           2.2225e-013       0.0050009       0.0007418       0.0007418
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              265:        0.27380E+01

===============================================================


 INSTANT    0.266000000E+03   TIME STEP NUMBER             266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61076E-02 0.87804E+00
   Friction velocity        uk    :  0.61076E-02 0.87804E+00
   Dimensionless distance   yplus :  0.49170E-01 0.70688E+01
   Friction thermal sca.    tstar : -0.12222E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36686E-01 0.52741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48361E-02      35   0.79425E-03   0.77260E+01 0.17542E+03 
c  Velocity[X]                                      0.42692E+01 
c  Velocity[Y]                                      0.34568E+01 
c  Velocity[Z]                                      0.14996E-29 
c  Pressure     0.16717E-06     488   0.95369E-08   0.15661E+00 0.82639E+03 
c  nu_tilda     0.34812E-05      34   0.12344E-04   0.50073E-06 0.31977E+03 
c  TempC        0.21628E+02      30   0.81155E-03   0.17364E+02 0.43494E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5588          9.2649          4.5729          4.5729
v  Velocity[Y]            -3.7227          7.0833       0.0025766       0.0025766
v  Velocity[Z]       -6.9287e-015     6.5456e-015    -1.0204e-017    -1.0204e-017
v  ǁVelocityǁ        0.00060742          9.2773          4.8138          4.8138
v  Pressure               -40.774          17.941         0.16737         0.16737
v  nu_tilda           6.9921e-007       0.0042435      0.00064195      0.00064195
v  TempC                       21          73.227          21.294          21.294
v  TurbVisc           2.1695e-013       0.0050011      0.00074258      0.00074258
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              266:        0.27810E+01

===============================================================


 INSTANT    0.267000000E+03   TIME STEP NUMBER             267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49549E-02 0.87914E+00
   Friction velocity        uk    :  0.49549E-02 0.87914E+00
   Dimensionless distance   yplus :  0.39890E-01 0.70777E+01
   Friction thermal sca.    tstar : -0.23835E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29762E-01 0.52807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48403E-02      35   0.82156E-03   0.77060E+01 0.17567E+03 
c  Velocity[X]                                      0.42543E+01 
c  Velocity[Y]                                      0.34517E+01 
c  Velocity[Z]                                      0.13561E-29 
c  Pressure     0.13578E-06     517   0.99231E-08   0.13136E+00 0.10245E+04 
c  nu_tilda     0.34854E-05      34   0.15802E-04   0.49913E-06 0.31878E+03 
c  TempC        0.21645E+02      30   0.78817E-03   0.20852E+02 0.48777E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5692          9.2707          4.5729          4.5729
v  Velocity[Y]            -3.7466          7.0619       0.0026041       0.0026041
v  Velocity[Z]       -6.9287e-015      6.394e-015    -1.0244e-017    -1.0244e-017
v  ǁVelocityǁ          0.002004          9.2837          4.8146          4.8146
v  Pressure               -40.953          17.828         0.11357         0.11357
v  nu_tilda            6.927e-007       0.0042437      0.00064256      0.00064256
v  TempC                       21          73.176          21.295          21.295
v  TurbVisc           2.1027e-013       0.0050014      0.00074336      0.00074336
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              267:        0.29390E+01

===============================================================


 INSTANT    0.268000000E+03   TIME STEP NUMBER             268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82656E-02 0.87848E+00
   Friction velocity        uk    :  0.82656E-02 0.87848E+00
   Dimensionless distance   yplus :  0.66544E-01 0.70724E+01
   Friction thermal sca.    tstar : -0.17046E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49649E-01 0.52768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48445E-02      35   0.79656E-03   0.77223E+01 0.17599E+03 
c  Velocity[X]                                      0.42331E+01 
c  Velocity[Y]                                      0.34892E+01 
c  Velocity[Z]                                      0.11639E-29 
c  Pressure     0.13641E-06     489   0.92538E-08   0.13022E+00 0.97419E+03 
c  nu_tilda     0.34897E-05      34   0.12340E-04   0.49756E-06 0.31779E+03 
c  TempC        0.21662E+02      30   0.69862E-03   0.20787E+02 0.48460E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5787          9.2754          4.5729          4.5729
v  Velocity[Y]            -3.7701          7.0828       0.0026308       0.0026308
v  Velocity[Z]       -6.9287e-015     6.1346e-015    -1.0283e-017    -1.0283e-017
v  ǁVelocityǁ         0.0036815          9.2902          4.8153          4.8153
v  Pressure               -41.091          17.961          0.1436          0.1436
v  nu_tilda           6.8591e-007        0.004244      0.00064326      0.00064326
v  TempC                       21          73.186          21.295          21.295
v  TurbVisc           2.0256e-013       0.0050017      0.00074413      0.00074413
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              268:        0.28350E+01

===============================================================


 INSTANT    0.269000000E+03   TIME STEP NUMBER             269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13105E-01 0.87960E+00
   Friction velocity        uk    :  0.13105E-01 0.87960E+00
   Dimensionless distance   yplus :  0.10550E+00 0.70814E+01
   Friction thermal sca.    tstar : -0.29457E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78717E-01 0.52835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48487E-02      35   0.78491E-03   0.77206E+01 0.17622E+03 
c  Velocity[X]                                      0.42085E+01 
c  Velocity[Y]                                      0.35121E+01 
c  Velocity[Z]                                      0.15481E-29 
c  Pressure     0.15246E-06     490   0.97090E-08   0.14399E+00 0.77802E+03 
c  nu_tilda     0.34939E-05      34   0.15761E-04   0.49598E-06 0.31682E+03 
c  TempC        0.21679E+02      30   0.65510E-03   0.19289E+02 0.46220E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5883          9.2804          4.5729          4.5729
v  Velocity[Y]             -3.794          7.0838       0.0026593       0.0026593
v  Velocity[Z]       -6.9287e-015     6.1302e-015    -1.0326e-017    -1.0326e-017
v  ǁVelocityǁ         0.0026661          9.2965          4.8161          4.8161
v  Pressure               -41.267          17.895        0.099139        0.099139
v  nu_tilda           6.7632e-007       0.0042442      0.00064387      0.00064387
v  TempC                       21          73.231          21.296          21.296
v  TurbVisc           1.9473e-013       0.0050019      0.00074491      0.00074491
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              269:        0.26730E+01

===============================================================


 INSTANT    0.270000000E+03   TIME STEP NUMBER             270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68561E-02 0.87924E+00
   Friction velocity        uk    :  0.68561E-02 0.87924E+00
   Dimensionless distance   yplus :  0.55197E-01 0.70785E+01
   Friction thermal sca.    tstar : -0.29960E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41183E-01 0.52813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48529E-02      35   0.79190E-03   0.77790E+01 0.17671E+03 
c  Velocity[X]                                      0.42538E+01 
c  Velocity[Y]                                      0.35251E+01 
c  Velocity[Z]                                      0.21840E-29 
c  Pressure     0.15113E-06     279   0.89606E-08   0.14702E+00 0.37094E+03 
c  nu_tilda     0.34981E-05      34   0.12369E-04   0.49446E-06 0.31585E+03 
c  TempC        0.21696E+02      30   0.58406E-03   0.19743E+02 0.45982E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5981          9.2858          4.5729          4.5729
v  Velocity[Y]            -3.8174           7.056       0.0026858       0.0026858
v  Velocity[Z]       -6.9287e-015     6.1991e-015    -1.0376e-017    -1.0376e-017
v  ǁVelocityǁ         0.0021953          9.3024          4.8168          4.8168
v  Pressure               -41.386           17.88        0.097334        0.097334
v  nu_tilda            6.667e-007       0.0042444      0.00064457      0.00064457
v  TempC                       21          73.198          21.296          21.296
v  TurbVisc           1.8407e-013       0.0050022      0.00074569      0.00074569
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              270:        0.20320E+01

===============================================================


 INSTANT    0.271000000E+03   TIME STEP NUMBER             271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24844E-02 0.87807E+00
   Friction velocity        uk    :  0.24844E-02 0.87807E+00
   Dimensionless distance   yplus :  0.20001E-01 0.70691E+01
   Friction thermal sca.    tstar : -0.19352E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14923E-01 0.52743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48571E-02      35   0.82756E-03   0.77810E+01 0.17697E+03 
c  Velocity[X]                                      0.42139E+01 
c  Velocity[Y]                                      0.35671E+01 
c  Velocity[Z]                                      0.15707E-29 
c  Pressure     0.13140E-06     458   0.93845E-08   0.12473E+00 0.50553E+03 
c  nu_tilda     0.35023E-05      34   0.15723E-04   0.49292E-06 0.31488E+03 
c  TempC        0.21713E+02      30   0.85439E-03   0.18484E+02 0.45428E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6079            9.29          4.5729          4.5729
v  Velocity[Y]            -3.8407          7.0801       0.0027148       0.0027148
v  Velocity[Z]       -6.9287e-015     6.1407e-015    -1.0429e-017    -1.0429e-017
v  ǁVelocityǁ          0.001841          9.3087          4.8176          4.8176
v  Pressure                -41.57          17.911        0.073206        0.073206
v  nu_tilda           6.5668e-007       0.0042446      0.00064518      0.00064518
v  TempC                       21          73.232          21.297          21.297
v  TurbVisc           1.7382e-013       0.0050024      0.00074647      0.00074647
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              271:        0.25400E+01

===============================================================


 INSTANT    0.272000000E+03   TIME STEP NUMBER             272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99819E-02 0.87943E+00
   Friction velocity        uk    :  0.99819E-02 0.87943E+00
   Dimensionless distance   yplus :  0.80361E-01 0.70800E+01
   Friction thermal sca.    tstar : -0.14178E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59958E-01 0.52825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48613E-02      35   0.79894E-03   0.78000E+01 0.17724E+03 
c  Velocity[X]                                      0.42310E+01 
c  Velocity[Y]                                      0.35689E+01 
c  Velocity[Z]                                      0.11482E-29 
c  Pressure     0.14034E-06     390   0.95521E-08   0.13505E+00 0.43111E+03 
c  nu_tilda     0.35065E-05      34   0.12375E-04   0.49141E-06 0.31393E+03 
c  TempC        0.21730E+02      30   0.74204E-03   0.22922E+02 0.51177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6143          9.2943          4.5729          4.5729
v  Velocity[Y]            -3.8636          7.0506       0.0027421       0.0027421
v  Velocity[Z]       -6.9287e-015     6.2293e-015    -1.0484e-017    -1.0484e-017
v  ǁVelocityǁ         0.0015386          9.3146          4.8183          4.8183
v  Pressure               -41.686          17.871        0.067201        0.067201
v  nu_tilda           6.4604e-007       0.0042448      0.00064587      0.00064587
v  TempC                       21          73.273          21.298          21.298
v  TurbVisc            1.636e-013       0.0050027      0.00074724      0.00074724
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              272:        0.23710E+01

===============================================================


 INSTANT    0.273000000E+03   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62629E-02 0.87876E+00
   Friction velocity        uk    :  0.62629E-02 0.87876E+00
   Dimensionless distance   yplus :  0.50421E-01 0.70746E+01
   Friction thermal sca.    tstar : -0.13169E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37620E-01 0.52785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48655E-02      35   0.77826E-03   0.78098E+01 0.17750E+03 
c  Velocity[X]                                      0.42101E+01 
c  Velocity[Y]                                      0.35997E+01 
c  Velocity[Z]                                      0.13438E-29 
c  Pressure     0.12534E-06     457   0.92383E-08   0.11885E+00 0.51323E+03 
c  nu_tilda     0.35107E-05      34   0.15684E-04   0.48993E-06 0.31299E+03 
c  TempC        0.21747E+02      30   0.59133E-03   0.20945E+02 0.48103E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6232           9.299          4.5729          4.5729
v  Velocity[Y]            -3.8859            7.08       0.0027706       0.0027706
v  Velocity[Z]       -6.9287e-015     6.7405e-015     -1.054e-017     -1.054e-017
v  ǁVelocityǁ         0.0019249          9.3199          4.8191          4.8191
v  Pressure               -41.861          17.914         0.04559         0.04559
v  nu_tilda           6.3556e-007        0.004245      0.00064649      0.00064649
v  TempC                       21          73.258          21.298          21.298
v  TurbVisc           1.5325e-013       0.0050029      0.00074802      0.00074802
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              273:        0.26560E+01

===============================================================


 INSTANT    0.274000000E+03   TIME STEP NUMBER             274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11023E-01 0.88056E+00
   Friction velocity        uk    :  0.11023E-01 0.88056E+00
   Dimensionless distance   yplus :  0.88739E-01 0.70891E+01
   Friction thermal sca.    tstar : -0.11935E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66209E-01 0.52893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48697E-02      35   0.78182E-03   0.78090E+01 0.17773E+03 
c  Velocity[X]                                      0.41755E+01 
c  Velocity[Y]                                      0.36336E+01 
c  Velocity[Z]                                      0.14095E-29 
c  Pressure     0.12122E-06     454   0.91751E-08   0.11657E+00 0.43734E+03 
c  nu_tilda     0.35148E-05      34   0.12380E-04   0.48850E-06 0.31205E+03 
c  TempC        0.21764E+02      30   0.69455E-03   0.18550E+02 0.44185E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6314          9.3043          4.5729          4.5729
v  Velocity[Y]            -3.9086          7.0922       0.0027987       0.0027987
v  Velocity[Z]       -6.9287e-015     6.4669e-015    -1.0595e-017    -1.0595e-017
v  ǁVelocityǁ         0.0021119          9.3256          4.8199          4.8199
v  Pressure               -41.976          17.959        0.055739        0.055739
v  nu_tilda           6.2424e-007       0.0042452      0.00064718      0.00064718
v  TempC                       21          73.205          21.299          21.299
v  TurbVisc           1.4355e-013       0.0050032      0.00074879      0.00074879
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              274:        0.25370E+01

===============================================================


 INSTANT    0.275000000E+03   TIME STEP NUMBER             275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13512E-01 0.88030E+00
   Friction velocity        uk    :  0.13512E-01 0.88030E+00
   Dimensionless distance   yplus :  0.10878E+00 0.70870E+01
   Friction thermal sca.    tstar : -0.19316E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81164E-01 0.52877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48739E-02      35   0.78279E-03   0.78660E+01 0.17817E+03 
c  Velocity[X]                                      0.42190E+01 
c  Velocity[Y]                                      0.36470E+01 
c  Velocity[Z]                                      0.16717E-29 
c  Pressure     0.17297E-06     506   0.93278E-08   0.16445E+00 0.11787E+04 
c  nu_tilda     0.35190E-05      34   0.15644E-04   0.48706E-06 0.31113E+03 
c  TempC        0.21781E+02      30   0.59568E-03   0.21328E+02 0.46995E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.636          9.3108          4.5729          4.5729
v  Velocity[Y]            -3.9308          7.0633       0.0028282       0.0028282
v  Velocity[Z]       -6.9287e-015     6.6508e-015    -1.0646e-017    -1.0646e-017
v  ǁVelocityǁ         0.0033601           9.331          4.8206          4.8206
v  Pressure               -42.143          17.826      -0.0054225      -0.0054225
v  nu_tilda           6.1306e-007       0.0042454      0.00064779      0.00064779
v  TempC                       21          73.241          21.299          21.299
v  TurbVisc           1.3359e-013       0.0050034      0.00074958      0.00074958
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              275:        0.26890E+01

===============================================================


 INSTANT    0.276000000E+03   TIME STEP NUMBER             276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19005E-01 0.87930E+00
   Friction velocity        uk    :  0.19005E-01 0.87930E+00
   Dimensionless distance   yplus :  0.15301E+00 0.70789E+01
   Friction thermal sca.    tstar : -0.11350E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11416E+00 0.52817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48780E-02      35   0.79009E-03   0.78634E+01 0.17838E+03 
c  Velocity[X]                                      0.41975E+01 
c  Velocity[Y]                                      0.36660E+01 
c  Velocity[Z]                                      0.14504E-29 
c  Pressure     0.13369E-06     488   0.99742E-08   0.12793E+00 0.97939E+03 
c  nu_tilda     0.35231E-05      34   0.12420E-04   0.48564E-06 0.31021E+03 
c  TempC        0.21798E+02      30   0.66834E-03   0.19249E+02 0.45873E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6436          9.3163          4.5729          4.5729
v  Velocity[Y]            -3.9526          7.0864        0.002856        0.002856
v  Velocity[Z]       -6.9287e-015     6.7901e-015    -1.0699e-017    -1.0699e-017
v  ǁVelocityǁ         0.0035055          9.3359          4.8214          4.8214
v  Pressure               -42.244          17.959        0.028388        0.028388
v  nu_tilda           6.0214e-007       0.0042456      0.00064849      0.00064849
v  TempC                       21          73.224            21.3            21.3
v  TurbVisc           1.2428e-013       0.0050037      0.00075035      0.00075035
v  total_pressure     1.0128e+005     1.0134e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP              276:        0.26410E+01

===============================================================


 INSTANT    0.277000000E+03   TIME STEP NUMBER             277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19764E-01 0.88075E+00
   Friction velocity        uk    :  0.19764E-01 0.88075E+00
   Dimensionless distance   yplus :  0.15911E+00 0.70907E+01
   Friction thermal sca.    tstar : -0.11229E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11872E+00 0.52904E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48822E-02      35   0.80486E-03   0.78693E+01 0.17863E+03 
c  Velocity[X]                                      0.41628E+01 
c  Velocity[Y]                                      0.37065E+01 
c  Velocity[Z]                                      0.15349E-29 
c  Pressure     0.12734E-06     505   0.99218E-08   0.12439E+00 0.10161E+04 
c  nu_tilda     0.35272E-05      34   0.15595E-04   0.48421E-06 0.30929E+03 
c  TempC        0.21815E+02      30   0.56014E-03   0.20079E+02 0.45718E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6491          9.3216          4.5729          4.5729
v  Velocity[Y]            -3.9738          7.0677       0.0028851       0.0028851
v  Velocity[Z]       -6.9287e-015      7.079e-015    -1.0756e-017    -1.0756e-017
v  ǁVelocityǁ         0.0045505          9.3409          4.8222          4.8222
v  Pressure               -42.412          17.859       -0.027537       -0.027537
v  nu_tilda           5.9069e-007       0.0042458       0.0006491       0.0006491
v  TempC                       21          73.228            21.3            21.3
v  TurbVisc           1.1565e-013       0.0050039      0.00075113      0.00075113
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              277:        0.31840E+01

===============================================================


 INSTANT    0.278000000E+03   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22879E-01 0.88012E+00
   Friction velocity        uk    :  0.22879E-01 0.88012E+00
   Dimensionless distance   yplus :  0.18419E+00 0.70856E+01
   Friction thermal sca.    tstar : -0.10934E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13743E+00 0.52866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48864E-02      35   0.77954E-03   0.79000E+01 0.17896E+03 
c  Velocity[X]                                      0.41658E+01 
c  Velocity[Y]                                      0.37342E+01 
c  Velocity[Z]                                      0.14601E-29 
c  Pressure     0.16276E-06     473   0.94440E-08   0.15272E+00 0.63819E+03 
c  nu_tilda     0.35313E-05      34   0.12432E-04   0.48280E-06 0.30839E+03 
c  TempC        0.21832E+02      30   0.75622E-03   0.18452E+02 0.45052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6552          9.3271          4.5729          4.5729
v  Velocity[Y]            -3.9957          7.0905       0.0029144       0.0029144
v  Velocity[Z]       -6.9287e-015     7.3041e-015    -1.0808e-017    -1.0808e-017
v  ǁVelocityǁ         0.0046562          9.3457          4.8229          4.8229
v  Pressure               -42.513          17.943      -0.0073826      -0.0073826
v  nu_tilda           5.7892e-007        0.004246       0.0006498       0.0006498
v  TempC                       21          73.246          21.301          21.301
v  TurbVisc            1.071e-013       0.0050041       0.0007519       0.0007519
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              278:        0.30070E+01

===============================================================


 INSTANT    0.279000000E+03   TIME STEP NUMBER             279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21444E-01 0.88216E+00
   Friction velocity        uk    :  0.21444E-01 0.88216E+00
   Dimensionless distance   yplus :  0.17264E+00 0.71020E+01
   Friction thermal sca.    tstar : -0.12777E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12881E+00 0.52989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48906E-02      35   0.79048E-03   0.78988E+01 0.17909E+03 
c  Velocity[X]                                      0.41422E+01 
c  Velocity[Y]                                      0.37566E+01 
c  Velocity[Z]                                      0.13928E-29 
c  Pressure     0.14488E-06     488   0.99328E-08   0.13956E+00 0.49685E+03 
c  nu_tilda     0.35354E-05      34   0.15563E-04   0.48146E-06 0.30749E+03 
c  TempC        0.21849E+02      30   0.65802E-03   0.20027E+02 0.46874E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6587          9.3319          4.5729          4.5729
v  Velocity[Y]            -4.0167          7.1046       0.0029438       0.0029438
v  Velocity[Z]       -6.9287e-015     7.5784e-015    -1.0858e-017    -1.0858e-017
v  ǁVelocityǁ         0.0039406          9.3517          4.8237          4.8237
v  Pressure               -42.666          17.951       -0.036569       -0.036569
v  nu_tilda           5.6657e-007       0.0042462      0.00065041      0.00065041
v  TempC                       21          73.329          21.301          21.301
v  TurbVisc           9.8819e-014       0.0050044      0.00075268      0.00075268
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              279:        0.26460E+01

===============================================================


 INSTANT    0.280000000E+03   TIME STEP NUMBER             280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12880E-01 0.88186E+00
   Friction velocity        uk    :  0.12880E-01 0.88186E+00
   Dimensionless distance   yplus :  0.10369E+00 0.70996E+01
   Friction thermal sca.    tstar : -0.11613E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77367E-01 0.52971E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48948E-02      35   0.79264E-03   0.79505E+01 0.17951E+03 
c  Velocity[X]                                      0.41517E+01 
c  Velocity[Y]                                      0.37988E+01 
c  Velocity[Z]                                      0.13630E-29 
c  Pressure     0.14209E-06     409   0.96474E-08   0.13830E+00 0.47454E+03 
c  nu_tilda     0.35395E-05      34   0.12454E-04   0.48015E-06 0.30661E+03 
c  TempC        0.21866E+02      30   0.59688E-03   0.21708E+02 0.48319E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6644          9.3369          4.5729          4.5729
v  Velocity[Y]            -4.0372          7.0787       0.0029727       0.0029727
v  Velocity[Z]       -6.9287e-015     7.8005e-015    -1.0915e-017    -1.0915e-017
v  ǁVelocityǁ         0.0032321          9.3573          4.8245          4.8245
v  Pressure               -42.756          17.902        -0.04518        -0.04518
v  nu_tilda           5.5337e-007       0.0042464       0.0006511       0.0006511
v  TempC                       21          73.231          21.302          21.302
v  TurbVisc           9.0652e-014       0.0050046      0.00075345      0.00075345
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              280:        0.25830E+01

===============================================================


 INSTANT    0.281000000E+03   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18442E-01 0.88113E+00
   Friction velocity        uk    :  0.18442E-01 0.88113E+00
   Dimensionless distance   yplus :  0.14847E+00 0.70937E+01
   Friction thermal sca.    tstar : -0.13477E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11078E+00 0.52927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48989E-02      35   0.75785E-03   0.79661E+01 0.17977E+03 
c  Velocity[X]                                      0.41528E+01 
c  Velocity[Y]                                      0.38134E+01 
c  Velocity[Z]                                      0.19426E-29 
c  Pressure     0.20092E-06     488   0.98024E-08   0.19457E+00 0.51582E+03 
c  nu_tilda     0.35435E-05      34   0.15524E-04   0.47879E-06 0.30572E+03 
c  TempC        0.21882E+02      30   0.50088E-03   0.18177E+02 0.45439E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6671          9.3407          4.5729          4.5729
v  Velocity[Y]            -4.0575          7.1067       0.0030028       0.0030028
v  Velocity[Z]       -6.9287e-015     8.0021e-015    -1.0959e-017    -1.0959e-017
v  ǁVelocityǁ         0.0012458           9.363          4.8252          4.8252
v  Pressure                -42.93          17.941       -0.072024       -0.072024
v  nu_tilda           5.4002e-007       0.0042466      0.00065171      0.00065171
v  TempC                       21          73.192          21.302          21.302
v  TurbVisc           8.2496e-014       0.0050048      0.00075423      0.00075423
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              281:        0.27800E+01

===============================================================


 INSTANT    0.282000000E+03   TIME STEP NUMBER             282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69823E-02 0.88260E+00
   Friction velocity        uk    :  0.69823E-02 0.88260E+00
   Dimensionless distance   yplus :  0.56212E-01 0.71056E+01
   Friction thermal sca.    tstar : -0.24945E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41940E-01 0.53015E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49031E-02      35   0.80098E-03   0.79590E+01 0.17983E+03 
c  Velocity[X]                                      0.41198E+01 
c  Velocity[Y]                                      0.38392E+01 
c  Velocity[Z]                                      0.15417E-29 
c  Pressure     0.16489E-06     440   0.99772E-08   0.16289E+00 0.33642E+03 
c  nu_tilda     0.35476E-05      34   0.12468E-04   0.47747E-06 0.30485E+03 
c  TempC        0.21899E+02      30   0.86057E-03   0.17986E+02 0.44069E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6724          9.3445          4.5729          4.5729
v  Velocity[Y]            -4.0776          7.0896       0.0030328       0.0030328
v  Velocity[Z]       -6.9287e-015     8.0832e-015    -1.1005e-017    -1.1005e-017
v  ǁVelocityǁ         0.0014626          9.3681           4.826           4.826
v  Pressure               -42.994          17.941       -0.064492       -0.064492
v  nu_tilda           5.2648e-007       0.0042468       0.0006524       0.0006524
v  TempC                       21          73.152          21.303          21.303
v  TurbVisc           7.4816e-014       0.0050051        0.000755        0.000755
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              282:        0.32400E+01

===============================================================


 INSTANT    0.283000000E+03   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10364E-01 0.88220E+00
   Friction velocity        uk    :  0.10364E-01 0.88220E+00
   Dimensionless distance   yplus :  0.83440E-01 0.71024E+01
   Friction thermal sca.    tstar : -0.20766E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62255E-01 0.52991E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49073E-02      35   0.78861E-03   0.79775E+01 0.18009E+03 
c  Velocity[X]                                      0.41042E+01 
c  Velocity[Y]                                      0.38733E+01 
c  Velocity[Z]                                      0.13256E-29 
c  Pressure     0.13351E-06     488   0.93331E-08   0.12777E+00 0.50756E+03 
c  nu_tilda     0.35516E-05      34   0.15469E-04   0.47613E-06 0.30398E+03 
c  TempC        0.21916E+02      31   0.75951E-03   0.30336E+02 0.56330E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6737          9.3484          4.5729          4.5729
v  Velocity[Y]            -4.0976          7.1156       0.0030626       0.0030626
v  Velocity[Z]       -6.9287e-015     8.1727e-015    -1.1053e-017    -1.1053e-017
v  ǁVelocityǁ         0.0011282           9.373          4.8268          4.8268
v  Pressure               -43.154          17.981       -0.090695       -0.090695
v  nu_tilda           5.1313e-007        0.004247      0.00065301      0.00065301
v  TempC                       21          73.193          21.303          21.303
v  TurbVisc           6.7592e-014       0.0050053      0.00075578      0.00075578
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              283:        0.30460E+01

===============================================================


 INSTANT    0.284000000E+03   TIME STEP NUMBER             284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57519E-02 0.88390E+00
   Friction velocity        uk    :  0.57519E-02 0.88390E+00
   Dimensionless distance   yplus :  0.46306E-01 0.71160E+01
   Friction thermal sca.    tstar : -0.22441E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34550E-01 0.53093E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49115E-02      35   0.77855E-03   0.79698E+01 0.18024E+03 
c  Velocity[X]                                      0.40722E+01 
c  Velocity[Y]                                      0.38976E+01 
c  Velocity[Z]                                      0.15347E-29 
c  Pressure     0.11821E-06     456   0.96882E-08   0.11418E+00 0.39949E+03 
c  nu_tilda     0.35557E-05      34   0.12497E-04   0.47487E-06 0.30312E+03 
c  TempC        0.21933E+02      30   0.66307E-03   0.21134E+02 0.48024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6755          9.3515          4.5729          4.5729
v  Velocity[Y]            -4.1169          7.1309       0.0030926       0.0030926
v  Velocity[Z]       -6.9287e-015     7.9809e-015    -1.1094e-017    -1.1094e-017
v  ǁVelocityǁ         0.0013791          9.3779          4.8276          4.8276
v  Pressure               -43.235          18.021       -0.080134       -0.080134
v  nu_tilda           4.9966e-007       0.0042472      0.00065371      0.00065371
v  TempC                       21           73.25          21.304          21.304
v  TurbVisc           6.0992e-014       0.0050055      0.00075655      0.00075655
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              284:        0.26110E+01

===============================================================


 INSTANT    0.285000000E+03   TIME STEP NUMBER             285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82757E-02 0.88407E+00
   Friction velocity        uk    :  0.82757E-02 0.88407E+00
   Dimensionless distance   yplus :  0.66625E-01 0.71173E+01
   Friction thermal sca.    tstar : -0.49521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49710E-01 0.53103E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49156E-02      35   0.78654E-03   0.79955E+01 0.18045E+03 
c  Velocity[X]                                      0.40747E+01 
c  Velocity[Y]                                      0.39208E+01 
c  Velocity[Z]                                      0.14926E-29 
c  Pressure     0.16136E-06     522   0.94094E-08   0.15983E+00 0.74936E+03 
c  nu_tilda     0.35597E-05      34   0.15435E-04   0.47359E-06 0.30227E+03 
c  TempC        0.21950E+02      30   0.51928E-03   0.20829E+02 0.48204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6794          9.3549          4.5729          4.5729
v  Velocity[Y]            -4.1361          7.1113       0.0031233       0.0031233
v  Velocity[Z]       -6.9287e-015     7.9198e-015    -1.1132e-017    -1.1132e-017
v  ǁVelocityǁ         0.0018906          9.3819          4.8284          4.8284
v  Pressure               -43.371          17.955        -0.12398        -0.12398
v  nu_tilda           4.8687e-007       0.0042474      0.00065432      0.00065432
v  TempC                       21          73.307          21.304          21.304
v  TurbVisc           5.4836e-014       0.0050057      0.00075732      0.00075732
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              285:        0.27420E+01

===============================================================


 INSTANT    0.286000000E+03   TIME STEP NUMBER             286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99245E-02 0.88289E+00
   Friction velocity        uk    :  0.99245E-02 0.88289E+00
   Dimensionless distance   yplus :  0.79899E-01 0.71078E+01
   Friction thermal sca.    tstar : -0.32764E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59613E-01 0.53032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49198E-02      35   0.80558E-03   0.80285E+01 0.18079E+03 
c  Velocity[X]                                      0.40704E+01 
c  Velocity[Y]                                      0.39581E+01 
c  Velocity[Z]                                      0.14257E-29 
c  Pressure     0.18561E-06     472   0.93856E-08   0.17800E+00 0.50416E+03 
c  nu_tilda     0.35637E-05      34   0.12525E-04   0.47235E-06 0.30142E+03 
c  TempC        0.21966E+02      30   0.60161E-03   0.17688E+02 0.44179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6787           9.359          4.5729          4.5729
v  Velocity[Y]            -4.1549          7.1295       0.0031535       0.0031535
v  Velocity[Z]       -6.9287e-015     8.0316e-015    -1.1161e-017    -1.1161e-017
v  ǁVelocityǁ         0.0022976          9.3862          4.8291          4.8291
v  Pressure               -43.457          18.023        -0.11063        -0.11063
v  nu_tilda           4.7466e-007       0.0042476      0.00065501      0.00065501
v  TempC                       21          73.356          21.305          21.305
v  TurbVisc           4.9434e-014        0.005006      0.00075809      0.00075809
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              286:        0.25630E+01

===============================================================


 INSTANT    0.287000000E+03   TIME STEP NUMBER             287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63959E-02 0.88464E+00
   Friction velocity        uk    :  0.63959E-02 0.88464E+00
   Dimensionless distance   yplus :  0.51491E-01 0.71220E+01
   Friction thermal sca.    tstar : -0.21440E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38418E-01 0.53138E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49240E-02      35   0.77775E-03   0.80563E+01 0.18112E+03 
c  Velocity[X]                                      0.40662E+01 
c  Velocity[Y]                                      0.39900E+01 
c  Velocity[Z]                                      0.15746E-29 
c  Pressure     0.14666E-06     520   0.99746E-08   0.14314E+00 0.81168E+03 
c  nu_tilda     0.35677E-05      34   0.15411E-04   0.47110E-06 0.30059E+03 
c  TempC        0.21983E+02      30   0.85605E-03   0.19277E+02 0.46590E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6808          9.3638          4.5729          4.5729
v  Velocity[Y]            -4.1736          7.1168        0.003185        0.003185
v  Velocity[Z]       -6.9287e-015     8.0187e-015     -1.118e-017     -1.118e-017
v  ǁVelocityǁ          0.002485            9.39          4.8299          4.8299
v  Pressure               -43.592          17.949        -0.15796        -0.15796
v  nu_tilda           4.6265e-007       0.0042478      0.00065562      0.00065562
v  TempC                       21          73.205          21.306          21.306
v  TurbVisc           4.4657e-014       0.0050062      0.00075887      0.00075887
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              287:        0.28710E+01

===============================================================


 INSTANT    0.288000000E+03   TIME STEP NUMBER             288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11617E-01 0.88443E+00
   Friction velocity        uk    :  0.11617E-01 0.88443E+00
   Dimensionless distance   yplus :  0.93524E-01 0.71202E+01
   Friction thermal sca.    tstar : -0.15133E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69779E-01 0.53125E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49281E-02      35   0.80027E-03   0.80403E+01 0.18105E+03 
c  Velocity[X]                                      0.40341E+01 
c  Velocity[Y]                                      0.40062E+01 
c  Velocity[Z]                                      0.14346E-29 
c  Pressure     0.17413E-06     537   0.97483E-08   0.16592E+00 0.12127E+04 
c  nu_tilda     0.35716E-05      34   0.12538E-04   0.46984E-06 0.29975E+03 
c  TempC        0.22000E+02      30   0.60440E-03   0.24932E+02 0.54685E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6803           9.368          4.5729          4.5729
v  Velocity[Y]            -4.1916          7.1483       0.0032155       0.0032155
v  Velocity[Z]       -6.9287e-015     7.9346e-015    -1.1201e-017    -1.1201e-017
v  ǁVelocityǁ         0.0029438          9.3933          4.8307          4.8307
v  Pressure               -43.666           18.12        -0.11374        -0.11374
v  nu_tilda           4.5049e-007       0.0042479      0.00065631      0.00065631
v  TempC                       21          73.058          21.306          21.306
v  TurbVisc           4.0306e-014       0.0050064      0.00075964      0.00075964
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              288:        0.28540E+01

===============================================================


 INSTANT    0.289000000E+03   TIME STEP NUMBER             289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15381E-01 0.88610E+00
   Friction velocity        uk    :  0.15381E-01 0.88610E+00
   Dimensionless distance   yplus :  0.12383E+00 0.71337E+01
   Friction thermal sca.    tstar : -0.11822E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92390E-01 0.53226E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49323E-02      35   0.81035E-03   0.80376E+01 0.18119E+03 
c  Velocity[X]                                      0.39933E+01 
c  Velocity[Y]                                      0.40444E+01 
c  Velocity[Z]                                      0.13790E-29 
c  Pressure     0.13895E-06     505   0.92734E-08   0.13199E+00 0.70959E+03 
c  nu_tilda     0.35756E-05      34   0.15361E-04   0.46857E-06 0.29892E+03 
c  TempC        0.22016E+02      30   0.54223E-03   0.19408E+02 0.47153E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6797          9.3722          4.5729          4.5729
v  Velocity[Y]            -4.2089          7.1609       0.0032469       0.0032469
v  Velocity[Z]       -6.9287e-015     7.9022e-015    -1.1222e-017    -1.1222e-017
v  ǁVelocityǁ         0.0030743          9.3969          4.8315          4.8315
v  Pressure               -43.806          18.073        -0.15804        -0.15804
v  nu_tilda           4.3817e-007       0.0042481      0.00065692      0.00065692
v  TempC                       21          73.161          21.307          21.307
v  TurbVisc           3.6234e-014       0.0050066      0.00076042      0.00076042
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              289:        0.26530E+01

===============================================================


 INSTANT    0.290000000E+03   TIME STEP NUMBER             290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17303E-01 0.88634E+00
   Friction velocity        uk    :  0.17303E-01 0.88634E+00
   Dimensionless distance   yplus :  0.13930E+00 0.71356E+01
   Friction thermal sca.    tstar : -0.10615E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10393E+00 0.53240E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49364E-02      35   0.78173E-03   0.81058E+01 0.18166E+03 
c  Velocity[X]                                      0.40429E+01 
c  Velocity[Y]                                      0.40630E+01 
c  Velocity[Z]                                      0.13679E-29 
c  Pressure     0.19192E-06     329   0.97316E-08   0.18667E+00 0.36115E+03 
c  nu_tilda     0.35796E-05      34   0.12568E-04   0.46735E-06 0.29810E+03 
c  TempC        0.22033E+02      30   0.49006E-03   0.17184E+02 0.44175E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6799          9.3754          4.5729          4.5729
v  Velocity[Y]            -4.2269          7.1394       0.0032781       0.0032781
v  Velocity[Z]       -6.9287e-015     7.8647e-015    -1.1236e-017    -1.1236e-017
v  ǁVelocityǁ         0.0022835          9.3996          4.8323          4.8323
v  Pressure               -43.873          18.052        -0.16103        -0.16103
v  nu_tilda           4.2556e-007       0.0042483      0.00065761      0.00065761
v  TempC                       21          73.024          21.307          21.307
v  TurbVisc            3.243e-014       0.0050068      0.00076119      0.00076119
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              290:        0.23430E+01

===============================================================


 INSTANT    0.291000000E+03   TIME STEP NUMBER             291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14548E-01 0.88550E+00
   Friction velocity        uk    :  0.14548E-01 0.88550E+00
   Dimensionless distance   yplus :  0.11712E+00 0.71289E+01
   Friction thermal sca.    tstar : -0.95322E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87387E-01 0.53189E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49406E-02      35   0.79161E-03   0.80632E+01 0.18152E+03 
c  Velocity[X]                                      0.39826E+01 
c  Velocity[Y]                                      0.40806E+01 
c  Velocity[Z]                                      0.13024E-29 
c  Pressure     0.13506E-06     394   0.95287E-08   0.12922E+00 0.61409E+03 
c  nu_tilda     0.35835E-05      34   0.15349E-04   0.46612E-06 0.29728E+03 
c  TempC        0.22050E+02      30   0.77661E-03   0.16947E+02 0.45341E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6771           9.379          4.5729          4.5729
v  Velocity[Y]            -4.2441          7.1702       0.0033102       0.0033102
v  Velocity[Z]       -6.9287e-015     7.8264e-015    -1.1239e-017    -1.1239e-017
v  ǁVelocityǁ          0.002044          9.4028          4.8331          4.8331
v  Pressure               -44.015          18.135        -0.17393        -0.17393
v  nu_tilda           4.1289e-007       0.0042485      0.00065822      0.00065822
v  TempC                       21              73          21.308          21.308
v  TurbVisc           2.8855e-014        0.005007      0.00076196      0.00076196
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              291:        0.25080E+01

===============================================================


 INSTANT    0.292000000E+03   TIME STEP NUMBER             292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12011E-01 0.88689E+00
   Friction velocity        uk    :  0.12011E-01 0.88689E+00
   Dimensionless distance   yplus :  0.96699E-01 0.71401E+01
   Friction thermal sca.    tstar : -0.80769E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72148E-01 0.53273E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49448E-02      35   0.81280E-03   0.80917E+01 0.18174E+03 
c  Velocity[X]                                      0.39697E+01 
c  Velocity[Y]                                      0.41220E+01 
c  Velocity[Z]                                      0.13335E-29 
c  Pressure     0.17584E-06     360   0.94944E-08   0.16952E+00 0.37610E+03 
c  nu_tilda     0.35874E-05      34   0.12589E-04   0.46491E-06 0.29647E+03 
c  TempC        0.22066E+02      30   0.54975E-03   0.21889E+02 0.51459E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6774          9.3813          4.5729          4.5729
v  Velocity[Y]            -4.2608          7.1474       0.0033413       0.0033413
v  Velocity[Z]       -6.9287e-015     7.6001e-015    -1.1248e-017    -1.1248e-017
v  ǁVelocityǁ         0.0032654          9.4072          4.8339          4.8339
v  Pressure               -44.046          18.103         -0.1738         -0.1738
v  nu_tilda           4.0012e-007       0.0042486      0.00065891      0.00065891
v  TempC                       21          73.027          21.309          21.309
v  TurbVisc           2.5568e-014       0.0050072      0.00076273      0.00076273
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              292:        0.23390E+01

===============================================================


 INSTANT    0.293000000E+03   TIME STEP NUMBER             293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82225E-02 0.88665E+00
   Friction velocity        uk    :  0.82225E-02 0.88665E+00
   Dimensionless distance   yplus :  0.66197E-01 0.71381E+01
   Friction thermal sca.    tstar : -0.77709E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49390E-01 0.53258E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49489E-02      35   0.74331E-03   0.80996E+01 0.18191E+03 
c  Velocity[X]                                      0.39588E+01 
c  Velocity[Y]                                      0.41408E+01 
c  Velocity[Z]                                      0.16161E-29 
c  Pressure     0.12769E-06     426   0.99302E-08   0.12073E+00 0.53626E+03 
c  nu_tilda     0.35913E-05      34   0.15290E-04   0.46365E-06 0.29566E+03 
c  TempC        0.22083E+02      30   0.54980E-03   0.18376E+02 0.47045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6736          9.3835          4.5729          4.5729
v  Velocity[Y]            -4.2773          7.1806       0.0033733       0.0033733
v  Velocity[Z]       -6.9287e-015     7.5032e-015    -1.1261e-017    -1.1261e-017
v  ǁVelocityǁ          0.000719          9.4108          4.8347          4.8347
v  Pressure                -44.19          18.165        -0.19399        -0.19399
v  nu_tilda            3.873e-007       0.0042488      0.00065952      0.00065952
v  TempC                       21          73.083          21.309          21.309
v  TurbVisc            2.255e-014       0.0050075      0.00076351      0.00076351
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              293:        0.24120E+01

===============================================================


 INSTANT    0.294000000E+03   TIME STEP NUMBER             294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92596E-02 0.88858E+00
   Friction velocity        uk    :  0.92596E-02 0.88858E+00
   Dimensionless distance   yplus :  0.74546E-01 0.71537E+01
   Friction thermal sca.    tstar : -0.91045E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55620E-01 0.53375E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49531E-02      35   0.79623E-03   0.80736E+01 0.18183E+03 
c  Velocity[X]                                      0.39191E+01 
c  Velocity[Y]                                      0.41545E+01 
c  Velocity[Z]                                      0.16031E-29 
c  Pressure     0.17756E-06     469   0.99980E-08   0.17061E+00 0.47782E+03 
c  nu_tilda     0.35952E-05      34   0.12605E-04   0.46244E-06 0.29486E+03 
c  TempC        0.22100E+02      30   0.59657E-03   0.17440E+02 0.45979E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6715          9.3858          4.5729          4.5729
v  Velocity[Y]            -4.2938          7.1987       0.0034055       0.0034055
v  Velocity[Z]       -6.9287e-015     8.0788e-015    -1.1263e-017    -1.1263e-017
v  ǁVelocityǁ         0.0015802          9.4141          4.8355          4.8355
v  Pressure               -44.253          18.239        -0.17998        -0.17998
v  nu_tilda           3.7438e-007        0.004249      0.00066021      0.00066021
v  TempC                       21           73.17           21.31           21.31
v  TurbVisc           1.9796e-014       0.0050077      0.00076428      0.00076428
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              294:        0.25650E+01

===============================================================


 INSTANT    0.295000000E+03   TIME STEP NUMBER             295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12911E-01 0.88845E+00
   Friction velocity        uk    :  0.12911E-01 0.88845E+00
   Dimensionless distance   yplus :  0.10395E+00 0.71527E+01
   Friction thermal sca.    tstar : -0.28134E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77555E-01 0.53367E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49572E-02      35   0.79154E-03   0.81463E+01 0.18225E+03 
c  Velocity[X]                                      0.39506E+01 
c  Velocity[Y]                                      0.41957E+01 
c  Velocity[Z]                                      0.13958E-29 
c  Pressure     0.19866E-06     522   0.94480E-08   0.19145E+00 0.79221E+03 
c  nu_tilda     0.35991E-05      34   0.15267E-04   0.46121E-06 0.29407E+03 
c  TempC        0.22116E+02      30   0.77185E-03   0.17028E+02 0.45485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6677          9.3874          4.5729          4.5729
v  Velocity[Y]            -4.3094          7.1719       0.0034384       0.0034384
v  Velocity[Z]       -6.9287e-015     7.4261e-015    -1.1254e-017    -1.1254e-017
v  ǁVelocityǁ        0.00038247          9.4173          4.8363          4.8363
v  Pressure               -44.355          18.161        -0.22461        -0.22461
v  nu_tilda           3.6123e-007       0.0042492      0.00066082      0.00066082
v  TempC                       21          73.069          21.311          21.311
v  TurbVisc           1.7283e-014       0.0050079      0.00076505      0.00076505
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              295:        0.27230E+01

===============================================================


 INSTANT    0.296000000E+03   TIME STEP NUMBER             296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33376E-02 0.88759E+00
   Friction velocity        uk    :  0.33376E-02 0.88759E+00
   Dimensionless distance   yplus :  0.26870E-01 0.71457E+01
   Friction thermal sca.    tstar : -0.14036E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20048E-01 0.53315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49613E-02      35   0.78610E-03   0.81376E+01 0.18239E+03 
c  Velocity[X]                                      0.39193E+01 
c  Velocity[Y]                                      0.42183E+01 
c  Velocity[Z]                                      0.14754E-29 
c  Pressure     0.11663E-06     489   0.95746E-08   0.11166E+00 0.83027E+03 
c  nu_tilda     0.36030E-05      34   0.12634E-04   0.46002E-06 0.29328E+03 
c  TempC        0.22133E+02      30   0.65628E-03   0.19420E+02 0.50263E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.665          9.3893          4.5729          4.5729
v  Velocity[Y]            -4.3244           7.199       0.0034701       0.0034701
v  Velocity[Z]       -6.9287e-015     7.3804e-015    -1.1246e-017    -1.1246e-017
v  ǁVelocityǁ        0.00018584          9.4196          4.8371          4.8371
v  Pressure               -44.409            18.3        -0.19662        -0.19662
v  nu_tilda           3.4792e-007       0.0042493      0.00066151      0.00066151
v  TempC                       21          73.075          21.311          21.311
v  TurbVisc           1.4979e-014       0.0050081      0.00076582      0.00076582
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              296:        0.26340E+01

===============================================================


 INSTANT    0.297000000E+03   TIME STEP NUMBER             297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47843E-02 0.88930E+00
   Friction velocity        uk    :  0.47843E-02 0.88930E+00
   Dimensionless distance   yplus :  0.38517E-01 0.71595E+01
   Friction thermal sca.    tstar : -0.10401E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28738E-01 0.53418E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49655E-02      35   0.79121E-03   0.81105E+01 0.18228E+03 
c  Velocity[X]                                      0.38805E+01 
c  Velocity[Y]                                      0.42300E+01 
c  Velocity[Z]                                      0.13339E-29 
c  Pressure     0.13376E-06     520   0.99158E-08   0.12953E+00 0.85509E+03 
c  nu_tilda     0.36069E-05      34   0.15222E-04   0.45882E-06 0.29249E+03 
c  TempC        0.22149E+02      30   0.57791E-03   0.17793E+02 0.46850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6594          9.3906          4.5729          4.5729
v  Velocity[Y]            -4.3406          7.1857       0.0035033       0.0035033
v  Velocity[Z]       -6.9287e-015     7.3732e-015     -1.123e-017     -1.123e-017
v  ǁVelocityǁ         0.0014482          9.4226          4.8379          4.8379
v  Pressure               -44.522          18.225        -0.24664        -0.24664
v  nu_tilda           3.3455e-007       0.0042495      0.00066212      0.00066212
v  TempC                       21          73.068          21.312          21.312
v  TurbVisc           1.2891e-014       0.0050083       0.0007666       0.0007666
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              297:        0.29880E+01

===============================================================


 INSTANT    0.298000000E+03   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13410E-01 0.88890E+00
   Friction velocity        uk    :  0.13410E-01 0.88890E+00
   Dimensionless distance   yplus :  0.10796E+00 0.71563E+01
   Friction thermal sca.    tstar : -0.80189E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80552E-01 0.53394E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49696E-02      35   0.79835E-03   0.81319E+01 0.18241E+03 
c  Velocity[X]                                      0.38698E+01 
c  Velocity[Y]                                      0.42622E+01 
c  Velocity[Z]                                      0.14341E-29 
c  Pressure     0.15713E-06     505   0.96846E-08   0.14792E+00 0.97925E+03 
c  nu_tilda     0.36108E-05      34   0.12651E-04   0.45764E-06 0.29172E+03 
c  TempC        0.22166E+02      30   0.58768E-03   0.17021E+02 0.46670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6566          9.3936          4.5729          4.5729
v  Velocity[Y]            -4.3551          7.2113       0.0035367       0.0035367
v  Velocity[Z]       -6.9287e-015     7.2965e-015     -1.121e-017     -1.121e-017
v  ǁVelocityǁ        0.00093706          9.4245          4.8388          4.8388
v  Pressure               -44.563          18.378        -0.21059        -0.21059
v  nu_tilda            3.212e-007       0.0042497      0.00066281      0.00066281
v  TempC                       21          73.086          21.313          21.313
v  TurbVisc            1.102e-014       0.0050085      0.00076737      0.00076737
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              298:        0.29880E+01

===============================================================


 INSTANT    0.299000000E+03   TIME STEP NUMBER             299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39776E-02 0.89075E+00
   Friction velocity        uk    :  0.39776E-02 0.89075E+00
   Dimensionless distance   yplus :  0.32023E-01 0.71712E+01
   Friction thermal sca.    tstar : -0.13829E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23892E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49738E-02      35   0.78360E-03   0.81070E+01 0.18242E+03 
c  Velocity[X]                                      0.38310E+01 
c  Velocity[Y]                                      0.42759E+01 
c  Velocity[Z]                                      0.16370E-29 
c  Pressure     0.11335E-06     490   0.93378E-08   0.10780E+00 0.63090E+03 
c  nu_tilda     0.36146E-05      34   0.15176E-04   0.45640E-06 0.29094E+03 
c  TempC        0.22182E+02      30   0.10927E-02   0.14388E+02 0.43420E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6502          9.3962          4.5729          4.5729
v  Velocity[Y]            -4.3691          7.2312       0.0035695       0.0035695
v  Velocity[Z]       -6.9287e-015     7.7385e-015    -1.1188e-017    -1.1188e-017
v  ǁVelocityǁ         0.0017271          9.4265          4.8396          4.8396
v  Pressure               -44.677           18.36        -0.25202        -0.25202
v  nu_tilda           3.0795e-007       0.0042498      0.00066341      0.00066341
v  TempC                       21          73.687          21.314          21.314
v  TurbVisc           9.3641e-015       0.0050087      0.00076814      0.00076814
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              299:        0.26250E+01

===============================================================


 INSTANT    0.300000000E+03   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48495E-02 0.89105E+00
   Friction velocity        uk    :  0.48495E-02 0.89105E+00
   Dimensionless distance   yplus :  0.39041E-01 0.71735E+01
   Friction thermal sca.    tstar : -0.23628E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29129E-01 0.53523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49779E-02      35   0.77799E-03   0.81271E+01 0.18251E+03 
c  Velocity[X]                                      0.38343E+01 
c  Velocity[Y]                                      0.42929E+01 
c  Velocity[Z]                                      0.12630E-29 
c  Pressure     0.16344E-06     426   0.92964E-08   0.16052E+00 0.39254E+03 
c  nu_tilda     0.36184E-05      34   0.12675E-04   0.45521E-06 0.29017E+03 
c  TempC        0.22199E+02      30   0.55742E-03   0.19643E+02 0.50247E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6458          9.3985          4.5729          4.5729
v  Velocity[Y]            -4.3834          7.2095       0.0036028       0.0036028
v  Velocity[Z]       -6.9287e-015     7.0387e-015    -1.1159e-017    -1.1159e-017
v  ǁVelocityǁ         0.0011502          9.4281          4.8404          4.8404
v  Pressure                -44.71          18.391         -0.2387         -0.2387
v  nu_tilda           2.9473e-007         0.00425       0.0006641       0.0006641
v  TempC                       21          73.088          21.315          21.315
v  TurbVisc           7.9122e-015       0.0050089      0.00076891      0.00076891
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              300:        0.25400E+01

===============================================================


 INSTANT    0.301000000E+03   TIME STEP NUMBER             301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69282E-02 0.88990E+00
   Friction velocity        uk    :  0.69282E-02 0.88990E+00
   Dimensionless distance   yplus :  0.55777E-01 0.71643E+01
   Friction thermal sca.    tstar : -0.15154E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41616E-01 0.53453E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49820E-02      35   0.79548E-03   0.81396E+01 0.18266E+03 
c  Velocity[X]                                      0.38141E+01 
c  Velocity[Y]                                      0.43255E+01 
c  Velocity[Z]                                      0.15230E-29 
c  Pressure     0.13113E-06     489   0.96985E-08   0.12438E+00 0.50344E+03 
c  nu_tilda     0.36223E-05      34   0.15138E-04   0.45399E-06 0.28940E+03 
c  TempC        0.22215E+02      30   0.60079E-03   0.15247E+02 0.45001E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6388          9.4004          4.5729          4.5729
v  Velocity[Y]            -4.3975          7.2319       0.0036362       0.0036362
v  Velocity[Z]       -6.9287e-015     6.9377e-015    -1.1122e-017    -1.1122e-017
v  ǁVelocityǁ        0.00064955          9.4293          4.8412          4.8412
v  Pressure               -44.819          18.418        -0.27167        -0.27167
v  nu_tilda           2.8158e-007       0.0042502      0.00066471      0.00066471
v  TempC                       21          73.091          21.315          21.315
v  TurbVisc           6.6385e-015        0.005009      0.00076969      0.00076969
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              301:        0.32460E+01

===============================================================


 INSTANT    0.302000000E+03   TIME STEP NUMBER             302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82531E-02 0.89154E+00
   Friction velocity        uk    :  0.82531E-02 0.89154E+00
   Dimensionless distance   yplus :  0.66443E-01 0.71775E+01
   Friction thermal sca.    tstar : -0.95947E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49574E-01 0.53552E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49861E-02      35   0.80716E-03   0.81508E+01 0.18280E+03 
c  Velocity[X]                                      0.38136E+01 
c  Velocity[Y]                                      0.43372E+01 
c  Velocity[Z]                                      0.13633E-29 
c  Pressure     0.14241E-06     393   0.96777E-08   0.13842E+00 0.32150E+03 
c  nu_tilda     0.36261E-05      34   0.12690E-04   0.45282E-06 0.28864E+03 
c  TempC        0.22232E+02      30   0.61023E-03   0.15633E+02 0.45890E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6323          9.4021          4.5729          4.5729
v  Velocity[Y]            -4.4105          7.2162         0.00367         0.00367
v  Velocity[Z]       -6.9287e-015     6.8377e-015    -1.1079e-017    -1.1079e-017
v  ǁVelocityǁ        0.00073655          9.4305           4.842           4.842
v  Pressure               -44.851          18.423        -0.26674        -0.26674
v  nu_tilda           2.6856e-007       0.0042503       0.0006654       0.0006654
v  TempC                       21            73.1          21.316          21.316
v  TurbVisc           5.5308e-015       0.0050092      0.00077045      0.00077045
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              302:        0.29040E+01

===============================================================


 INSTANT    0.303000000E+03   TIME STEP NUMBER             303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36108E-02 0.89126E+00
   Friction velocity        uk    :  0.36108E-02 0.89126E+00
   Dimensionless distance   yplus :  0.29070E-01 0.71752E+01
   Friction thermal sca.    tstar : -0.18907E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21689E-01 0.53535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49903E-02      35   0.79273E-03   0.81159E+01 0.18261E+03 
c  Velocity[X]                                      0.37683E+01 
c  Velocity[Y]                                      0.43476E+01 
c  Velocity[Z]                                      0.13768E-29 
c  Pressure     0.12511E-06     410   0.94760E-08   0.11933E+00 0.52259E+03 
c  nu_tilda     0.36299E-05      34   0.15112E-04   0.45163E-06 0.28789E+03 
c  TempC        0.22248E+02      30   0.68245E-03   0.17096E+02 0.46506E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6256          9.4031          4.5729          4.5729
v  Velocity[Y]            -4.4233          7.2494       0.0037041       0.0037041
v  Velocity[Z]       -6.9287e-015     6.7649e-015    -1.1034e-017    -1.1034e-017
v  ǁVelocityǁ         0.0009361          9.4314          4.8429          4.8429
v  Pressure                -44.94          18.504        -0.28479        -0.28479
v  nu_tilda           2.5562e-007       0.0042505      0.00066601      0.00066601
v  TempC                       21          73.114          21.317          21.317
v  TurbVisc           4.5763e-015       0.0050094      0.00077123      0.00077123
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              303:        0.26810E+01

===============================================================


 INSTANT    0.304000000E+03   TIME STEP NUMBER             304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77288E-02 0.89288E+00
   Friction velocity        uk    :  0.77288E-02 0.89288E+00
   Dimensionless distance   yplus :  0.62222E-01 0.71883E+01
   Friction thermal sca.    tstar : -0.97604E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46425E-01 0.53633E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49944E-02      35   0.81055E-03   0.81098E+01 0.18262E+03 
c  Velocity[X]                                      0.37326E+01 
c  Velocity[Y]                                      0.43772E+01 
c  Velocity[Z]                                      0.13307E-29 
c  Pressure     0.13045E-06     489   0.98758E-08   0.12481E+00 0.53117E+03 
c  nu_tilda     0.36337E-05      34   0.12702E-04   0.45047E-06 0.28714E+03 
c  TempC        0.22264E+02      30   0.68274E-03   0.15639E+02 0.46096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6182          9.4041          4.5729          4.5729
v  Velocity[Y]            -4.4366          7.2593       0.0037379       0.0037379
v  Velocity[Z]       -6.9287e-015     7.1858e-015     -1.099e-017     -1.099e-017
v  ǁVelocityǁ        0.00076751           9.433          4.8437          4.8437
v  Pressure               -44.975          18.581        -0.26667        -0.26667
v  nu_tilda           2.4276e-007       0.0042506       0.0006667       0.0006667
v  TempC                       21          73.511          21.318          21.318
v  TurbVisc           3.7562e-015       0.0050096        0.000772        0.000772
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              304:        0.26330E+01

===============================================================


 INSTANT    0.305000000E+03   TIME STEP NUMBER             305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70281E-02 0.89300E+00
   Friction velocity        uk    :  0.70281E-02 0.89300E+00
   Dimensionless distance   yplus :  0.56581E-01 0.71893E+01
   Friction thermal sca.    tstar : -0.29825E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42216E-01 0.53640E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49985E-02      35   0.75212E-03   0.81416E+01 0.18285E+03 
c  Velocity[X]                                      0.37450E+01 
c  Velocity[Y]                                      0.43966E+01 
c  Velocity[Z]                                      0.15214E-29 
c  Pressure     0.15487E-06     504   0.99670E-08   0.15002E+00 0.82009E+03 
c  nu_tilda     0.36374E-05      34   0.15063E-04   0.44927E-06 0.28640E+03 
c  TempC        0.22281E+02      30   0.53487E-03   0.16293E+02 0.45437E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6117          9.4044          4.5729          4.5729
v  Velocity[Y]            -4.4489          7.2401       0.0037717       0.0037717
v  Velocity[Z]       -6.9287e-015     6.6655e-015    -1.0941e-017    -1.0941e-017
v  ǁVelocityǁ        0.00053773           9.435          4.8445          4.8445
v  Pressure               -45.056          18.501        -0.31437        -0.31437
v  nu_tilda           2.2992e-007       0.0042508      0.00066731      0.00066731
v  TempC                       21           73.18          21.319          21.319
v  TurbVisc           3.0556e-015       0.0050098      0.00077277      0.00077277
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              305:        0.26590E+01

===============================================================


 INSTANT    0.306000000E+03   TIME STEP NUMBER             306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70497E-02 0.89228E+00
   Friction velocity        uk    :  0.70497E-02 0.89228E+00
   Dimensionless distance   yplus :  0.56755E-01 0.71835E+01
   Friction thermal sca.    tstar : -0.14005E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42346E-01 0.53597E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50026E-02      35   0.78952E-03   0.81034E+01 0.18261E+03 
c  Velocity[X]                                      0.37061E+01 
c  Velocity[Y]                                      0.43973E+01 
c  Velocity[Z]                                      0.13801E-29 
c  Pressure     0.14029E-06     520   0.98297E-08   0.13638E+00 0.10159E+04 
c  nu_tilda     0.36412E-05      34   0.12722E-04   0.44809E-06 0.28565E+03 
c  TempC        0.22297E+02      30   0.59691E-03   0.14785E+02 0.43974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6021          9.4049          4.5729          4.5729
v  Velocity[Y]            -4.4612          7.2667       0.0038057       0.0038057
v  Velocity[Z]       -6.9287e-015     6.5534e-015    -1.0889e-017    -1.0889e-017
v  ǁVelocityǁ        0.00090161           9.436          4.8454          4.8454
v  Pressure               -45.095          18.663        -0.27823        -0.27823
v  nu_tilda           2.1716e-007        0.004251        0.000668        0.000668
v  TempC                       21          73.184           21.32           21.32
v  TurbVisc           2.4585e-015         0.00501      0.00077354      0.00077354
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              306:        0.29990E+01

===============================================================


 INSTANT    0.307000000E+03   TIME STEP NUMBER             307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64843E-02 0.89355E+00
   Friction velocity        uk    :  0.64843E-02 0.89355E+00
   Dimensionless distance   yplus :  0.52203E-01 0.71937E+01
   Friction thermal sca.    tstar : -0.11523E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38949E-01 0.53673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50067E-02      35   0.81403E-03   0.81312E+01 0.18275E+03 
c  Velocity[X]                                      0.37028E+01 
c  Velocity[Y]                                      0.44284E+01 
c  Velocity[Z]                                      0.14379E-29 
c  Pressure     0.15404E-06     522   0.98383E-08   0.14753E+00 0.10299E+04 
c  nu_tilda     0.36450E-05      34   0.15015E-04   0.44689E-06 0.28491E+03 
c  TempC        0.22313E+02      30   0.80950E-03   0.14816E+02 0.44389E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5938          9.4044          4.5729          4.5729
v  Velocity[Y]             -4.473          7.2461       0.0038412       0.0038412
v  Velocity[Z]       -6.9287e-015     6.5508e-015    -1.0837e-017    -1.0837e-017
v  ǁVelocityǁ       5.3806e-005          9.4374          4.8462          4.8462
v  Pressure               -45.162          18.553        -0.33486        -0.33486
v  nu_tilda           2.0454e-007       0.0042511       0.0006686       0.0006686
v  TempC                       21          73.588          21.321          21.321
v  TurbVisc           1.9564e-015       0.0050102      0.00077432      0.00077432
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              307:        0.31480E+01

===============================================================


 INSTANT    0.308000000E+03   TIME STEP NUMBER             308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82479E-02 0.89328E+00
   Friction velocity        uk    :  0.82479E-02 0.89328E+00
   Dimensionless distance   yplus :  0.66401E-01 0.71915E+01
   Friction thermal sca.    tstar : -0.19434E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49543E-01 0.53657E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50108E-02      35   0.77503E-03   0.81152E+01 0.18271E+03 
c  Velocity[X]                                      0.36845E+01 
c  Velocity[Y]                                      0.44307E+01 
c  Velocity[Z]                                      0.15221E-29 
c  Pressure     0.11701E-06     521   0.96243E-08   0.11267E+00 0.96140E+03 
c  nu_tilda     0.36487E-05      34   0.12742E-04   0.44577E-06 0.28418E+03 
c  TempC        0.22330E+02      30   0.59917E-03   0.19385E+02 0.49186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5848          9.4043          4.5729          4.5729
v  Velocity[Y]            -4.4842          7.2761       0.0038749       0.0038749
v  Velocity[Z]       -6.9287e-015     6.5625e-015    -1.0783e-017    -1.0783e-017
v  ǁVelocityǁ        0.00069307           9.438           4.847           4.847
v  Pressure               -45.186          18.709        -0.30076        -0.30076
v  nu_tilda           1.9209e-007       0.0042513      0.00066929      0.00066929
v  TempC                       21          73.205          21.323          21.323
v  TurbVisc           1.5398e-015       0.0050104      0.00077508      0.00077508
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              308:        0.28080E+01

===============================================================


 INSTANT    0.309000000E+03   TIME STEP NUMBER             309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77693E-02 0.89488E+00
   Friction velocity        uk    :  0.77693E-02 0.89488E+00
   Dimensionless distance   yplus :  0.62548E-01 0.72044E+01
   Friction thermal sca.    tstar : -0.28384E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46668E-01 0.53753E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50149E-02      35   0.78533E-03   0.80556E+01 0.18236E+03 
c  Velocity[X]                                      0.36187E+01 
c  Velocity[Y]                                      0.44369E+01 
c  Velocity[Z]                                      0.13709E-29 
c  Pressure     0.13320E-06     474   0.96008E-08   0.12938E+00 0.45145E+03 
c  nu_tilda     0.36524E-05      34   0.14978E-04   0.44458E-06 0.28345E+03 
c  TempC        0.22346E+02      30   0.47180E-03   0.15185E+02 0.44271E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.576          9.4039          4.5729          4.5729
v  Velocity[Y]             -4.495          7.2938         0.00391         0.00391
v  Velocity[Z]       -6.9287e-015     6.5468e-015    -1.0727e-017    -1.0727e-017
v  ǁVelocityǁ        0.00060243          9.4386          4.8479          4.8479
v  Pressure               -45.273          18.735         -0.3269         -0.3269
v  nu_tilda           1.8007e-007       0.0042514       0.0006699       0.0006699
v  TempC                       21          73.218          21.324          21.324
v  TurbVisc           1.1978e-015       0.0050105      0.00077586      0.00077586
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              309:        0.25560E+01

===============================================================


 INSTANT    0.310000000E+03   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46492E-02 0.89454E+00
   Friction velocity        uk    :  0.46492E-02 0.89454E+00
   Dimensionless distance   yplus :  0.37429E-01 0.72017E+01
   Friction thermal sca.    tstar : -0.58160E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27926E-01 0.53732E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50190E-02      35   0.78871E-03   0.80898E+01 0.18255E+03 
c  Velocity[X]                                      0.36216E+01 
c  Velocity[Y]                                      0.44682E+01 
c  Velocity[Z]                                      0.13828E-29 
c  Pressure     0.11787E-06     394   0.92668E-08   0.11539E+00 0.41297E+03 
c  nu_tilda     0.36562E-05      34   0.12750E-04   0.44346E-06 0.28273E+03 
c  TempC        0.22362E+02      30   0.56919E-03   0.13483E+02 0.41441E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5668          9.4049          4.5729          4.5729
v  Velocity[Y]             -4.506           7.263        0.003945        0.003945
v  Velocity[Z]       -6.9287e-015      6.467e-015     -1.067e-017     -1.067e-017
v  ǁVelocityǁ        0.00050986          9.4388          4.8487          4.8487
v  Pressure                -45.28          18.699        -0.33112        -0.33112
v  nu_tilda           1.6867e-007       0.0042516      0.00067059      0.00067059
v  TempC                       21          73.272          21.325          21.325
v  TurbVisc           9.2498e-016       0.0050107      0.00077663      0.00077663
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              310:        0.23540E+01

===============================================================


 INSTANT    0.311000000E+03   TIME STEP NUMBER             311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66847E-02 0.89349E+00
   Friction velocity        uk    :  0.66847E-02 0.89349E+00
   Dimensionless distance   yplus :  0.53816E-01 0.71932E+01
   Friction thermal sca.    tstar : -0.14901E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40153E-01 0.53669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50231E-02      35   0.74877E-03   0.80601E+01 0.18236E+03 
c  Velocity[X]                                      0.35990E+01 
c  Velocity[Y]                                      0.44612E+01 
c  Velocity[Z]                                      0.15617E-29 
c  Pressure     0.13505E-06     346   0.94815E-08   0.12893E+00 0.59951E+03 
c  nu_tilda     0.36599E-05      34   0.14942E-04   0.44227E-06 0.28201E+03 
c  TempC        0.22378E+02      30   0.56005E-03   0.13605E+02 0.41045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5569          9.4053          4.5729          4.5729
v  Velocity[Y]            -4.5164          7.2891       0.0039807       0.0039807
v  Velocity[Z]       -6.9287e-015     6.3651e-015    -1.0611e-017    -1.0611e-017
v  ǁVelocityǁ        0.00047189          9.4386          4.8496          4.8496
v  Pressure               -45.361          18.793        -0.34347        -0.34347
v  nu_tilda           1.5856e-007       0.0042517       0.0006712       0.0006712
v  TempC                       21          73.195          21.326          21.326
v  TurbVisc           7.1205e-016       0.0050109       0.0007774       0.0007774
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              311:        0.21920E+01

===============================================================


 INSTANT    0.312000000E+03   TIME STEP NUMBER             312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64325E-02 0.89502E+00
   Friction velocity        uk    :  0.64325E-02 0.89502E+00
   Dimensionless distance   yplus :  0.51786E-01 0.72055E+01
   Friction thermal sca.    tstar : -0.13883E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38638E-01 0.53761E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50272E-02      35   0.80448E-03   0.80494E+01 0.18226E+03 
c  Velocity[X]                                      0.35809E+01 
c  Velocity[Y]                                      0.44685E+01 
c  Velocity[Z]                                      0.13586E-29 
c  Pressure     0.13026E-06     392   0.99223E-08   0.12850E+00 0.32353E+03 
c  nu_tilda     0.36636E-05      33   0.12760E-04   0.44113E-06 0.28129E+03 
c  TempC        0.22394E+02      30   0.82008E-03   0.14929E+02 0.42586E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5459          9.4057          4.5729          4.5729
v  Velocity[Y]            -4.5259           7.273       0.0040155       0.0040155
v  Velocity[Z]       -6.9287e-015     6.2547e-015    -1.0551e-017    -1.0551e-017
v  ǁVelocityǁ        0.00041457          9.4386          4.8505          4.8505
v  Pressure               -45.366          18.799        -0.33995        -0.33995
v  nu_tilda           1.5034e-007       0.0042519      0.00067188      0.00067188
v  TempC                       21          73.246          21.328          21.328
v  TurbVisc           5.5614e-016       0.0050111      0.00077817      0.00077817
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              312:        0.23390E+01

===============================================================


 INSTANT    0.313000000E+03   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60341E-02 0.89437E+00
   Friction velocity        uk    :  0.60341E-02 0.89437E+00
   Dimensionless distance   yplus :  0.48578E-01 0.72003E+01
   Friction thermal sca.    tstar : -0.11242E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36245E-01 0.53722E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50313E-02      35   0.82311E-03   0.80694E+01 0.18232E+03 
c  Velocity[X]                                      0.35745E+01 
c  Velocity[Y]                                      0.44949E+01 
c  Velocity[Z]                                      0.15377E-29 
c  Pressure     0.14485E-06     440   0.97843E-08   0.13777E+00 0.53177E+03 
c  nu_tilda     0.36673E-05      33   0.14904E-04   0.43998E-06 0.28058E+03 
c  TempC        0.22411E+02      30   0.68823E-03   0.19145E+02 0.49871E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5353          9.4054          4.5729          4.5729
v  Velocity[Y]             -4.536          7.2975       0.0040516       0.0040516
v  Velocity[Z]       -6.9287e-015     6.1626e-015     -1.049e-017     -1.049e-017
v  ǁVelocityǁ        0.00037844          9.4377          4.8513          4.8513
v  Pressure               -45.444          18.875        -0.35605        -0.35605
v  nu_tilda           1.4436e-007        0.004252      0.00067249      0.00067249
v  TempC                       21          73.028          21.329          21.329
v  TurbVisc           4.4945e-016       0.0050112      0.00077895      0.00077895
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              313:        0.24670E+01

===============================================================


 INSTANT    0.314000000E+03   TIME STEP NUMBER             314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54639E-02 0.89598E+00
   Friction velocity        uk    :  0.54639E-02 0.89598E+00
   Dimensionless distance   yplus :  0.43988E-01 0.72132E+01
   Friction thermal sca.    tstar : -0.11334E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32820E-01 0.53819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50353E-02      35   0.76830E-03   0.80382E+01 0.18215E+03 
c  Velocity[X]                                      0.35428E+01 
c  Velocity[Y]                                      0.44954E+01 
c  Velocity[Z]                                      0.14254E-29 
c  Pressure     0.12197E-06     488   0.96962E-08   0.11809E+00 0.53422E+03 
c  nu_tilda     0.36709E-05      33   0.12767E-04   0.43886E-06 0.27988E+03 
c  TempC        0.22427E+02      30   0.49664E-03   0.15848E+02 0.45375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5244          9.4052          4.5729          4.5729
v  Velocity[Y]            -4.5454          7.3111       0.0040867       0.0040867
v  Velocity[Z]       -6.9287e-015     6.0994e-015    -1.0427e-017    -1.0427e-017
v  ǁVelocityǁ        0.00031956          9.4372          4.8522          4.8522
v  Pressure                -45.45          18.951        -0.33746        -0.33746
v  nu_tilda           1.4069e-007       0.0042522      0.00067318      0.00067318
v  TempC                       21          73.486           21.33           21.33
v  TurbVisc            3.821e-016       0.0050114      0.00077971      0.00077971
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              314:        0.26210E+01

===============================================================


 INSTANT    0.315000000E+03   TIME STEP NUMBER             315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52625E-02 0.89581E+00
   Friction velocity        uk    :  0.52625E-02 0.89581E+00
   Dimensionless distance   yplus :  0.42366E-01 0.72118E+01
   Friction thermal sca.    tstar : -0.11209E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31610E-01 0.53808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50394E-02      35   0.76567E-03   0.80093E+01 0.18187E+03 
c  Velocity[X]                                      0.35203E+01 
c  Velocity[Y]                                      0.44890E+01 
c  Velocity[Z]                                      0.12776E-29 
c  Pressure     0.13047E-06     490   0.99365E-08   0.12794E+00 0.65985E+03 
c  nu_tilda     0.36746E-05      33   0.14858E-04   0.43772E-06 0.27917E+03 
c  TempC        0.22443E+02      30   0.60306E-03   0.15146E+02 0.42384E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5135          9.4043          4.5729          4.5729
v  Velocity[Y]            -4.5541          7.2882       0.0041233       0.0041233
v  Velocity[Z]       -6.9287e-015     5.9777e-015    -1.0369e-017    -1.0369e-017
v  ǁVelocityǁ        0.00024776          9.4358          4.8531          4.8531
v  Pressure               -45.518          18.896         -0.3786         -0.3786
v  nu_tilda           1.3915e-007       0.0042523      0.00067379      0.00067379
v  TempC                       21          73.174          21.331          21.331
v  TurbVisc           3.4468e-016       0.0050116      0.00078049      0.00078049
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              315:        0.26300E+01

===============================================================


 INSTANT    0.316000000E+03   TIME STEP NUMBER             316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45932E-02 0.89480E+00
   Friction velocity        uk    :  0.45932E-02 0.89480E+00
   Dimensionless distance   yplus :  0.36979E-01 0.72037E+01
   Friction thermal sca.    tstar : -0.12056E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27590E-01 0.53748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50435E-02      35   0.78567E-03   0.79867E+01 0.18172E+03 
c  Velocity[X]                                      0.34800E+01 
c  Velocity[Y]                                      0.45067E+01 
c  Velocity[Z]                                      0.13977E-29 
c  Pressure     0.12689E-06     505   0.94445E-08   0.12195E+00 0.10418E+04 
c  nu_tilda     0.36783E-05      33   0.12787E-04   0.43659E-06 0.27847E+03 
c  TempC        0.22459E+02      30   0.48005E-03   0.14650E+02 0.42661E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5028          9.4035          4.5729          4.5729
v  Velocity[Y]            -4.5631          7.3123       0.0041585       0.0041585
v  Velocity[Z]       -6.9287e-015     5.9803e-015    -1.0311e-017    -1.0311e-017
v  ǁVelocityǁ        0.00019593          9.4349          4.8539          4.8539
v  Pressure               -45.521          19.058           -0.34           -0.34
v  nu_tilda           1.3949e-007       0.0042524      0.00067448      0.00067448
v  TempC                       21          73.195          21.333          21.333
v  TurbVisc           3.2986e-016       0.0050118      0.00078125      0.00078125
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              316:        0.26780E+01

===============================================================


 INSTANT    0.317000000E+03   TIME STEP NUMBER             317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40240E-02 0.89605E+00
   Friction velocity        uk    :  0.40240E-02 0.89605E+00
   Dimensionless distance   yplus :  0.32396E-01 0.72138E+01
   Friction thermal sca.    tstar : -0.12736E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24171E-01 0.53823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50476E-02      35   0.79956E-03   0.79918E+01 0.18164E+03 
c  Velocity[X]                                      0.34898E+01 
c  Velocity[Y]                                      0.45020E+01 
c  Velocity[Z]                                      0.15195E-29 
c  Pressure     0.15516E-06     505   0.99160E-08   0.14828E+00 0.10015E+04 
c  nu_tilda     0.36819E-05      33   0.14810E-04   0.43542E-06 0.27777E+03 
c  TempC        0.22475E+02      30   0.67509E-03   0.14155E+02 0.41405E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4907          9.4019          4.5729          4.5729
v  Velocity[Y]            -4.5719          7.2867       0.0041951       0.0041951
v  Velocity[Z]       -6.9287e-015     5.9374e-015    -1.0256e-017    -1.0256e-017
v  ǁVelocityǁ        0.00010406          9.4348          4.8548          4.8548
v  Pressure               -45.596          18.941        -0.39689        -0.39689
v  nu_tilda           1.4136e-007       0.0042526      0.00067508      0.00067508
v  TempC                       21          73.172          21.334          21.334
v  TurbVisc           3.3305e-016       0.0050119      0.00078203      0.00078203
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              317:        0.26210E+01

===============================================================


 INSTANT    0.318000000E+03   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27829E-02 0.89571E+00
   Friction velocity        uk    :  0.27829E-02 0.89571E+00
   Dimensionless distance   yplus :  0.22404E-01 0.72111E+01
   Friction thermal sca.    tstar : -0.16005E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16716E-01 0.53803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50516E-02      35   0.77371E-03   0.79769E+01 0.18146E+03 
c  Velocity[X]                                      0.34809E+01 
c  Velocity[Y]                                      0.44960E+01 
c  Velocity[Z]                                      0.14524E-29 
c  Pressure     0.11669E-06     554   0.99408E-08   0.11173E+00 0.12612E+04 
c  nu_tilda     0.36856E-05      33   0.12796E-04   0.43435E-06 0.27708E+03 
c  TempC        0.22491E+02      30   0.65795E-03   0.16307E+02 0.43298E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4791          9.4006          4.5729          4.5729
v  Velocity[Y]            -4.5794          7.3153       0.0042312       0.0042312
v  Velocity[Z]       -6.9287e-015     5.8766e-015    -1.0196e-017    -1.0196e-017
v  ǁVelocityǁ       5.0234e-005           9.434          4.8557          4.8557
v  Pressure                 -45.6          19.134        -0.34954        -0.34954
v  nu_tilda           1.4449e-007       0.0042527      0.00067577      0.00067577
v  TempC                       21          73.206          21.335          21.335
v  TurbVisc           3.5128e-016       0.0050121       0.0007828       0.0007828
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              318:        0.29870E+01

===============================================================


 INSTANT    0.319000000E+03   TIME STEP NUMBER             319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15267E-02 0.89727E+00
   Friction velocity        uk    :  0.15267E-02 0.89727E+00
   Dimensionless distance   yplus :  0.12291E-01 0.72237E+01
   Friction thermal sca.    tstar : -0.20228E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91702E-02 0.53897E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50557E-02      35   0.76285E-03   0.79364E+01 0.18113E+03 
c  Velocity[X]                                      0.34199E+01 
c  Velocity[Y]                                      0.45165E+01 
c  Velocity[Z]                                      0.14481E-29 
c  Pressure     0.19408E-06     474   0.93515E-08   0.18783E+00 0.44594E+03 
c  nu_tilda     0.36892E-05      33   0.14767E-04   0.43322E-06 0.27639E+03 
c  TempC        0.22507E+02      30   0.95006E-03   0.20618E+02 0.48503E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4678          9.3984          4.5729          4.5729
v  Velocity[Y]            -4.5874          7.3309       0.0042681       0.0042681
v  Velocity[Z]       -6.9287e-015     5.7914e-015     -1.014e-017     -1.014e-017
v  ǁVelocityǁ         4.31e-005          9.4335          4.8566          4.8566
v  Pressure               -45.661          19.166        -0.37358        -0.37358
v  nu_tilda           1.4865e-007       0.0042529      0.00067638      0.00067638
v  TempC                       21          73.476          21.337          21.337
v  TurbVisc           3.8347e-016       0.0050123      0.00078357      0.00078357
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              319:        0.30900E+01

===============================================================


 INSTANT    0.320000000E+03   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98318E-03 0.89686E+00
   Friction velocity        uk    :  0.98318E-03 0.89686E+00
   Dimensionless distance   yplus :  0.79152E-02 0.72204E+01
   Friction thermal sca.    tstar : -0.46647E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59057E-02 0.53872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50598E-02      35   0.77043E-03   0.79340E+01 0.18106E+03 
c  Velocity[X]                                      0.34107E+01 
c  Velocity[Y]                                      0.45233E+01 
c  Velocity[Z]                                      0.13482E-29 
c  Pressure     0.14741E-06     281   0.96134E-08   0.14597E+00 0.34416E+03 
c  nu_tilda     0.36928E-05      33   0.12799E-04   0.43216E-06 0.27571E+03 
c  TempC        0.22523E+02      30   0.72445E-03   0.24139E+02 0.53194E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4556          9.3966          4.5729          4.5729
v  Velocity[Y]            -4.5954          7.3065       0.0043042       0.0043042
v  Velocity[Z]       -6.9287e-015     5.7419e-015    -1.0089e-017    -1.0089e-017
v  ǁVelocityǁ        0.00014908          9.4323          4.8574          4.8574
v  Pressure               -45.665          19.144        -0.37325        -0.37325
v  nu_tilda            1.536e-007        0.004253      0.00067707      0.00067707
v  TempC                       21          73.226          21.338          21.338
v  TurbVisc           4.2955e-016       0.0050124      0.00078434      0.00078434
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              320:        0.23140E+01

===============================================================


 INSTANT    0.321000000E+03   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32001E-02 0.89552E+00
   Friction velocity        uk    :  0.32001E-02 0.89552E+00
   Dimensionless distance   yplus :  0.25763E-01 0.72096E+01
   Friction thermal sca.    tstar : -0.13472E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19222E-01 0.53791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50638E-02      35   0.82221E-03   0.79151E+01 0.18079E+03 
c  Velocity[X]                                      0.34069E+01 
c  Velocity[Y]                                      0.45082E+01 
c  Velocity[Z]                                      0.12595E-29 
c  Pressure     0.17488E-06     426   0.97085E-08   0.16520E+00 0.54836E+03 
c  nu_tilda     0.36964E-05      33   0.14732E-04   0.43102E-06 0.27502E+03 
c  TempC        0.22539E+02      30   0.40917E-03   0.18119E+02 0.45485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4436          9.3941          4.5729          4.5729
v  Velocity[Y]             -4.602          7.3252        0.004342        0.004342
v  Velocity[Z]       -6.9287e-015     5.5968e-015    -1.0042e-017    -1.0042e-017
v  ǁVelocityǁ        0.00022723          9.4312          4.8583          4.8583
v  Pressure               -45.738          19.215        -0.38778        -0.38778
v  nu_tilda            1.592e-007       0.0042531      0.00067767      0.00067767
v  TempC                       21          73.203          21.339          21.339
v  TurbVisc           4.8967e-016       0.0050126      0.00078511      0.00078511
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              321:        0.24470E+01

===============================================================


 INSTANT    0.322000000E+03   TIME STEP NUMBER             322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40825E-02 0.89693E+00
   Friction velocity        uk    :  0.40825E-02 0.89693E+00
   Dimensionless distance   yplus :  0.32867E-01 0.72209E+01
   Friction thermal sca.    tstar : -0.13533E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24522E-01 0.53876E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50679E-02      35   0.78728E-03   0.79305E+01 0.18086E+03 
c  Velocity[X]                                      0.34006E+01 
c  Velocity[Y]                                      0.45300E+01 
c  Velocity[Z]                                      0.15203E-29 
c  Pressure     0.14310E-06     425   0.97267E-08   0.13967E+00 0.36086E+03 
c  nu_tilda     0.37000E-05      33   0.12802E-04   0.42994E-06 0.27434E+03 
c  TempC        0.22555E+02      30   0.89315E-03   0.15203E+02 0.40539E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4313          9.3917          4.5729          4.5729
v  Velocity[Y]            -4.6091          7.3035       0.0043783       0.0043783
v  Velocity[Z]       -6.9287e-015     5.4527e-015    -9.9926e-018    -9.9926e-018
v  ǁVelocityǁ        0.00033403          9.4296          4.8592          4.8592
v  Pressure               -45.726          19.236        -0.37771        -0.37771
v  nu_tilda           1.6533e-007       0.0042533      0.00067836      0.00067836
v  TempC                       21           73.63           21.34           21.34
v  TurbVisc           5.6511e-016       0.0050127      0.00078588      0.00078588
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              322:        0.24500E+01

===============================================================


 INSTANT    0.323000000E+03   TIME STEP NUMBER             323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50631E-02 0.89646E+00
   Friction velocity        uk    :  0.50631E-02 0.89646E+00
   Dimensionless distance   yplus :  0.40762E-01 0.72171E+01
   Friction thermal sca.    tstar : -0.14790E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30413E-01 0.53848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50719E-02      35   0.74225E-03   0.78739E+01 0.18038E+03 
c  Velocity[X]                                      0.33609E+01 
c  Velocity[Y]                                      0.45130E+01 
c  Velocity[Z]                                      0.17245E-29 
c  Pressure     0.15335E-06     408   0.94644E-08   0.14805E+00 0.66565E+03 
c  nu_tilda     0.37036E-05      33   0.14695E-04   0.42882E-06 0.27367E+03 
c  TempC        0.22571E+02      30   0.64718E-03   0.22058E+02 0.50181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4198            9.39          4.5729          4.5729
v  Velocity[Y]            -4.6158           7.333       0.0044162       0.0044162
v  Velocity[Z]       -6.9287e-015     5.1256e-015    -9.9496e-018    -9.9496e-018
v  ǁVelocityǁ        0.00041635           9.428          4.8601          4.8601
v  Pressure               -45.792          19.339        -0.38618        -0.38618
v  nu_tilda           1.7196e-007       0.0042534      0.00067897      0.00067897
v  TempC                       21          73.268          21.341          21.341
v  TurbVisc           6.5737e-016       0.0050129      0.00078665      0.00078665
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              323:        0.24180E+01

===============================================================


 INSTANT    0.324000000E+03   TIME STEP NUMBER             324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56947E-02 0.89778E+00
   Friction velocity        uk    :  0.56947E-02 0.89778E+00
   Dimensionless distance   yplus :  0.45846E-01 0.72277E+01
   Friction thermal sca.    tstar : -0.40334E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34206E-01 0.53927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50760E-02      35   0.84363E-03   0.78482E+01 0.18008E+03 
c  Velocity[X]                                      0.33402E+01 
c  Velocity[Y]                                      0.45080E+01 
c  Velocity[Z]                                      0.12741E-29 
c  Pressure     0.17324E-06     326   0.91374E-08   0.16725E+00 0.36269E+03 
c  nu_tilda     0.37072E-05      33   0.12804E-04   0.42779E-06 0.27300E+03 
c  TempC        0.22587E+02      30   0.49230E-03   0.17915E+02 0.43712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4069          9.3886          4.5729          4.5729
v  Velocity[Y]            -4.6215          7.3072        0.004453        0.004453
v  Velocity[Z]       -6.9287e-015     5.0131e-015    -9.9055e-018    -9.9055e-018
v  ǁVelocityǁ        0.00053861          9.4261          4.8609          4.8609
v  Pressure               -45.785          19.311        -0.38794        -0.38794
v  nu_tilda           1.7898e-007       0.0042535      0.00067966      0.00067966
v  TempC                       21          73.326          21.343          21.343
v  TurbVisc           7.6928e-016       0.0050131      0.00078742      0.00078742
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              324:        0.23570E+01

===============================================================


 INSTANT    0.325000000E+03   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60704E-02 0.89705E+00
   Friction velocity        uk    :  0.60704E-02 0.89705E+00
   Dimensionless distance   yplus :  0.48871E-01 0.72219E+01
   Friction thermal sca.    tstar : -0.44818E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36463E-01 0.53883E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50800E-02      35   0.69025E-03   0.78596E+01 0.18004E+03 
c  Velocity[X]                                      0.33401E+01 
c  Velocity[Y]                                      0.45194E+01 
c  Velocity[Z]                                      0.14201E-29 
c  Pressure     0.13254E-06     310   0.86059E-08   0.12798E+00 0.74505E+03 
c  nu_tilda     0.37107E-05      33   0.14665E-04   0.42671E-06 0.27233E+03 
c  TempC        0.22602E+02      30   0.54359E-03   0.15993E+02 0.40163E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3953          9.3866          4.5729          4.5729
v  Velocity[Y]             -4.628          7.3348       0.0044913       0.0044913
v  Velocity[Z]       -6.9287e-015      5.021e-015    -9.8663e-018    -9.8663e-018
v  ǁVelocityǁ        0.00037886          9.4238          4.8618          4.8618
v  Pressure                -45.85          19.431        -0.39374        -0.39374
v  nu_tilda           1.8621e-007       0.0042537      0.00068027      0.00068027
v  TempC                       21           73.48          21.344          21.344
v  TurbVisc           9.0272e-016       0.0050132       0.0007882       0.0007882
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              325:        0.36750E+01

===============================================================


 INSTANT    0.326000000E+03   TIME STEP NUMBER             326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48063E-02 0.89838E+00
   Friction velocity        uk    :  0.48063E-02 0.89838E+00
   Dimensionless distance   yplus :  0.38694E-01 0.72326E+01
   Friction thermal sca.    tstar : -0.13516E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28870E-01 0.53963E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50840E-02      35   0.75998E-03   0.77763E+01 0.17942E+03 
c  Velocity[X]                                      0.32668E+01 
c  Velocity[Y]                                      0.45094E+01 
c  Velocity[Z]                                      0.13929E-29 
c  Pressure     0.16243E-06     473   0.91338E-08   0.15650E+00 0.74078E+03 
c  nu_tilda     0.37143E-05      33   0.12809E-04   0.42567E-06 0.27167E+03 
c  TempC        0.22618E+02      30   0.54313E-03   0.16065E+02 0.40074E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3838          9.3846          4.5729          4.5729
v  Velocity[Y]            -4.6338          7.3463       0.0045287       0.0045287
v  Velocity[Z]       -6.9287e-015     5.0309e-015    -9.8277e-018    -9.8277e-018
v  ǁVelocityǁ        0.00023558          9.4215          4.8627          4.8627
v  Pressure               -45.829          19.523        -0.36381        -0.36381
v  nu_tilda           1.9368e-007       0.0042538      0.00068095      0.00068095
v  TempC                       21          73.452          21.345          21.345
v  TurbVisc           1.0578e-015       0.0050134      0.00078896      0.00078896
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              326:        0.43550E+01

===============================================================


 INSTANT    0.327000000E+03   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29993E-02 0.89803E+00
   Friction velocity        uk    :  0.29993E-02 0.89803E+00
   Dimensionless distance   yplus :  0.24147E-01 0.72297E+01
   Friction thermal sca.    tstar : -0.10398E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18016E-01 0.53942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50881E-02      35   0.79760E-03   0.77842E+01 0.17929E+03 
c  Velocity[X]                                      0.32754E+01 
c  Velocity[Y]                                      0.45088E+01 
c  Velocity[Z]                                      0.12469E-29 
c  Pressure     0.13412E-06     504   0.99020E-08   0.13136E+00 0.67827E+03 
c  nu_tilda     0.37178E-05      33   0.14618E-04   0.42460E-06 0.27101E+03 
c  TempC        0.22634E+02      30   0.55922E-03   0.16905E+02 0.42643E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3719          9.3821          4.5729          4.5729
v  Velocity[Y]            -4.6387          7.3217       0.0045671       0.0045671
v  Velocity[Z]       -6.9287e-015     5.0378e-015    -9.8034e-018    -9.8034e-018
v  ǁVelocityǁ        0.00036038          9.4187          4.8636          4.8636
v  Pressure               -45.889          19.457        -0.40795        -0.40795
v  nu_tilda           2.0124e-007       0.0042539      0.00068156      0.00068156
v  TempC                       21          73.516          21.346          21.346
v  TurbVisc            1.238e-015       0.0050135      0.00078974      0.00078974
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              327:        0.28140E+01

===============================================================


 INSTANT    0.328000000E+03   TIME STEP NUMBER             328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37636E-02 0.89673E+00
   Friction velocity        uk    :  0.37636E-02 0.89673E+00
   Dimensionless distance   yplus :  0.30299E-01 0.72193E+01
   Friction thermal sca.    tstar : -0.92917E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22607E-01 0.53864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50921E-02      35   0.82915E-03   0.77702E+01 0.17915E+03 
c  Velocity[X]                                      0.32482E+01 
c  Velocity[Y]                                      0.45220E+01 
c  Velocity[Z]                                      0.11430E-29 
c  Pressure     0.14240E-06     504   0.98005E-08   0.13784E+00 0.11548E+04 
c  nu_tilda     0.37214E-05      33   0.12810E-04   0.42357E-06 0.27035E+03 
c  TempC        0.22650E+02      30   0.59492E-03   0.15932E+02 0.40829E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3606          9.3795          4.5729          4.5729
v  Velocity[Y]            -4.6444          7.3398       0.0046053       0.0046053
v  Velocity[Z]       -6.9287e-015     5.0481e-015    -9.7727e-018    -9.7727e-018
v  ǁVelocityǁ        0.00056253          9.4161          4.8645          4.8645
v  Pressure               -45.873          19.627        -0.36366        -0.36366
v  nu_tilda           2.0896e-007       0.0042541      0.00068225      0.00068225
v  TempC                       21          73.569          21.347          21.347
v  TurbVisc           1.4428e-015       0.0050137       0.0007905       0.0007905
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              328:        0.25340E+01

===============================================================


 INSTANT    0.329000000E+03   TIME STEP NUMBER             329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64659E-02 0.89773E+00
   Friction velocity        uk    :  0.64659E-02 0.89773E+00
   Dimensionless distance   yplus :  0.52055E-01 0.72274E+01
   Friction thermal sca.    tstar : -0.95858E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38839E-01 0.53924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50962E-02      35   0.74659E-03   0.77956E+01 0.17917E+03 
c  Velocity[X]                                      0.32735E+01 
c  Velocity[Y]                                      0.45221E+01 
c  Velocity[Z]                                      0.15925E-29 
c  Pressure     0.14285E-06     501   0.95852E-08   0.14049E+00 0.63741E+03 
c  nu_tilda     0.37249E-05      33   0.14594E-04   0.42250E-06 0.26970E+03 
c  TempC        0.22665E+02      30   0.61371E-03   0.16540E+02 0.40061E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3489          9.3765          4.5729          4.5729
v  Velocity[Y]            -4.6492          7.3249       0.0046437       0.0046437
v  Velocity[Z]       -6.9287e-015      5.053e-015    -9.7507e-018    -9.7507e-018
v  ǁVelocityǁ        0.00084187          9.4129          4.8654          4.8654
v  Pressure               -45.931          19.569        -0.40619        -0.40619
v  nu_tilda           2.1676e-007       0.0042542      0.00068285      0.00068285
v  TempC                       21          73.623          21.348          21.348
v  TurbVisc           1.6774e-015       0.0050138      0.00079128      0.00079128
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              329:        0.25160E+01

===============================================================


 INSTANT    0.330000000E+03   TIME STEP NUMBER             330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72837E-02 0.89682E+00
   Friction velocity        uk    :  0.72837E-02 0.89682E+00
   Dimensionless distance   yplus :  0.58639E-01 0.72200E+01
   Friction thermal sca.    tstar : -0.11060E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43751E-01 0.53869E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51002E-02      35   0.76378E-03   0.77157E+01 0.17848E+03 
c  Velocity[X]                                      0.32160E+01 
c  Velocity[Y]                                      0.44997E+01 
c  Velocity[Z]                                      0.14243E-29 
c  Pressure     0.11733E-06     538   0.94661E-08   0.11243E+00 0.12127E+04 
c  nu_tilda     0.37284E-05      33   0.12804E-04   0.42150E-06 0.26905E+03 
c  TempC        0.22681E+02      30   0.89698E-03   0.17595E+02 0.42820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3375          9.3734          4.5729          4.5729
v  Velocity[Y]            -4.6535          7.3472        0.004683        0.004683
v  Velocity[Z]       -6.9287e-015     5.0614e-015    -9.7202e-018    -9.7202e-018
v  ǁVelocityǁ        0.00074732            9.41          4.8663          4.8663
v  Pressure               -45.909          19.748        -0.35971        -0.35971
v  nu_tilda           2.2454e-007       0.0042543      0.00068354      0.00068354
v  TempC                       21          73.675          21.349          21.349
v  TurbVisc           1.9422e-015        0.005014      0.00079204      0.00079204
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              330:        0.27820E+01

===============================================================


 INSTANT    0.331000000E+03   TIME STEP NUMBER             331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92240E-02 0.89774E+00
   Friction velocity        uk    :  0.92240E-02 0.89774E+00
   Dimensionless distance   yplus :  0.74259E-01 0.72274E+01
   Friction thermal sca.    tstar : -0.12613E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55406E-01 0.53925E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51042E-02      35   0.82483E-03   0.77122E+01 0.17832E+03 
c  Velocity[X]                                      0.32000E+01 
c  Velocity[Y]                                      0.45122E+01 
c  Velocity[Z]                                      0.13687E-29 
c  Pressure     0.12968E-06     504   0.99194E-08   0.12496E+00 0.74461E+03 
c  nu_tilda     0.37319E-05      33   0.14563E-04   0.42046E-06 0.26840E+03 
c  TempC        0.22697E+02      30   0.62939E-03   0.24073E+02 0.51703E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3259          9.3699          4.5729          4.5729
v  Velocity[Y]            -4.6583          7.3154       0.0047215       0.0047215
v  Velocity[Z]       -6.9287e-015     5.0663e-015    -9.7024e-018    -9.7024e-018
v  ǁVelocityǁ         0.0001792          9.4065          4.8672          4.8672
v  Pressure               -45.963          19.663        -0.40677        -0.40677
v  nu_tilda           2.3228e-007       0.0042544      0.00068415      0.00068415
v  TempC                       21          73.723           21.35           21.35
v  TurbVisc           2.2364e-015       0.0050141      0.00079282      0.00079282
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              331:        0.28280E+01

===============================================================


 INSTANT    0.332000000E+03   TIME STEP NUMBER             332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31960E-02 0.89680E+00
   Friction velocity        uk    :  0.31960E-02 0.89680E+00
   Dimensionless distance   yplus :  0.25730E-01 0.72199E+01
   Friction thermal sca.    tstar : -0.14498E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19197E-01 0.53868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51082E-02      35   0.66869E-03   0.77157E+01 0.17816E+03 
c  Velocity[X]                                      0.32180E+01 
c  Velocity[Y]                                      0.44977E+01 
c  Velocity[Z]                                      0.12149E-29 
c  Pressure     0.12783E-06     506   0.97839E-08   0.12294E+00 0.12740E+04 
c  nu_tilda     0.37354E-05      33   0.12802E-04   0.41948E-06 0.26776E+03 
c  TempC        0.22712E+02      30   0.57754E-03   0.19028E+02 0.43273E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3147          9.3663          4.5729          4.5729
v  Velocity[Y]            -4.6622          7.3409        0.004761        0.004761
v  Velocity[Z]       -6.9287e-015      5.075e-015    -9.6788e-018    -9.6788e-018
v  ǁVelocityǁ        0.00037208          9.4032          4.8681          4.8681
v  Pressure               -45.941          19.852        -0.35812        -0.35812
v  nu_tilda            2.399e-007       0.0042546      0.00068483      0.00068483
v  TempC                       21          73.772          21.351          21.351
v  TurbVisc           2.5611e-015       0.0050143      0.00079358      0.00079358
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              332:        0.24550E+01

===============================================================


 INSTANT    0.333000000E+03   TIME STEP NUMBER             333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67805E-02 0.89805E+00
   Friction velocity        uk    :  0.67805E-02 0.89805E+00
   Dimensionless distance   yplus :  0.54588E-01 0.72299E+01
   Friction thermal sca.    tstar : -0.20004E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40729E-01 0.53943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51123E-02      35   0.78967E-03   0.76319E+01 0.17749E+03 
c  Velocity[X]                                      0.31459E+01 
c  Velocity[Y]                                      0.44860E+01 
c  Velocity[Z]                                      0.10637E-29 
c  Pressure     0.12025E-06     457   0.93966E-08   0.11628E+00 0.44063E+03 
c  nu_tilda     0.37389E-05      33   0.14527E-04   0.41846E-06 0.26712E+03 
c  TempC        0.22728E+02      30   0.43726E-03   0.16604E+02 0.40340E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3037          9.3624          4.5729          4.5729
v  Velocity[Y]             -4.666          7.3524          0.0048          0.0048
v  Velocity[Z]       -6.9287e-015     5.0823e-015    -9.6515e-018    -9.6515e-018
v  ǁVelocityǁ        0.00093806          9.4008           4.869           4.869
v  Pressure               -45.986          19.877        -0.38197        -0.38197
v  nu_tilda           2.4744e-007       0.0042547      0.00068544      0.00068544
v  TempC                       21          73.816          21.352          21.352
v  TurbVisc           2.9139e-015       0.0050144      0.00079436      0.00079436
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              333:        0.25380E+01

===============================================================


 INSTANT    0.334000000E+03   TIME STEP NUMBER             334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10715E-01 0.89753E+00
   Friction velocity        uk    :  0.10715E-01 0.89753E+00
   Dimensionless distance   yplus :  0.86262E-01 0.72257E+01
   Friction thermal sca.    tstar : -0.35359E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64361E-01 0.53912E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51163E-02      35   0.79102E-03   0.76724E+01 0.17749E+03 
c  Velocity[X]                                      0.31681E+01 
c  Velocity[Y]                                      0.45043E+01 
c  Velocity[Z]                                      0.13090E-29 
c  Pressure     0.16238E-06     457   0.93161E-08   0.15964E+00 0.47916E+03 
c  nu_tilda     0.37424E-05      33   0.12795E-04   0.41751E-06 0.26648E+03 
c  TempC        0.22744E+02      30   0.57096E-03   0.16165E+02 0.40668E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2932          9.3585          4.5729          4.5729
v  Velocity[Y]            -4.6698          7.3229       0.0048393       0.0048393
v  Velocity[Z]       -6.9287e-015     5.0906e-015    -9.6193e-018    -9.6193e-018
v  ǁVelocityǁ        0.00090684          9.3974          4.8699          4.8699
v  Pressure               -45.958          19.906        -0.36335        -0.36335
v  nu_tilda           2.5491e-007       0.0042548      0.00068613      0.00068613
v  TempC                       21          73.849          21.353          21.353
v  TurbVisc           3.2979e-015       0.0050146      0.00079512      0.00079512
v  total_pressure     1.0128e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              334:        0.23240E+01

===============================================================


 INSTANT    0.335000000E+03   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10377E-01 0.89633E+00
   Friction velocity        uk    :  0.10377E-01 0.89633E+00
   Dimensionless distance   yplus :  0.83541E-01 0.72161E+01
   Friction thermal sca.    tstar : -0.28110E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62331E-01 0.53840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51203E-02      35   0.78000E-03   0.76464E+01 0.17725E+03 
c  Velocity[X]                                      0.31431E+01 
c  Velocity[Y]                                      0.45033E+01 
c  Velocity[Z]                                      0.14808E-29 
c  Pressure     0.12441E-06     360   0.96927E-08   0.12053E+00 0.62769E+03 
c  nu_tilda     0.37458E-05      33   0.14483E-04   0.41650E-06 0.26585E+03 
c  TempC        0.22759E+02      30   0.55011E-03   0.16068E+02 0.40153E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2829          9.3541          4.5729          4.5729
v  Velocity[Y]            -4.6727          7.3426       0.0048794       0.0048794
v  Velocity[Z]       -6.9287e-015     5.0971e-015    -9.5976e-018    -9.5976e-018
v  ǁVelocityǁ        0.00029678          9.3945          4.8708          4.8708
v  Pressure               -46.007          20.001        -0.37537        -0.37537
v  nu_tilda           2.6222e-007       0.0042549      0.00068673      0.00068673
v  TempC                       21          73.873          21.354          21.354
v  TurbVisc           3.7148e-015       0.0050147       0.0007959       0.0007959
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              335:        0.22530E+01

===============================================================


 INSTANT    0.336000000E+03   TIME STEP NUMBER             336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54713E-02 0.89747E+00
   Friction velocity        uk    :  0.54713E-02 0.89747E+00
   Dimensionless distance   yplus :  0.44048E-01 0.72252E+01
   Friction thermal sca.    tstar : -0.17891E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32864E-01 0.53908E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51244E-02      35   0.79731E-03   0.76498E+01 0.17706E+03 
c  Velocity[X]                                      0.31707E+01 
c  Velocity[Y]                                      0.44792E+01 
c  Velocity[Z]                                      0.14815E-29 
c  Pressure     0.13709E-06     442   0.96921E-08   0.13442E+00 0.38366E+03 
c  nu_tilda     0.37493E-05      33   0.12787E-04   0.41556E-06 0.26522E+03 
c  TempC        0.22775E+02      30   0.56399E-03   0.17437E+02 0.42078E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2738          9.3497          4.5729          4.5729
v  Velocity[Y]            -4.6762          7.3234       0.0049191       0.0049191
v  Velocity[Z]       -6.9287e-015     5.1042e-015    -9.5778e-018    -9.5778e-018
v  ǁVelocityǁ        0.00070555          9.3907          4.8717          4.8717
v  Pressure               -45.975          20.008        -0.36273        -0.36273
v  nu_tilda           2.6944e-007       0.0042551      0.00068742      0.00068742
v  TempC                       21          73.889          21.355          21.355
v  TurbVisc           4.1594e-015       0.0050149      0.00079666      0.00079666
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              336:        0.32050E+01

===============================================================


 INSTANT    0.337000000E+03   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77075E-02 0.89685E+00
   Friction velocity        uk    :  0.77075E-02 0.89685E+00
   Dimensionless distance   yplus :  0.62051E-01 0.72202E+01
   Friction thermal sca.    tstar : -0.13109E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46297E-01 0.53871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51284E-02      35   0.73671E-03   0.76099E+01 0.17663E+03 
c  Velocity[X]                                      0.31161E+01 
c  Velocity[Y]                                      0.44939E+01 
c  Velocity[Z]                                      0.15895E-29 
c  Pressure     0.15420E-06     345   0.97265E-08   0.14783E+00 0.77503E+03 
c  nu_tilda     0.37527E-05      33   0.14457E-04   0.41458E-06 0.26459E+03 
c  TempC        0.22790E+02      30   0.86804E-03   0.16661E+02 0.41287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2652          9.3451          4.5729          4.5729
v  Velocity[Y]            -4.6789          7.3478       0.0049595       0.0049595
v  Velocity[Z]       -6.9287e-015     5.1125e-015    -9.5443e-018    -9.5443e-018
v  ǁVelocityǁ         0.0014693          9.3874          4.8726          4.8726
v  Pressure               -46.018          20.128        -0.36677        -0.36677
v  nu_tilda           2.7648e-007       0.0042552      0.00068803      0.00068803
v  TempC                       21          73.897          21.356          21.356
v  TurbVisc           4.6369e-015        0.005015      0.00079743      0.00079743
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              337:        0.25470E+01

===============================================================


 INSTANT    0.338000000E+03   TIME STEP NUMBER             338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42626E-02 0.89790E+00
   Friction velocity        uk    :  0.42626E-02 0.89790E+00
   Dimensionless distance   yplus :  0.34317E-01 0.72287E+01
   Friction thermal sca.    tstar : -0.11731E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25604E-01 0.53934E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51324E-02      35   0.78670E-03   0.75717E+01 0.17619E+03 
c  Velocity[X]                                      0.31021E+01 
c  Velocity[Y]                                      0.44696E+01 
c  Velocity[Z]                                      0.13391E-29 
c  Pressure     0.12918E-06     406   0.96902E-08   0.12433E+00 0.33584E+03 
c  nu_tilda     0.37562E-05      33   0.12774E-04   0.41368E-06 0.26397E+03 
c  TempC        0.22806E+02      30   0.60035E-03   0.20238E+02 0.44406E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2561          9.3404          4.5729          4.5729
v  Velocity[Y]            -4.6814          7.3152       0.0049996       0.0049996
v  Velocity[Z]       -6.9287e-015     5.1173e-015    -9.5275e-018    -9.5275e-018
v  ǁVelocityǁ         0.0014343          9.3833          4.8735          4.8735
v  Pressure               -45.988          20.108        -0.36062        -0.36062
v  nu_tilda           2.8368e-007       0.0042553      0.00068871      0.00068871
v  TempC                       21          73.897          21.357          21.357
v  TurbVisc           5.1405e-015       0.0050152       0.0007982       0.0007982
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              338:        0.25270E+01

===============================================================


 INSTANT    0.339000000E+03   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10668E-01 0.89703E+00
   Friction velocity        uk    :  0.10668E-01 0.89703E+00
   Dimensionless distance   yplus :  0.85883E-01 0.72217E+01
   Friction thermal sca.    tstar : -0.99274E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64078E-01 0.53882E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51364E-02      35   0.70881E-03   0.75899E+01 0.17610E+03 
c  Velocity[X]                                      0.31293E+01 
c  Velocity[Y]                                      0.44605E+01 
c  Velocity[Z]                                      0.14130E-29 
c  Pressure     0.13592E-06     313   0.91248E-08   0.13104E+00 0.77206E+03 
c  nu_tilda     0.37596E-05      33   0.14431E-04   0.41271E-06 0.26335E+03 
c  TempC        0.22821E+02      30   0.65000E-03   0.18173E+02 0.43520E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2477          9.3353          4.5729          4.5729
v  Velocity[Y]            -4.6837          7.3423       0.0050404       0.0050404
v  Velocity[Z]       -6.9287e-015     5.1232e-015    -9.4988e-018    -9.4988e-018
v  ǁVelocityǁ        0.00073619          9.3795          4.8744          4.8744
v  Pressure               -46.031          20.228        -0.36523        -0.36523
v  nu_tilda           2.9112e-007       0.0042554      0.00068932      0.00068932
v  TempC                       21          73.892          21.357          21.357
v  TurbVisc           5.6973e-015       0.0050153      0.00079897      0.00079897
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              339:        0.22170E+01

===============================================================


 INSTANT    0.340000000E+03   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65245E-02 0.89812E+00
   Friction velocity        uk    :  0.65245E-02 0.89812E+00
   Dimensionless distance   yplus :  0.52527E-01 0.72305E+01
   Friction thermal sca.    tstar : -0.10702E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39191E-01 0.53947E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51405E-02      35   0.77853E-03   0.75353E+01 0.17565E+03 
c  Velocity[X]                                      0.30570E+01 
c  Velocity[Y]                                      0.44783E+01 
c  Velocity[Z]                                      0.13006E-29 
c  Pressure     0.11199E-06     489   0.92262E-08   0.10861E+00 0.73127E+03 
c  nu_tilda     0.37630E-05      33   0.12756E-04   0.41184E-06 0.26274E+03 
c  TempC        0.22837E+02      30   0.74506E-03   0.18229E+02 0.43894E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2389          9.3305          4.5729          4.5729
v  Velocity[Y]            -4.6855          7.3509       0.0050808       0.0050808
v  Velocity[Z]       -6.9287e-015     5.1267e-015    -9.4847e-018    -9.4847e-018
v  ǁVelocityǁ        0.00057947           9.375          4.8754          4.8754
v  Pressure               -45.998          20.325        -0.33746        -0.33746
v  nu_tilda           2.9856e-007       0.0042555         0.00069         0.00069
v  TempC                       21          73.881          21.358          21.358
v  TurbVisc           6.3187e-015       0.0050154      0.00079973      0.00079973
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              340:        0.26940E+01

===============================================================


 INSTANT    0.341000000E+03   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63788E-02 0.89749E+00
   Friction velocity        uk    :  0.63788E-02 0.89749E+00
   Dimensionless distance   yplus :  0.51354E-01 0.72254E+01
   Friction thermal sca.    tstar : -0.36867E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38316E-01 0.53909E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51445E-02      35   0.74564E-03   0.75381E+01 0.17542E+03 
c  Velocity[X]                                      0.30719E+01 
c  Velocity[Y]                                      0.44662E+01 
c  Velocity[Z]                                      0.15595E-29 
c  Pressure     0.13895E-06     490   0.95068E-08   0.13703E+00 0.53710E+03 
c  nu_tilda     0.37664E-05      33   0.14410E-04   0.41091E-06 0.26213E+03 
c  TempC        0.22852E+02      30   0.65255E-03   0.19460E+02 0.45665E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2309          9.3259          4.5729          4.5729
v  Velocity[Y]            -4.6867          7.3257       0.0051222       0.0051222
v  Velocity[Z]       -6.9287e-015     5.1316e-015    -9.4574e-018    -9.4574e-018
v  ǁVelocityǁ         0.0015903           9.371          4.8763          4.8763
v  Pressure               -46.035          20.274        -0.37451        -0.37451
v  nu_tilda           3.0592e-007       0.0042556      0.00069061      0.00069061
v  TempC                       21          73.865          21.359          21.359
v  TurbVisc           6.9901e-015       0.0050156      0.00080051      0.00080051
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              341:        0.27310E+01

===============================================================


 INSTANT    0.342000000E+03   TIME STEP NUMBER             342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42512E-02 0.89589E+00
   Friction velocity        uk    :  0.42512E-02 0.89589E+00
   Dimensionless distance   yplus :  0.34225E-01 0.72125E+01
   Friction thermal sca.    tstar : -0.12836E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25536E-01 0.53813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51485E-02      35   0.81118E-03   0.75252E+01 0.17510E+03 
c  Velocity[X]                                      0.30835E+01 
c  Velocity[Y]                                      0.44417E+01 
c  Velocity[Z]                                      0.13546E-29 
c  Pressure     0.15441E-06     488   0.98800E-08   0.14563E+00 0.91383E+03 
c  nu_tilda     0.37698E-05      33   0.12743E-04   0.41005E-06 0.26152E+03 
c  TempC        0.22868E+02      30   0.98091E-03   0.17646E+02 0.42110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2242          9.3213          4.5729          4.5729
v  Velocity[Y]             -4.689           7.338       0.0051629       0.0051629
v  Velocity[Z]       -6.9287e-015     5.1362e-015    -9.4489e-018    -9.4489e-018
v  ǁVelocityǁ        0.00062268           9.366          4.8772          4.8772
v  Pressure               -46.004          20.402        -0.33996        -0.33996
v  nu_tilda           3.1309e-007       0.0042558      0.00069129      0.00069129
v  TempC                       21          73.846           21.36           21.36
v  TurbVisc           7.7051e-015       0.0050157      0.00080127      0.00080127
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              342:        0.33870E+01

===============================================================


 INSTANT    0.343000000E+03   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96468E-02 0.89710E+00
   Friction velocity        uk    :  0.96468E-02 0.89710E+00
   Dimensionless distance   yplus :  0.77663E-01 0.72223E+01
   Friction thermal sca.    tstar : -0.12479E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57946E-01 0.53886E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51525E-02      35   0.75179E-03   0.75552E+01 0.17512E+03 
c  Velocity[X]                                      0.31070E+01 
c  Velocity[Y]                                      0.44483E+01 
c  Velocity[Z]                                      0.13011E-29 
c  Pressure     0.14354E-06     473   0.96565E-08   0.14011E+00 0.44269E+03 
c  nu_tilda     0.37732E-05      33   0.14377E-04   0.40915E-06 0.26092E+03 
c  TempC        0.22883E+02      30   0.60665E-03   0.23225E+02 0.48584E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2177          9.3162          4.5729          4.5729
v  Velocity[Y]              -4.69           7.316       0.0052043       0.0052043
v  Velocity[Z]       -6.9287e-015     5.1428e-015    -9.4226e-018    -9.4226e-018
v  ǁVelocityǁ         0.0020902          9.3615          4.8781          4.8781
v  Pressure               -46.038          20.385        -0.36953        -0.36953
v  nu_tilda           3.2013e-007       0.0042559       0.0006919       0.0006919
v  TempC                       21          73.823           21.36           21.36
v  TurbVisc           8.4534e-015       0.0050158      0.00080204      0.00080204
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              343:        0.27680E+01

===============================================================


 INSTANT    0.344000000E+03   TIME STEP NUMBER             344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92301E-02 0.89637E+00
   Friction velocity        uk    :  0.92301E-02 0.89637E+00
   Dimensionless distance   yplus :  0.74309E-01 0.72164E+01
   Friction thermal sca.    tstar : -0.74218E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55443E-01 0.53842E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51565E-02      35   0.73126E-03   0.74796E+01 0.17444E+03 
c  Velocity[X]                                      0.30505E+01 
c  Velocity[Y]                                      0.44290E+01 
c  Velocity[Z]                                      0.15708E-29 
c  Pressure     0.11943E-06     488   0.98101E-08   0.11493E+00 0.11581E+04 
c  nu_tilda     0.37766E-05      33   0.12719E-04   0.40834E-06 0.26032E+03 
c  TempC        0.22899E+02      30   0.60714E-03   0.18546E+02 0.43499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2113          9.3116          4.5729          4.5729
v  Velocity[Y]            -4.6912          7.3382       0.0052451       0.0052451
v  Velocity[Z]       -6.9287e-015     5.1493e-015    -9.3997e-018    -9.3997e-018
v  ǁVelocityǁ         0.0018993          9.3564          4.8791          4.8791
v  Pressure               -46.002          20.559        -0.32543        -0.32543
v  nu_tilda            3.271e-007        0.004256      0.00069258      0.00069258
v  TempC                       21          73.797          21.361          21.361
v  TurbVisc           9.2398e-015        0.005016       0.0008028       0.0008028
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              344:        0.28650E+01

===============================================================


 INSTANT    0.345000000E+03   TIME STEP NUMBER             345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66747E-02 0.89771E+00
   Friction velocity        uk    :  0.66747E-02 0.89771E+00
   Dimensionless distance   yplus :  0.53736E-01 0.72271E+01
   Friction thermal sca.    tstar : -0.69121E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40093E-01 0.53923E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51606E-02      35   0.79732E-03   0.74590E+01 0.17405E+03 
c  Velocity[X]                                      0.30444E+01 
c  Velocity[Y]                                      0.44146E+01 
c  Velocity[Z]                                      0.13661E-29 
c  Pressure     0.15612E-06     504   0.96090E-08   0.15276E+00 0.62577E+03 
c  nu_tilda     0.37800E-05      33   0.14333E-04   0.40745E-06 0.25972E+03 
c  TempC        0.22914E+02      30   0.63500E-03   0.17269E+02 0.42396E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2053          9.3065          4.5729          4.5729
v  Velocity[Y]            -4.6924          7.3134        0.005287        0.005287
v  Velocity[Z]       -6.9287e-015     5.1548e-015    -9.3863e-018    -9.3863e-018
v  ǁVelocityǁ        0.00095478          9.3516            4.88            4.88
v  Pressure               -46.034          20.486        -0.36765        -0.36765
v  nu_tilda             3.34e-007       0.0042561      0.00069318      0.00069318
v  TempC                       21           73.77          21.362          21.362
v  TurbVisc           1.0071e-014       0.0050161      0.00080357      0.00080357
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              345:        0.30770E+01

===============================================================


 INSTANT    0.346000000E+03   TIME STEP NUMBER             346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79789E-02 0.89683E+00
   Friction velocity        uk    :  0.79789E-02 0.89683E+00
   Dimensionless distance   yplus :  0.64236E-01 0.72201E+01
   Friction thermal sca.    tstar : -0.69743E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47927E-01 0.53870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51646E-02      35   0.74841E-03   0.74685E+01 0.17399E+03 
c  Velocity[X]                                      0.30425E+01 
c  Velocity[Y]                                      0.44260E+01 
c  Velocity[Z]                                      0.13266E-29 
c  Pressure     0.11691E-06     501   0.98056E-08   0.11279E+00 0.11776E+04 
c  nu_tilda     0.37833E-05      33   0.12696E-04   0.40665E-06 0.25913E+03 
c  TempC        0.22929E+02      30   0.78305E-03   0.18087E+02 0.43501E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1998          9.3007          4.5729          4.5729
v  Velocity[Y]            -4.6925          7.3342       0.0053285       0.0053285
v  Velocity[Z]       -6.9287e-015     5.1605e-015    -9.3753e-018    -9.3753e-018
v  ǁVelocityǁ         0.0011171          9.3461          4.8809          4.8809
v  Pressure               -45.999          20.662        -0.32301        -0.32301
v  nu_tilda            3.407e-007       0.0042562      0.00069386      0.00069386
v  TempC                       21           73.74          21.362          21.362
v  TurbVisc           1.0949e-014       0.0050162      0.00080434      0.00080434
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              346:        0.30400E+01

===============================================================


 INSTANT    0.347000000E+03   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77180E-02 0.89800E+00
   Friction velocity        uk    :  0.77180E-02 0.89800E+00
   Dimensionless distance   yplus :  0.62135E-01 0.72295E+01
   Friction thermal sca.    tstar : -0.68360E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46360E-01 0.53940E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51686E-02      35   0.73719E-03   0.74685E+01 0.17380E+03 
c  Velocity[X]                                      0.30542E+01 
c  Velocity[Y]                                      0.44143E+01 
c  Velocity[Z]                                      0.11580E-29 
c  Pressure     0.13250E-06     486   0.91739E-08   0.12830E+00 0.43497E+03 
c  nu_tilda     0.37867E-05      33   0.14292E-04   0.40580E-06 0.25854E+03 
c  TempC        0.22945E+02      30   0.69423E-03   0.17556E+02 0.43327E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1953          9.2951          4.5729          4.5729
v  Velocity[Y]            -4.6936          7.3455       0.0053703       0.0053703
v  Velocity[Z]       -6.9287e-015     5.1633e-015    -9.3679e-018    -9.3679e-018
v  ǁVelocityǁ         0.0018464           9.341          4.8819          4.8819
v  Pressure               -46.032          20.664        -0.35337        -0.35337
v  nu_tilda           3.4705e-007       0.0042563      0.00069447      0.00069447
v  TempC                       21           73.71          21.363          21.363
v  TurbVisc           1.1854e-014       0.0050164      0.00080511      0.00080511
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              347:        0.28860E+01

===============================================================


 INSTANT    0.348000000E+03   TIME STEP NUMBER             348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99596E-02 0.89741E+00
   Friction velocity        uk    :  0.99596E-02 0.89741E+00
   Dimensionless distance   yplus :  0.80182E-01 0.72248E+01
   Friction thermal sca.    tstar : -0.63967E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59824E-01 0.53905E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51726E-02      35   0.74207E-03   0.74202E+01 0.17319E+03 
c  Velocity[X]                                      0.30390E+01 
c  Velocity[Y]                                      0.43812E+01 
c  Velocity[Z]                                      0.16997E-29 
c  Pressure     0.15300E-06     442   0.95518E-08   0.14862E+00 0.49814E+03 
c  nu_tilda     0.37900E-05      33   0.12678E-04   0.40504E-06 0.25795E+03 
c  TempC        0.22960E+02      30   0.71351E-03   0.16998E+02 0.43418E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1914           9.289          4.5729          4.5729
v  Velocity[Y]            -4.6938          7.3177       0.0054123       0.0054123
v  Velocity[Z]       -6.9287e-015     7.0714e-015    -9.3483e-018    -9.3483e-018
v  ǁVelocityǁ         0.0028923          9.3352          4.8828          4.8828
v  Pressure               -45.987          20.698        -0.33341        -0.33341
v  nu_tilda           3.5318e-007       0.0042564      0.00069515      0.00069515
v  TempC                       21          73.678          21.364          21.364
v  TurbVisc           1.2762e-014       0.0050165      0.00080587      0.00080587
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              348:        0.33320E+01

===============================================================


 INSTANT    0.349000000E+03   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83881E-02 0.89602E+00
   Friction velocity        uk    :  0.83881E-02 0.89602E+00
   Dimensionless distance   yplus :  0.67530E-01 0.72136E+01
   Friction thermal sca.    tstar : -0.65205E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50385E-01 0.53821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51766E-02      35   0.77802E-03   0.74161E+01 0.17296E+03 
c  Velocity[X]                                      0.30246E+01 
c  Velocity[Y]                                      0.43915E+01 
c  Velocity[Z]                                      0.14180E-29 
c  Pressure     0.12744E-06     457   0.99594E-08   0.12109E+00 0.50578E+03 
c  nu_tilda     0.37934E-05      33   0.14256E-04   0.40421E-06 0.25737E+03 
c  TempC        0.22975E+02      30   0.58392E-03   0.17266E+02 0.43267E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1875          9.2829          4.5729          4.5729
v  Velocity[Y]            -4.6936          7.3329       0.0054544       0.0054544
v  Velocity[Z]       -6.9287e-015     5.7126e-015    -9.3579e-018    -9.3579e-018
v  ǁVelocityǁ         0.0032775          9.3298          4.8838          4.8838
v  Pressure               -46.024          20.758        -0.35395        -0.35395
v  nu_tilda           3.5917e-007       0.0042565      0.00069575      0.00069575
v  TempC                       21          73.646          21.364          21.364
v  TurbVisc           1.3688e-014       0.0050166      0.00080664      0.00080664
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              349:        0.27290E+01

===============================================================


 INSTANT    0.350000000E+03   TIME STEP NUMBER             350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14669E-01 0.89702E+00
   Friction velocity        uk    :  0.14669E-01 0.89702E+00
   Dimensionless distance   yplus :  0.11810E+00 0.72216E+01
   Friction thermal sca.    tstar : -0.63633E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88115E-01 0.53881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51806E-02      35   0.71980E-03   0.74272E+01 0.17280E+03 
c  Velocity[X]                                      0.30619E+01 
c  Velocity[Y]                                      0.43653E+01 
c  Velocity[Z]                                      0.12101E-29 
c  Pressure     0.14251E-06     442   0.98520E-08   0.13911E+00 0.50810E+03 
c  nu_tilda     0.37967E-05      33   0.12648E-04   0.40347E-06 0.25679E+03 
c  TempC        0.22990E+02      30   0.60107E-03   0.16026E+02 0.41937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.184          9.2765          4.5729          4.5729
v  Velocity[Y]            -4.6936          7.3129       0.0054967       0.0054967
v  Velocity[Z]       -6.9287e-015     7.8362e-015    -9.3559e-018    -9.3559e-018
v  ǁVelocityǁ         0.0032465          9.3235          4.8847          4.8847
v  Pressure               -45.975          20.799        -0.33378        -0.33378
v  nu_tilda           3.6501e-007       0.0042566      0.00069643      0.00069643
v  TempC                       21          73.614          21.365          21.365
v  TurbVisc           1.4641e-014       0.0050168       0.0008074       0.0008074
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              350:        0.23490E+01

===============================================================


 INSTANT    0.351000000E+03   TIME STEP NUMBER             351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18343E-01 0.89612E+00
   Friction velocity        uk    :  0.18343E-01 0.89612E+00
   Dimensionless distance   yplus :  0.14767E+00 0.72144E+01
   Friction thermal sca.    tstar : -0.74933E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11018E+00 0.53827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51846E-02      35   0.76136E-03   0.73595E+01 0.17220E+03 
c  Velocity[X]                                      0.30148E+01 
c  Velocity[Y]                                      0.43446E+01 
c  Velocity[Z]                                      0.13077E-29 
c  Pressure     0.10513E-06     457   0.96585E-08   0.10152E+00 0.53673E+03 
c  nu_tilda     0.38000E-05      33   0.14229E-04   0.40269E-06 0.25622E+03 
c  TempC        0.23006E+02      30   0.60783E-03   0.16218E+02 0.42633E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1813          9.2699          4.5729          4.5729
v  Velocity[Y]            -4.6929          7.3366       0.0055392       0.0055392
v  Velocity[Z]       -6.9287e-015      6.319e-015    -9.3774e-018    -9.3774e-018
v  ǁVelocityǁ         0.0036705          9.3179          4.8856          4.8856
v  Pressure               -46.014          20.869        -0.35266        -0.35266
v  nu_tilda           3.7063e-007       0.0042568      0.00069704      0.00069704
v  TempC                       21          73.582          21.366          21.366
v  TurbVisc           1.5616e-014       0.0050169      0.00080816      0.00080816
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              351:        0.27860E+01

===============================================================


 INSTANT    0.352000000E+03   TIME STEP NUMBER             352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39395E-02 0.89696E+00
   Friction velocity        uk    :  0.39395E-02 0.89696E+00
   Dimensionless distance   yplus :  0.31715E-01 0.72212E+01
   Friction thermal sca.    tstar : -0.10380E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23663E-01 0.53878E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51887E-02      35   0.78385E-03   0.73721E+01 0.17204E+03 
c  Velocity[X]                                      0.30193E+01 
c  Velocity[Y]                                      0.43528E+01 
c  Velocity[Z]                                      0.16808E-29 
c  Pressure     0.12613E-06     424   0.94476E-08   0.12233E+00 0.39750E+03 
c  nu_tilda     0.38033E-05      33   0.12617E-04   0.40198E-06 0.25565E+03 
c  TempC        0.23021E+02      30   0.61645E-03   0.17350E+02 0.42765E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1796          9.2631          4.5729          4.5729
v  Velocity[Y]            -4.6927          7.3015       0.0055822       0.0055822
v  Velocity[Z]       -6.9287e-015     8.5944e-015    -9.3814e-018    -9.3814e-018
v  ǁVelocityǁ         0.0028492          9.3114          4.8866          4.8866
v  Pressure               -45.964          20.883        -0.33843        -0.33843
v  nu_tilda           3.7598e-007       0.0042569      0.00069772      0.00069772
v  TempC                       21          73.549          21.366          21.366
v  TurbVisc           1.6601e-014        0.005017      0.00080892      0.00080892
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              352:        0.36560E+01

===============================================================


 INSTANT    0.353000000E+03   TIME STEP NUMBER             353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15388E-01 0.89585E+00
   Friction velocity        uk    :  0.15388E-01 0.89585E+00
   Dimensionless distance   yplus :  0.12388E+00 0.72122E+01
   Friction thermal sca.    tstar : -0.20155E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92432E-01 0.53811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51927E-02      35   0.70918E-03   0.73578E+01 0.17177E+03 
c  Velocity[X]                                      0.30278E+01 
c  Velocity[Y]                                      0.43300E+01 
c  Velocity[Z]                                      0.14057E-29 
c  Pressure     0.12643E-06     409   0.97791E-08   0.12102E+00 0.63288E+03 
c  nu_tilda     0.38066E-05      33   0.14200E-04   0.40122E-06 0.25508E+03 
c  TempC        0.23036E+02      30   0.60137E-03   0.16517E+02 0.42820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1781          9.2561          4.5729          4.5729
v  Velocity[Y]            -4.6918          7.3271       0.0056249       0.0056249
v  Velocity[Z]       -6.9287e-015     9.0299e-015    -9.3972e-018    -9.3972e-018
v  ǁVelocityǁ         0.0023637          9.3054          4.8875          4.8875
v  Pressure               -45.996          20.974        -0.35083        -0.35083
v  nu_tilda           3.8101e-007        0.004257      0.00069832      0.00069832
v  TempC                       21          73.517          21.367          21.367
v  TurbVisc           1.7581e-014       0.0050171      0.00080969      0.00080969
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              353:        0.31110E+01

===============================================================


 INSTANT    0.354000000E+03   TIME STEP NUMBER             354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15956E-01 0.89728E+00
   Friction velocity        uk    :  0.15956E-01 0.89728E+00
   Dimensionless distance   yplus :  0.12846E+00 0.72237E+01
   Friction thermal sca.    tstar : -0.12886E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95843E-01 0.53897E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.51967E-02      35   0.76329E-03   0.73450E+01 0.17138E+03 
c  Velocity[X]                                      0.30507E+01 
c  Velocity[Y]                                      0.42943E+01 
c  Velocity[Z]                                      0.12123E-29 
c  Pressure     0.15502E-06     456   0.99812E-08   0.14900E+00 0.65971E+03 
c  nu_tilda     0.38099E-05      33   0.12582E-04   0.40052E-06 0.25451E+03 
c  TempC        0.23051E+02      30   0.59260E-03   0.15915E+02 0.42445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1766           9.249          4.5729          4.5729
v  Velocity[Y]            -4.6902           7.337       0.0056679       0.0056679
v  Velocity[Z]       -6.9287e-015      7.424e-015    -9.4257e-018    -9.4257e-018
v  ǁVelocityǁ         0.0018516          9.2987          4.8885          4.8885
v  Pressure               -45.947          21.055        -0.32499        -0.32499
v  nu_tilda           3.8571e-007       0.0042571        0.000699        0.000699
v  TempC                       21          73.486          21.367          21.367
v  TurbVisc           1.8541e-014       0.0050173      0.00081045      0.00081045
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              354:        0.26840E+01

===============================================================


 INSTANT    0.355000000E+03   TIME STEP NUMBER             355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94372E-02 0.89688E+00
   Friction velocity        uk    :  0.94372E-02 0.89688E+00
   Dimensionless distance   yplus :  0.75976E-01 0.72205E+01
   Friction thermal sca.    tstar : -0.85504E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56687E-01 0.53873E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52007E-02      35   0.69226E-03   0.73575E+01 0.17118E+03 
c  Velocity[X]                                      0.30530E+01 
c  Velocity[Y]                                      0.43045E+01 
c  Velocity[Z]                                      0.11322E-29 
c  Pressure     0.13794E-06     501   0.98057E-08   0.13187E+00 0.67290E+03 
c  nu_tilda     0.38132E-05      33   0.14156E-04   0.39976E-06 0.25395E+03 
c  TempC        0.23066E+02      30   0.61594E-03   0.17349E+02 0.43693E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1754          9.2418          4.5729          4.5729
v  Velocity[Y]            -4.6888          7.3072       0.0057112       0.0057112
v  Velocity[Z]       -6.9287e-015     8.2306e-015    -9.4482e-018    -9.4482e-018
v  ǁVelocityǁ         0.0019294          9.2924          4.8894          4.8894
v  Pressure               -45.974          20.977        -0.37212        -0.37212
v  nu_tilda           3.9026e-007       0.0042572       0.0006996       0.0006996
v  TempC                       21          73.454          21.368          21.368
v  TurbVisc           1.9472e-014       0.0050174      0.00081122      0.00081122
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              355:        0.26640E+01

===============================================================


 INSTANT    0.356000000E+03   TIME STEP NUMBER             356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80712E-02 0.89539E+00
   Friction velocity        uk    :  0.80712E-02 0.89539E+00
   Dimensionless distance   yplus :  0.64979E-01 0.72085E+01
   Friction thermal sca.    tstar : -0.70919E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48481E-01 0.53783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52047E-02      35   0.71554E-03   0.72646E+01 0.17040E+03 
c  Velocity[X]                                      0.30048E+01 
c  Velocity[Y]                                      0.42597E+01 
c  Velocity[Z]                                      0.12588E-29 
c  Pressure     0.99804E-07     489   0.94192E-08   0.96664E-01 0.10203E+04 
c  nu_tilda     0.38165E-05      33   0.12556E-04   0.39910E-06 0.25339E+03 
c  TempC        0.23082E+02      30   0.61747E-03   0.16034E+02 0.42968E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1758          9.2342          4.5729          4.5729
v  Velocity[Y]            -4.6875          7.3235       0.0057542       0.0057542
v  Velocity[Z]       -6.9287e-015     8.4547e-015    -9.4725e-018    -9.4725e-018
v  ǁVelocityǁ         0.0022734          9.2856          4.8904          4.8904
v  Pressure                -45.93          21.129        -0.33338        -0.33338
v  nu_tilda            3.946e-007       0.0042573      0.00070028      0.00070028
v  TempC                       21          73.424          21.368          21.368
v  TurbVisc           2.0407e-014       0.0050175      0.00081198      0.00081198
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              356:        0.30900E+01

===============================================================


 INSTANT    0.357000000E+03   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11967E-01 0.89624E+00
   Friction velocity        uk    :  0.11967E-01 0.89624E+00
   Dimensionless distance   yplus :  0.96346E-01 0.72153E+01
   Friction thermal sca.    tstar : -0.11014E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71885E-01 0.53835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52087E-02      35   0.81139E-03   0.72593E+01 0.17015E+03 
c  Velocity[X]                                      0.30265E+01 
c  Velocity[Y]                                      0.42329E+01 
c  Velocity[Z]                                      0.11492E-29 
c  Pressure     0.14799E-06     489   0.99068E-08   0.14428E+00 0.69385E+03 
c  nu_tilda     0.38197E-05      33   0.14124E-04   0.39839E-06 0.25284E+03 
c  TempC        0.23097E+02      30   0.63719E-03   0.15285E+02 0.42861E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1762          9.2268          4.5729          4.5729
v  Velocity[Y]            -4.6854          7.3038       0.0057982       0.0057982
v  Velocity[Z]       -7.1273e-015      9.431e-015    -9.4983e-018    -9.4983e-018
v  ǁVelocityǁ         0.0030306          9.2788          4.8913          4.8913
v  Pressure               -45.951          21.041        -0.38083        -0.38083
v  nu_tilda           3.9869e-007       0.0042574      0.00070088      0.00070088
v  TempC                       21          73.393          21.369          21.369
v  TurbVisc           2.1331e-014       0.0050176      0.00081274      0.00081274
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              357:        0.26480E+01

===============================================================


 INSTANT    0.358000000E+03   TIME STEP NUMBER             358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17092E-01 0.89545E+00
   Friction velocity        uk    :  0.17092E-01 0.89545E+00
   Dimensionless distance   yplus :  0.13760E+00 0.72089E+01
   Friction thermal sca.    tstar : -0.56690E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10267E+00 0.53787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52127E-02      35   0.77285E-03   0.72986E+01 0.17017E+03 
c  Velocity[X]                                      0.30682E+01 
c  Velocity[Y]                                      0.42304E+01 
c  Velocity[Z]                                      0.13798E-29 
c  Pressure     0.13504E-06     501   0.98198E-08   0.12971E+00 0.10178E+04 
c  nu_tilda     0.38230E-05      33   0.12519E-04   0.39777E-06 0.25229E+03 
c  TempC        0.23112E+02      30   0.56846E-03   0.16852E+02 0.43555E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1763          9.2188          4.5729          4.5729
v  Velocity[Y]            -4.6841          7.3254       0.0058417       0.0058417
v  Velocity[Z]       -7.9667e-015     8.4526e-015    -9.5308e-018    -9.5308e-018
v  ǁVelocityǁ         0.0037029          9.2719          4.8923          4.8923
v  Pressure               -45.909          21.199        -0.34296        -0.34296
v  nu_tilda           4.0251e-007       0.0042575      0.00070156      0.00070156
v  TempC                       21          73.364          21.369          21.369
v  TurbVisc           2.2228e-014       0.0050177       0.0008135       0.0008135
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              358:        0.31530E+01

===============================================================


 INSTANT    0.359000000E+03   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13648E-02 0.89647E+00
   Friction velocity        uk    :  0.13648E-02 0.89647E+00
   Dimensionless distance   yplus :  0.10987E-01 0.72172E+01
   Friction thermal sca.    tstar : -0.56061E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81979E-02 0.53848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52167E-02      35   0.71894E-03   0.72691E+01 0.16965E+03 
c  Velocity[X]                                      0.30637E+01 
c  Velocity[Y]                                      0.42054E+01 
c  Velocity[Z]                                      0.13640E-29 
c  Pressure     0.16200E-06     517   0.99382E-08   0.15359E+00 0.80156E+03 
c  nu_tilda     0.38262E-05      33   0.14083E-04   0.39708E-06 0.25174E+03 
c  TempC        0.23127E+02      30   0.49363E-03   0.15771E+02 0.42894E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1767          9.2114          4.5729          4.5729
v  Velocity[Y]            -4.6818          7.2936       0.0058859       0.0058859
v  Velocity[Z]       -8.7915e-015     9.4536e-015    -9.5625e-018    -9.5625e-018
v  ǁVelocityǁ         0.0044066          9.2646          4.8932          4.8932
v  Pressure               -45.928          21.092        -0.39563        -0.39563
v  nu_tilda           4.0609e-007       0.0042576      0.00070216      0.00070216
v  TempC                       21          73.334           21.37           21.37
v  TurbVisc           2.3092e-014       0.0050179      0.00081427      0.00081427
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              359:        0.28430E+01

===============================================================


 INSTANT    0.360000000E+03   TIME STEP NUMBER             360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20489E-01 0.89546E+00
   Friction velocity        uk    :  0.20489E-01 0.89546E+00
   Dimensionless distance   yplus :  0.16495E+00 0.72091E+01
   Friction thermal sca.    tstar : -0.52786E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12307E+00 0.53788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52207E-02      35   0.70285E-03   0.71932E+01 0.16900E+03 
c  Velocity[X]                                      0.30190E+01 
c  Velocity[Y]                                      0.41742E+01 
c  Velocity[Z]                                      0.10998E-29 
c  Pressure     0.10834E-06     490   0.94927E-08   0.10384E+00 0.10197E+04 
c  nu_tilda     0.38295E-05      33   0.12491E-04   0.39645E-06 0.25120E+03 
c  TempC        0.23142E+02      30   0.68435E-03   0.13853E+02 0.40186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1784          9.2031          4.5729          4.5729
v  Velocity[Y]            -4.6797          7.3176       0.0059296       0.0059296
v  Velocity[Z]        -9.437e-015     8.8399e-015    -9.5956e-018    -9.5956e-018
v  ǁVelocityǁ         0.0048407          9.2575          4.8942          4.8942
v  Pressure               -45.887          21.251        -0.35795        -0.35795
v  nu_tilda            4.094e-007       0.0042577      0.00070284      0.00070284
v  TempC                       21          73.306          21.371          21.371
v  TurbVisc           2.3925e-014        0.005018      0.00081502      0.00081502
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              360:        0.34710E+01

===============================================================


 INSTANT    0.361000000E+03   TIME STEP NUMBER             361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20615E-01 0.89661E+00
   Friction velocity        uk    :  0.20615E-01 0.89661E+00
   Dimensionless distance   yplus :  0.16596E+00 0.72183E+01
   Friction thermal sca.    tstar : -0.66833E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12383E+00 0.53857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52247E-02      35   0.76128E-03   0.71766E+01 0.16870E+03 
c  Velocity[X]                                      0.30113E+01 
c  Velocity[Y]                                      0.41653E+01 
c  Velocity[Z]                                      0.13413E-29 
c  Pressure     0.13892E-06     472   0.94904E-08   0.13307E+00 0.42093E+03 
c  nu_tilda     0.38327E-05      33   0.14043E-04   0.39574E-06 0.25065E+03 
c  TempC        0.23157E+02      30   0.61841E-03   0.20303E+02 0.48181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1801          9.1949          4.5729          4.5729
v  Velocity[Y]            -4.6772           7.327       0.0059743       0.0059743
v  Velocity[Z]       -9.9372e-015      9.606e-015    -9.6233e-018    -9.6233e-018
v  ǁVelocityǁ         0.0049082          9.2498          4.8951          4.8951
v  Pressure               -45.911          21.255        -0.38865        -0.38865
v  nu_tilda           4.1248e-007       0.0042578      0.00070344      0.00070344
v  TempC                       21          73.278          21.371          21.371
v  TurbVisc           2.4715e-014       0.0050181      0.00081579      0.00081579
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              361:        0.35010E+01

===============================================================


 INSTANT    0.362000000E+03   TIME STEP NUMBER             362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16675E-01 0.89625E+00
   Friction velocity        uk    :  0.16675E-01 0.89625E+00
   Dimensionless distance   yplus :  0.13424E+00 0.72154E+01
   Friction thermal sca.    tstar : -0.58215E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10016E+00 0.53835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52287E-02      35   0.70766E-03   0.72076E+01 0.16860E+03 
c  Velocity[X]                                      0.30783E+01 
c  Velocity[Y]                                      0.41294E+01 
c  Velocity[Z]                                      0.12908E-29 
c  Pressure     0.14994E-06     360   0.99365E-08   0.14502E+00 0.30677E+03 
c  nu_tilda     0.38359E-05      33   0.12460E-04   0.39513E-06 0.25011E+03 
c  TempC        0.23172E+02      30   0.65231E-03   0.16034E+02 0.43631E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1815          9.1865          4.5729          4.5729
v  Velocity[Y]            -4.6741          7.3014       0.0060182       0.0060182
v  Velocity[Z]       -1.0305e-014     8.8572e-015    -9.6542e-018    -9.6542e-018
v  ǁVelocityǁ         0.0046731          9.2426           4.896           4.896
v  Pressure               -45.856          21.232        -0.38492        -0.38492
v  nu_tilda           4.1551e-007       0.0042579      0.00070411      0.00070411
v  TempC                       21          73.251          21.371          21.371
v  TurbVisc           2.5466e-014       0.0050182      0.00081654      0.00081654
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              362:        0.27330E+01

===============================================================


 INSTANT    0.363000000E+03   TIME STEP NUMBER             363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81660E-02 0.89490E+00
   Friction velocity        uk    :  0.81660E-02 0.89490E+00
   Dimensionless distance   yplus :  0.65741E-01 0.72046E+01
   Friction thermal sca.    tstar : -0.64495E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49051E-01 0.53754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52327E-02      35   0.72134E-03   0.71729E+01 0.16802E+03 
c  Velocity[X]                                      0.30662E+01 
c  Velocity[Y]                                      0.41067E+01 
c  Velocity[Z]                                      0.11850E-29 
c  Pressure     0.18182E-06     458   0.98133E-08   0.17119E+00 0.45113E+03 
c  nu_tilda     0.38392E-05      33   0.13988E-04   0.39447E-06 0.24958E+03 
c  TempC        0.23187E+02      30   0.48398E-03   0.15287E+02 0.43109E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1834          9.1778          4.5729          4.5729
v  Velocity[Y]             -4.671          7.3155       0.0060633       0.0060633
v  Velocity[Z]       -1.0532e-014     8.1838e-015    -9.6963e-018    -9.6963e-018
v  ǁVelocityǁ         0.0048817          9.2346           4.897           4.897
v  Pressure               -45.877          21.276        -0.40771        -0.40771
v  nu_tilda           4.1841e-007        0.004258      0.00070472      0.00070472
v  TempC                       21          73.224          21.372          21.372
v  TurbVisc           2.6223e-014       0.0050183      0.00081731      0.00081731
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              363:        0.29410E+01

===============================================================


 INSTANT    0.364000000E+03   TIME STEP NUMBER             364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10650E-01 0.89596E+00
   Friction velocity        uk    :  0.10650E-01 0.89596E+00
   Dimensionless distance   yplus :  0.85736E-01 0.72131E+01
   Friction thermal sca.    tstar : -0.75592E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63969E-01 0.53817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52367E-02      35   0.72142E-03   0.71173E+01 0.16751E+03 
c  Velocity[X]                                      0.30316E+01 
c  Velocity[Y]                                      0.40858E+01 
c  Velocity[Z]                                      0.13392E-29 
c  Pressure     0.13212E-06     329   0.93935E-08   0.12899E+00 0.28761E+03 
c  nu_tilda     0.38424E-05      33   0.12427E-04   0.39388E-06 0.24905E+03 
c  TempC        0.23203E+02      30   0.58985E-03   0.12093E+02 0.38558E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1858          9.1692          4.5729          4.5729
v  Velocity[Y]             -4.668          7.2927       0.0061072       0.0061072
v  Velocity[Z]       -9.9193e-015     7.3901e-015    -9.7345e-018    -9.7345e-018
v  ǁVelocityǁ         0.0040968          9.2271          4.8979          4.8979
v  Pressure                -45.83          21.265        -0.40504        -0.40504
v  nu_tilda           4.2116e-007       0.0042581      0.00070539      0.00070539
v  TempC                       21          73.197          21.372          21.372
v  TurbVisc           2.6964e-014       0.0050184      0.00081806      0.00081806
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              364:        0.23320E+01

===============================================================


 INSTANT    0.365000000E+03   TIME STEP NUMBER             365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18001E-01 0.89508E+00
   Friction velocity        uk    :  0.18001E-01 0.89508E+00
   Dimensionless distance   yplus :  0.14492E+00 0.72060E+01
   Friction thermal sca.    tstar : -0.90895E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10813E+00 0.53765E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52407E-02      35   0.77296E-03   0.70849E+01 0.16709E+03 
c  Velocity[X]                                      0.30402E+01 
c  Velocity[Y]                                      0.40447E+01 
c  Velocity[Z]                                      0.14335E-29 
c  Pressure     0.12220E-06     458   0.92600E-08   0.11651E+00 0.46664E+03 
c  nu_tilda     0.38456E-05      33   0.13959E-04   0.39322E-06 0.24852E+03 
c  TempC        0.23218E+02      30   0.47698E-03   0.12582E+02 0.39114E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1884          9.1603          4.5729          4.5729
v  Velocity[Y]            -4.6644          7.3172       0.0061529       0.0061529
v  Velocity[Z]       -9.8144e-015     8.4387e-015    -9.7642e-018    -9.7642e-018
v  ǁVelocityǁ         0.0036855          9.2189          4.8989          4.8989
v  Pressure               -45.855          21.318        -0.42856        -0.42856
v  nu_tilda           4.2371e-007       0.0042582      0.00070599      0.00070599
v  TempC                       21          73.171          21.373          21.373
v  TurbVisc            2.768e-014       0.0050185      0.00081883      0.00081883
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              365:        0.33550E+01

===============================================================


 INSTANT    0.366000000E+03   TIME STEP NUMBER             366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10182E-01 0.89605E+00
   Friction velocity        uk    :  0.10182E-01 0.89605E+00
   Dimensionless distance   yplus :  0.81972E-01 0.72138E+01
   Friction thermal sca.    tstar : -0.14853E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61160E-01 0.53823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52448E-02      35   0.72197E-03   0.71243E+01 0.16703E+03 
c  Velocity[X]                                      0.30903E+01 
c  Velocity[Y]                                      0.40340E+01 
c  Velocity[Z]                                      0.14174E-29 
c  Pressure     0.18815E-06     408   0.93384E-08   0.18164E+00 0.33159E+03 
c  nu_tilda     0.38488E-05      33   0.12389E-04   0.39259E-06 0.24798E+03 
c  TempC        0.23233E+02      30   0.60543E-03   0.12101E+02 0.39622E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1911          9.1517          4.5729          4.5729
v  Velocity[Y]            -4.6612          7.2909       0.0061977       0.0061977
v  Velocity[Z]       -9.9887e-015     7.9483e-015     -9.792e-018     -9.792e-018
v  ǁVelocityǁ         0.0023999          9.2111          4.8998          4.8998
v  Pressure               -45.796          21.313        -0.41909        -0.41909
v  nu_tilda             4.26e-007       0.0042582      0.00070667      0.00070667
v  TempC                       21          73.199          21.373          21.373
v  TurbVisc           2.8355e-014       0.0050187      0.00081958      0.00081958
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              366:        0.30410E+01

===============================================================


 INSTANT    0.367000000E+03   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46790E-02 0.89490E+00
   Friction velocity        uk    :  0.46790E-02 0.89490E+00
   Dimensionless distance   yplus :  0.37669E-01 0.72046E+01
   Friction thermal sca.    tstar : -0.73302E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28106E-01 0.53754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52488E-02      35   0.63870E-03   0.70383E+01 0.16620E+03 
c  Velocity[X]                                      0.30503E+01 
c  Velocity[Y]                                      0.39881E+01 
c  Velocity[Z]                                      0.12123E-29 
c  Pressure     0.12075E-06     456   0.94601E-08   0.11402E+00 0.45088E+03 
c  nu_tilda     0.38519E-05      33   0.13910E-04   0.39194E-06 0.24746E+03 
c  TempC        0.23248E+02      30   0.54405E-03   0.14015E+02 0.41913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1935          9.1425          4.5729          4.5729
v  Velocity[Y]            -4.6574          7.3153       0.0062432       0.0062432
v  Velocity[Z]       -1.0003e-014      7.307e-015    -9.8299e-018    -9.8299e-018
v  ǁVelocityǁ         0.0023615          9.2029          4.9007          4.9007
v  Pressure               -45.822          21.361        -0.44613        -0.44613
v  nu_tilda           4.2813e-007       0.0042583      0.00070727      0.00070727
v  TempC                       21          73.181          21.374          21.374
v  TurbVisc           2.8974e-014       0.0050188      0.00082035      0.00082035
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              367:        0.33340E+01

===============================================================


 INSTANT    0.368000000E+03   TIME STEP NUMBER             368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94973E-02 0.89581E+00
   Friction velocity        uk    :  0.94973E-02 0.89581E+00
   Dimensionless distance   yplus :  0.76459E-01 0.72119E+01
   Friction thermal sca.    tstar : -0.12505E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57047E-01 0.53809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52528E-02      35   0.78173E-03   0.69763E+01 0.16554E+03 
c  Velocity[X]                                      0.30304E+01 
c  Velocity[Y]                                      0.39459E+01 
c  Velocity[Z]                                      0.12805E-29 
c  Pressure     0.16113E-06     410   0.97265E-08   0.15048E+00 0.35331E+03 
c  nu_tilda     0.38551E-05      33   0.12354E-04   0.39135E-06 0.24694E+03 
c  TempC        0.23263E+02      30   0.61871E-03   0.12147E+02 0.39593E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1964          9.1332          4.5729          4.5729
v  Velocity[Y]            -4.6538          7.3114       0.0062884       0.0062884
v  Velocity[Z]       -9.9329e-015     7.2012e-015    -9.8641e-018    -9.8641e-018
v  ǁVelocityǁ         0.0023051          9.1944          4.9017          4.9017
v  Pressure               -45.768          21.379        -0.43484        -0.43484
v  nu_tilda            4.302e-007       0.0042584      0.00070794      0.00070794
v  TempC                       21          73.206          21.374          21.374
v  TurbVisc           2.9558e-014       0.0050189       0.0008211       0.0008211
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              368:        0.30790E+01

===============================================================


 INSTANT    0.369000000E+03   TIME STEP NUMBER             369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51786E-02 0.89544E+00
   Friction velocity        uk    :  0.51786E-02 0.89544E+00
   Dimensionless distance   yplus :  0.41691E-01 0.72089E+01
   Friction thermal sca.    tstar : -0.96408E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31106E-01 0.53787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52568E-02      35   0.72915E-03   0.70276E+01 0.16559E+03 
c  Velocity[X]                                      0.30942E+01 
c  Velocity[Y]                                      0.39334E+01 
c  Velocity[Z]                                      0.15102E-29 
c  Pressure     0.15809E-06     505   0.92296E-08   0.15207E+00 0.65493E+03 
c  nu_tilda     0.38583E-05      33   0.13873E-04   0.39070E-06 0.24641E+03 
c  TempC        0.23278E+02      30   0.52487E-03   0.14895E+02 0.44066E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2001          9.1239          4.5729          4.5729
v  Velocity[Y]            -4.6497          7.2874       0.0063339       0.0063339
v  Velocity[Z]       -1.0561e-014     6.9373e-015    -9.9015e-018    -9.9015e-018
v  ǁVelocityǁ         0.0025173          9.1862          4.9026          4.9026
v  Pressure               -45.789          21.306        -0.48314        -0.48314
v  nu_tilda           4.3221e-007       0.0042585      0.00070854      0.00070854
v  TempC                       21          73.205          21.375          21.375
v  TurbVisc           3.0132e-014        0.005019      0.00082187      0.00082187
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              369:        0.40410E+01

===============================================================


 INSTANT    0.370000000E+03   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11723E-01 0.89431E+00
   Friction velocity        uk    :  0.11723E-01 0.89431E+00
   Dimensionless distance   yplus :  0.94382E-01 0.71998E+01
   Friction thermal sca.    tstar : -0.11347E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70419E-01 0.53718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52608E-02      35   0.68699E-03   0.69527E+01 0.16484E+03 
c  Velocity[X]                                      0.30541E+01 
c  Velocity[Y]                                      0.38986E+01 
c  Velocity[Z]                                      0.15678E-29 
c  Pressure     0.15765E-06     489   0.97750E-08   0.14997E+00 0.96646E+03 
c  nu_tilda     0.38614E-05      33   0.12318E-04   0.39011E-06 0.24590E+03 
c  TempC        0.23293E+02      30   0.61579E-03   0.12305E+02 0.39760E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2038          9.1145          4.5729          4.5729
v  Velocity[Y]            -4.6451          7.3083       0.0063797       0.0063797
v  Velocity[Z]        -9.704e-015     6.5427e-015    -9.9395e-018    -9.9395e-018
v  ǁVelocityǁ         0.0029085          9.1773          4.9035          4.9035
v  Pressure                -45.74          21.454        -0.44566        -0.44566
v  nu_tilda           4.3406e-007       0.0042586      0.00070922      0.00070922
v  TempC                       21          73.264          21.375          21.375
v  TurbVisc             3.07e-014       0.0050191      0.00082262      0.00082262
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              370:        0.46890E+01

===============================================================


 INSTANT    0.371000000E+03   TIME STEP NUMBER             371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15009E-01 0.89548E+00
   Friction velocity        uk    :  0.15009E-01 0.89548E+00
   Dimensionless distance   yplus :  0.12083E+00 0.72092E+01
   Friction thermal sca.    tstar : -0.66384E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90156E-01 0.53789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52648E-02      35   0.73044E-03   0.69203E+01 0.16433E+03 
c  Velocity[X]                                      0.30585E+01 
c  Velocity[Y]                                      0.38618E+01 
c  Velocity[Z]                                      0.15344E-29 
c  Pressure     0.13461E-06     490   0.98405E-08   0.12911E+00 0.10132E+04 
c  nu_tilda     0.38646E-05      33   0.13829E-04   0.38942E-06 0.24538E+03 
c  TempC        0.23308E+02      30   0.48089E-03   0.13237E+02 0.41681E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.207          9.1052          4.5729          4.5729
v  Velocity[Y]            -4.6408          7.2855       0.0064255       0.0064255
v  Velocity[Z]       -9.4757e-015      6.282e-015    -9.9888e-018    -9.9888e-018
v  ǁVelocityǁ         0.0037901          9.1691          4.9045          4.9045
v  Pressure               -45.761          21.312        -0.51012        -0.51012
v  nu_tilda           4.3588e-007       0.0042587      0.00070982      0.00070982
v  TempC                       21          73.232          21.376          21.376
v  TurbVisc            3.123e-014       0.0050192      0.00082338      0.00082338
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              371:        0.34620E+01

===============================================================


 INSTANT    0.372000000E+03   TIME STEP NUMBER             372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19646E-01 0.89465E+00
   Friction velocity        uk    :  0.19646E-01 0.89465E+00
   Dimensionless distance   yplus :  0.15817E+00 0.72026E+01
   Friction thermal sca.    tstar : -0.64499E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11801E+00 0.53739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52688E-02      35   0.71586E-03   0.68981E+01 0.16397E+03 
c  Velocity[X]                                      0.30506E+01 
c  Velocity[Y]                                      0.38475E+01 
c  Velocity[Z]                                      0.13751E-29 
c  Pressure     0.14131E-06     490   0.95847E-08   0.13499E+00 0.98000E+03 
c  nu_tilda     0.38677E-05      33   0.12282E-04   0.38881E-06 0.24486E+03 
c  TempC        0.23323E+02      30   0.56918E-03   0.10931E+02 0.38128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2103          9.0955          4.5729          4.5729
v  Velocity[Y]            -4.6363          7.3057       0.0064718       0.0064718
v  Velocity[Z]        -9.233e-015       6.39e-015    -1.0024e-017    -1.0024e-017
v  ǁVelocityǁ         0.0044212          9.1603          4.9054          4.9054
v  Pressure               -45.711          21.462        -0.47226        -0.47226
v  nu_tilda           4.3752e-007       0.0042588      0.00071049      0.00071049
v  TempC                       21          73.233          21.376          21.376
v  TurbVisc           3.1756e-014       0.0050193      0.00082414      0.00082414
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              372:        0.33370E+01

===============================================================


 INSTANT    0.373000000E+03   TIME STEP NUMBER             373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14988E-01 0.89574E+00
   Friction velocity        uk    :  0.14988E-01 0.89574E+00
   Dimensionless distance   yplus :  0.12066E+00 0.72113E+01
   Friction thermal sca.    tstar : -0.56158E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90027E-01 0.53805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52728E-02      35   0.72305E-03   0.68696E+01 0.16355E+03 
c  Velocity[X]                                      0.30647E+01 
c  Velocity[Y]                                      0.38050E+01 
c  Velocity[Z]                                      0.13291E-29 
c  Pressure     0.11544E-06     520   0.92874E-08   0.11110E+00 0.10677E+04 
c  nu_tilda     0.38709E-05      33   0.13810E-04   0.38813E-06 0.24435E+03 
c  TempC        0.23338E+02      30   0.52173E-03   0.11232E+02 0.38859E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.214          9.0857          4.5729          4.5729
v  Velocity[Y]            -4.6314          7.2865       0.0065181       0.0065181
v  Velocity[Z]       -8.9801e-015     6.5461e-015    -1.0066e-017    -1.0066e-017
v  ǁVelocityǁ         0.0043356          9.1514          4.9063          4.9063
v  Pressure               -45.731          21.313        -0.53943        -0.53943
v  nu_tilda           4.3902e-007       0.0042589      0.00071109      0.00071109
v  TempC                       21          73.204          21.376          21.376
v  TurbVisc           3.2237e-014       0.0050194       0.0008249       0.0008249
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              373:        0.35950E+01

===============================================================


 INSTANT    0.374000000E+03   TIME STEP NUMBER             374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20144E-01 0.89481E+00
   Friction velocity        uk    :  0.20144E-01 0.89481E+00
   Dimensionless distance   yplus :  0.16217E+00 0.72039E+01
   Friction thermal sca.    tstar : -0.51770E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12100E+00 0.53749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52768E-02      34   0.64660E-03   0.68677E+01 0.16321E+03 
c  Velocity[X]                                      0.30989E+01 
c  Velocity[Y]                                      0.37689E+01 
c  Velocity[Z]                                      0.15401E-29 
c  Pressure     0.15237E-06     520   0.92234E-08   0.14205E+00 0.88815E+03 
c  nu_tilda     0.38740E-05      33   0.12249E-04   0.38750E-06 0.24384E+03 
c  TempC        0.23353E+02      30   0.55242E-03   0.11209E+02 0.38846E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.218          9.0761          4.5729          4.5729
v  Velocity[Y]            -4.6267           7.308       0.0065648       0.0065648
v  Velocity[Z]       -8.6206e-015     6.8106e-015    -1.0099e-017    -1.0099e-017
v  ǁVelocityǁ         0.0046075          9.1427          4.9072          4.9072
v  Pressure               -45.681          21.447        -0.50531        -0.50531
v  nu_tilda           4.4043e-007        0.004259      0.00071176      0.00071176
v  TempC                       21          73.129          21.377          21.377
v  TurbVisc           3.2681e-014       0.0050195      0.00082565      0.00082565
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              374:        0.36300E+01

===============================================================


 INSTANT    0.375000000E+03   TIME STEP NUMBER             375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14206E-01 0.89593E+00
   Friction velocity        uk    :  0.14206E-01 0.89593E+00
   Dimensionless distance   yplus :  0.11437E+00 0.72128E+01
   Friction thermal sca.    tstar : -0.30692E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85330E-01 0.53816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52809E-02      34   0.66605E-03   0.67912E+01 0.16240E+03 
c  Velocity[X]                                      0.30604E+01 
c  Velocity[Y]                                      0.37308E+01 
c  Velocity[Z]                                      0.14820E-29 
c  Pressure     0.14029E-06     488   0.99608E-08   0.13236E+00 0.53760E+03 
c  nu_tilda     0.38771E-05      33   0.13791E-04   0.38682E-06 0.24333E+03 
c  TempC        0.23368E+02      30   0.53205E-03   0.12248E+02 0.40743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2217          9.0662          4.5729          4.5729
v  Velocity[Y]            -4.6215          7.3066       0.0066114       0.0066114
v  Velocity[Z]       -8.2193e-015     7.0542e-015    -1.0143e-017    -1.0143e-017
v  ǁVelocityǁ         0.0045771          9.1333          4.9081          4.9081
v  Pressure               -45.704          21.409        -0.54846        -0.54846
v  nu_tilda           4.4165e-007       0.0042591      0.00071237      0.00071237
v  TempC                       21           73.18          21.377          21.377
v  TurbVisc           3.3103e-014       0.0050196      0.00082642      0.00082642
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              375:        0.35630E+01

===============================================================


 INSTANT    0.376000000E+03   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11892E-01 0.89497E+00
   Friction velocity        uk    :  0.11892E-01 0.89497E+00
   Dimensionless distance   yplus :  0.95741E-01 0.72051E+01
   Friction thermal sca.    tstar : -0.49611E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71433E-01 0.53758E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52849E-02      34   0.75492E-03   0.67563E+01 0.16190E+03 
c  Velocity[X]                                      0.30656E+01 
c  Velocity[Y]                                      0.36907E+01 
c  Velocity[Z]                                      0.14864E-29 
c  Pressure     0.14330E-06     297   0.97928E-08   0.13834E+00 0.30759E+03 
c  nu_tilda     0.38802E-05      33   0.12223E-04   0.38620E-06 0.24282E+03 
c  TempC        0.23383E+02      30   0.57401E-03   0.11371E+02 0.38646E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2252          9.0563          4.5729          4.5729
v  Velocity[Y]            -4.6166          7.2822       0.0066578       0.0066578
v  Velocity[Z]       -7.7676e-015     7.6635e-015    -1.0179e-017    -1.0179e-017
v  ǁVelocityǁ         0.0041279          9.1247          4.9091          4.9091
v  Pressure               -45.649          21.373        -0.54786        -0.54786
v  nu_tilda           4.4283e-007       0.0042591      0.00071304      0.00071304
v  TempC                       21          73.156          21.378          21.378
v  TurbVisc           3.3473e-014       0.0050197      0.00082717      0.00082717
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              376:        0.28240E+01

===============================================================


 INSTANT    0.377000000E+03   TIME STEP NUMBER             377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21505E-01 0.89394E+00
   Friction velocity        uk    :  0.21505E-01 0.89394E+00
   Dimensionless distance   yplus :  0.17313E+00 0.71968E+01
   Friction thermal sca.    tstar : -0.55262E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12917E+00 0.53696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52889E-02      34   0.70755E-03   0.67637E+01 0.16172E+03 
c  Velocity[X]                                      0.30893E+01 
c  Velocity[Y]                                      0.36744E+01 
c  Velocity[Z]                                      0.15640E-29 
c  Pressure     0.14898E-06     472   0.99149E-08   0.14152E+00 0.43566E+03 
c  nu_tilda     0.38833E-05      33   0.13756E-04   0.38547E-06 0.24231E+03 
c  TempC        0.23398E+02      30   0.70114E-03   0.11032E+02 0.38815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2286          9.0465          4.5729          4.5729
v  Velocity[Y]             -4.611          7.3032        0.006705        0.006705
v  Velocity[Z]       -7.3416e-015     8.2725e-015    -1.0212e-017    -1.0212e-017
v  ǁVelocityǁ         0.0042048          9.1155            4.91            4.91
v  Pressure               -45.678          21.416        -0.57573        -0.57573
v  nu_tilda           4.4389e-007       0.0042592      0.00071364      0.00071364
v  TempC                       21          73.184          21.378          21.378
v  TurbVisc           3.3831e-014       0.0050198      0.00082793      0.00082793
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              377:        0.34500E+01

===============================================================


 INSTANT    0.378000000E+03   TIME STEP NUMBER             378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21531E-01 0.89482E+00
   Friction velocity        uk    :  0.21531E-01 0.89482E+00
   Dimensionless distance   yplus :  0.17334E+00 0.72039E+01
   Friction thermal sca.    tstar : -0.57756E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12933E+00 0.53749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52929E-02      34   0.68210E-03   0.67152E+01 0.16116E+03 
c  Velocity[X]                                      0.30692E+01 
c  Velocity[Y]                                      0.36460E+01 
c  Velocity[Z]                                      0.13546E-29 
c  Pressure     0.12601E-06     376   0.93987E-08   0.12105E+00 0.32724E+03 
c  nu_tilda     0.38864E-05      33   0.12189E-04   0.38479E-06 0.24180E+03 
c  TempC        0.23413E+02      30   0.65234E-03   0.12199E+02 0.40483E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2324          9.0366          4.5729          4.5729
v  Velocity[Y]             -4.605          7.2761       0.0067518       0.0067518
v  Velocity[Z]       -6.9287e-015     8.8407e-015    -1.0248e-017    -1.0248e-017
v  ǁVelocityǁ         0.0038455          9.1061          4.9109          4.9109
v  Pressure               -45.628          21.374        -0.57853        -0.57853
v  nu_tilda           4.4483e-007       0.0042593      0.00071431      0.00071431
v  TempC                       21          73.168          21.379          21.379
v  TurbVisc           3.4156e-014       0.0050199      0.00082868      0.00082868
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              378:        0.31790E+01

===============================================================


 INSTANT    0.379000000E+03   TIME STEP NUMBER             379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20587E-01 0.89383E+00
   Friction velocity        uk    :  0.20587E-01 0.89383E+00
   Dimensionless distance   yplus :  0.16574E+00 0.71959E+01
   Friction thermal sca.    tstar : -0.60546E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12366E+00 0.53690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.52970E-02      34   0.70586E-03   0.66636E+01 0.16047E+03 
c  Velocity[X]                                      0.30731E+01 
c  Velocity[Y]                                      0.35905E+01 
c  Velocity[Z]                                      0.15550E-29 
c  Pressure     0.15314E-06     441   0.99746E-08   0.14424E+00 0.49724E+03 
c  nu_tilda     0.38895E-05      33   0.13731E-04   0.38405E-06 0.24129E+03 
c  TempC        0.23428E+02      29   0.61243E-03   0.12614E+02 0.41281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2367          9.0267          4.5729          4.5729
v  Velocity[Y]            -4.5993          7.3034       0.0067993       0.0067993
v  Velocity[Z]       -7.0918e-015     9.2533e-015    -1.0274e-017    -1.0274e-017
v  ǁVelocityǁ         0.0040843          9.0971          4.9118          4.9118
v  Pressure               -45.657          21.442        -0.59973        -0.59973
v  nu_tilda           4.4571e-007       0.0042594      0.00071491      0.00071491
v  TempC                       21          73.201          21.379          21.379
v  TurbVisc           3.4445e-014         0.00502      0.00082945      0.00082945
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              379:        0.34180E+01

===============================================================


 INSTANT    0.380000000E+03   TIME STEP NUMBER             380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18948E-01 0.89508E+00
   Friction velocity        uk    :  0.18948E-01 0.89508E+00
   Dimensionless distance   yplus :  0.15254E+00 0.72060E+01
   Friction thermal sca.    tstar : -0.84770E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11381E+00 0.53765E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53010E-02      34   0.73830E-03   0.66686E+01 0.16025E+03 
c  Velocity[X]                                      0.30926E+01 
c  Velocity[Y]                                      0.35761E+01 
c  Velocity[Z]                                      0.16411E-29 
c  Pressure     0.15110E-06     426   0.97841E-08   0.14261E+00 0.54550E+03 
c  nu_tilda     0.38926E-05      33   0.12164E-04   0.38336E-06 0.24079E+03 
c  TempC        0.23443E+02      29   0.54010E-03   0.12426E+02 0.40730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2404          9.0167          4.5729          4.5729
v  Velocity[Y]            -4.5935          7.2741       0.0068464       0.0068464
v  Velocity[Z]       -6.9287e-015     9.4866e-015    -1.0317e-017    -1.0317e-017
v  ǁVelocityǁ         0.0035031          9.0877          4.9127          4.9127
v  Pressure               -45.606          21.346         -0.6133         -0.6133
v  nu_tilda           4.4667e-007       0.0042595      0.00071558      0.00071558
v  TempC                       21          73.196          21.379          21.379
v  TurbVisc           3.4721e-014       0.0050201       0.0008302       0.0008302
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              380:        0.32940E+01

===============================================================


 INSTANT    0.381000000E+03   TIME STEP NUMBER             381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19432E-01 0.89451E+00
   Friction velocity        uk    :  0.19432E-01 0.89451E+00
   Dimensionless distance   yplus :  0.15644E+00 0.72015E+01
   Friction thermal sca.    tstar : -0.72548E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11672E+00 0.53731E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53051E-02      34   0.64814E-03   0.66676E+01 0.15999E+03 
c  Velocity[X]                                      0.31313E+01 
c  Velocity[Y]                                      0.35364E+01 
c  Velocity[Z]                                      0.15522E-29 
c  Pressure     0.16235E-06     453   0.95549E-08   0.15278E+00 0.48387E+03 
c  nu_tilda     0.38957E-05      33   0.13707E-04   0.38262E-06 0.24029E+03 
c  TempC        0.23458E+02      30   0.65285E-03   0.11211E+02 0.37742E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.244           9.007          4.5729          4.5729
v  Velocity[Y]            -4.5876          7.3004       0.0068944       0.0068944
v  Velocity[Z]       -6.9287e-015     9.6555e-015    -1.0346e-017    -1.0346e-017
v  ǁVelocityǁ         0.0036239          9.0783          4.9136          4.9136
v  Pressure               -45.636          21.409         -0.6355         -0.6355
v  nu_tilda            4.478e-007       0.0042596      0.00071618      0.00071618
v  TempC                       21          73.138           21.38           21.38
v  TurbVisc           3.5019e-014       0.0050202      0.00083096      0.00083096
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              381:        0.33840E+01

===============================================================


 INSTANT    0.382000000E+03   TIME STEP NUMBER             382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19585E-01 0.89569E+00
   Friction velocity        uk    :  0.19585E-01 0.89569E+00
   Dimensionless distance   yplus :  0.15767E+00 0.72109E+01
   Friction thermal sca.    tstar : -0.90232E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11764E+00 0.53802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53092E-02      34   0.68483E-03   0.65483E+01 0.15893E+03 
c  Velocity[X]                                      0.30619E+01 
c  Velocity[Y]                                      0.34864E+01 
c  Velocity[Z]                                      0.16435E-29 
c  Pressure     0.12972E-06     440   0.99102E-08   0.12290E+00 0.34771E+03 
c  nu_tilda     0.38987E-05      33   0.12133E-04   0.38190E-06 0.23978E+03 
c  TempC        0.23473E+02      30   0.64350E-03   0.12590E+02 0.40110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2474          8.9973          4.5729          4.5729
v  Velocity[Y]            -4.5814          7.3069       0.0069414       0.0069414
v  Velocity[Z]       -6.9287e-015      9.747e-015    -1.0379e-017    -1.0379e-017
v  ǁVelocityǁ         0.0035934          9.0692          4.9145          4.9145
v  Pressure               -45.588          21.438        -0.62426        -0.62426
v  nu_tilda            4.491e-007       0.0042596      0.00071685      0.00071685
v  TempC                       21          73.192           21.38           21.38
v  TurbVisc           3.5374e-014       0.0050203      0.00083172      0.00083172
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              382:        0.32590E+01

===============================================================


 INSTANT    0.383000000E+03   TIME STEP NUMBER             383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90780E-03 0.89512E+00
   Friction velocity        uk    :  0.90780E-03 0.89512E+00
   Dimensionless distance   yplus :  0.73084E-02 0.72063E+01
   Friction thermal sca.    tstar : -0.10440E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54529E-02 0.53767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53132E-02      34   0.68257E-03   0.65544E+01 0.15865E+03 
c  Velocity[X]                                      0.30788E+01 
c  Velocity[Y]                                      0.34757E+01 
c  Velocity[Z]                                      0.15447E-29 
c  Pressure     0.16889E-06     505   0.94732E-08   0.16437E+00 0.75986E+03 
c  nu_tilda     0.39018E-05      33   0.13677E-04   0.38109E-06 0.23927E+03 
c  TempC        0.23488E+02      29   0.59192E-03   0.12257E+02 0.41052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2515          8.9878          4.5729          4.5729
v  Velocity[Y]            -4.5748          7.2828       0.0069894       0.0069894
v  Velocity[Z]       -6.9287e-015      9.798e-015    -1.0414e-017    -1.0414e-017
v  ǁVelocityǁ         0.0031886          9.0598          4.9154          4.9154
v  Pressure               -45.611          21.336         -0.6773         -0.6773
v  nu_tilda           4.5059e-007       0.0042597      0.00071746      0.00071746
v  TempC                       21          73.173          21.381          21.381
v  TurbVisc           3.5788e-014       0.0050204      0.00083248      0.00083248
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              383:        0.35530E+01

===============================================================


 INSTANT    0.384000000E+03   TIME STEP NUMBER             384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16951E-01 0.89359E+00
   Friction velocity        uk    :  0.16951E-01 0.89359E+00
   Dimensionless distance   yplus :  0.13647E+00 0.71940E+01
   Friction thermal sca.    tstar : -0.12790E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10182E+00 0.53675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53173E-02      34   0.73255E-03   0.65185E+01 0.15813E+03 
c  Velocity[X]                                      0.30969E+01 
c  Velocity[Y]                                      0.34216E+01 
c  Velocity[Z]                                      0.14089E-29 
c  Pressure     0.15028E-06     456   0.92638E-08   0.14093E+00 0.48298E+03 
c  nu_tilda     0.39048E-05      33   0.12110E-04   0.38033E-06 0.23877E+03 
c  TempC        0.23503E+02      29   0.50833E-03   0.11109E+02 0.38904E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2558          8.9784          4.5729          4.5729
v  Velocity[Y]            -4.5683          7.2944       0.0070369       0.0070369
v  Velocity[Z]       -6.9287e-015      9.069e-015    -1.0445e-017    -1.0445e-017
v  ǁVelocityǁ         0.0027289          9.0503          4.9163          4.9163
v  Pressure               -45.569          21.403        -0.66049        -0.66049
v  nu_tilda           4.5213e-007       0.0042598      0.00071813      0.00071813
v  TempC                       21          73.247          21.381          21.381
v  TurbVisc           3.6266e-014       0.0050205      0.00083323      0.00083323
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              384:        0.33280E+01

===============================================================


 INSTANT    0.385000000E+03   TIME STEP NUMBER             385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10179E-01 0.89462E+00
   Friction velocity        uk    :  0.10179E-01 0.89462E+00
   Dimensionless distance   yplus :  0.81944E-01 0.72023E+01
   Friction thermal sca.    tstar : -0.22807E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61140E-01 0.53737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53214E-02      34   0.70909E-03   0.65091E+01 0.15776E+03 
c  Velocity[X]                                      0.31288E+01 
c  Velocity[Y]                                      0.33803E+01 
c  Velocity[Z]                                      0.13702E-29 
c  Pressure     0.15116E-06     505   0.96990E-08   0.14582E+00 0.81021E+03 
c  nu_tilda     0.39079E-05      33   0.13660E-04   0.37954E-06 0.23826E+03 
c  TempC        0.23518E+02      29   0.66013E-03   0.11024E+02 0.38697E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2598          8.9693          4.5729          4.5729
v  Velocity[Y]            -4.5619          7.2776       0.0070853       0.0070853
v  Velocity[Z]       -6.9287e-015     9.0561e-015    -1.0478e-017    -1.0478e-017
v  ǁVelocityǁ         0.0020597          9.0411          4.9172          4.9172
v  Pressure               -45.597          21.291        -0.71641        -0.71641
v  nu_tilda           4.5362e-007       0.0042599      0.00071873      0.00071873
v  TempC                       21          73.233          21.382          21.382
v  TurbVisc           3.6764e-014       0.0050206      0.00083399      0.00083399
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              385:        0.35470E+01

===============================================================


 INSTANT    0.386000000E+03   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10566E-01 0.89393E+00
   Friction velocity        uk    :  0.10566E-01 0.89393E+00
   Dimensionless distance   yplus :  0.85064E-01 0.71967E+01
   Friction thermal sca.    tstar : -0.29965E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63468E-01 0.53696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53254E-02      34   0.67612E-03   0.64559E+01 0.15719E+03 
c  Velocity[X]                                      0.30813E+01 
c  Velocity[Y]                                      0.33746E+01 
c  Velocity[Z]                                      0.14645E-29 
c  Pressure     0.12794E-06     474   0.99805E-08   0.12218E+00 0.73297E+03 
c  nu_tilda     0.39109E-05      33   0.12085E-04   0.37877E-06 0.23776E+03 
c  TempC        0.23533E+02      30   0.61099E-03   0.12289E+02 0.40578E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2634          8.9604          4.5729          4.5729
v  Velocity[Y]            -4.5552          7.2969       0.0071332       0.0071332
v  Velocity[Z]       -6.9287e-015     8.9766e-015    -1.0506e-017    -1.0506e-017
v  ǁVelocityǁ         0.0020022          9.0319          4.9181          4.9181
v  Pressure               -45.561          21.411         -0.6899         -0.6899
v  nu_tilda           4.5495e-007         0.00426       0.0007194       0.0007194
v  TempC                       21           73.19          21.382          21.382
v  TurbVisc           3.7252e-014       0.0050207      0.00083475      0.00083475
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              386:        0.31380E+01

===============================================================


 INSTANT    0.387000000E+03   TIME STEP NUMBER             387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10889E-01 0.89494E+00
   Friction velocity        uk    :  0.10889E-01 0.89494E+00
   Dimensionless distance   yplus :  0.87662E-01 0.72049E+01
   Friction thermal sca.    tstar : -0.16453E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65406E-01 0.53756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53295E-02      34   0.71347E-03   0.63964E+01 0.15654E+03 
c  Velocity[X]                                      0.30643E+01 
c  Velocity[Y]                                      0.33321E+01 
c  Velocity[Z]                                      0.15150E-29 
c  Pressure     0.14439E-06     504   0.95994E-08   0.13826E+00 0.88158E+03 
c  nu_tilda     0.39139E-05      33   0.13645E-04   0.37795E-06 0.23725E+03 
c  TempC        0.23548E+02      29   0.62568E-03   0.12128E+02 0.40538E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2668           8.952          4.5729          4.5729
v  Velocity[Y]            -4.5485          7.2728       0.0071823       0.0071823
v  Velocity[Z]       -6.9287e-015     8.8987e-015    -1.0538e-017    -1.0538e-017
v  ǁVelocityǁ         0.0015457          9.0226           4.919           4.919
v  Pressure               -45.592           21.29        -0.74935        -0.74935
v  nu_tilda           4.5615e-007         0.00426         0.00072         0.00072
v  TempC                       21          73.203          21.382          21.382
v  TurbVisc            3.769e-014       0.0050208      0.00083551      0.00083551
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              387:        0.33840E+01

===============================================================


 INSTANT    0.388000000E+03   TIME STEP NUMBER             388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69606E-02 0.89398E+00
   Friction velocity        uk    :  0.69606E-02 0.89398E+00
   Dimensionless distance   yplus :  0.56037E-01 0.71972E+01
   Friction thermal sca.    tstar : -0.10781E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41810E-01 0.53699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53336E-02      34   0.64672E-03   0.63908E+01 0.15616E+03 
c  Velocity[X]                                      0.31059E+01 
c  Velocity[Y]                                      0.32849E+01 
c  Velocity[Z]                                      0.15552E-29 
c  Pressure     0.14794E-06     488   0.96053E-08   0.14018E+00 0.68084E+03 
c  nu_tilda     0.39170E-05      33   0.12063E-04   0.37712E-06 0.23674E+03 
c  TempC        0.23563E+02      29   0.51838E-03   0.12309E+02 0.40657E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.27          8.9453          4.5729          4.5729
v  Velocity[Y]            -4.5412          7.2991       0.0072301       0.0072301
v  Velocity[Z]       -6.9287e-015     8.7638e-015    -1.0565e-017    -1.0565e-017
v  ǁVelocityǁ         0.0016974          9.0134          4.9199          4.9199
v  Pressure               -45.554          21.395        -0.72364        -0.72364
v  nu_tilda           4.5741e-007       0.0042601      0.00072067      0.00072067
v  TempC                       21          73.223          21.383          21.383
v  TurbVisc            3.809e-014       0.0050209      0.00083626      0.00083626
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              388:        0.43010E+01

===============================================================


 INSTANT    0.389000000E+03   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99583E-02 0.89514E+00
   Friction velocity        uk    :  0.99583E-02 0.89514E+00
   Dimensionless distance   yplus :  0.80171E-01 0.72065E+01
   Friction thermal sca.    tstar : -0.86605E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59816E-01 0.53768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53377E-02      34   0.66022E-03   0.63488E+01 0.15559E+03 
c  Velocity[X]                                      0.30839E+01 
c  Velocity[Y]                                      0.32649E+01 
c  Velocity[Z]                                      0.15561E-29 
c  Pressure     0.18014E-06     504   0.97985E-08   0.16956E+00 0.68081E+03 
c  nu_tilda     0.39200E-05      33   0.13615E-04   0.37630E-06 0.23624E+03 
c  TempC        0.23578E+02      30   0.53874E-03   0.10668E+02 0.37820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2746          8.9571          4.5729          4.5729
v  Velocity[Y]            -4.5339           7.297       0.0072793       0.0072793
v  Velocity[Z]       -6.9287e-015     8.6067e-015    -1.0589e-017    -1.0589e-017
v  ǁVelocityǁ         0.0020892          9.0046          4.9208          4.9208
v  Pressure               -45.586          21.311        -0.77391        -0.77391
v  nu_tilda            4.585e-007       0.0042602      0.00072128      0.00072128
v  TempC                       21          73.236          21.383          21.383
v  TurbVisc           3.8512e-014        0.005021      0.00083702      0.00083702
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              389:        0.39900E+01

===============================================================


 INSTANT    0.390000000E+03   TIME STEP NUMBER             390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12851E-01 0.89465E+00
   Friction velocity        uk    :  0.12851E-01 0.89465E+00
   Dimensionless distance   yplus :  0.10346E+00 0.72026E+01
   Friction thermal sca.    tstar : -0.81013E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77194E-01 0.53739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53418E-02      34   0.63648E-03   0.63095E+01 0.15503E+03 
c  Velocity[X]                                      0.30773E+01 
c  Velocity[Y]                                      0.32322E+01 
c  Velocity[Z]                                      0.14610E-29 
c  Pressure     0.12004E-06     362   0.97554E-08   0.11645E+00 0.25664E+03 
c  nu_tilda     0.39230E-05      33   0.12047E-04   0.37548E-06 0.23573E+03 
c  TempC        0.23593E+02      29   0.46343E-03   0.99066E+01 0.36768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2787          8.9718          4.5729          4.5729
v  Velocity[Y]            -4.5269          7.2726       0.0073275       0.0073275
v  Velocity[Z]       -6.9287e-015     8.4298e-015    -1.0621e-017    -1.0621e-017
v  ǁVelocityǁ         0.0020248          8.9958          4.9216          4.9216
v  Pressure               -45.549          21.308        -0.77067        -0.77067
v  nu_tilda            4.595e-007       0.0042603      0.00072195      0.00072195
v  TempC                       21          73.238          21.384          21.384
v  TurbVisc            3.888e-014       0.0050211      0.00083778      0.00083778
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              390:        0.28090E+01

===============================================================


 INSTANT    0.391000000E+03   TIME STEP NUMBER             391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11329E-01 0.89311E+00
   Friction velocity        uk    :  0.11329E-01 0.89311E+00
   Dimensionless distance   yplus :  0.91204E-01 0.71902E+01
   Friction thermal sca.    tstar : -0.92435E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68048E-01 0.53647E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53458E-02      34   0.72202E-03   0.62350E+01 0.15433E+03 
c  Velocity[X]                                      0.30521E+01 
c  Velocity[Y]                                      0.31829E+01 
c  Velocity[Z]                                      0.15573E-29 
c  Pressure     0.12461E-06     504   0.91764E-08   0.12016E+00 0.45693E+03 
c  nu_tilda     0.39260E-05      33   0.13601E-04   0.37462E-06 0.23523E+03 
c  TempC        0.23608E+02      29   0.61680E-03   0.10513E+02 0.37605E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2825           8.987          4.5729          4.5729
v  Velocity[Y]            -4.5194          7.2946       0.0073771       0.0073771
v  Velocity[Z]       -6.9287e-015     8.2526e-015    -1.0654e-017    -1.0654e-017
v  ǁVelocityǁ          0.002021          8.9876          4.9225          4.9225
v  Pressure               -45.587          21.289         -0.8097         -0.8097
v  nu_tilda           4.6037e-007       0.0042604      0.00072255      0.00072255
v  TempC                       21          73.244          21.384          21.384
v  TurbVisc            3.922e-014       0.0050212      0.00083854      0.00083854
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              391:        0.29040E+01

===============================================================


 INSTANT    0.392000000E+03   TIME STEP NUMBER             392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94609E-02 0.89415E+00
   Friction velocity        uk    :  0.94609E-02 0.89415E+00
   Dimensionless distance   yplus :  0.76166E-01 0.71985E+01
   Friction thermal sca.    tstar : -0.99052E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56829E-01 0.53709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53499E-02      34   0.72902E-03   0.63031E+01 0.15445E+03 
c  Velocity[X]                                      0.31117E+01 
c  Velocity[Y]                                      0.31914E+01 
c  Velocity[Z]                                      0.14333E-29 
c  Pressure     0.16992E-06     296   0.92696E-08   0.16406E+00 0.26785E+03 
c  nu_tilda     0.39290E-05      33   0.12023E-04   0.37378E-06 0.23472E+03 
c  TempC        0.23623E+02      29   0.53052E-03   0.12598E+02 0.40538E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.286          9.0028          4.5729          4.5729
v  Velocity[Y]            -4.5122          7.2673       0.0074257       0.0074257
v  Velocity[Z]       -6.9287e-015     8.1501e-015    -1.0685e-017    -1.0685e-017
v  ǁVelocityǁ         0.0017771          9.0028          4.9234          4.9234
v  Pressure               -45.551          21.265        -0.80929        -0.80929
v  nu_tilda           4.6119e-007       0.0042604      0.00072322      0.00072322
v  TempC                       21          73.273          21.385          21.385
v  TurbVisc           3.9517e-014       0.0050212      0.00083929      0.00083929
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              392:        0.22480E+01

===============================================================


 INSTANT    0.393000000E+03   TIME STEP NUMBER             393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67049E-02 0.89314E+00
   Friction velocity        uk    :  0.67049E-02 0.89314E+00
   Dimensionless distance   yplus :  0.53979E-01 0.71904E+01
   Friction thermal sca.    tstar : -0.12012E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40274E-01 0.53648E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53540E-02      34   0.67411E-03   0.62229E+01 0.15375E+03 
c  Velocity[X]                                      0.30826E+01 
c  Velocity[Y]                                      0.31404E+01 
c  Velocity[Z]                                      0.15412E-29 
c  Pressure     0.12511E-06     490   0.98890E-08   0.11881E+00 0.42762E+03 
c  nu_tilda     0.39319E-05      33   0.13590E-04   0.37291E-06 0.23422E+03 
c  TempC        0.23638E+02      29   0.61501E-03   0.10530E+02 0.37844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2894          9.0187          4.5729          4.5729
v  Velocity[Y]            -4.5045           7.294       0.0074758       0.0074758
v  Velocity[Z]       -6.9287e-015     8.0096e-015    -1.0719e-017    -1.0719e-017
v  ǁVelocityǁ         0.0018874          9.0187          4.9243          4.9243
v  Pressure               -45.592          21.267        -0.84553        -0.84553
v  nu_tilda           4.6193e-007       0.0042605      0.00072383      0.00072383
v  TempC                       21          73.285          21.385          21.385
v  TurbVisc           3.9799e-014       0.0050213      0.00084006      0.00084006
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              393:        0.28820E+01

===============================================================


 INSTANT    0.394000000E+03   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50704E-02 0.89441E+00
   Friction velocity        uk    :  0.50704E-02 0.89441E+00
   Dimensionless distance   yplus :  0.40820E-01 0.72006E+01
   Friction thermal sca.    tstar : -0.14510E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30456E-01 0.53725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53581E-02      34   0.71615E-03   0.61690E+01 0.15300E+03 
c  Velocity[X]                                      0.30704E+01 
c  Velocity[Y]                                      0.30986E+01 
c  Velocity[Z]                                      0.13799E-29 
c  Pressure     0.15675E-06     410   0.97130E-08   0.14842E+00 0.42537E+03 
c  nu_tilda     0.39349E-05      33   0.12010E-04   0.37210E-06 0.23372E+03 
c  TempC        0.23653E+02      29   0.52571E-03   0.11564E+02 0.39967E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2935          9.0349          4.5729          4.5729
v  Velocity[Y]            -4.4967          7.2635       0.0075247       0.0075247
v  Velocity[Z]       -6.9287e-015     7.8394e-015    -1.0753e-017    -1.0753e-017
v  ǁVelocityǁ          0.001753          9.0349          4.9252          4.9252
v  Pressure               -45.555          21.195        -0.85404        -0.85404
v  nu_tilda           4.6271e-007       0.0042606       0.0007245       0.0007245
v  TempC                       21           73.31          21.386          21.386
v  TurbVisc           4.0056e-014       0.0050214      0.00084081      0.00084081
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              394:        0.26130E+01

===============================================================


 INSTANT    0.395000000E+03   TIME STEP NUMBER             395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65877E-02 0.89372E+00
   Friction velocity        uk    :  0.65877E-02 0.89372E+00
   Dimensionless distance   yplus :  0.53036E-01 0.71950E+01
   Friction thermal sca.    tstar : -0.24536E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39571E-01 0.53683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53622E-02      34   0.61237E-03   0.61619E+01 0.15269E+03 
c  Velocity[X]                                      0.30886E+01 
c  Velocity[Y]                                      0.30733E+01 
c  Velocity[Z]                                      0.13566E-29 
c  Pressure     0.16767E-06     456   0.93017E-08   0.16009E+00 0.50885E+03 
c  nu_tilda     0.39379E-05      33   0.13563E-04   0.37118E-06 0.23321E+03 
c  TempC        0.23668E+02      29   0.51629E-03   0.10835E+02 0.37937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.298          9.0511          4.5729          4.5729
v  Velocity[Y]            -4.4892          7.2886       0.0075746       0.0075746
v  Velocity[Z]       -6.9287e-015     7.6593e-015     -1.079e-017     -1.079e-017
v  ǁVelocityǁ         0.0018748          9.0512           4.926           4.926
v  Pressure               -45.602          21.269        -0.87433        -0.87433
v  nu_tilda           4.6332e-007       0.0042606       0.0007251       0.0007251
v  TempC                       21          73.298          21.386          21.386
v  TurbVisc           4.0328e-014       0.0050215      0.00084157      0.00084157
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              395:        0.27390E+01

===============================================================


 INSTANT    0.396000000E+03   TIME STEP NUMBER             396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57844E-02 0.89494E+00
   Friction velocity        uk    :  0.57844E-02 0.89494E+00
   Dimensionless distance   yplus :  0.46569E-01 0.72049E+01
   Friction thermal sca.    tstar : -0.34888E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34745E-01 0.53757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53663E-02      34   0.64627E-03   0.60901E+01 0.15198E+03 
c  Velocity[X]                                      0.30468E+01 
c  Velocity[Y]                                      0.30433E+01 
c  Velocity[Z]                                      0.14773E-29 
c  Pressure     0.12078E-06     392   0.97138E-08   0.11586E+00 0.26324E+03 
c  nu_tilda     0.39408E-05      33   0.11990E-04   0.37028E-06 0.23270E+03 
c  TempC        0.23683E+02      30   0.53777E-03   0.12217E+02 0.37771E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.302          9.0675          4.5729          4.5729
v  Velocity[Y]             -4.481          7.3011       0.0076237       0.0076237
v  Velocity[Z]       -6.9287e-015     7.4868e-015    -1.0831e-017    -1.0831e-017
v  ǁVelocityǁ         0.0017363          9.0676          4.9269          4.9269
v  Pressure               -45.574           21.28        -0.86877        -0.86877
v  nu_tilda           4.6381e-007       0.0042607      0.00072577      0.00072577
v  TempC                       21          73.304          21.387          21.387
v  TurbVisc           4.0539e-014       0.0050216      0.00084233      0.00084233
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              396:        0.25730E+01

===============================================================


 INSTANT    0.397000000E+03   TIME STEP NUMBER             397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63479E-02 0.89449E+00
   Friction velocity        uk    :  0.63479E-02 0.89449E+00
   Dimensionless distance   yplus :  0.51105E-01 0.72013E+01
   Friction thermal sca.    tstar : -0.16200E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38130E-01 0.53729E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53704E-02      34   0.65942E-03   0.60615E+01 0.15148E+03 
c  Velocity[X]                                      0.30573E+01 
c  Velocity[Y]                                      0.30042E+01 
c  Velocity[Z]                                      0.13334E-29 
c  Pressure     0.14251E-06     520   0.98198E-08   0.13751E+00 0.10393E+04 
c  nu_tilda     0.39438E-05      33   0.13545E-04   0.36937E-06 0.23219E+03 
c  TempC        0.23698E+02      29   0.54518E-03   0.10488E+02 0.36921E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3058           9.084          4.5729          4.5729
v  Velocity[Y]            -4.4731          7.2657       0.0076741       0.0076741
v  Velocity[Z]       -6.9287e-015     7.3586e-015    -1.0873e-017    -1.0873e-017
v  ǁVelocityǁ          0.002226          9.0841          4.9278          4.9278
v  Pressure               -45.616          21.124        -0.93464        -0.93464
v  nu_tilda            4.643e-007       0.0042608      0.00072638      0.00072638
v  TempC                       21          73.324          21.387          21.387
v  TurbVisc           4.0711e-014       0.0050217      0.00084309      0.00084309
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              397:        0.29450E+01

===============================================================


 INSTANT    0.398000000E+03   TIME STEP NUMBER             398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12444E-01 0.89293E+00
   Friction velocity        uk    :  0.12444E-01 0.89293E+00
   Dimensionless distance   yplus :  0.10018E+00 0.71887E+01
   Friction thermal sca.    tstar : -0.11698E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74747E-01 0.53636E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53744E-02      34   0.65163E-03   0.60317E+01 0.15105E+03 
c  Velocity[X]                                      0.30301E+01 
c  Velocity[Y]                                      0.30017E+01 
c  Velocity[Z]                                      0.14532E-29 
c  Pressure     0.12955E-06     458   0.96678E-08   0.12558E+00 0.66184E+03 
c  nu_tilda     0.39467E-05      33   0.11984E-04   0.36852E-06 0.23169E+03 
c  TempC        0.23713E+02      29   0.58246E-03   0.11052E+02 0.38862E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3093          9.1004          4.5729          4.5729
v  Velocity[Y]            -4.4651           7.283       0.0077235       0.0077235
v  Velocity[Z]       -6.9287e-015     7.2036e-015    -1.0915e-017    -1.0915e-017
v  ǁVelocityǁ         0.0020352          9.1005          4.9286          4.9286
v  Pressure               -45.595          21.229        -0.91052        -0.91052
v  nu_tilda           4.6484e-007       0.0042609      0.00072705      0.00072705
v  TempC                       21          73.345          21.387          21.387
v  TurbVisc           4.0886e-014       0.0050218      0.00084384      0.00084384
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              398:        0.27840E+01

===============================================================


 INSTANT    0.399000000E+03   TIME STEP NUMBER             399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10429E-01 0.89392E+00
   Friction velocity        uk    :  0.10429E-01 0.89392E+00
   Dimensionless distance   yplus :  0.83962E-01 0.71967E+01
   Friction thermal sca.    tstar : -0.99106E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62645E-01 0.53695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53785E-02      34   0.71188E-03   0.59946E+01 0.15057E+03 
c  Velocity[X]                                      0.30234E+01 
c  Velocity[Y]                                      0.29712E+01 
c  Velocity[Z]                                      0.16908E-29 
c  Pressure     0.12311E-06     505   0.98058E-08   0.11956E+00 0.10210E+04 
c  nu_tilda     0.39497E-05      33   0.13540E-04   0.36762E-06 0.23118E+03 
c  TempC        0.23728E+02      29   0.56713E-03   0.11741E+02 0.40132E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3133          9.1168          4.5729          4.5729
v  Velocity[Y]            -4.4572           7.265       0.0077744       0.0077744
v  Velocity[Z]       -6.9287e-015     7.0762e-015    -1.0964e-017    -1.0964e-017
v  ǁVelocityǁ         0.0027015          9.1169          4.9295          4.9295
v  Pressure                -45.64          21.077        -0.97598        -0.97598
v  nu_tilda           4.6544e-007       0.0042609      0.00072765      0.00072765
v  TempC                       21          73.293          21.388          21.388
v  TurbVisc           4.1074e-014       0.0050219      0.00084461      0.00084461
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              399:        0.30070E+01

===============================================================


 INSTANT    0.400000000E+03   TIME STEP NUMBER             400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45457E-02 0.89329E+00
   Friction velocity        uk    :  0.45457E-02 0.89329E+00
   Dimensionless distance   yplus :  0.36596E-01 0.71916E+01
   Friction thermal sca.    tstar : -0.83074E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27305E-01 0.53657E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53826E-02      34   0.65765E-03   0.59952E+01 0.15023E+03 
c  Velocity[X]                                      0.30572E+01 
c  Velocity[Y]                                      0.29380E+01 
c  Velocity[Z]                                      0.14851E-29 
c  Pressure     0.15994E-06     474   0.93101E-08   0.14991E+00 0.72172E+03 
c  nu_tilda     0.39526E-05      33   0.11967E-04   0.36675E-06 0.23068E+03 
c  TempC        0.23743E+02      29   0.64099E-03   0.12311E+02 0.39019E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3178          9.1331          4.5729          4.5729
v  Velocity[Y]            -4.4489          7.2881       0.0078242       0.0078242
v  Velocity[Z]       -6.9287e-015     6.9337e-015    -1.1015e-017    -1.1015e-017
v  ǁVelocityǁ         0.0025011          9.1332          4.9304          4.9304
v  Pressure               -45.619          21.189        -0.94833        -0.94833
v  nu_tilda           4.6599e-007        0.004261      0.00072832      0.00072832
v  TempC                       21          73.332          21.388          21.388
v  TurbVisc           4.1288e-014       0.0050219      0.00084536      0.00084536
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              400:        0.27790E+01

===============================================================


 INSTANT    0.401000000E+03   TIME STEP NUMBER             401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80589E-02 0.89463E+00
   Friction velocity        uk    :  0.80589E-02 0.89463E+00
   Dimensionless distance   yplus :  0.64879E-01 0.72024E+01
   Friction thermal sca.    tstar : -0.76995E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48407E-01 0.53738E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53867E-02      34   0.62482E-03   0.59366E+01 0.14955E+03 
c  Velocity[X]                                      0.30332E+01 
c  Velocity[Y]                                      0.29035E+01 
c  Velocity[Z]                                      0.13498E-29 
c  Pressure     0.15743E-06     504   0.93040E-08   0.15175E+00 0.94938E+03 
c  nu_tilda     0.39555E-05      33   0.13513E-04   0.36586E-06 0.23018E+03 
c  TempC        0.23758E+02      29   0.62152E-03   0.12072E+02 0.39712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3222          9.1494          4.5729          4.5729
v  Velocity[Y]            -4.4402          7.2613       0.0078749       0.0078749
v  Velocity[Z]       -6.9287e-015     6.8077e-015    -1.1071e-017    -1.1071e-017
v  ǁVelocityǁ         0.0032123          9.1495          4.9312          4.9312
v  Pressure               -45.667          21.053         -1.0105         -1.0105
v  nu_tilda           4.6633e-007       0.0042611      0.00072893      0.00072893
v  TempC                       21          73.334          21.389          21.389
v  TurbVisc           4.1482e-014        0.005022      0.00084613      0.00084613
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              401:        0.29260E+01

===============================================================


 INSTANT    0.402000000E+03   TIME STEP NUMBER             402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97531E-03 0.89344E+00
   Friction velocity        uk    :  0.97531E-03 0.89344E+00
   Dimensionless distance   yplus :  0.78519E-02 0.71928E+01
   Friction thermal sca.    tstar : -0.67621E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58584E-02 0.53666E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53908E-02      34   0.64344E-03   0.58722E+01 0.14887E+03 
c  Velocity[X]                                      0.30064E+01 
c  Velocity[Y]                                      0.28659E+01 
c  Velocity[Z]                                      0.15017E-29 
c  Pressure     0.11410E-06     472   0.97467E-08   0.10914E+00 0.60891E+03 
c  nu_tilda     0.39585E-05      33   0.11967E-04   0.36500E-06 0.22969E+03 
c  TempC        0.23773E+02      29   0.54196E-03   0.11996E+02 0.39494E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3261          9.1655          4.5729          4.5729
v  Velocity[Y]            -4.4316          7.2832       0.0079247       0.0079247
v  Velocity[Z]       -6.9287e-015     6.7698e-015    -1.1124e-017    -1.1124e-017
v  ǁVelocityǁ         0.0030514          9.1656          4.9321          4.9321
v  Pressure                -45.65          21.148        -0.98845        -0.98845
v  nu_tilda            4.665e-007       0.0042611       0.0007296       0.0007296
v  TempC                       21          73.314          21.389          21.389
v  TurbVisc           4.1604e-014       0.0050221      0.00084688      0.00084688
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              402:        0.28080E+01

===============================================================


 INSTANT    0.403000000E+03   TIME STEP NUMBER             403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98317E-02 0.89461E+00
   Friction velocity        uk    :  0.98317E-02 0.89461E+00
   Dimensionless distance   yplus :  0.79152E-01 0.72022E+01
   Friction thermal sca.    tstar : -0.64309E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59056E-01 0.53737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53949E-02      34   0.68366E-03   0.58643E+01 0.14861E+03 
c  Velocity[X]                                      0.30103E+01 
c  Velocity[Y]                                      0.28540E+01 
c  Velocity[Z]                                      0.14584E-29 
c  Pressure     0.14612E-06     505   0.94831E-08   0.14114E+00 0.59111E+03 
c  nu_tilda     0.39614E-05      33   0.13494E-04   0.36411E-06 0.22919E+03 
c  TempC        0.23788E+02      29   0.55584E-03   0.11470E+02 0.38859E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.33          9.1814          4.5729          4.5729
v  Velocity[Y]            -4.4232          7.2927        0.007976        0.007976
v  Velocity[Z]       -6.9287e-015     6.5615e-015    -1.1182e-017    -1.1182e-017
v  ǁVelocityǁ         0.0034703          9.1815           4.933           4.933
v  Pressure               -45.705          21.092         -1.0361         -1.0361
v  nu_tilda           4.6657e-007       0.0042612       0.0007302       0.0007302
v  TempC                       21          73.338           21.39           21.39
v  TurbVisc           4.1665e-014       0.0050222      0.00084764      0.00084764
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              403:        0.29080E+01

===============================================================


 INSTANT    0.404000000E+03   TIME STEP NUMBER             404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19082E-01 0.89400E+00
   Friction velocity        uk    :  0.19082E-01 0.89400E+00
   Dimensionless distance   yplus :  0.15363E+00 0.71973E+01
   Friction thermal sca.    tstar : -0.62155E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11462E+00 0.53700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53990E-02      34   0.61302E-03   0.58468E+01 0.14823E+03 
c  Velocity[X]                                      0.30116E+01 
c  Velocity[Y]                                      0.28352E+01 
c  Velocity[Z]                                      0.13642E-29 
c  Pressure     0.11940E-06     377   0.96426E-08   0.11669E+00 0.32327E+03 
c  nu_tilda     0.39643E-05      33   0.11956E-04   0.36320E-06 0.22869E+03 
c  TempC        0.23803E+02      29   0.55799E-03   0.12398E+02 0.39204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3341          9.1971          4.5729          4.5729
v  Velocity[Y]            -4.4147          7.2608       0.0080261       0.0080261
v  Velocity[Z]       -6.9287e-015      6.622e-015    -1.1239e-017    -1.1239e-017
v  ǁVelocityǁ         0.0038169          9.1973          4.9338          4.9338
v  Pressure               -45.686          21.046         -1.0418         -1.0418
v  nu_tilda           4.6666e-007       0.0042613      0.00073087      0.00073087
v  TempC                       21          73.371           21.39           21.39
v  TurbVisc           4.1691e-014       0.0050223       0.0008484       0.0008484
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              404:        0.25090E+01

===============================================================


 INSTANT    0.405000000E+03   TIME STEP NUMBER             405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16985E-01 0.89264E+00
   Friction velocity        uk    :  0.16985E-01 0.89264E+00
   Dimensionless distance   yplus :  0.13674E+00 0.71863E+01
   Friction thermal sca.    tstar : -0.61813E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10202E+00 0.53618E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54031E-02      34   0.66471E-03   0.57858E+01 0.14758E+03 
c  Velocity[X]                                      0.29871E+01 
c  Velocity[Y]                                      0.27987E+01 
c  Velocity[Z]                                      0.14195E-29 
c  Pressure     0.12931E-06     473   0.93222E-08   0.12451E+00 0.41077E+03 
c  nu_tilda     0.39672E-05      33   0.13492E-04   0.36229E-06 0.22819E+03 
c  TempC        0.23818E+02      29   0.63075E-03   0.11530E+02 0.38614E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3389          9.2127          4.5729          4.5729
v  Velocity[Y]             -4.406          7.2872       0.0080778       0.0080778
v  Velocity[Z]       -6.9287e-015     6.3215e-015    -1.1299e-017    -1.1299e-017
v  ǁVelocityǁ         0.0040958          9.2128          4.9347          4.9347
v  Pressure               -45.747          21.058         -1.0755         -1.0755
v  nu_tilda           4.6672e-007       0.0042613      0.00073148      0.00073148
v  TempC                       21          73.379          21.391          21.391
v  TurbVisc           4.1723e-014       0.0050223      0.00084916      0.00084916
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              405:        0.28170E+01

===============================================================


 INSTANT    0.406000000E+03   TIME STEP NUMBER             406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59825E-02 0.89375E+00
   Friction velocity        uk    :  0.59825E-02 0.89375E+00
   Dimensionless distance   yplus :  0.48163E-01 0.71953E+01
   Friction thermal sca.    tstar : -0.63841E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35935E-01 0.53685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54071E-02      34   0.67143E-03   0.58065E+01 0.14738E+03 
c  Velocity[X]                                      0.30096E+01 
c  Velocity[Y]                                      0.27969E+01 
c  Velocity[Z]                                      0.12920E-29 
c  Pressure     0.19498E-06     393   0.94470E-08   0.18578E+00 0.41455E+03 
c  nu_tilda     0.39700E-05      33   0.11945E-04   0.36139E-06 0.22769E+03 
c  TempC        0.23833E+02      29   0.62876E-03   0.12291E+02 0.40045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3436          9.2285          4.5729          4.5729
v  Velocity[Y]            -4.3971          7.2559       0.0081283       0.0081283
v  Velocity[Z]       -6.9287e-015     6.3585e-015     -1.136e-017     -1.136e-017
v  ǁVelocityǁ         0.0046719          9.2287          4.9355          4.9355
v  Pressure               -45.725          20.983          -1.081          -1.081
v  nu_tilda           4.6676e-007       0.0042614      0.00073215      0.00073215
v  TempC                       21          73.397          21.392          21.392
v  TurbVisc           4.1745e-014       0.0050224      0.00084992      0.00084992
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              406:        0.25420E+01

===============================================================


 INSTANT    0.407000000E+03   TIME STEP NUMBER             407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84612E-02 0.89317E+00
   Friction velocity        uk    :  0.84612E-02 0.89317E+00
   Dimensionless distance   yplus :  0.68118E-01 0.71906E+01
   Friction thermal sca.    tstar : -0.69240E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50824E-01 0.53650E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54112E-02      34   0.62169E-03   0.57579E+01 0.14683E+03 
c  Velocity[X]                                      0.30023E+01 
c  Velocity[Y]                                      0.27556E+01 
c  Velocity[Z]                                      0.14687E-29 
c  Pressure     0.11607E-06     474   0.95605E-08   0.11156E+00 0.42776E+03 
c  nu_tilda     0.39729E-05      33   0.13457E-04   0.36050E-06 0.22719E+03 
c  TempC        0.23848E+02      29   0.80468E-03   0.12275E+02 0.39981E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3481          9.2447          4.5729          4.5729
v  Velocity[Y]            -4.3879           7.282       0.0081796       0.0081796
v  Velocity[Z]       -6.9287e-015     6.0968e-015    -1.1423e-017    -1.1423e-017
v  ǁVelocityǁ         0.0048537          9.2449          4.9364          4.9364
v  Pressure               -45.794          21.013         -1.1149         -1.1149
v  nu_tilda           4.6668e-007       0.0042615      0.00073276      0.00073276
v  TempC                       21          73.381          21.392          21.392
v  TurbVisc            4.176e-014       0.0050225      0.00085068      0.00085068
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              407:        0.28200E+01

===============================================================


 INSTANT    0.408000000E+03   TIME STEP NUMBER             408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19284E-01 0.89425E+00
   Friction velocity        uk    :  0.19284E-01 0.89425E+00
   Dimensionless distance   yplus :  0.15525E+00 0.71993E+01
   Friction thermal sca.    tstar : -0.71293E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11583E+00 0.53715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54153E-02      34   0.65775E-03   0.56942E+01 0.14618E+03 
c  Velocity[X]                                      0.29701E+01 
c  Velocity[Y]                                      0.27241E+01 
c  Velocity[Z]                                      0.12584E-29 
c  Pressure     0.12787E-06     393   0.92520E-08   0.12453E+00 0.40417E+03 
c  nu_tilda     0.39758E-05      33   0.11935E-04   0.35965E-06 0.22670E+03 
c  TempC        0.23862E+02      29   0.56400E-03   0.18224E+02 0.47424E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3523          9.2608          4.5729          4.5729
v  Velocity[Y]            -4.3792          7.2615       0.0082307       0.0082307
v  Velocity[Z]       -6.9287e-015     6.1447e-015    -1.1487e-017    -1.1487e-017
v  ǁVelocityǁ         0.0053467          9.2609          4.9372          4.9372
v  Pressure               -45.778          20.945         -1.1228         -1.1228
v  nu_tilda           4.6651e-007       0.0042615      0.00073343      0.00073343
v  TempC                       21          73.353          21.393          21.393
v  TurbVisc           4.1729e-014       0.0050226      0.00085144      0.00085144
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              408:        0.25480E+01

===============================================================


 INSTANT    0.409000000E+03   TIME STEP NUMBER             409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10604E-01 0.89336E+00
   Friction velocity        uk    :  0.10604E-01 0.89336E+00
   Dimensionless distance   yplus :  0.85371E-01 0.71922E+01
   Friction thermal sca.    tstar : -0.77153E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63696E-01 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54194E-02      34   0.60157E-03   0.56720E+01 0.14583E+03 
c  Velocity[X]                                      0.29484E+01 
c  Velocity[Y]                                      0.27236E+01 
c  Velocity[Z]                                      0.14056E-29 
c  Pressure     0.11682E-06     489   0.94636E-08   0.11311E+00 0.42836E+03 
c  nu_tilda     0.39787E-05      33   0.13449E-04   0.35877E-06 0.22621E+03 
c  TempC        0.23877E+02      29   0.54024E-03   0.12901E+02 0.39248E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3569          9.2766          4.5729          4.5729
v  Velocity[Y]            -4.3702           7.286       0.0082822       0.0082822
v  Velocity[Z]       -6.9287e-015     5.8783e-015    -1.1555e-017    -1.1555e-017
v  ǁVelocityǁ         0.0054793          9.2766          4.9381          4.9381
v  Pressure               -45.851          20.978          -1.156          -1.156
v  nu_tilda           4.6625e-007       0.0042616      0.00073404      0.00073404
v  TempC                       21          73.369          21.393          21.393
v  TurbVisc            4.167e-014       0.0050227       0.0008522       0.0008522
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              409:        0.28290E+01

===============================================================


 INSTANT    0.410000000E+03   TIME STEP NUMBER             410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16107E-01 0.89402E+00
   Friction velocity        uk    :  0.16107E-01 0.89402E+00
   Dimensionless distance   yplus :  0.12968E+00 0.71975E+01
   Friction thermal sca.    tstar : -0.80197E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96753E-01 0.53701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54235E-02      34   0.69223E-03   0.56442E+01 0.14539E+03 
c  Velocity[X]                                      0.29391E+01 
c  Velocity[Y]                                      0.27051E+01 
c  Velocity[Z]                                      0.11751E-29 
c  Pressure     0.15524E-06     344   0.97430E-08   0.14779E+00 0.26163E+03 
c  nu_tilda     0.39815E-05      33   0.11928E-04   0.35790E-06 0.22572E+03 
c  TempC        0.23892E+02      29   0.51239E-03   0.12565E+02 0.38686E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3621          9.2922          4.5729          4.5729
v  Velocity[Y]            -4.3612          7.2816       0.0083339       0.0083339
v  Velocity[Z]       -6.9287e-015     5.8961e-015    -1.1617e-017    -1.1617e-017
v  ǁVelocityǁ         0.0053799          9.2923          4.9389          4.9389
v  Pressure                -45.84          20.954         -1.1555         -1.1555
v  nu_tilda           4.6592e-007       0.0042617      0.00073471      0.00073471
v  TempC                       21          73.344          21.394          21.394
v  TurbVisc           4.1576e-014       0.0050227      0.00085296      0.00085296
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              410:        0.24020E+01

===============================================================


 INSTANT    0.411000000E+03   TIME STEP NUMBER             411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10566E-01 0.89340E+00
   Friction velocity        uk    :  0.10566E-01 0.89340E+00
   Dimensionless distance   yplus :  0.85065E-01 0.71925E+01
   Friction thermal sca.    tstar : -0.88689E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63468E-01 0.53664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54275E-02      34   0.68169E-03   0.56516E+01 0.14516E+03 
c  Velocity[X]                                      0.29782E+01 
c  Velocity[Y]                                      0.26733E+01 
c  Velocity[Z]                                      0.13487E-29 
c  Pressure     0.14646E-06     505   0.96147E-08   0.14305E+00 0.89296E+03 
c  nu_tilda     0.39844E-05      33   0.13446E-04   0.35703E-06 0.22524E+03 
c  TempC        0.23907E+02      29   0.71802E-03   0.12752E+02 0.39641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3668          9.3077          4.5729          4.5729
v  Velocity[Y]            -4.3519          7.2565       0.0083856       0.0083856
v  Velocity[Z]       -6.9287e-015      5.882e-015    -1.1684e-017    -1.1684e-017
v  ǁVelocityǁ         0.0051242          9.3077          4.9397          4.9397
v  Pressure               -45.907          20.827         -1.2168         -1.2168
v  nu_tilda            4.656e-007       0.0042617      0.00073532      0.00073532
v  TempC                       21          73.377          21.394          21.394
v  TurbVisc           4.1459e-014       0.0050228      0.00085373      0.00085373
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              411:        0.35110E+01

===============================================================


 INSTANT    0.412000000E+03   TIME STEP NUMBER             412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21640E-01 0.89218E+00
   Friction velocity        uk    :  0.21640E-01 0.89218E+00
   Dimensionless distance   yplus :  0.17421E+00 0.71827E+01
   Friction thermal sca.    tstar : -0.87301E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12998E+00 0.53591E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54316E-02      34   0.62282E-03   0.56043E+01 0.14466E+03 
c  Velocity[X]                                      0.29331E+01 
c  Velocity[Y]                                      0.26712E+01 
c  Velocity[Z]                                      0.14469E-29 
c  Pressure     0.14982E-06     472   0.98467E-08   0.14338E+00 0.69424E+03 
c  nu_tilda     0.39872E-05      33   0.11925E-04   0.35614E-06 0.22475E+03 
c  TempC        0.23922E+02      29   0.58987E-03   0.15331E+02 0.43390E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3716          9.3228          4.5729          4.5729
v  Velocity[Y]            -4.3426           7.275       0.0084369       0.0084369
v  Velocity[Z]       -6.9287e-015     5.7828e-015    -1.1748e-017    -1.1748e-017
v  ǁVelocityǁ         0.0048194          9.3228          4.9406          4.9406
v  Pressure               -45.903          20.932         -1.1892         -1.1892
v  nu_tilda            4.652e-007       0.0042618      0.00073599      0.00073599
v  TempC                       21          73.418          21.395          21.395
v  TurbVisc           4.1346e-014       0.0050229      0.00085448      0.00085448
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              412:        0.30390E+01

===============================================================


 INSTANT    0.413000000E+03   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21528E-01 0.89337E+00
   Friction velocity        uk    :  0.21528E-01 0.89337E+00
   Dimensionless distance   yplus :  0.17332E+00 0.71922E+01
   Friction thermal sca.    tstar : -0.93592E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12932E+00 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54357E-02      34   0.58385E-03   0.55391E+01 0.14390E+03 
c  Velocity[X]                                      0.29047E+01 
c  Velocity[Y]                                      0.26344E+01 
c  Velocity[Z]                                      0.12506E-29 
c  Pressure     0.13678E-06     506   0.99590E-08   0.13467E+00 0.84370E+03 
c  nu_tilda     0.39901E-05      33   0.13420E-04   0.35528E-06 0.22426E+03 
c  TempC        0.23937E+02      29   0.57148E-03   0.13690E+02 0.40534E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3762          9.3378          4.5729          4.5729
v  Velocity[Y]            -4.3335          7.2529       0.0084891       0.0084891
v  Velocity[Z]       -6.9287e-015     5.8521e-015    -1.1815e-017    -1.1815e-017
v  ǁVelocityǁ         0.0038948          9.3378          4.9414          4.9414
v  Pressure               -45.976          20.822         -1.2492         -1.2492
v  nu_tilda            4.648e-007       0.0042619      0.00073659      0.00073659
v  TempC                       21          73.437          21.396          21.396
v  TurbVisc           4.1204e-014        0.005023      0.00085525      0.00085525
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              413:        0.29030E+01

===============================================================


 INSTANT    0.414000000E+03   TIME STEP NUMBER             414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10705E-01 0.89234E+00
   Friction velocity        uk    :  0.10705E-01 0.89234E+00
   Dimensionless distance   yplus :  0.86183E-01 0.71839E+01
   Friction thermal sca.    tstar : -0.10621E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64302E-01 0.53600E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54398E-02      34   0.66764E-03   0.55065E+01 0.14347E+03 
c  Velocity[X]                                      0.28843E+01 
c  Velocity[Y]                                      0.26222E+01 
c  Velocity[Z]                                      0.11662E-29 
c  Pressure     0.14026E-06     472   0.92926E-08   0.13514E+00 0.50490E+03 
c  nu_tilda     0.39929E-05      33   0.11921E-04   0.35442E-06 0.22378E+03 
c  TempC        0.23952E+02      29   0.49095E-03   0.11955E+02 0.38692E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3813          9.3523          4.5729          4.5729
v  Velocity[Y]             -4.324          7.2767       0.0085409       0.0085409
v  Velocity[Z]       -6.9287e-015     5.9043e-015    -1.1881e-017    -1.1881e-017
v  ǁVelocityǁ         0.0040673          9.3523          4.9423          4.9423
v  Pressure               -45.976          20.895         -1.2302         -1.2302
v  nu_tilda           4.6429e-007       0.0042619      0.00073726      0.00073726
v  TempC                       21          73.412          21.396          21.396
v  TurbVisc           4.1061e-014        0.005023        0.000856        0.000856
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              414:        0.28160E+01

===============================================================


 INSTANT    0.415000000E+03   TIME STEP NUMBER             415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21403E-01 0.89369E+00
   Friction velocity        uk    :  0.21403E-01 0.89369E+00
   Dimensionless distance   yplus :  0.17231E+00 0.71948E+01
   Friction thermal sca.    tstar : -0.11391E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12856E+00 0.53681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54438E-02      34   0.63790E-03   0.55187E+01 0.14333E+03 
c  Velocity[X]                                      0.29003E+01 
c  Velocity[Y]                                      0.26184E+01 
c  Velocity[Z]                                      0.15121E-29 
c  Pressure     0.16118E-06     522   0.93472E-08   0.15406E+00 0.12272E+04 
c  nu_tilda     0.39957E-05      33   0.13405E-04   0.35359E-06 0.22330E+03 
c  TempC        0.23966E+02      29   0.50887E-03   0.10833E+02 0.36611E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3867          9.3666          4.5729          4.5729
v  Velocity[Y]            -4.3145          7.2558       0.0085932       0.0085932
v  Velocity[Z]       -6.9287e-015     6.0221e-015    -1.1951e-017    -1.1951e-017
v  ǁVelocityǁ         0.0027476          9.3666          4.9431          4.9431
v  Pressure                -46.05          20.709         -1.3059         -1.3059
v  nu_tilda           4.6382e-007        0.004262      0.00073787      0.00073787
v  TempC                       21          73.375          21.397          21.397
v  TurbVisc           4.0883e-014       0.0050231      0.00085677      0.00085677
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              415:        0.30910E+01

===============================================================


 INSTANT    0.416000000E+03   TIME STEP NUMBER             416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18078E-01 0.89307E+00
   Friction velocity        uk    :  0.18078E-01 0.89307E+00
   Dimensionless distance   yplus :  0.14554E+00 0.71899E+01
   Friction thermal sca.    tstar : -0.12356E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10859E+00 0.53644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54479E-02      34   0.57966E-03   0.54712E+01 0.14279E+03 
c  Velocity[X]                                      0.28879E+01 
c  Velocity[Y]                                      0.25833E+01 
c  Velocity[Z]                                      0.13670E-29 
c  Pressure     0.14261E-06     488   0.98237E-08   0.13869E+00 0.88101E+03 
c  nu_tilda     0.39986E-05      33   0.11917E-04   0.35275E-06 0.22282E+03 
c  TempC        0.23981E+02      30   0.63254E-03   0.11601E+02 0.36673E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3918          9.3805          4.5729          4.5729
v  Velocity[Y]            -4.3051          7.2773       0.0086454       0.0086454
v  Velocity[Z]       -6.9287e-015      6.196e-015    -1.2014e-017    -1.2014e-017
v  ǁVelocityǁ         0.0039958          9.3806          4.9439          4.9439
v  Pressure               -46.056          20.854         -1.2718         -1.2718
v  nu_tilda           4.6325e-007        0.004262      0.00073854      0.00073854
v  TempC                       21          73.348          21.397          21.397
v  TurbVisc           4.0715e-014       0.0050232      0.00085753      0.00085753
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              416:        0.28640E+01

===============================================================


 INSTANT    0.417000000E+03   TIME STEP NUMBER             417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14922E-01 0.89375E+00
   Friction velocity        uk    :  0.14922E-01 0.89375E+00
   Dimensionless distance   yplus :  0.12013E+00 0.71953E+01
   Friction thermal sca.    tstar : -0.22525E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89630E-01 0.53685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54520E-02      34   0.64661E-03   0.54216E+01 0.14226E+03 
c  Velocity[X]                                      0.28356E+01 
c  Velocity[Y]                                      0.25860E+01 
c  Velocity[Z]                                      0.12543E-29 
c  Pressure     0.15759E-06     501   0.97345E-08   0.15327E+00 0.58922E+03 
c  nu_tilda     0.40014E-05      33   0.13392E-04   0.35191E-06 0.22235E+03 
c  TempC        0.23996E+02      30   0.70176E-03   0.13948E+02 0.41400E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.397          9.3942          4.5729          4.5729
v  Velocity[Y]            -4.2958          7.2771       0.0086982       0.0086982
v  Velocity[Z]       -6.9287e-015     6.2309e-015    -1.2083e-017    -1.2083e-017
v  ǁVelocityǁ         0.0031326          9.3942          4.9447          4.9447
v  Pressure               -46.131           20.79         -1.3189         -1.3189
v  nu_tilda           4.6271e-007       0.0042621      0.00073916      0.00073916
v  TempC                       21          73.381          21.398          21.398
v  TurbVisc           4.0517e-014       0.0050232      0.00085829      0.00085829
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              417:        0.29030E+01

===============================================================


 INSTANT    0.418000000E+03   TIME STEP NUMBER             418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18804E-01 0.89279E+00
   Friction velocity        uk    :  0.18804E-01 0.89279E+00
   Dimensionless distance   yplus :  0.15138E+00 0.71876E+01
   Friction thermal sca.    tstar : -0.17577E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11295E+00 0.53627E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54560E-02      34   0.62094E-03   0.54283E+01 0.14200E+03 
c  Velocity[X]                                      0.28693E+01 
c  Velocity[Y]                                      0.25590E+01 
c  Velocity[Z]                                      0.11946E-29 
c  Pressure     0.14570E-06     408   0.99897E-08   0.14309E+00 0.39285E+03 
c  nu_tilda     0.40042E-05      33   0.11912E-04   0.35106E-06 0.22187E+03 
c  TempC        0.24011E+02      29   0.59561E-03   0.14151E+02 0.42227E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4018          9.4075          4.5729          4.5729
v  Velocity[Y]            -4.2862           7.251       0.0087498       0.0087498
v  Velocity[Z]       -6.9287e-015     6.2675e-015    -1.2155e-017    -1.2155e-017
v  ǁVelocityǁ         0.0020037          9.4075          4.9456          4.9456
v  Pressure               -46.137          20.725         -1.3282         -1.3282
v  nu_tilda           4.6217e-007       0.0042622      0.00073983      0.00073983
v  TempC                       21          73.369          21.398          21.398
v  TurbVisc           4.0327e-014       0.0050233      0.00085905      0.00085905
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              418:        0.26040E+01

===============================================================


 INSTANT    0.419000000E+03   TIME STEP NUMBER             419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13709E-01 0.89137E+00
   Friction velocity        uk    :  0.13709E-01 0.89137E+00
   Dimensionless distance   yplus :  0.11037E+00 0.71762E+01
   Friction thermal sca.    tstar : -0.17638E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82349E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54601E-02      34   0.62558E-03   0.53944E+01 0.14156E+03 
c  Velocity[X]                                      0.28467E+01 
c  Velocity[Y]                                      0.25477E+01 
c  Velocity[Z]                                      0.12392E-29 
c  Pressure     0.16055E-06     489   0.94087E-08   0.15328E+00 0.45262E+03 
c  nu_tilda     0.40070E-05      33   0.13377E-04   0.35023E-06 0.22140E+03 
c  TempC        0.24026E+02      29   0.68476E-03   0.11143E+02 0.37283E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4076          9.4209          4.5729          4.5729
v  Velocity[Y]            -4.2764           7.266       0.0088033       0.0088033
v  Velocity[Z]       -6.9287e-015     6.2498e-015    -1.2222e-017    -1.2222e-017
v  ǁVelocityǁ         0.0015052          9.4209          4.9464          4.9464
v  Pressure                -46.22          20.706         -1.3679         -1.3679
v  nu_tilda            4.614e-007       0.0042622      0.00074044      0.00074044
v  TempC                       21          73.353          21.399          21.399
v  TurbVisc           4.0138e-014       0.0050234      0.00085982      0.00085982
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              419:        0.29290E+01

===============================================================


 INSTANT    0.420000000E+03   TIME STEP NUMBER             420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95544E-02 0.89261E+00
   Friction velocity        uk    :  0.95544E-02 0.89261E+00
   Dimensionless distance   yplus :  0.76919E-01 0.71861E+01
   Friction thermal sca.    tstar : -0.22689E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57390E-01 0.53616E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54642E-02      34   0.62205E-03   0.53612E+01 0.14114E+03 
c  Velocity[X]                                      0.28159E+01 
c  Velocity[Y]                                      0.25452E+01 
c  Velocity[Z]                                      0.14307E-29 
c  Pressure     0.11718E-06     362   0.99744E-08   0.11636E+00 0.28906E+03 
c  nu_tilda     0.40098E-05      33   0.11910E-04   0.34940E-06 0.22093E+03 
c  TempC        0.24040E+02      29   0.53665E-03   0.11859E+02 0.38172E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4132          9.4352          4.5729          4.5729
v  Velocity[Y]            -4.2665          7.2461       0.0088551       0.0088551
v  Velocity[Z]       -6.9287e-015     6.3133e-015     -1.229e-017     -1.229e-017
v  ǁVelocityǁ         0.0013921          9.4352          4.9472          4.9472
v  Pressure               -46.231           20.67         -1.3731         -1.3731
v  nu_tilda           4.6067e-007       0.0042623      0.00074111      0.00074111
v  TempC                       21          73.353            21.4            21.4
v  TurbVisc           3.9872e-014       0.0050235      0.00086058      0.00086058
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              420:        0.24550E+01

===============================================================


 INSTANT    0.421000000E+03   TIME STEP NUMBER             421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51549E-02 0.89175E+00
   Friction velocity        uk    :  0.51549E-02 0.89175E+00
   Dimensionless distance   yplus :  0.41501E-01 0.71792E+01
   Friction thermal sca.    tstar : -0.28591E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30964E-01 0.53565E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54682E-02      34   0.67757E-03   0.53211E+01 0.14070E+03 
c  Velocity[X]                                      0.28057E+01 
c  Velocity[Y]                                      0.25154E+01 
c  Velocity[Z]                                      0.11391E-29 
c  Pressure     0.13220E-06     489   0.93252E-08   0.12851E+00 0.41619E+03 
c  nu_tilda     0.40126E-05      33   0.13363E-04   0.34859E-06 0.22046E+03 
c  TempC        0.24055E+02      29   0.71628E-03   0.10568E+02 0.36246E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4186          9.4491          4.5729          4.5729
v  Velocity[Y]             -4.257          7.2707        0.008909        0.008909
v  Velocity[Z]       -6.9287e-015     6.2608e-015     -1.236e-017     -1.236e-017
v  ǁVelocityǁ        0.00097347          9.4491           4.948           4.948
v  Pressure               -46.318          20.674         -1.4089         -1.4089
v  nu_tilda           4.5976e-007       0.0042623      0.00074172      0.00074172
v  TempC                       21          73.382            21.4            21.4
v  TurbVisc           3.9622e-014       0.0050235      0.00086134      0.00086134
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              421:        0.28620E+01

===============================================================


 INSTANT    0.422000000E+03   TIME STEP NUMBER             422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18223E-02 0.89279E+00
   Friction velocity        uk    :  0.18223E-02 0.89279E+00
   Dimensionless distance   yplus :  0.14670E-01 0.71876E+01
   Friction thermal sca.    tstar : -0.10162E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10946E-01 0.53628E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54723E-02      34   0.62496E-03   0.53640E+01 0.14076E+03 
c  Velocity[X]                                      0.28390E+01 
c  Velocity[Y]                                      0.25250E+01 
c  Velocity[Z]                                      0.11294E-29 
c  Pressure     0.19215E-06     377   0.92640E-08   0.18980E+00 0.26408E+03 
c  nu_tilda     0.40153E-05      33   0.11904E-04   0.34778E-06 0.22000E+03 
c  TempC        0.24070E+02      30   0.54732E-03   0.13537E+02 0.40502E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.424          9.4628          4.5729          4.5729
v  Velocity[Y]            -4.2473          7.2411       0.0089612       0.0089612
v  Velocity[Z]       -6.9287e-015     6.1507e-015    -1.2429e-017    -1.2429e-017
v  ǁVelocityǁ        0.00059669          9.4628          4.9488          4.9488
v  Pressure               -46.323          20.649         -1.4064         -1.4064
v  nu_tilda           4.5888e-007       0.0042624      0.00074239      0.00074239
v  TempC                       21          73.424          21.401          21.401
v  TurbVisc           3.9308e-014       0.0050236       0.0008621       0.0008621
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              422:        0.24990E+01

===============================================================


 INSTANT    0.423000000E+03   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49544E-02 0.89169E+00
   Friction velocity        uk    :  0.49544E-02 0.89169E+00
   Dimensionless distance   yplus :  0.39886E-01 0.71787E+01
   Friction thermal sca.    tstar : -0.46168E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29759E-01 0.53561E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54763E-02      34   0.51400E-03   0.52761E+01 0.13994E+03 
c  Velocity[X]                                      0.27815E+01 
c  Velocity[Y]                                      0.24946E+01 
c  Velocity[Z]                                      0.15210E-29 
c  Pressure     0.11787E-06     489   0.91606E-08   0.11386E+00 0.49428E+03 
c  nu_tilda     0.40181E-05      33   0.13327E-04   0.34698E-06 0.21953E+03 
c  TempC        0.24085E+02      29   0.59623E-03   0.11624E+02 0.38417E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4289           9.476          4.5729          4.5729
v  Velocity[Y]            -4.2375          7.2678       0.0090146       0.0090146
v  Velocity[Z]       -6.9287e-015     6.1145e-015    -1.2502e-017    -1.2502e-017
v  ǁVelocityǁ         0.0010496           9.476          4.9496          4.9496
v  Pressure                -46.42          20.633         -1.4505         -1.4505
v  nu_tilda           4.5786e-007       0.0042625        0.000743        0.000743
v  TempC                       21          73.401          21.402          21.402
v  TurbVisc           3.9008e-014       0.0050237      0.00086287      0.00086287
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              423:        0.25690E+01

===============================================================


 INSTANT    0.424000000E+03   TIME STEP NUMBER             424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72706E-02 0.89293E+00
   Friction velocity        uk    :  0.72706E-02 0.89293E+00
   Dimensionless distance   yplus :  0.58533E-01 0.71887E+01
   Friction thermal sca.    tstar : -0.23146E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43672E-01 0.53636E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54804E-02      34   0.68155E-03   0.52315E+01 0.13937E+03 
c  Velocity[X]                                      0.27557E+01 
c  Velocity[Y]                                      0.24758E+01 
c  Velocity[Z]                                      0.12360E-29 
c  Pressure     0.14651E-06     378   0.97010E-08   0.14022E+00 0.24051E+03 
c  nu_tilda     0.40209E-05      33   0.11904E-04   0.34617E-06 0.21907E+03 
c  TempC        0.24099E+02      29   0.49265E-03   0.10915E+02 0.37344E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4349          9.4889          4.5729          4.5729
v  Velocity[Y]            -4.2278          7.2638       0.0090674       0.0090674
v  Velocity[Z]       -6.9287e-015     5.9139e-015    -1.2571e-017    -1.2571e-017
v  ǁVelocityǁ        0.00062447          9.4889          4.9505          4.9505
v  Pressure               -46.433          20.638         -1.4457         -1.4457
v  nu_tilda           4.5685e-007       0.0042625      0.00074367      0.00074367
v  TempC                       21          73.424          21.402          21.402
v  TurbVisc           3.8663e-014       0.0050237      0.00086363      0.00086363
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              424:        0.21490E+01

===============================================================


 INSTANT    0.425000000E+03   TIME STEP NUMBER             425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87502E-02 0.89236E+00
   Friction velocity        uk    :  0.87502E-02 0.89236E+00
   Dimensionless distance   yplus :  0.70445E-01 0.71841E+01
   Friction thermal sca.    tstar : -0.19284E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52560E-01 0.53602E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54844E-02      34   0.62932E-03   0.52864E+01 0.13957E+03 
c  Velocity[X]                                      0.28031E+01 
c  Velocity[Y]                                      0.24833E+01 
c  Velocity[Z]                                      0.11807E-29 
c  Pressure     0.18903E-06     520   0.93865E-08   0.18748E+00 0.78281E+03 
c  nu_tilda     0.40236E-05      33   0.13319E-04   0.34537E-06 0.21861E+03 
c  TempC        0.24114E+02      29   0.59248E-03   0.10533E+02 0.35022E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4409          9.5015          4.5729          4.5729
v  Velocity[Y]            -4.2182          7.2413       0.0091211       0.0091211
v  Velocity[Z]       -6.9287e-015     5.8106e-015    -1.2646e-017    -1.2646e-017
v  ǁVelocityǁ        0.00013761          9.5016          4.9513          4.9513
v  Pressure               -46.519           20.52         -1.5007         -1.5007
v  nu_tilda            4.559e-007       0.0042626      0.00074428      0.00074428
v  TempC                       21          73.409          21.403          21.403
v  TurbVisc           3.8324e-014       0.0050238      0.00086439      0.00086439
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              425:        0.23750E+01

===============================================================


 INSTANT    0.426000000E+03   TIME STEP NUMBER             426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39149E-02 0.89119E+00
   Friction velocity        uk    :  0.39149E-02 0.89119E+00
   Dimensionless distance   yplus :  0.31518E-01 0.71747E+01
   Friction thermal sca.    tstar : -0.21348E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23516E-01 0.53531E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54885E-02      34   0.60471E-03   0.52030E+01 0.13886E+03 
c  Velocity[X]                                      0.27310E+01 
c  Velocity[Y]                                      0.24720E+01 
c  Velocity[Z]                                      0.12708E-29 
c  Pressure     0.13982E-06     474   0.93421E-08   0.13637E+00 0.59382E+03 
c  nu_tilda     0.40264E-05      33   0.11905E-04   0.34458E-06 0.21815E+03 
c  TempC        0.24129E+02      29   0.10391E-02   0.12741E+02 0.39861E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4465          9.5136          4.5729          4.5729
v  Velocity[Y]            -4.2084          7.2592       0.0091738       0.0091738
v  Velocity[Z]       -6.9287e-015     5.5449e-015    -1.2724e-017    -1.2724e-017
v  ǁVelocityǁ        0.00023203          9.5137          4.9521          4.9521
v  Pressure               -46.539          20.619         -1.4788         -1.4788
v  nu_tilda           4.5493e-007       0.0042626      0.00074496      0.00074496
v  TempC                       21          73.397          21.404          21.404
v  TurbVisc           3.8006e-014       0.0050239      0.00086515      0.00086515
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              426:        0.24720E+01

===============================================================


 INSTANT    0.427000000E+03   TIME STEP NUMBER             427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53267E-02 0.89196E+00
   Friction velocity        uk    :  0.53267E-02 0.89196E+00
   Dimensionless distance   yplus :  0.42884E-01 0.71809E+01
   Friction thermal sca.    tstar : -0.36547E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31996E-01 0.53578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54925E-02      34   0.63561E-03   0.51819E+01 0.13845E+03 
c  Velocity[X]                                      0.27270E+01 
c  Velocity[Y]                                      0.24549E+01 
c  Velocity[Z]                                      0.12592E-29 
c  Pressure     0.14096E-06     537   0.95700E-08   0.13874E+00 0.11446E+04 
c  nu_tilda     0.40291E-05      33   0.13281E-04   0.34380E-06 0.21770E+03 
c  TempC        0.24143E+02      30   0.68136E-03   0.22307E+02 0.49876E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4518          9.5254          4.5729          4.5729
v  Velocity[Y]            -4.1982          7.2309        0.009228        0.009228
v  Velocity[Z]       -6.9287e-015     5.2976e-015    -1.2801e-017    -1.2801e-017
v  ǁVelocityǁ        0.00034115          9.5257          4.9529          4.9529
v  Pressure               -46.632          20.442         -1.5513         -1.5513
v  nu_tilda           4.5407e-007       0.0042627      0.00074557      0.00074557
v  TempC                       21           73.43          21.404          21.404
v  TurbVisc           3.7684e-014       0.0050239      0.00086592      0.00086592
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              427:        0.25870E+01

===============================================================


 INSTANT    0.428000000E+03   TIME STEP NUMBER             428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64698E-02 0.89099E+00
   Friction velocity        uk    :  0.64698E-02 0.89099E+00
   Dimensionless distance   yplus :  0.52086E-01 0.71731E+01
   Friction thermal sca.    tstar : -0.19100E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38862E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54966E-02      34   0.61087E-03   0.51658E+01 0.13819E+03 
c  Velocity[X]                                      0.27014E+01 
c  Velocity[Y]                                      0.24644E+01 
c  Velocity[Z]                                      0.12219E-29 
c  Pressure     0.17429E-06     490   0.94549E-08   0.17108E+00 0.85128E+03 
c  nu_tilda     0.40319E-05      33   0.11903E-04   0.34302E-06 0.21724E+03 
c  TempC        0.24158E+02      29   0.61765E-03   0.13188E+02 0.40110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4573          9.5366          4.5729          4.5729
v  Velocity[Y]            -4.1881          7.2509       0.0092812       0.0092812
v  Velocity[Z]       -6.9287e-015     4.7926e-015    -1.2873e-017    -1.2873e-017
v  ǁVelocityǁ        0.00057845          9.5369          4.9537          4.9537
v  Pressure               -46.649           20.58         -1.5172         -1.5172
v  nu_tilda           4.5307e-007       0.0042627      0.00074624      0.00074624
v  TempC                       21          73.426          21.405          21.405
v  TurbVisc             3.74e-014        0.005024      0.00086668      0.00086668
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              428:        0.26900E+01

===============================================================


 INSTANT    0.429000000E+03   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83968E-02 0.89209E+00
   Friction velocity        uk    :  0.83968E-02 0.89209E+00
   Dimensionless distance   yplus :  0.67600E-01 0.71819E+01
   Friction thermal sca.    tstar : -0.15254E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50437E-01 0.53585E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55006E-02      34   0.62890E-03   0.51448E+01 0.13790E+03 
c  Velocity[X]                                      0.26987E+01 
c  Velocity[Y]                                      0.24461E+01 
c  Velocity[Z]                                      0.13650E-29 
c  Pressure     0.13097E-06     536   0.95864E-08   0.12900E+00 0.11195E+04 
c  nu_tilda     0.40346E-05      33   0.13255E-04   0.34225E-06 0.21679E+03 
c  TempC        0.24173E+02      29   0.52546E-03   0.11190E+02 0.37123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4638          9.5475          4.5729          4.5729
v  Velocity[Y]            -4.1783          7.2349       0.0093352       0.0093352
v  Velocity[Z]       -6.9287e-015     4.4494e-015    -1.2951e-017    -1.2951e-017
v  ǁVelocityǁ        0.00096801           9.548          4.9545          4.9545
v  Pressure               -46.744          20.406         -1.5884         -1.5884
v  nu_tilda           4.5203e-007       0.0042628      0.00074685      0.00074685
v  TempC                       21           73.42          21.406          21.406
v  TurbVisc            3.707e-014       0.0050241      0.00086745      0.00086745
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              429:        0.33690E+01

===============================================================


 INSTANT    0.430000000E+03   TIME STEP NUMBER             430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10960E-01 0.89139E+00
   Friction velocity        uk    :  0.10960E-01 0.89139E+00
   Dimensionless distance   yplus :  0.88236E-01 0.71763E+01
   Friction thermal sca.    tstar : -0.16851E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65834E-01 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55047E-02      34   0.57552E-03   0.51364E+01 0.13761E+03 
c  Velocity[X]                                      0.27102E+01 
c  Velocity[Y]                                      0.24262E+01 
c  Velocity[Z]                                      0.12285E-29 
c  Pressure     0.16520E-06     488   0.96629E-08   0.15985E+00 0.75759E+03 
c  nu_tilda     0.40374E-05      33   0.11903E-04   0.34147E-06 0.21634E+03 
c  TempC        0.24188E+02      29   0.48729E-03   0.11351E+02 0.37605E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4699          9.5593          4.5729          4.5729
v  Velocity[Y]            -4.1683          7.2572       0.0093886       0.0093886
v  Velocity[Z]       -6.9287e-015     4.4023e-015    -1.3023e-017    -1.3023e-017
v  ǁVelocityǁ        0.00061712          9.5594          4.9553          4.9553
v  Pressure               -46.766          20.533         -1.5591         -1.5591
v  nu_tilda           4.5094e-007       0.0042628      0.00074752      0.00074752
v  TempC                       21          73.455          21.406          21.406
v  TurbVisc           3.6731e-014       0.0050241      0.00086821      0.00086821
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              430:        0.29780E+01

===============================================================


 INSTANT    0.431000000E+03   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87541E-02 0.89229E+00
   Friction velocity        uk    :  0.87541E-02 0.89229E+00
   Dimensionless distance   yplus :  0.70477E-01 0.71835E+01
   Friction thermal sca.    tstar : -0.15473E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52584E-01 0.53597E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55087E-02      34   0.60927E-03   0.50934E+01 0.13718E+03 
c  Velocity[X]                                      0.26512E+01 
c  Velocity[Y]                                      0.24422E+01 
c  Velocity[Z]                                      0.12886E-29 
c  Pressure     0.12656E-06     521   0.94413E-08   0.12373E+00 0.75898E+03 
c  nu_tilda     0.40401E-05      33   0.13238E-04   0.34071E-06 0.21590E+03 
c  TempC        0.24202E+02      29   0.62044E-03   0.97628E+01 0.34837E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4755          9.5712          4.5729          4.5729
v  Velocity[Y]            -4.1584          7.2523       0.0094429       0.0094429
v  Velocity[Z]       -6.9287e-015      4.382e-015    -1.3099e-017    -1.3099e-017
v  ǁVelocityǁ        0.00089305          9.5716          4.9561          4.9561
v  Pressure                -46.87          20.441         -1.6166         -1.6166
v  nu_tilda           4.4982e-007       0.0042629      0.00074814      0.00074814
v  TempC                       21          73.446          21.407          21.407
v  TurbVisc           3.6378e-014       0.0050242      0.00086898      0.00086898
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              431:        0.33900E+01

===============================================================


 INSTANT    0.432000000E+03   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10532E-01 0.89162E+00
   Friction velocity        uk    :  0.10532E-01 0.89162E+00
   Dimensionless distance   yplus :  0.84788E-01 0.71782E+01
   Friction thermal sca.    tstar : -0.14460E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63262E-01 0.53557E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55127E-02      34   0.62415E-03   0.50775E+01 0.13690E+03 
c  Velocity[X]                                      0.26494E+01 
c  Velocity[Y]                                      0.24281E+01 
c  Velocity[Z]                                      0.13610E-29 
c  Pressure     0.13470E-06     345   0.96394E-08   0.13404E+00 0.31226E+03 
c  nu_tilda     0.40428E-05      33   0.11914E-04   0.33995E-06 0.21545E+03 
c  TempC        0.24217E+02      29   0.69964E-03   0.15662E+02 0.43162E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.481          9.5828          4.5729          4.5729
v  Velocity[Y]            -4.1484          7.2262       0.0094965       0.0094965
v  Velocity[Z]       -6.9287e-015      4.362e-015    -1.3172e-017    -1.3172e-017
v  ǁVelocityǁ         0.0015439          9.5831          4.9569          4.9569
v  Pressure                -46.89          20.392         -1.6201         -1.6201
v  nu_tilda           4.4871e-007        0.004263      0.00074881      0.00074881
v  TempC                       21          73.321          21.408          21.408
v  TurbVisc            3.602e-014       0.0050243      0.00086974      0.00086974
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              432:        0.33220E+01

===============================================================


 INSTANT    0.433000000E+03   TIME STEP NUMBER             433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98123E-02 0.89065E+00
   Friction velocity        uk    :  0.98123E-02 0.89065E+00
   Dimensionless distance   yplus :  0.78996E-01 0.71704E+01
   Friction thermal sca.    tstar : -0.16727E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58940E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55168E-02      34   0.61344E-03   0.50618E+01 0.13659E+03 
c  Velocity[X]                                      0.26558E+01 
c  Velocity[Y]                                      0.24060E+01 
c  Velocity[Z]                                      0.12489E-29 
c  Pressure     0.18274E-06     472   0.97867E-08   0.17949E+00 0.40810E+03 
c  nu_tilda     0.40455E-05      33   0.13208E-04   0.33919E-06 0.21501E+03 
c  TempC        0.24231E+02      29   0.71349E-03   0.13174E+02 0.41988E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.487          9.5943          4.5729          4.5729
v  Velocity[Y]            -4.1386          7.2511       0.0095513       0.0095513
v  Velocity[Z]       -6.9287e-015     4.3464e-015    -1.3242e-017    -1.3242e-017
v  ǁVelocityǁ        0.00076481          9.5946          4.9577          4.9577
v  Pressure               -46.989          20.424          -1.648          -1.648
v  nu_tilda           4.4756e-007        0.004263      0.00074942      0.00074942
v  TempC                       21          73.322          21.408          21.408
v  TurbVisc           3.5663e-014       0.0050243      0.00087051      0.00087051
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              433:        0.33480E+01

===============================================================


 INSTANT    0.434000000E+03   TIME STEP NUMBER             434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81264E-02 0.89162E+00
   Friction velocity        uk    :  0.81264E-02 0.89162E+00
   Dimensionless distance   yplus :  0.65423E-01 0.71782E+01
   Friction thermal sca.    tstar : -0.14757E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48813E-01 0.53557E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55208E-02      34   0.59839E-03   0.50451E+01 0.13634E+03 
c  Velocity[X]                                      0.26247E+01 
c  Velocity[Y]                                      0.24204E+01 
c  Velocity[Z]                                      0.11087E-29 
c  Pressure     0.13070E-06     426   0.97331E-08   0.12931E+00 0.41214E+03 
c  nu_tilda     0.40482E-05      33   0.11911E-04   0.33843E-06 0.21457E+03 
c  TempC        0.24246E+02      29   0.59810E-03   0.13323E+02 0.41376E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4936          9.6052          4.5729          4.5729
v  Velocity[Y]            -4.1286          7.2215       0.0096048       0.0096048
v  Velocity[Z]       -6.9287e-015     4.3256e-015    -1.3313e-017    -1.3313e-017
v  ǁVelocityǁ        0.00097012          9.6058          4.9584          4.9584
v  Pressure               -47.016          20.356         -1.6586         -1.6586
v  nu_tilda           4.4643e-007       0.0042631      0.00075009      0.00075009
v  TempC                       21          73.304          21.409          21.409
v  TurbVisc           3.5301e-014       0.0050244      0.00087127      0.00087127
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              434:        0.30640E+01

===============================================================


 INSTANT    0.435000000E+03   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44959E-02 0.89052E+00
   Friction velocity        uk    :  0.44959E-02 0.89052E+00
   Dimensionless distance   yplus :  0.36195E-01 0.71693E+01
   Friction thermal sca.    tstar : -0.18918E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27006E-01 0.53491E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55248E-02      34   0.56791E-03   0.50110E+01 0.13590E+03 
c  Velocity[X]                                      0.26079E+01 
c  Velocity[Y]                                      0.24031E+01 
c  Velocity[Z]                                      0.14392E-29 
c  Pressure     0.16617E-06     458   0.94467E-08   0.16423E+00 0.49068E+03 
c  nu_tilda     0.40509E-05      33   0.13178E-04   0.33767E-06 0.21413E+03 
c  TempC        0.24261E+02      29   0.57531E-03   0.11876E+02 0.38863E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4999          9.6156          4.5729          4.5729
v  Velocity[Y]            -4.1184          7.2486       0.0096596       0.0096596
v  Velocity[Z]       -6.9287e-015     4.3158e-015    -1.3381e-017    -1.3381e-017
v  ǁVelocityǁ         0.0010614          9.6161          4.9592          4.9592
v  Pressure               -47.125           20.42         -1.6798         -1.6798
v  nu_tilda           4.4524e-007       0.0042631      0.00075071      0.00075071
v  TempC                       21            73.3           21.41           21.41
v  TurbVisc           3.4945e-014       0.0050244      0.00087203      0.00087203
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              435:        0.23120E+01

===============================================================


 INSTANT    0.436000000E+03   TIME STEP NUMBER             436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49606E-02 0.89124E+00
   Friction velocity        uk    :  0.49606E-02 0.89124E+00
   Dimensionless distance   yplus :  0.39937E-01 0.71751E+01
   Friction thermal sca.    tstar : -0.15682E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29797E-01 0.53534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55289E-02      34   0.66606E-03   0.50077E+01 0.13571E+03 
c  Velocity[X]                                      0.26108E+01 
c  Velocity[Y]                                      0.23969E+01 
c  Velocity[Z]                                      0.12749E-29 
c  Pressure     0.16459E-06     486   0.92068E-08   0.16153E+00 0.71181E+03 
c  nu_tilda     0.40536E-05      33   0.11911E-04   0.33691E-06 0.21369E+03 
c  TempC        0.24275E+02      29   0.58425E-03   0.98449E+01 0.35148E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5057          9.6258          4.5729          4.5729
v  Velocity[Y]            -4.1081          7.2158       0.0097135       0.0097135
v  Velocity[Z]       -6.9287e-015     4.2933e-015    -1.3441e-017    -1.3441e-017
v  ǁVelocityǁ        0.00036444          9.6264            4.96            4.96
v  Pressure               -47.149          20.294          -1.703          -1.703
v  nu_tilda           4.4407e-007       0.0042632      0.00075138      0.00075138
v  TempC                       21          73.333           21.41           21.41
v  TurbVisc           3.4573e-014       0.0050245       0.0008728       0.0008728
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              436:        0.23980E+01

===============================================================


 INSTANT    0.437000000E+03   TIME STEP NUMBER             437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45935E-02 0.89032E+00
   Friction velocity        uk    :  0.45935E-02 0.89032E+00
   Dimensionless distance   yplus :  0.36980E-01 0.71677E+01
   Friction thermal sca.    tstar : -0.18668E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27592E-01 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55329E-02      34   0.51576E-03   0.50071E+01 0.13562E+03 
c  Velocity[X]                                      0.26209E+01 
c  Velocity[Y]                                      0.23861E+01 
c  Velocity[Z]                                      0.10850E-29 
c  Pressure     0.15372E-06     474   0.93123E-08   0.15060E+00 0.42605E+03 
c  nu_tilda     0.40563E-05      33   0.13165E-04   0.33615E-06 0.21325E+03 
c  TempC        0.24290E+02      29   0.72934E-03   0.11160E+02 0.38188E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5114          9.6355          4.5729          4.5729
v  Velocity[Y]            -4.0983          7.2404       0.0097687       0.0097687
v  Velocity[Z]       -6.9287e-015     4.2852e-015    -1.3503e-017    -1.3503e-017
v  ǁVelocityǁ        0.00061271          9.6363          4.9608          4.9608
v  Pressure               -47.256          20.335         -1.7309         -1.7309
v  nu_tilda           4.4276e-007       0.0042632        0.000752        0.000752
v  TempC                       21          73.336          21.411          21.411
v  TurbVisc            3.421e-014       0.0050246      0.00087356      0.00087356
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              437:        0.23510E+01

===============================================================


 INSTANT    0.438000000E+03   TIME STEP NUMBER             438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77514E-02 0.89139E+00
   Friction velocity        uk    :  0.77514E-02 0.89139E+00
   Dimensionless distance   yplus :  0.62404E-01 0.71763E+01
   Friction thermal sca.    tstar : -0.17324E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46560E-01 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55369E-02      34   0.58611E-03   0.49259E+01 0.13484E+03 
c  Velocity[X]                                      0.25556E+01 
c  Velocity[Y]                                      0.23703E+01 
c  Velocity[Z]                                      0.13544E-29 
c  Pressure     0.16656E-06     457   0.99443E-08   0.16466E+00 0.42497E+03 
c  nu_tilda     0.40590E-05      33   0.11910E-04   0.33541E-06 0.21282E+03 
c  TempC        0.24304E+02      29   0.63535E-03   0.14152E+02 0.42582E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5177          9.6446          4.5729          4.5729
v  Velocity[Y]            -4.0882          7.2449       0.0098228       0.0098228
v  Velocity[Z]       -6.9287e-015     4.2732e-015    -1.3558e-017    -1.3558e-017
v  ǁVelocityǁ        0.00051656          9.6455          4.9616          4.9616
v  Pressure               -47.282          20.383         -1.7135         -1.7135
v  nu_tilda           4.4138e-007       0.0042633      0.00075267      0.00075267
v  TempC                       21          73.331          21.412          21.412
v  TurbVisc            3.381e-014       0.0050246      0.00087433      0.00087433
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              438:        0.22900E+01

===============================================================


 INSTANT    0.439000000E+03   TIME STEP NUMBER             439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37648E-02 0.89070E+00
   Friction velocity        uk    :  0.37648E-02 0.89070E+00
   Dimensionless distance   yplus :  0.30309E-01 0.71708E+01
   Friction thermal sca.    tstar : -0.17587E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22614E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55410E-02      34   0.64145E-03   0.49397E+01 0.13480E+03 
c  Velocity[X]                                      0.25550E+01 
c  Velocity[Y]                                      0.23847E+01 
c  Velocity[Z]                                      0.12842E-29 
c  Pressure     0.15402E-06     520   0.95108E-08   0.15483E+00 0.86557E+03 
c  nu_tilda     0.40616E-05      33   0.13112E-04   0.33466E-06 0.21239E+03 
c  TempC        0.24319E+02      29   0.53317E-03   0.11378E+02 0.38046E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5245          9.6533          4.5729          4.5729
v  Velocity[Y]             -4.078          7.2214       0.0098778       0.0098778
v  Velocity[Z]       -6.9287e-015     4.2571e-015    -1.3607e-017    -1.3607e-017
v  ǁVelocityǁ        0.00027725          9.6546          4.9624          4.9624
v  Pressure               -47.387          20.257         -1.7744         -1.7744
v  nu_tilda           4.4006e-007       0.0042633      0.00075328      0.00075328
v  TempC                       21           73.36          21.413          21.413
v  TurbVisc           3.3391e-014       0.0050247       0.0008751       0.0008751
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              439:        0.24510E+01

===============================================================


 INSTANT    0.440000000E+03   TIME STEP NUMBER             440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45494E-02 0.88918E+00
   Friction velocity        uk    :  0.45494E-02 0.88918E+00
   Dimensionless distance   yplus :  0.36625E-01 0.71585E+01
   Friction thermal sca.    tstar : -0.22640E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27327E-01 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55450E-02      34   0.63405E-03   0.49428E+01 0.13476E+03 
c  Velocity[X]                                      0.25595E+01 
c  Velocity[Y]                                      0.23833E+01 
c  Velocity[Z]                                      0.11268E-29 
c  Pressure     0.16778E-06     458   0.96076E-08   0.16306E+00 0.44092E+03 
c  nu_tilda     0.40643E-05      33   0.11920E-04   0.33391E-06 0.21196E+03 
c  TempC        0.24334E+02      29   0.62248E-03   0.97488E+01 0.34563E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5308          9.6629          4.5729          4.5729
v  Velocity[Y]            -4.0681          7.2316       0.0099324       0.0099324
v  Velocity[Z]       -6.9287e-015     4.2344e-015    -1.3651e-017    -1.3651e-017
v  ǁVelocityǁ        0.00023334          9.6634          4.9632          4.9632
v  Pressure               -47.421          20.318         -1.7579         -1.7579
v  nu_tilda           4.3868e-007       0.0042634      0.00075395      0.00075395
v  TempC                       21          73.362          21.413          21.413
v  TurbVisc           3.2991e-014       0.0050247      0.00087586      0.00087586
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              440:        0.27760E+01

===============================================================


 INSTANT    0.441000000E+03   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35016E-02 0.89020E+00
   Friction velocity        uk    :  0.35016E-02 0.89020E+00
   Dimensionless distance   yplus :  0.28190E-01 0.71667E+01
   Friction thermal sca.    tstar : -0.27132E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21033E-01 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55490E-02      34   0.62144E-03   0.49373E+01 0.13453E+03 
c  Velocity[X]                                      0.25757E+01 
c  Velocity[Y]                                      0.23616E+01 
c  Velocity[Z]                                      0.12741E-29 
c  Pressure     0.12945E-06     520   0.98617E-08   0.12997E+00 0.89923E+03 
c  nu_tilda     0.40670E-05      33   0.13097E-04   0.33314E-06 0.21153E+03 
c  TempC        0.24348E+02      29   0.62817E-03   0.12441E+02 0.39863E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5368          9.6729          4.5729          4.5729
v  Velocity[Y]             -4.058           7.211       0.0099875       0.0099875
v  Velocity[Z]       -6.9287e-015     4.2168e-015    -1.3697e-017    -1.3697e-017
v  ǁVelocityǁ        0.00042996          9.6738          4.9639          4.9639
v  Pressure                -47.53          20.188         -1.8211         -1.8211
v  nu_tilda            4.373e-007       0.0042634      0.00075457      0.00075457
v  TempC                       21          73.393          21.414          21.414
v  TurbVisc           3.2579e-014       0.0050248      0.00087663      0.00087663
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              441:        0.28960E+01

===============================================================


 INSTANT    0.442000000E+03   TIME STEP NUMBER             442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28536E-02 0.88961E+00
   Friction velocity        uk    :  0.28536E-02 0.88961E+00
   Dimensionless distance   yplus :  0.22973E-01 0.71620E+01
   Friction thermal sca.    tstar : -0.12952E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17141E-01 0.53437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55531E-02      34   0.57201E-03   0.48851E+01 0.13405E+03 
c  Velocity[X]                                      0.25130E+01 
c  Velocity[Y]                                      0.23721E+01 
c  Velocity[Z]                                      0.11509E-29 
c  Pressure     0.12669E-06     490   0.98662E-08   0.12547E+00 0.82434E+03 
c  nu_tilda     0.40696E-05      33   0.11915E-04   0.33237E-06 0.21110E+03 
c  TempC        0.24363E+02      29   0.52424E-03   0.11723E+02 0.37702E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5426          9.6825          4.5729          4.5729
v  Velocity[Y]             -4.048          7.2312        0.010043        0.010043
v  Velocity[Z]       -6.9287e-015     4.1997e-015    -1.3735e-017    -1.3735e-017
v  ǁVelocityǁ        0.00023408          9.6833          4.9647          4.9647
v  Pressure               -47.567          20.327         -1.7889         -1.7889
v  nu_tilda           4.3591e-007       0.0042635      0.00075524      0.00075524
v  TempC                       21          73.387          21.415          21.415
v  TurbVisc           3.2171e-014       0.0050249      0.00087739      0.00087739
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              442:        0.29120E+01

===============================================================


 INSTANT    0.443000000E+03   TIME STEP NUMBER             443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47487E-02 0.89066E+00
   Friction velocity        uk    :  0.47487E-02 0.89066E+00
   Dimensionless distance   yplus :  0.38231E-01 0.71704E+01
   Friction thermal sca.    tstar : -0.61326E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28524E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55571E-02      34   0.63212E-03   0.48346E+01 0.13349E+03 
c  Velocity[X]                                      0.24866E+01 
c  Velocity[Y]                                      0.23480E+01 
c  Velocity[Z]                                      0.11862E-29 
c  Pressure     0.17606E-06     522   0.96293E-08   0.17739E+00 0.85082E+03 
c  nu_tilda     0.40723E-05      33   0.13068E-04   0.33164E-06 0.21067E+03 
c  TempC        0.24377E+02      29   0.80692E-03   0.10637E+02 0.37736E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5492          9.6917          4.5729          4.5729
v  Velocity[Y]            -4.0381          7.2075        0.010098        0.010098
v  Velocity[Z]       -6.9287e-015     4.1865e-015    -1.3768e-017    -1.3768e-017
v  ǁVelocityǁ         0.0001685          9.6929          4.9655          4.9655
v  Pressure               -47.665          20.193         -1.8468         -1.8468
v  nu_tilda           4.3459e-007       0.0042635      0.00075586      0.00075586
v  TempC                       21          73.404          21.416          21.416
v  TurbVisc           3.1766e-014       0.0050249      0.00087816      0.00087816
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              443:        0.33000E+01

===============================================================


 INSTANT    0.444000000E+03   TIME STEP NUMBER             444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44349E-02 0.88935E+00
   Friction velocity        uk    :  0.44349E-02 0.88935E+00
   Dimensionless distance   yplus :  0.35704E-01 0.71599E+01
   Friction thermal sca.    tstar : -0.27580E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26639E-01 0.53421E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55611E-02      34   0.55787E-03   0.48564E+01 0.13351E+03 
c  Velocity[X]                                      0.25177E+01 
c  Velocity[Y]                                      0.23387E+01 
c  Velocity[Z]                                      0.13964E-29 
c  Pressure     0.13697E-06     473   0.95163E-08   0.13459E+00 0.57399E+03 
c  nu_tilda     0.40749E-05      33   0.11921E-04   0.33089E-06 0.21025E+03 
c  TempC        0.24392E+02      29   0.68857E-03   0.17617E+02 0.47789E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.556          9.7004          4.5729          4.5729
v  Velocity[Y]             -4.028          7.2305        0.010152        0.010152
v  Velocity[Z]       -6.9287e-015      4.162e-015    -1.3798e-017    -1.3798e-017
v  ǁVelocityǁ        0.00034562          9.7015          4.9663          4.9663
v  Pressure               -47.707          20.286          -1.826          -1.826
v  nu_tilda           4.3319e-007       0.0042636      0.00075653      0.00075653
v  TempC                       21          73.398          21.416          21.416
v  TurbVisc           3.1383e-014        0.005025      0.00087892      0.00087892
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              444:        0.28220E+01

===============================================================


 INSTANT    0.445000000E+03   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53055E-02 0.89028E+00
   Friction velocity        uk    :  0.53055E-02 0.89028E+00
   Dimensionless distance   yplus :  0.42713E-01 0.71674E+01
   Friction thermal sca.    tstar : -0.23631E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31869E-01 0.53477E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55651E-02      34   0.59987E-03   0.48367E+01 0.13322E+03 
c  Velocity[X]                                      0.24829E+01 
c  Velocity[Y]                                      0.23538E+01 
c  Velocity[Z]                                      0.12241E-29 
c  Pressure     0.17460E-06     504   0.93154E-08   0.17065E+00 0.57387E+03 
c  nu_tilda     0.40776E-05      33   0.13034E-04   0.33014E-06 0.20983E+03 
c  TempC        0.24406E+02      29   0.50001E-03   0.12241E+02 0.40258E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5625           9.709          4.5729          4.5729
v  Velocity[Y]            -4.0181          7.2278        0.010208        0.010208
v  Velocity[Z]       -6.9287e-015     4.1554e-015    -1.3822e-017    -1.3822e-017
v  ǁVelocityǁ        0.00048365          9.7103          4.9671          4.9671
v  Pressure               -47.811          20.227         -1.8733         -1.8733
v  nu_tilda           4.3168e-007       0.0042636      0.00075715      0.00075715
v  TempC                       21          73.414          21.417          21.417
v  TurbVisc           3.0979e-014        0.005025      0.00087969      0.00087969
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              445:        0.33160E+01

===============================================================


 INSTANT    0.446000000E+03   TIME STEP NUMBER             446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45263E-02 0.88947E+00
   Friction velocity        uk    :  0.45263E-02 0.88947E+00
   Dimensionless distance   yplus :  0.36439E-01 0.71608E+01
   Friction thermal sca.    tstar : -0.20840E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27188E-01 0.53428E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55692E-02      34   0.55107E-03   0.48123E+01 0.13292E+03 
c  Velocity[X]                                      0.24679E+01 
c  Velocity[Y]                                      0.23444E+01 
c  Velocity[Z]                                      0.10939E-29 
c  Pressure     0.14915E-06     377   0.94376E-08   0.15132E+00 0.31854E+03 
c  nu_tilda     0.40802E-05      33   0.11927E-04   0.32939E-06 0.20941E+03 
c  TempC        0.24421E+02      29   0.60239E-03   0.82831E+01 0.32961E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5686           9.717          4.5729          4.5729
v  Velocity[Y]            -4.0082          7.1986        0.010263        0.010263
v  Velocity[Z]       -6.9287e-015      4.172e-015    -1.3847e-017    -1.3847e-017
v  ǁVelocityǁ        0.00049745          9.7185          4.9678          4.9678
v  Pressure               -47.849          20.175         -1.8787         -1.8787
v  nu_tilda           4.3022e-007       0.0042637      0.00075782      0.00075782
v  TempC                       21          73.424          21.418          21.418
v  TurbVisc           3.0551e-014       0.0050251      0.00088045      0.00088045
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              446:        0.25220E+01

===============================================================


 INSTANT    0.447000000E+03   TIME STEP NUMBER             447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20440E-02 0.88807E+00
   Friction velocity        uk    :  0.20440E-02 0.88807E+00
   Dimensionless distance   yplus :  0.16455E-01 0.71496E+01
   Friction thermal sca.    tstar : -0.28772E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12278E-01 0.53344E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55732E-02      34   0.62719E-03   0.47482E+01 0.13238E+03 
c  Velocity[X]                                      0.24276E+01 
c  Velocity[Y]                                      0.23207E+01 
c  Velocity[Z]                                      0.12859E-29 
c  Pressure     0.12932E-06     489   0.99436E-08   0.12817E+00 0.40228E+03 
c  nu_tilda     0.40828E-05      33   0.13021E-04   0.32864E-06 0.20899E+03 
c  TempC        0.24435E+02      29   0.68415E-03   0.10140E+02 0.36040E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5746          9.7244          4.5729          4.5729
v  Velocity[Y]            -3.9982          7.2198        0.010319        0.010319
v  Velocity[Z]       -6.9287e-015     4.1931e-015    -1.3865e-017    -1.3865e-017
v  ǁVelocityǁ         0.0011027          9.7262          4.9686          4.9686
v  Pressure               -47.959          20.195         -1.9105         -1.9105
v  nu_tilda           4.2873e-007       0.0042637      0.00075843      0.00075843
v  TempC                       21          73.436          21.419          21.419
v  TurbVisc           3.0139e-014       0.0050251      0.00088122      0.00088122
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              447:        0.27280E+01

===============================================================


 INSTANT    0.448000000E+03   TIME STEP NUMBER             448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68565E-02 0.88901E+00
   Friction velocity        uk    :  0.68565E-02 0.88901E+00
   Dimensionless distance   yplus :  0.55199E-01 0.71572E+01
   Friction thermal sca.    tstar : -0.13697E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41185E-01 0.53400E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55772E-02      34   0.63976E-03   0.47975E+01 0.13259E+03 
c  Velocity[X]                                      0.24712E+01 
c  Velocity[Y]                                      0.23263E+01 
c  Velocity[Z]                                      0.11395E-29 
c  Pressure     0.18727E-06     394   0.98943E-08   0.18882E+00 0.27971E+03 
c  nu_tilda     0.40854E-05      33   0.11924E-04   0.32788E-06 0.20857E+03 
c  TempC        0.24449E+02      29   0.55380E-03   0.13761E+02 0.41626E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5812          9.7315          4.5729          4.5729
v  Velocity[Y]            -3.9884          7.1971        0.010374        0.010374
v  Velocity[Z]       -6.9287e-015     4.2145e-015    -1.3884e-017    -1.3884e-017
v  ǁVelocityǁ          0.001134          9.7336          4.9694          4.9694
v  Pressure               -47.986          20.164         -1.9066         -1.9066
v  nu_tilda           4.2727e-007       0.0042637       0.0007591       0.0007591
v  TempC                       21          73.423          21.419          21.419
v  TurbVisc           2.9723e-014       0.0050252      0.00088198      0.00088198
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              448:        0.24700E+01

===============================================================


 INSTANT    0.449000000E+03   TIME STEP NUMBER             449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25653E-02 0.88813E+00
   Friction velocity        uk    :  0.25653E-02 0.88813E+00
   Dimensionless distance   yplus :  0.20652E-01 0.71501E+01
   Friction thermal sca.    tstar : -0.47169E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15409E-01 0.53348E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55812E-02      34   0.54867E-03   0.47682E+01 0.13224E+03 
c  Velocity[X]                                      0.24578E+01 
c  Velocity[Y]                                      0.23104E+01 
c  Velocity[Z]                                      0.11392E-29 
c  Pressure     0.15344E-06     488   0.99406E-08   0.14807E+00 0.43311E+03 
c  nu_tilda     0.40881E-05      33   0.12967E-04   0.32712E-06 0.20815E+03 
c  TempC        0.24464E+02      29   0.64169E-03   0.10944E+02 0.36954E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5883           9.738          4.5729          4.5729
v  Velocity[Y]            -3.9785          7.2133         0.01043         0.01043
v  Velocity[Z]       -6.9287e-015     4.2339e-015    -1.3898e-017    -1.3898e-017
v  ǁVelocityǁ         0.0010704          9.7404          4.9702          4.9702
v  Pressure               -48.101           20.16         -1.9454         -1.9454
v  nu_tilda           4.2573e-007       0.0042638      0.00075972      0.00075972
v  TempC                       21          73.404           21.42           21.42
v  TurbVisc            2.932e-014       0.0050253      0.00088275      0.00088275
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              449:        0.27820E+01

===============================================================


 INSTANT    0.450000000E+03   TIME STEP NUMBER             450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32223E-02 0.88938E+00
   Friction velocity        uk    :  0.32223E-02 0.88938E+00
   Dimensionless distance   yplus :  0.25942E-01 0.71601E+01
   Friction thermal sca.    tstar : -0.11281E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19356E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55853E-02      34   0.60035E-03   0.46999E+01 0.13156E+03 
c  Velocity[X]                                      0.24015E+01 
c  Velocity[Y]                                      0.22984E+01 
c  Velocity[Z]                                      0.14007E-29 
c  Pressure     0.14693E-06     394   0.94475E-08   0.14874E+00 0.26693E+03 
c  nu_tilda     0.40907E-05      33   0.11929E-04   0.32636E-06 0.20773E+03 
c  TempC        0.24478E+02      29   0.57118E-03   0.10326E+02 0.35422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.595           9.746          4.5729          4.5729
v  Velocity[Y]            -3.9688          7.1924        0.010485        0.010485
v  Velocity[Z]       -6.9287e-015     4.2508e-015    -1.3916e-017    -1.3916e-017
v  ǁVelocityǁ         0.0012054          9.7475          4.9709          4.9709
v  Pressure               -48.134          20.153         -1.9385         -1.9385
v  nu_tilda           4.2417e-007       0.0042638      0.00076039      0.00076039
v  TempC                       21          73.333          21.421          21.421
v  TurbVisc           2.8901e-014       0.0050253      0.00088352      0.00088352
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              450:        0.22420E+01

===============================================================


 INSTANT    0.451000000E+03   TIME STEP NUMBER             451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67143E-02 0.88836E+00
   Friction velocity        uk    :  0.67143E-02 0.88836E+00
   Dimensionless distance   yplus :  0.54055E-01 0.71519E+01
   Friction thermal sca.    tstar : -0.10365E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40331E-01 0.53361E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55893E-02      34   0.58124E-03   0.46891E+01 0.13147E+03 
c  Velocity[X]                                      0.23797E+01 
c  Velocity[Y]                                      0.23093E+01 
c  Velocity[Z]                                      0.12568E-29 
c  Pressure     0.11447E-06     489   0.98830E-08   0.11375E+00 0.41360E+03 
c  nu_tilda     0.40933E-05      33   0.12940E-04   0.32558E-06 0.20732E+03 
c  TempC        0.24493E+02      29   0.10347E-02   0.10627E+02 0.36899E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6014          9.7539          4.5729          4.5729
v  Velocity[Y]            -3.9589          7.2125        0.010542        0.010542
v  Velocity[Z]       -6.9287e-015      4.269e-015    -1.3928e-017    -1.3928e-017
v  ǁVelocityǁ         0.0019574          9.7555          4.9717          4.9717
v  Pressure               -48.252          20.177         -1.9721         -1.9721
v  nu_tilda           4.2258e-007       0.0042639      0.00076101      0.00076101
v  TempC                       21          73.379          21.421          21.421
v  TurbVisc           2.8478e-014       0.0050254      0.00088429      0.00088429
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              451:        0.28020E+01

===============================================================


 INSTANT    0.452000000E+03   TIME STEP NUMBER             452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13738E-01 0.88932E+00
   Friction velocity        uk    :  0.13738E-01 0.88932E+00
   Dimensionless distance   yplus :  0.11060E+00 0.71596E+01
   Friction thermal sca.    tstar : -0.11296E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82521E-01 0.53419E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55933E-02      34   0.59296E-03   0.46932E+01 0.13133E+03 
c  Velocity[X]                                      0.23918E+01 
c  Velocity[Y]                                      0.23014E+01 
c  Velocity[Z]                                      0.11323E-29 
c  Pressure     0.15536E-06     408   0.91419E-08   0.15182E+00 0.26586E+03 
c  nu_tilda     0.40959E-05      33   0.11925E-04   0.32481E-06 0.20690E+03 
c  TempC        0.24507E+02      29   0.65012E-03   0.15525E+02 0.44020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6076          9.7614          4.5729          4.5729
v  Velocity[Y]            -3.9493          7.2087        0.010597        0.010597
v  Velocity[Z]       -6.9287e-015     4.2875e-015    -1.3942e-017    -1.3942e-017
v  ǁVelocityǁ         0.0025008          9.7634          4.9725          4.9725
v  Pressure               -48.288          20.177         -1.9653         -1.9653
v  nu_tilda           4.2102e-007       0.0042639      0.00076168      0.00076168
v  TempC                       21          72.945          21.422          21.422
v  TurbVisc           2.8054e-014       0.0050254      0.00088505      0.00088505
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              452:        0.34170E+01

===============================================================


 INSTANT    0.453000000E+03   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16195E-01 0.88892E+00
   Friction velocity        uk    :  0.16195E-01 0.88892E+00
   Dimensionless distance   yplus :  0.13038E+00 0.71564E+01
   Friction thermal sca.    tstar : -0.87899E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97280E-01 0.53395E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.55973E-02      34   0.59164E-03   0.46738E+01 0.13108E+03 
c  Velocity[X]                                      0.23925E+01 
c  Velocity[Y]                                      0.22812E+01 
c  Velocity[Z]                                      0.14836E-29 
c  Pressure     0.14966E-06     520   0.95790E-08   0.15238E+00 0.70168E+03 
c  nu_tilda     0.40985E-05      33   0.12917E-04   0.32404E-06 0.20649E+03 
c  TempC        0.24521E+02      29   0.52877E-03   0.11805E+02 0.39043E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6141          9.7685          4.5729          4.5729
v  Velocity[Y]            -3.9395          7.1847        0.010653        0.010653
v  Velocity[Z]       -6.9287e-015      4.308e-015    -1.3953e-017    -1.3953e-017
v  ǁVelocityǁ         0.0026913          9.7706          4.9732          4.9732
v  Pressure               -48.396           20.08         -2.0184         -2.0184
v  nu_tilda           4.1952e-007        0.004264       0.0007623       0.0007623
v  TempC                       21          72.947          21.423          21.423
v  TurbVisc           2.7642e-014       0.0050255      0.00088582      0.00088582
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              453:        0.41110E+01

===============================================================


 INSTANT    0.454000000E+03   TIME STEP NUMBER             454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14993E-01 0.88753E+00
   Friction velocity        uk    :  0.14993E-01 0.88753E+00
   Dimensionless distance   yplus :  0.12070E+00 0.71452E+01
   Friction thermal sca.    tstar : -0.85904E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90057E-01 0.53311E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56013E-02      34   0.59078E-03   0.46317E+01 0.13070E+03 
c  Velocity[X]                                      0.23402E+01 
c  Velocity[Y]                                      0.22915E+01 
c  Velocity[Z]                                      0.12757E-29 
c  Pressure     0.15003E-06     474   0.97695E-08   0.14990E+00 0.74872E+03 
c  nu_tilda     0.41011E-05      33   0.11932E-04   0.32328E-06 0.20608E+03 
c  TempC        0.24536E+02      29   0.52173E-03   0.92697E+01 0.34190E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6213          9.7755          4.5729          4.5729
v  Velocity[Y]              -3.93          7.2031        0.010709        0.010709
v  Velocity[Z]       -6.9287e-015     4.3268e-015    -1.3959e-017    -1.3959e-017
v  ǁVelocityǁ         0.0035421          9.7777           4.974           4.974
v  Pressure               -48.434          20.194          -1.988          -1.988
v  nu_tilda           4.1791e-007        0.004264      0.00076297      0.00076297
v  TempC                       21          72.951          21.424          21.424
v  TurbVisc            2.725e-014       0.0050255      0.00088658      0.00088658
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              454:        0.30790E+01

===============================================================


 INSTANT    0.455000000E+03   TIME STEP NUMBER             455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18612E-01 0.88851E+00
   Friction velocity        uk    :  0.18612E-01 0.88851E+00
   Dimensionless distance   yplus :  0.14984E+00 0.71531E+01
   Friction thermal sca.    tstar : -0.79472E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11180E+00 0.53370E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56054E-02      34   0.55483E-03   0.46132E+01 0.13039E+03 
c  Velocity[X]                                      0.23466E+01 
c  Velocity[Y]                                      0.22665E+01 
c  Velocity[Z]                                      0.14481E-29 
c  Pressure     0.14238E-06     505   0.91751E-08   0.14327E+00 0.82419E+03 
c  nu_tilda     0.41036E-05      33   0.12875E-04   0.32251E-06 0.20567E+03 
c  TempC        0.24550E+02      29   0.75281E-03   0.96513E+01 0.35307E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6281           9.782          4.5729          4.5729
v  Velocity[Y]            -3.9204          7.1869        0.010766        0.010766
v  Velocity[Z]       -6.9287e-015     4.3446e-015    -1.3969e-017    -1.3969e-017
v  ǁVelocityǁ         0.0036764          9.7842          4.9748          4.9748
v  Pressure               -48.545          20.074         -2.0474         -2.0474
v  nu_tilda           4.1637e-007       0.0042641      0.00076359      0.00076359
v  TempC                       21          73.432          21.424          21.424
v  TurbVisc           2.6834e-014       0.0050256      0.00088735      0.00088735
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              455:        0.31480E+01

===============================================================


 INSTANT    0.456000000E+03   TIME STEP NUMBER             456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18616E-01 0.88735E+00
   Friction velocity        uk    :  0.18616E-01 0.88735E+00
   Dimensionless distance   yplus :  0.14987E+00 0.71438E+01
   Friction thermal sca.    tstar : -0.77308E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11182E+00 0.53301E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56094E-02      34   0.57128E-03   0.45893E+01 0.13003E+03 
c  Velocity[X]                                      0.23410E+01 
c  Velocity[Y]                                      0.22484E+01 
c  Velocity[Z]                                      0.13823E-29 
c  Pressure     0.17126E-06     472   0.94355E-08   0.16758E+00 0.58988E+03 
c  nu_tilda     0.41062E-05      33   0.11933E-04   0.32173E-06 0.20525E+03 
c  TempC        0.24564E+02      29   0.61160E-03   0.15877E+02 0.43409E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6347          9.7878          4.5729          4.5729
v  Velocity[Y]             -3.911             7.2        0.010821        0.010821
v  Velocity[Z]       -6.9287e-015     4.3616e-015    -1.3971e-017    -1.3971e-017
v  ǁVelocityǁ          0.004064          9.7906          4.9756          4.9756
v  Pressure               -48.583          20.159         -2.0239         -2.0239
v  nu_tilda           4.1477e-007       0.0042641      0.00076426      0.00076426
v  TempC                       21          72.955          21.425          21.425
v  TurbVisc           2.6442e-014       0.0050256      0.00088812      0.00088812
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              456:        0.36710E+01

===============================================================


 INSTANT    0.457000000E+03   TIME STEP NUMBER             457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18504E-01 0.88839E+00
   Friction velocity        uk    :  0.18504E-01 0.88839E+00
   Dimensionless distance   yplus :  0.14897E+00 0.71522E+01
   Friction thermal sca.    tstar : -0.70977E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11115E+00 0.53363E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56134E-02      34   0.61898E-03   0.45411E+01 0.12965E+03 
c  Velocity[X]                                      0.22859E+01 
c  Velocity[Y]                                      0.22552E+01 
c  Velocity[Z]                                      0.12247E-29 
c  Pressure     0.14676E-06     490   0.92510E-08   0.14814E+00 0.40554E+03 
c  nu_tilda     0.41088E-05      33   0.12852E-04   0.32096E-06 0.20484E+03 
c  TempC        0.24579E+02      29   0.51180E-03   0.10391E+02 0.37019E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6412          9.7934          4.5729          4.5729
v  Velocity[Y]            -3.9014          7.2047        0.010878        0.010878
v  Velocity[Z]       -6.9287e-015     4.3794e-015    -1.3977e-017    -1.3977e-017
v  ǁVelocityǁ          0.004038          9.7962          4.9763          4.9763
v  Pressure               -48.694          20.152         -2.0592         -2.0592
v  nu_tilda           4.1321e-007       0.0042642      0.00076488      0.00076488
v  TempC                       21          72.958          21.426          21.426
v  TurbVisc           2.6036e-014       0.0050257      0.00088889      0.00088889
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              457:        0.31440E+01

===============================================================


 INSTANT    0.458000000E+03   TIME STEP NUMBER             458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18470E-01 0.88762E+00
   Friction velocity        uk    :  0.18470E-01 0.88762E+00
   Dimensionless distance   yplus :  0.14870E+00 0.71459E+01
   Friction thermal sca.    tstar : -0.67663E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11095E+00 0.53316E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56174E-02      34   0.58272E-03   0.45577E+01 0.12970E+03 
c  Velocity[X]                                      0.23072E+01 
c  Velocity[Y]                                      0.22505E+01 
c  Velocity[Z]                                      0.10158E-29 
c  Pressure     0.14036E-06     409   0.98372E-08   0.14343E+00 0.35808E+03 
c  nu_tilda     0.41113E-05      33   0.11933E-04   0.32017E-06 0.20443E+03 
c  TempC        0.24593E+02      29   0.46200E-03   0.87511E+01 0.32785E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6475          9.7984          4.5729          4.5729
v  Velocity[Y]            -3.8921          7.1777        0.010934        0.010934
v  Velocity[Z]       -6.9287e-015     4.3931e-015    -1.3978e-017    -1.3978e-017
v  ǁVelocityǁ         0.0039533          9.8018          4.9771          4.9771
v  Pressure               -48.734          20.092         -2.0675         -2.0675
v  nu_tilda           4.1171e-007       0.0042642      0.00076555      0.00076555
v  TempC                       21          73.084          21.427          21.427
v  TurbVisc           2.5649e-014       0.0050257      0.00088965      0.00088965
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              458:        0.28150E+01

===============================================================


 INSTANT    0.459000000E+03   TIME STEP NUMBER             459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18491E-01 0.88617E+00
   Friction velocity        uk    :  0.18491E-01 0.88617E+00
   Dimensionless distance   yplus :  0.14886E+00 0.71343E+01
   Friction thermal sca.    tstar : -0.67637E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11107E+00 0.53230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56215E-02      34   0.61298E-03   0.45495E+01 0.12947E+03 
c  Velocity[X]                                      0.23169E+01 
c  Velocity[Y]                                      0.22325E+01 
c  Velocity[Z]                                      0.14331E-29 
c  Pressure     0.17661E-06     426   0.96970E-08   0.17652E+00 0.46639E+03 
c  nu_tilda     0.41139E-05      33   0.12829E-04   0.31937E-06 0.20402E+03 
c  TempC        0.24607E+02      29   0.95967E-03   0.10248E+02 0.35051E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.655          9.8031          4.5729          4.5729
v  Velocity[Y]            -3.8827          7.1972        0.010991        0.010991
v  Velocity[Z]       -6.9287e-015     4.4122e-015    -1.3976e-017    -1.3976e-017
v  ǁVelocityǁ          0.003995          9.8067          4.9779          4.9779
v  Pressure               -48.837          20.145         -2.0865         -2.0865
v  nu_tilda           4.1018e-007       0.0042642      0.00076617      0.00076617
v  TempC                       21          73.586          21.427          21.427
v  TurbVisc           2.5278e-014       0.0050258      0.00089042      0.00089042
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              459:        0.34400E+01

===============================================================


 INSTANT    0.460000000E+03   TIME STEP NUMBER             460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18394E-01 0.88698E+00
   Friction velocity        uk    :  0.18394E-01 0.88698E+00
   Dimensionless distance   yplus :  0.14808E+00 0.71408E+01
   Friction thermal sca.    tstar : -0.11054E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11049E+00 0.53278E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56255E-02      34   0.57327E-03   0.45456E+01 0.12930E+03 
c  Velocity[X]                                      0.23036E+01 
c  Velocity[Y]                                      0.22420E+01 
c  Velocity[Z]                                      0.13866E-29 
c  Pressure     0.15426E-06     392   0.98174E-08   0.15341E+00 0.39463E+03 
c  nu_tilda     0.41165E-05      33   0.11934E-04   0.31859E-06 0.20362E+03 
c  TempC        0.24622E+02      29   0.50970E-03   0.13882E+02 0.41374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.662          9.8091          4.5729          4.5729
v  Velocity[Y]            -3.8733          7.1584        0.011047        0.011047
v  Velocity[Z]       -6.9287e-015     4.4253e-015    -1.3969e-017    -1.3969e-017
v  ǁVelocityǁ          0.003991          9.8116          4.9786          4.9786
v  Pressure               -48.876          20.075          -2.095          -2.095
v  nu_tilda           4.0868e-007       0.0042643      0.00076684      0.00076684
v  TempC                       21          72.964          21.428          21.428
v  TurbVisc           2.4904e-014       0.0050258      0.00089119      0.00089119
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              460:        0.30550E+01

===============================================================


 INSTANT    0.461000000E+03   TIME STEP NUMBER             461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10238E-01 0.88619E+00
   Friction velocity        uk    :  0.10238E-01 0.88619E+00
   Dimensionless distance   yplus :  0.82422E-01 0.71344E+01
   Friction thermal sca.    tstar : -0.12645E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61496E-01 0.53231E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56295E-02      34   0.56608E-03   0.44736E+01 0.12867E+03 
c  Velocity[X]                                      0.22570E+01 
c  Velocity[Y]                                      0.22165E+01 
c  Velocity[Z]                                      0.11468E-29 
c  Pressure     0.13579E-06     424   0.96308E-08   0.13600E+00 0.54980E+03 
c  nu_tilda     0.41190E-05      33   0.12776E-04   0.31780E-06 0.20321E+03 
c  TempC        0.24636E+02      29   0.44237E-03   0.91563E+01 0.34337E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.669          9.8151          4.5729          4.5729
v  Velocity[Y]            -3.8646           7.185        0.011104        0.011104
v  Velocity[Z]       -6.9287e-015     4.4451e-015    -1.3962e-017    -1.3962e-017
v  ǁVelocityǁ         0.0039377          9.8177          4.9794          4.9794
v  Pressure               -48.986          20.155         -2.1113         -2.1113
v  nu_tilda           4.0714e-007       0.0042643      0.00076746      0.00076746
v  TempC                       21          72.965          21.429          21.429
v  TurbVisc           2.4542e-014       0.0050259      0.00089196      0.00089196
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              461:        0.26360E+01

===============================================================


 INSTANT    0.462000000E+03   TIME STEP NUMBER             462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12869E-01 0.88747E+00
   Friction velocity        uk    :  0.12869E-01 0.88747E+00
   Dimensionless distance   yplus :  0.10360E+00 0.71447E+01
   Friction thermal sca.    tstar : -0.29526E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77299E-01 0.53308E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56335E-02      34   0.61512E-03   0.44383E+01 0.12838E+03 
c  Velocity[X]                                      0.22366E+01 
c  Velocity[Y]                                      0.22017E+01 
c  Velocity[Z]                                      0.13735E-29 
c  Pressure     0.11279E-06     409   0.95631E-08   0.11309E+00 0.27958E+03 
c  nu_tilda     0.41216E-05      33   0.11926E-04   0.31701E-06 0.20280E+03 
c  TempC        0.24650E+02      29   0.70983E-03   0.71131E+01 0.30433E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6755          9.8206          4.5729          4.5729
v  Velocity[Y]            -3.8554          7.1912         0.01116         0.01116
v  Velocity[Z]       -6.9287e-015     4.4622e-015    -1.3951e-017    -1.3951e-017
v  ǁVelocityǁ         0.0039275          9.8237          4.9802          4.9802
v  Pressure               -49.029          20.179         -2.1047         -2.1047
v  nu_tilda           4.0563e-007       0.0042644      0.00076813      0.00076813
v  TempC                       21          73.189           21.43           21.43
v  TurbVisc           2.4175e-014       0.0050259      0.00089272      0.00089272
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              462:        0.25970E+01

===============================================================


 INSTANT    0.463000000E+03   TIME STEP NUMBER             463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14553E-01 0.88720E+00
   Friction velocity        uk    :  0.14553E-01 0.88720E+00
   Dimensionless distance   yplus :  0.11716E+00 0.71426E+01
   Friction thermal sca.    tstar : -0.10002E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87416E-01 0.53292E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56376E-02      34   0.58311E-03   0.44949E+01 0.12868E+03 
c  Velocity[X]                                      0.22777E+01 
c  Velocity[Y]                                      0.22171E+01 
c  Velocity[Z]                                      0.12081E-29 
c  Pressure     0.15912E-06     520   0.99495E-08   0.16049E+00 0.71570E+03 
c  nu_tilda     0.41241E-05      33   0.12756E-04   0.31622E-06 0.20240E+03 
c  TempC        0.24664E+02      29   0.62797E-03   0.99227E+01 0.35820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.682          9.8259          4.5729          4.5729
v  Velocity[Y]            -3.8463          7.1681        0.011217        0.011217
v  Velocity[Z]       -6.9287e-015     4.4837e-015    -1.3947e-017    -1.3947e-017
v  ǁVelocityǁ         0.0039326          9.8292          4.9809          4.9809
v  Pressure               -49.134          20.069         -2.1573         -2.1573
v  nu_tilda           4.0424e-007       0.0042644      0.00076875      0.00076875
v  TempC                       21          73.429           21.43           21.43
v  TurbVisc           2.3817e-014        0.005026      0.00089349      0.00089349
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              463:        0.29310E+01

===============================================================


 INSTANT    0.464000000E+03   TIME STEP NUMBER             464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12145E-01 0.88574E+00
   Friction velocity        uk    :  0.12145E-01 0.88574E+00
   Dimensionless distance   yplus :  0.97779E-01 0.71308E+01
   Friction thermal sca.    tstar : -0.76787E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72954E-01 0.53204E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56416E-02      34   0.53342E-03   0.44469E+01 0.12809E+03 
c  Velocity[X]                                      0.22492E+01 
c  Velocity[Y]                                      0.21976E+01 
c  Velocity[Z]                                      0.11630E-29 
c  Pressure     0.16078E-06     458   0.98644E-08   0.15743E+00 0.57700E+03 
c  nu_tilda     0.41266E-05      33   0.11939E-04   0.31543E-06 0.20199E+03 
c  TempC        0.24679E+02      29   0.56682E-03   0.10748E+02 0.37831E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6893          9.8307          4.5729          4.5729
v  Velocity[Y]            -3.8374          7.1767        0.011274        0.011274
v  Velocity[Z]       -6.9287e-015     4.4982e-015    -1.3937e-017    -1.3937e-017
v  ǁVelocityǁ         0.0038949          9.8345          4.9817          4.9817
v  Pressure               -49.174          20.155          -2.135          -2.135
v  nu_tilda            4.029e-007       0.0042644      0.00076942      0.00076942
v  TempC                       21          73.748          21.431          21.431
v  TurbVisc           2.3492e-014        0.005026      0.00089426      0.00089426
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              464:        0.27380E+01

===============================================================


 INSTANT    0.465000000E+03   TIME STEP NUMBER             465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83101E-02 0.88684E+00
   Friction velocity        uk    :  0.83101E-02 0.88684E+00
   Dimensionless distance   yplus :  0.66902E-01 0.71396E+01
   Friction thermal sca.    tstar : -0.63728E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49916E-01 0.53270E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56456E-02      34   0.60866E-03   0.43851E+01 0.12754E+03 
c  Velocity[X]                                      0.22079E+01 
c  Velocity[Y]                                      0.21772E+01 
c  Velocity[Z]                                      0.11948E-29 
c  Pressure     0.15734E-06     504   0.97970E-08   0.16032E+00 0.60755E+03 
c  nu_tilda     0.41291E-05      33   0.12720E-04   0.31463E-06 0.20159E+03 
c  TempC        0.24693E+02      29   0.48189E-03   0.90628E+01 0.34414E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6967          9.8352          4.5729          4.5729
v  Velocity[Y]            -3.8287           7.157        0.011331        0.011331
v  Velocity[Z]       -6.9287e-015     4.5147e-015     -1.393e-017     -1.393e-017
v  ǁVelocityǁ          0.003878          9.8392          4.9824          4.9824
v  Pressure               -49.274          20.063         -2.1818         -2.1818
v  nu_tilda            4.016e-007       0.0042645      0.00077005      0.00077005
v  TempC                       21          72.974          21.432          21.432
v  TurbVisc           2.3182e-014       0.0050261      0.00089503      0.00089503
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              465:        0.29100E+01

===============================================================


 INSTANT    0.466000000E+03   TIME STEP NUMBER             466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53428E-02 0.88611E+00
   Friction velocity        uk    :  0.53428E-02 0.88611E+00
   Dimensionless distance   yplus :  0.43013E-01 0.71338E+01
   Friction thermal sca.    tstar : -0.53557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32093E-01 0.53226E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56496E-02      34   0.60894E-03   0.43790E+01 0.12748E+03 
c  Velocity[X]                                      0.22003E+01 
c  Velocity[Y]                                      0.21787E+01 
c  Velocity[Z]                                      0.11540E-29 
c  Pressure     0.14763E-06     472   0.99855E-08   0.14790E+00 0.66732E+03 
c  nu_tilda     0.41317E-05      33   0.11931E-04   0.31381E-06 0.20118E+03 
c  TempC        0.24707E+02      29   0.74354E-03   0.90308E+01 0.33920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7035          9.8392          4.5729          4.5729
v  Velocity[Y]            -3.8199          7.1761        0.011387        0.011387
v  Velocity[Z]       -6.9287e-015     4.5268e-015    -1.3923e-017    -1.3923e-017
v  ǁVelocityǁ         0.0038505          9.8438          4.9832          4.9832
v  Pressure               -49.323          20.181         -2.1585         -2.1585
v  nu_tilda           4.0032e-007       0.0042645      0.00077071      0.00077071
v  TempC                       21          72.977          21.433          21.433
v  TurbVisc           2.2884e-014       0.0050261      0.00089579      0.00089579
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              466:        0.28240E+01

===============================================================


 INSTANT    0.467000000E+03   TIME STEP NUMBER             467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94544E-02 0.88713E+00
   Friction velocity        uk    :  0.94544E-02 0.88713E+00
   Dimensionless distance   yplus :  0.76114E-01 0.71420E+01
   Friction thermal sca.    tstar : -0.49457E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56790E-01 0.53287E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56537E-02      34   0.57566E-03   0.43763E+01 0.12736E+03 
c  Velocity[X]                                      0.22114E+01 
c  Velocity[Y]                                      0.21649E+01 
c  Velocity[Z]                                      0.11932E-29 
c  Pressure     0.14623E-06     488   0.95809E-08   0.14639E+00 0.50375E+03 
c  nu_tilda     0.41342E-05      33   0.12688E-04   0.31298E-06 0.20077E+03 
c  TempC        0.24721E+02      29   0.64033E-03   0.14877E+02 0.43826E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.71          9.8429          4.5729          4.5729
v  Velocity[Y]            -3.8112          7.1858        0.011445        0.011445
v  Velocity[Z]       -6.9287e-015     4.5434e-015    -1.3912e-017    -1.3912e-017
v  ǁVelocityǁ         0.0038348          9.8477           4.984           4.984
v  Pressure               -49.431          20.127         -2.2018         -2.2018
v  nu_tilda           3.9906e-007       0.0042646      0.00077134      0.00077134
v  TempC                       21          73.062          21.433          21.433
v  TurbVisc           2.2593e-014       0.0050262      0.00089656      0.00089656
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              467:        0.32560E+01

===============================================================


 INSTANT    0.468000000E+03   TIME STEP NUMBER             468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14161E-01 0.88652E+00
   Friction velocity        uk    :  0.14161E-01 0.88652E+00
   Dimensionless distance   yplus :  0.11401E+00 0.71371E+01
   Friction thermal sca.    tstar : -0.49791E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85064E-01 0.53250E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56577E-02      34   0.56477E-03   0.43939E+01 0.12715E+03 
c  Velocity[X]                                      0.22429E+01 
c  Velocity[Y]                                      0.21510E+01 
c  Velocity[Z]                                      0.14091E-29 
c  Pressure     0.19661E-06     362   0.98473E-08   0.19522E+00 0.32189E+03 
c  nu_tilda     0.41367E-05      33   0.11937E-04   0.31217E-06 0.20037E+03 
c  TempC        0.24735E+02      29   0.49002E-03   0.11392E+02 0.38629E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7164          9.8462          4.5729          4.5729
v  Velocity[Y]            -3.8028          7.1475        0.011501        0.011501
v  Velocity[Z]       -6.9287e-015     4.5566e-015    -1.3903e-017    -1.3903e-017
v  ǁVelocityǁ         0.0038489          9.8517          4.9847          4.9847
v  Pressure               -49.461          20.077         -2.2055         -2.2055
v  nu_tilda           3.9791e-007       0.0042646        0.000772        0.000772
v  TempC                       21          73.541          21.434          21.434
v  TurbVisc           2.2311e-014       0.0050262      0.00089733      0.00089733
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              468:        0.32570E+01

===============================================================


 INSTANT    0.469000000E+03   TIME STEP NUMBER             469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15673E-01 0.88509E+00
   Friction velocity        uk    :  0.15673E-01 0.88509E+00
   Dimensionless distance   yplus :  0.12617E+00 0.71256E+01
   Friction thermal sca.    tstar : -0.49370E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94140E-01 0.53165E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56617E-02      34   0.59112E-03   0.43375E+01 0.12675E+03 
c  Velocity[X]                                      0.21747E+01 
c  Velocity[Y]                                      0.21628E+01 
c  Velocity[Z]                                      0.11290E-29 
c  Pressure     0.15171E-06     473   0.97424E-08   0.15210E+00 0.45407E+03 
c  nu_tilda     0.41392E-05      33   0.12655E-04   0.31134E-06 0.19996E+03 
c  TempC        0.24749E+02      29   0.52843E-03   0.80004E+01 0.31719E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7233          9.8494          4.5729          4.5729
v  Velocity[Y]            -3.7945          7.1669        0.011559        0.011559
v  Velocity[Z]       -6.9287e-015     4.5708e-015    -1.3891e-017    -1.3891e-017
v  ǁVelocityǁ         0.0037978          9.8548          4.9855          4.9855
v  Pressure               -49.577          20.129         -2.2304         -2.2304
v  nu_tilda           3.9676e-007       0.0042646      0.00077263      0.00077263
v  TempC                       21          72.986          21.435          21.435
v  TurbVisc           2.2055e-014       0.0050263       0.0008981       0.0008981
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              469:        0.31690E+01

===============================================================


 INSTANT    0.470000000E+03   TIME STEP NUMBER             470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17976E-01 0.88613E+00
   Friction velocity        uk    :  0.17976E-01 0.88613E+00
   Dimensionless distance   yplus :  0.14472E+00 0.71340E+01
   Friction thermal sca.    tstar : -0.55967E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10798E+00 0.53227E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56658E-02      34   0.59891E-03   0.43278E+01 0.12665E+03 
c  Velocity[X]                                      0.21702E+01 
c  Velocity[Y]                                      0.21576E+01 
c  Velocity[Z]                                      0.10857E-29 
c  Pressure     0.17203E-06     376   0.95175E-08   0.17477E+00 0.31403E+03 
c  nu_tilda     0.41417E-05      33   0.11930E-04   0.31053E-06 0.19956E+03 
c  TempC        0.24763E+02      29   0.49113E-03   0.94165E+01 0.34787E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7303          9.8525          4.5729          4.5729
v  Velocity[Y]            -3.7862          7.1448        0.011616        0.011616
v  Velocity[Z]       -6.9287e-015     4.5821e-015    -1.3871e-017    -1.3871e-017
v  ǁVelocityǁ          0.003804          9.8579          4.9862          4.9862
v  Pressure               -49.608          20.083         -2.2346         -2.2346
v  nu_tilda           3.9566e-007       0.0042647       0.0007733       0.0007733
v  TempC                       21          72.991          21.435          21.435
v  TurbVisc           2.1801e-014       0.0050263      0.00089886      0.00089886
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              470:        0.25100E+01

===============================================================


 INSTANT    0.471000000E+03   TIME STEP NUMBER             471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17996E-01 0.88537E+00
   Friction velocity        uk    :  0.17996E-01 0.88537E+00
   Dimensionless distance   yplus :  0.14488E+00 0.71278E+01
   Friction thermal sca.    tstar : -0.62299E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10809E+00 0.53181E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56698E-02      34   0.60994E-03   0.43228E+01 0.12650E+03 
c  Velocity[X]                                      0.21854E+01 
c  Velocity[Y]                                      0.21374E+01 
c  Velocity[Z]                                      0.13184E-29 
c  Pressure     0.16797E-06     458   0.93403E-08   0.16812E+00 0.41297E+03 
c  nu_tilda     0.41442E-05      33   0.12614E-04   0.30971E-06 0.19916E+03 
c  TempC        0.24778E+02      29   0.96447E-03   0.90305E+01 0.33346E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7369          9.8566          4.5729          4.5729
v  Velocity[Y]            -3.7779          7.1723        0.011673        0.011673
v  Velocity[Z]       -6.9287e-015     4.5943e-015    -1.3857e-017    -1.3857e-017
v  ǁVelocityǁ         0.0037699          9.8609           4.987           4.987
v  Pressure               -49.725          20.112         -2.2656         -2.2656
v  nu_tilda           3.9457e-007       0.0042647      0.00077392      0.00077392
v  TempC                       21          72.997          21.436          21.436
v  TurbVisc           2.1561e-014       0.0050264      0.00089964      0.00089964
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              471:        0.30620E+01

===============================================================


 INSTANT    0.472000000E+03   TIME STEP NUMBER             472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17220E-01 0.88654E+00
   Friction velocity        uk    :  0.17220E-01 0.88654E+00
   Dimensionless distance   yplus :  0.13863E+00 0.71372E+01
   Friction thermal sca.    tstar : -0.79630E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10344E+00 0.53252E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56738E-02      34   0.56840E-03   0.43279E+01 0.12640E+03 
c  Velocity[X]                                      0.21782E+01 
c  Velocity[Y]                                      0.21497E+01 
c  Velocity[Z]                                      0.11328E-29 
c  Pressure     0.20649E-06     361   0.91497E-08   0.20540E+00 0.30097E+03 
c  nu_tilda     0.41467E-05      33   0.11934E-04   0.30889E-06 0.19875E+03 
c  TempC        0.24792E+02      29   0.58088E-03   0.19338E+02 0.44978E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.743          9.8603          4.5729          4.5729
v  Velocity[Y]            -3.7701          7.1359        0.011731        0.011731
v  Velocity[Z]       -6.9287e-015     4.6045e-015    -1.3841e-017    -1.3841e-017
v  ǁVelocityǁ         0.0037696          9.8651          4.9877          4.9877
v  Pressure               -49.758          20.071         -2.2696         -2.2696
v  nu_tilda           3.9351e-007       0.0042648      0.00077459      0.00077459
v  TempC                       21           73.22          21.437          21.437
v  TurbVisc           2.1324e-014       0.0050264       0.0009004       0.0009004
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              472:        0.28240E+01

===============================================================


 INSTANT    0.473000000E+03   TIME STEP NUMBER             473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13142E-01 0.88566E+00
   Friction velocity        uk    :  0.13142E-01 0.88566E+00
   Dimensionless distance   yplus :  0.10581E+00 0.71301E+01
   Friction thermal sca.    tstar : -0.11634E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78943E-01 0.53199E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56778E-02      34   0.48605E-03   0.42435E+01 0.12572E+03 
c  Velocity[X]                                      0.21205E+01 
c  Velocity[Y]                                      0.21230E+01 
c  Velocity[Z]                                      0.11977E-29 
c  Pressure     0.17550E-06     472   0.97594E-08   0.17644E+00 0.43217E+03 
c  nu_tilda     0.41492E-05      32   0.12601E-04   0.30805E-06 0.19835E+03 
c  TempC        0.24806E+02      29   0.56536E-03   0.11327E+02 0.35755E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7487           9.864          4.5729          4.5729
v  Velocity[Y]            -3.7621          7.1639        0.011788        0.011788
v  Velocity[Z]       -6.9287e-015     4.6158e-015    -1.3822e-017    -1.3822e-017
v  ǁVelocityǁ         0.0037467          9.8688          4.9885          4.9885
v  Pressure               -49.873          20.114         -2.2979         -2.2979
v  nu_tilda           3.9247e-007       0.0042648      0.00077521      0.00077521
v  TempC                       21          73.593          21.438          21.438
v  TurbVisc           2.1096e-014       0.0050264      0.00090117      0.00090117
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              473:        0.33660E+01

===============================================================


 INSTANT    0.474000000E+03   TIME STEP NUMBER             474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15772E-01 0.88684E+00
   Friction velocity        uk    :  0.15772E-01 0.88684E+00
   Dimensionless distance   yplus :  0.12698E+00 0.71397E+01
   Friction thermal sca.    tstar : -0.34017E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94739E-01 0.53270E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56819E-02      34   0.62917E-03   0.42055E+01 0.12540E+03 
c  Velocity[X]                                      0.20984E+01 
c  Velocity[Y]                                      0.21071E+01 
c  Velocity[Z]                                      0.12201E-29 
c  Pressure     0.19441E-06     470   0.93012E-08   0.19578E+00 0.44043E+03 
c  nu_tilda     0.41517E-05      32   0.11932E-04   0.30721E-06 0.19794E+03 
c  TempC        0.24820E+02      29   0.65888E-03   0.10621E+02 0.34933E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7543          9.8672          4.5729          4.5729
v  Velocity[Y]            -3.7544          7.1727        0.011845        0.011845
v  Velocity[Z]       -6.9287e-015     4.6265e-015    -1.3799e-017    -1.3799e-017
v  ǁVelocityǁ         0.0037501          9.8721          4.9892          4.9892
v  Pressure               -49.903          20.166         -2.2805         -2.2805
v  nu_tilda           3.9147e-007       0.0042648      0.00077588      0.00077588
v  TempC                       21           73.71          21.438          21.438
v  TurbVisc           2.0874e-014       0.0050265      0.00090194      0.00090194
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              474:        0.28490E+01

===============================================================


 INSTANT    0.475000000E+03   TIME STEP NUMBER             475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17880E-01 0.88615E+00
   Friction velocity        uk    :  0.17880E-01 0.88615E+00
   Dimensionless distance   yplus :  0.14395E+00 0.71341E+01
   Friction thermal sca.    tstar : -0.10561E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10740E+00 0.53228E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56859E-02      34   0.59450E-03   0.42761E+01 0.12578E+03 
c  Velocity[X]                                      0.21560E+01 
c  Velocity[Y]                                      0.21201E+01 
c  Velocity[Z]                                      0.13066E-29 
c  Pressure     0.24083E-06     504   0.99559E-08   0.24508E+00 0.58138E+03 
c  nu_tilda     0.41541E-05      32   0.12558E-04   0.30636E-06 0.19754E+03 
c  TempC        0.24834E+02      29   0.69849E-03   0.12081E+02 0.37684E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7613          9.8698          4.5729          4.5729
v  Velocity[Y]            -3.7468          7.1453        0.011902        0.011902
v  Velocity[Z]       -6.9287e-015     4.6396e-015    -1.3787e-017    -1.3787e-017
v  ǁVelocityǁ         0.0037528          9.8755            4.99            4.99
v  Pressure               -49.993          20.073         -2.3249         -2.3249
v  nu_tilda           3.9052e-007       0.0042649       0.0007765       0.0007765
v  TempC                       21           73.02          21.439          21.439
v  TurbVisc           2.0662e-014       0.0050265      0.00090271      0.00090271
v  total_pressure     1.0128e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              475:        0.32580E+01

===============================================================


 INSTANT    0.476000000E+03   TIME STEP NUMBER             476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12243E-01 0.88453E+00
   Friction velocity        uk    :  0.12243E-01 0.88453E+00
   Dimensionless distance   yplus :  0.98561E-01 0.71211E+01
   Friction thermal sca.    tstar : -0.74684E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73538E-01 0.53131E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56899E-02      34   0.53378E-03   0.42366E+01 0.12523E+03 
c  Velocity[X]                                      0.21369E+01 
c  Velocity[Y]                                      0.20996E+01 
c  Velocity[Z]                                      0.13489E-29 
c  Pressure     0.19858E-06     474   0.96083E-08   0.19454E+00 0.60544E+03 
c  nu_tilda     0.41566E-05      32   0.11950E-04   0.30552E-06 0.19714E+03 
c  TempC        0.24848E+02      29   0.43846E-03   0.12930E+02 0.39367E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7677          9.8724          4.5729          4.5729
v  Velocity[Y]            -3.7395          7.1556        0.011959        0.011959
v  Velocity[Z]       -6.9287e-015     4.6483e-015    -1.3767e-017    -1.3767e-017
v  ǁVelocityǁ         0.0037252          9.8782          4.9908          4.9908
v  Pressure                -50.03          20.169         -2.3017         -2.3017
v  nu_tilda           3.8956e-007       0.0042649      0.00077717      0.00077717
v  TempC                       21          73.025           21.44           21.44
v  TurbVisc           2.0462e-014       0.0050266      0.00090347      0.00090347
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              476:        0.34180E+01

===============================================================


 INSTANT    0.477000000E+03   TIME STEP NUMBER             477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17820E-01 0.88549E+00
   Friction velocity        uk    :  0.17820E-01 0.88549E+00
   Dimensionless distance   yplus :  0.14346E+00 0.71288E+01
   Friction thermal sca.    tstar : -0.70970E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10704E+00 0.53189E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56940E-02      34   0.59931E-03   0.41852E+01 0.12469E+03 
c  Velocity[X]                                      0.21062E+01 
c  Velocity[Y]                                      0.20790E+01 
c  Velocity[Z]                                      0.12147E-29 
c  Pressure     0.17334E-06     489   0.99043E-08   0.17624E+00 0.53266E+03 
c  nu_tilda     0.41591E-05      32   0.12518E-04   0.30468E-06 0.19673E+03 
c  TempC        0.24862E+02      29   0.46924E-03   0.10233E+02 0.34513E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7741          9.8743          4.5729          4.5729
v  Velocity[Y]            -3.7322           7.134        0.012017        0.012017
v  Velocity[Z]       -6.9287e-015     4.6607e-015    -1.3757e-017    -1.3757e-017
v  ǁVelocityǁ         0.0037185          9.8809          4.9915          4.9915
v  Pressure               -50.125          20.095          -2.345          -2.345
v  nu_tilda           3.8862e-007       0.0042649       0.0007778       0.0007778
v  TempC                       21          73.078          21.441          21.441
v  TurbVisc           2.0262e-014       0.0050266      0.00090424      0.00090424
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              477:        0.37160E+01

===============================================================


 INSTANT    0.478000000E+03   TIME STEP NUMBER             478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17805E-01 0.88448E+00
   Friction velocity        uk    :  0.17805E-01 0.88448E+00
   Dimensionless distance   yplus :  0.14334E+00 0.71207E+01
   Friction thermal sca.    tstar : -0.82868E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10695E+00 0.53128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.56980E-02      34   0.59084E-03   0.41823E+01 0.12455E+03 
c  Velocity[X]                                      0.21031E+01 
c  Velocity[Y]                                      0.20793E+01 
c  Velocity[Z]                                      0.12430E-29 
c  Pressure     0.14515E-06     458   0.95497E-08   0.14572E+00 0.64723E+03 
c  nu_tilda     0.41615E-05      32   0.11951E-04   0.30383E-06 0.19633E+03 
c  TempC        0.24876E+02      29   0.57248E-03   0.10445E+02 0.35204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7801          9.8762          4.5729          4.5729
v  Velocity[Y]            -3.7253           7.153        0.012075        0.012075
v  Velocity[Z]       -6.9287e-015      4.669e-015    -1.3734e-017    -1.3734e-017
v  ǁVelocityǁ         0.0037027           9.883          4.9922          4.9922
v  Pressure               -50.164          20.207         -2.3214         -2.3214
v  nu_tilda           3.8767e-007        0.004265      0.00077846      0.00077846
v  TempC                       21          73.329          21.442          21.442
v  TurbVisc           2.0066e-014       0.0050267      0.00090501      0.00090501
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              478:        0.29810E+01

===============================================================


 INSTANT    0.479000000E+03   TIME STEP NUMBER             479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17771E-01 0.88548E+00
   Friction velocity        uk    :  0.17771E-01 0.88548E+00
   Dimensionless distance   yplus :  0.14307E+00 0.71288E+01
   Friction thermal sca.    tstar : -0.85314E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10674E+00 0.53188E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57020E-02      34   0.55766E-03   0.41795E+01 0.12456E+03 
c  Velocity[X]                                      0.21091E+01 
c  Velocity[Y]                                      0.20703E+01 
c  Velocity[Z]                                      0.13029E-29 
c  Pressure     0.17879E-06     488   0.96890E-08   0.17829E+00 0.47300E+03 
c  nu_tilda     0.41640E-05      32   0.12506E-04   0.30299E-06 0.19593E+03 
c  TempC        0.24890E+02      29   0.48776E-03   0.11152E+02 0.36611E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7858          9.8775          4.5729          4.5729
v  Velocity[Y]            -3.7185           7.165        0.012133        0.012133
v  Velocity[Z]       -6.9287e-015     4.6801e-015     -1.371e-017     -1.371e-017
v  ǁVelocityǁ         0.0036949          9.8851           4.993           4.993
v  Pressure               -50.264          20.166         -2.3638         -2.3638
v  nu_tilda           3.8676e-007        0.004265      0.00077909      0.00077909
v  TempC                       21          73.352          21.442          21.442
v  TurbVisc           1.9872e-014       0.0050267      0.00090578      0.00090578
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              479:        0.28260E+01

===============================================================


 INSTANT    0.480000000E+03   TIME STEP NUMBER             480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73606E-02 0.88486E+00
   Friction velocity        uk    :  0.73606E-02 0.88486E+00
   Dimensionless distance   yplus :  0.59258E-01 0.71237E+01
   Friction thermal sca.    tstar : -0.92198E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44213E-01 0.53151E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57061E-02      34   0.55450E-03   0.41857E+01 0.12427E+03 
c  Velocity[X]                                      0.21314E+01 
c  Velocity[Y]                                      0.20543E+01 
c  Velocity[Z]                                      0.18729E-29 
c  Pressure     0.20164E-06     314   0.96445E-08   0.20016E+00 0.32278E+03 
c  nu_tilda     0.41664E-05      32   0.11962E-04   0.30214E-06 0.19553E+03 
c  TempC        0.24904E+02      29   0.69615E-03   0.10234E+02 0.32898E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7929          9.8787          4.5729          4.5729
v  Velocity[Y]            -3.7119          7.1228        0.012191        0.012191
v  Velocity[Z]       -6.9287e-015     4.6893e-015    -1.3713e-017    -1.3713e-017
v  ǁVelocityǁ          0.003711          9.8866          4.9937          4.9937
v  Pressure               -50.278          20.118         -2.3626         -2.3626
v  nu_tilda           3.8597e-007       0.0042651      0.00077975      0.00077975
v  TempC                       21          73.484          21.443          21.443
v  TurbVisc           1.9686e-014       0.0050267      0.00090655      0.00090655
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              480:        0.23320E+01

===============================================================


 INSTANT    0.481000000E+03   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17803E-01 0.88348E+00
   Friction velocity        uk    :  0.17803E-01 0.88348E+00
   Dimensionless distance   yplus :  0.14332E+00 0.71126E+01
   Friction thermal sca.    tstar : -0.11370E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10693E+00 0.53068E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57101E-02      34   0.56560E-03   0.41314E+01 0.12394E+03 
c  Velocity[X]                                      0.20658E+01 
c  Velocity[Y]                                      0.20657E+01 
c  Velocity[Z]                                      0.13647E-29 
c  Pressure     0.15253E-06     457   0.91867E-08   0.15176E+00 0.46895E+03 
c  nu_tilda     0.41689E-05      32   0.12457E-04   0.30128E-06 0.19513E+03 
c  TempC        0.24918E+02      30   0.54722E-03   0.11135E+02 0.35304E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7994          9.8795          4.5729          4.5729
v  Velocity[Y]            -3.7054          7.1432        0.012249        0.012249
v  Velocity[Z]       -6.9287e-015     4.6953e-015    -1.3688e-017    -1.3688e-017
v  ǁVelocityǁ         0.0036826          9.8881          4.9945          4.9945
v  Pressure               -50.386          20.179          -2.387          -2.387
v  nu_tilda           3.8525e-007       0.0042651      0.00078038      0.00078038
v  TempC                       21          73.524          21.444          21.444
v  TurbVisc           1.9525e-014       0.0050268      0.00090732      0.00090732
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              481:        0.27460E+01

===============================================================


 INSTANT    0.482000000E+03   TIME STEP NUMBER             482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17737E-01 0.88465E+00
   Friction velocity        uk    :  0.17737E-01 0.88465E+00
   Dimensionless distance   yplus :  0.14279E+00 0.71220E+01
   Friction thermal sca.    tstar : -0.13176E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10654E+00 0.53138E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57142E-02      34   0.58269E-03   0.41307E+01 0.12386E+03 
c  Velocity[X]                                      0.20710E+01 
c  Velocity[Y]                                      0.20597E+01 
c  Velocity[Z]                                      0.15262E-29 
c  Pressure     0.19199E-06     293   0.91547E-08   0.19228E+00 0.28676E+03 
c  nu_tilda     0.41713E-05      32   0.11959E-04   0.30045E-06 0.19473E+03 
c  TempC        0.24932E+02      29   0.57015E-03   0.10358E+02 0.36323E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8058          9.8816          4.5729          4.5729
v  Velocity[Y]            -3.6994          7.1216        0.012307        0.012307
v  Velocity[Z]       -6.9287e-015     4.7002e-015    -1.3685e-017    -1.3685e-017
v  ǁVelocityǁ         0.0035339          9.8891          4.9952          4.9952
v  Pressure               -50.404          20.145         -2.3868         -2.3868
v  nu_tilda           3.8463e-007       0.0042651      0.00078104      0.00078104
v  TempC                       21          73.521          21.444          21.444
v  TurbVisc            1.938e-014       0.0050268      0.00090808      0.00090808
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              482:        0.22630E+01

===============================================================


 INSTANT    0.483000000E+03   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16073E-01 0.88394E+00
   Friction velocity        uk    :  0.16073E-01 0.88394E+00
   Dimensionless distance   yplus :  0.12939E+00 0.71163E+01
   Friction thermal sca.    tstar : -0.20590E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96543E-01 0.53095E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57182E-02      34   0.59750E-03   0.41325E+01 0.12374E+03 
c  Velocity[X]                                      0.20919E+01 
c  Velocity[Y]                                      0.20406E+01 
c  Velocity[Z]                                      0.16824E-29 
c  Pressure     0.19807E-06     458   0.92882E-08   0.19558E+00 0.40640E+03 
c  nu_tilda     0.41737E-05      32   0.12440E-04   0.29960E-06 0.19433E+03 
c  TempC        0.24945E+02      29   0.41523E-03   0.10713E+02 0.34997E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8117          9.8833          4.5729          4.5729
v  Velocity[Y]            -3.6934           7.149        0.012365        0.012365
v  Velocity[Z]       -6.9287e-015     4.7056e-015    -1.3635e-017    -1.3635e-017
v  ǁVelocityǁ         0.0030478          9.8901          4.9959          4.9959
v  Pressure               -50.504           20.18         -2.4145         -2.4145
v  nu_tilda           3.8403e-007       0.0042652      0.00078167      0.00078167
v  TempC                       21          73.605          21.445          21.445
v  TurbVisc           1.9254e-014       0.0050269      0.00090885      0.00090885
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              483:        0.27430E+01

===============================================================


 INSTANT    0.484000000E+03   TIME STEP NUMBER             484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50626E-02 0.88514E+00
   Friction velocity        uk    :  0.50626E-02 0.88514E+00
   Dimensionless distance   yplus :  0.40757E-01 0.71259E+01
   Friction thermal sca.    tstar : -0.69142E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30409E-01 0.53168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57222E-02      34   0.56167E-03   0.41407E+01 0.12365E+03 
c  Velocity[X]                                      0.20887E+01 
c  Velocity[Y]                                      0.20520E+01 
c  Velocity[Z]                                      0.17052E-29 
c  Pressure     0.19867E-06     329   0.94446E-08   0.19341E+00 0.28276E+03 
c  nu_tilda     0.41762E-05      32   0.11966E-04   0.29874E-06 0.19393E+03 
c  TempC        0.24959E+02      29   0.50614E-03   0.96749E+01 0.33221E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8175          9.8849          4.5729          4.5729
v  Velocity[Y]            -3.6877          7.1149        0.012422        0.012422
v  Velocity[Z]       -6.9287e-015     4.7101e-015    -1.3622e-017    -1.3622e-017
v  ǁVelocityǁ         0.0029382          9.8918          4.9967          4.9967
v  Pressure               -50.525          20.147         -2.4158         -2.4158
v  nu_tilda           3.8348e-007       0.0042652      0.00078234      0.00078234
v  TempC                       21          73.642          21.446          21.446
v  TurbVisc           1.9134e-014       0.0050269      0.00090962      0.00090962
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              484:        0.23440E+01

===============================================================


 INSTANT    0.485000000E+03   TIME STEP NUMBER             485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16626E-01 0.88432E+00
   Friction velocity        uk    :  0.16626E-01 0.88432E+00
   Dimensionless distance   yplus :  0.13385E+00 0.71194E+01
   Friction thermal sca.    tstar : -0.17520E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99868E-01 0.53118E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57263E-02      34   0.48536E-03   0.40745E+01 0.12296E+03 
c  Velocity[X]                                      0.20539E+01 
c  Velocity[Y]                                      0.20206E+01 
c  Velocity[Z]                                      0.20593E-29 
c  Pressure     0.22965E-06     357   0.89956E-08   0.22714E+00 0.60922E+03 
c  nu_tilda     0.41786E-05      32   0.12408E-04   0.29789E-06 0.19353E+03 
c  TempC        0.24973E+02      29   0.97110E-03   0.10709E+02 0.34820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8242          9.8861          4.5729          4.5729
v  Velocity[Y]            -3.6821          7.1417         0.01248         0.01248
v  Velocity[Z]       -1.0971e-014     4.7201e-015    -1.3637e-017    -1.3637e-017
v  ǁVelocityǁ         0.0024416          9.8937          4.9974          4.9974
v  Pressure               -50.608          20.232         -2.4232         -2.4232
v  nu_tilda           3.8294e-007       0.0042652      0.00078296      0.00078296
v  TempC                       21          73.626          21.446          21.446
v  TurbVisc           1.9025e-014        0.005027      0.00091039      0.00091039
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              485:        0.24290E+01

===============================================================


 INSTANT    0.486000000E+03   TIME STEP NUMBER             486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13029E-01 0.88548E+00
   Friction velocity        uk    :  0.13029E-01 0.88548E+00
   Dimensionless distance   yplus :  0.10489E+00 0.71287E+01
   Friction thermal sca.    tstar : -0.18912E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78262E-01 0.53188E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57303E-02      34   0.61070E-03   0.40378E+01 0.12269E+03 
c  Velocity[X]                                      0.20315E+01 
c  Velocity[Y]                                      0.20063E+01 
c  Velocity[Z]                                      0.29044E-29 
c  Pressure     0.18407E-06     362   0.99899E-08   0.18154E+00 0.23846E+03 
c  nu_tilda     0.41810E-05      32   0.11963E-04   0.29704E-06 0.19313E+03 
c  TempC        0.24987E+02      29   0.47652E-03   0.15252E+02 0.41811E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8309           9.887          4.5729          4.5729
v  Velocity[Y]            -3.6771          7.1475        0.012537        0.012537
v  Velocity[Z]       -6.9287e-015     4.7223e-015     -1.358e-017     -1.358e-017
v  ǁVelocityǁ         0.0020255          9.8949          4.9981          4.9981
v  Pressure               -50.641          20.251         -2.4209         -2.4209
v  nu_tilda           3.8249e-007       0.0042653      0.00078363      0.00078363
v  TempC                       21          73.682          21.447          21.447
v  TurbVisc           1.8919e-014        0.005027      0.00091116      0.00091116
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              486:        0.24510E+01

===============================================================


 INSTANT    0.487000000E+03   TIME STEP NUMBER             487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79339E-02 0.88487E+00
   Friction velocity        uk    :  0.79339E-02 0.88487E+00
   Dimensionless distance   yplus :  0.63873E-01 0.71238E+01
   Friction thermal sca.    tstar : -0.11053E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47657E-01 0.53152E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57343E-02      34   0.55477E-03   0.40857E+01 0.12296E+03 
c  Velocity[X]                                      0.20709E+01 
c  Velocity[Y]                                      0.20148E+01 
c  Velocity[Z]                                      0.17551E-29 
c  Pressure     0.18948E-06     473   0.98375E-08   0.18976E+00 0.62546E+03 
c  nu_tilda     0.41834E-05      32   0.12370E-04   0.29618E-06 0.19274E+03 
c  TempC        0.25001E+02      29   0.41083E-03   0.92243E+01 0.34087E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8374          9.8877          4.5729          4.5729
v  Velocity[Y]            -3.6724           7.123        0.012595        0.012595
v  Velocity[Z]       -7.7025e-015     4.7307e-015    -1.3584e-017    -1.3584e-017
v  ǁVelocityǁ         0.0020935          9.8964          4.9989          4.9989
v  Pressure               -50.722          20.151         -2.4689         -2.4689
v  nu_tilda           3.8221e-007       0.0042653      0.00078425      0.00078425
v  TempC                       21          73.691          21.448          21.448
v  TurbVisc           1.8829e-014        0.005027      0.00091193      0.00091193
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              487:        0.28730E+01

===============================================================


 INSTANT    0.488000000E+03   TIME STEP NUMBER             488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65723E-02 0.88343E+00
   Friction velocity        uk    :  0.65723E-02 0.88343E+00
   Dimensionless distance   yplus :  0.52912E-01 0.71122E+01
   Friction thermal sca.    tstar : -0.90404E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39478E-01 0.53065E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57384E-02      34   0.52907E-03   0.40339E+01 0.12240E+03 
c  Velocity[X]                                      0.20414E+01 
c  Velocity[Y]                                      0.19925E+01 
c  Velocity[Z]                                      0.22328E-29 
c  Pressure     0.21501E-06     472   0.97228E-08   0.20662E+00 0.57676E+03 
c  nu_tilda     0.41858E-05      32   0.11977E-04   0.29535E-06 0.19234E+03 
c  TempC        0.25015E+02      29   0.46663E-03   0.85988E+01 0.32042E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8439          9.8882          4.5729          4.5729
v  Velocity[Y]            -3.6681          7.1336        0.012652        0.012652
v  Velocity[Z]       -1.4136e-014     4.7366e-015    -1.3615e-017    -1.3615e-017
v  ǁVelocityǁ         0.0021747           9.897          4.9996          4.9996
v  Pressure               -50.739          20.242         -2.4458         -2.4458
v  nu_tilda           3.8197e-007       0.0042653      0.00078492      0.00078492
v  TempC                       21           73.69          21.448          21.448
v  TurbVisc           1.8776e-014       0.0050271      0.00091269      0.00091269
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              488:        0.29320E+01

===============================================================


 INSTANT    0.489000000E+03   TIME STEP NUMBER             489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62905E-02 0.88455E+00
   Friction velocity        uk    :  0.62905E-02 0.88455E+00
   Dimensionless distance   yplus :  0.50643E-01 0.71212E+01
   Friction thermal sca.    tstar : -0.83286E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37785E-01 0.53132E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57424E-02      34   0.58920E-03   0.40012E+01 0.12209E+03 
c  Velocity[X]                                      0.20154E+01 
c  Velocity[Y]                                      0.19857E+01 
c  Velocity[Z]                                      0.12940E-29 
c  Pressure     0.16370E-06     521   0.97498E-08   0.16342E+00 0.66741E+03 
c  nu_tilda     0.41882E-05      32   0.12334E-04   0.29449E-06 0.19195E+03 
c  TempC        0.25029E+02      29   0.47435E-03   0.94198E+01 0.32655E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8499          9.8882          4.5729          4.5729
v  Velocity[Y]             -3.664          7.1151         0.01271         0.01271
v  Velocity[Z]       -1.1937e-014     4.7424e-015    -1.3608e-017    -1.3608e-017
v  ǁVelocityǁ          0.002354          9.8979          5.0003          5.0003
v  Pressure               -50.831          20.153         -2.4995         -2.4995
v  nu_tilda           3.8176e-007       0.0042654      0.00078554      0.00078554
v  TempC                       21           73.19          21.449          21.449
v  TurbVisc           1.8727e-014       0.0050271      0.00091346      0.00091346
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              489:        0.30100E+01

===============================================================


 INSTANT    0.490000000E+03   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92317E-02 0.88355E+00
   Friction velocity        uk    :  0.92317E-02 0.88355E+00
   Dimensionless distance   yplus :  0.74322E-01 0.71132E+01
   Friction thermal sca.    tstar : -0.74787E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55452E-01 0.53072E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57465E-02      34   0.60341E-03   0.40033E+01 0.12208E+03 
c  Velocity[X]                                      0.20144E+01 
c  Velocity[Y]                                      0.19890E+01 
c  Velocity[Z]                                      0.17882E-29 
c  Pressure     0.18614E-06     504   0.92620E-08   0.18293E+00 0.75893E+03 
c  nu_tilda     0.41906E-05      32   0.11972E-04   0.29365E-06 0.19156E+03 
c  TempC        0.25042E+02      29   0.80245E-03   0.96896E+01 0.34670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.856          9.8881          4.5729          4.5729
v  Velocity[Y]            -3.6604          7.1337        0.012768        0.012768
v  Velocity[Z]       -1.7274e-014     4.7494e-015    -1.3656e-017    -1.3656e-017
v  ǁVelocityǁ         0.0028031          9.8981           5.001           5.001
v  Pressure               -50.846          20.273         -2.4674         -2.4674
v  nu_tilda           3.8151e-007       0.0042654      0.00078621      0.00078621
v  TempC                       21          73.245           21.45           21.45
v  TurbVisc           1.8686e-014       0.0050272      0.00091423      0.00091423
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              490:        0.33180E+01

===============================================================


 INSTANT    0.491000000E+03   TIME STEP NUMBER             491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13328E-01 0.88462E+00
   Friction velocity        uk    :  0.13328E-01 0.88462E+00
   Dimensionless distance   yplus :  0.10730E+00 0.71218E+01
   Friction thermal sca.    tstar : -0.70357E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80056E-01 0.53136E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57505E-02      34   0.53538E-03   0.39833E+01 0.12187E+03 
c  Velocity[X]                                      0.20013E+01 
c  Velocity[Y]                                      0.19820E+01 
c  Velocity[Z]                                      0.14661E-29 
c  Pressure     0.20563E-06     489   0.96417E-08   0.20172E+00 0.39471E+03 
c  nu_tilda     0.41930E-05      32   0.12294E-04   0.29280E-06 0.19116E+03 
c  TempC        0.25056E+02      29   0.54502E-03   0.18345E+02 0.46714E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8633          9.8876          4.5729          4.5729
v  Velocity[Y]            -3.6575          7.1378        0.012827        0.012827
v  Velocity[Z]        -1.956e-014     4.7563e-015    -1.3706e-017    -1.3706e-017
v  ǁVelocityǁ         0.0013643          9.8985          5.0018          5.0018
v  Pressure               -50.926           20.25         -2.5031         -2.5031
v  nu_tilda           3.8128e-007       0.0042654      0.00078684      0.00078684
v  TempC                       21          73.323           21.45           21.45
v  TurbVisc           1.8638e-014       0.0050272        0.000915        0.000915
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              491:        0.27880E+01

===============================================================


 INSTANT    0.492000000E+03   TIME STEP NUMBER             492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15260E-01 0.88399E+00
   Friction velocity        uk    :  0.15260E-01 0.88399E+00
   Dimensionless distance   yplus :  0.12286E+00 0.71167E+01
   Friction thermal sca.    tstar : -0.66321E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91664E-01 0.53099E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57546E-02      34   0.56810E-03   0.39579E+01 0.12151E+03 
c  Velocity[X]                                      0.19974E+01 
c  Velocity[Y]                                      0.19605E+01 
c  Velocity[Z]                                      0.23201E-29 
c  Pressure     0.18778E-06     456   0.93783E-08   0.18760E+00 0.45291E+03 
c  nu_tilda     0.41954E-05      32   0.11981E-04   0.29197E-06 0.19077E+03 
c  TempC        0.25070E+02      29   0.42529E-03   0.11313E+02 0.36856E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8698          9.8873          4.5729          4.5729
v  Velocity[Y]            -3.6549          7.1118        0.012884        0.012884
v  Velocity[Z]       -1.2852e-014     4.7584e-015    -1.3702e-017    -1.3702e-017
v  ǁVelocityǁ         0.0027473          9.8981          5.0025          5.0025
v  Pressure                -50.95          20.178         -2.5192         -2.5192
v  nu_tilda           3.8112e-007       0.0042655       0.0007875       0.0007875
v  TempC                       21          73.482          21.451          21.451
v  TurbVisc           1.8593e-014       0.0050272      0.00091576      0.00091576
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              492:        0.29650E+01

===============================================================


 INSTANT    0.493000000E+03   TIME STEP NUMBER             493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15066E-01 0.88270E+00
   Friction velocity        uk    :  0.15066E-01 0.88270E+00
   Dimensionless distance   yplus :  0.12129E+00 0.71063E+01
   Friction thermal sca.    tstar : -0.61618E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90497E-01 0.53021E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57586E-02      34   0.58403E-03   0.39595E+01 0.12141E+03 
c  Velocity[X]                                      0.19983E+01 
c  Velocity[Y]                                      0.19611E+01 
c  Velocity[Z]                                      0.17910E-29 
c  Pressure     0.18205E-06     456   0.99617E-08   0.17639E+00 0.38757E+03 
c  nu_tilda     0.41978E-05      32   0.12262E-04   0.29110E-06 0.19038E+03 
c  TempC        0.25084E+02      29   0.81906E-03   0.93583E+01 0.34244E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8761          9.8864          4.5729          4.5729
v  Velocity[Y]            -3.6531          7.1279        0.012943        0.012943
v  Velocity[Z]       -1.7811e-014     4.7659e-015     -1.379e-017     -1.379e-017
v  ǁVelocityǁ         0.0028369          9.8977          5.0032          5.0032
v  Pressure               -51.034           20.21         -2.5446         -2.5446
v  nu_tilda           3.8095e-007       0.0042655      0.00078813      0.00078813
v  TempC                       21          73.505          21.452          21.452
v  TurbVisc           1.8561e-014       0.0050273      0.00091653      0.00091653
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              493:        0.28260E+01

===============================================================


 INSTANT    0.494000000E+03   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16311E-01 0.88395E+00
   Friction velocity        uk    :  0.16311E-01 0.88395E+00
   Dimensionless distance   yplus :  0.13132E+00 0.71164E+01
   Friction thermal sca.    tstar : -0.75299E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97976E-01 0.53096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57626E-02      34   0.52738E-03   0.39451E+01 0.12126E+03 
c  Velocity[X]                                      0.20024E+01 
c  Velocity[Y]                                      0.19427E+01 
c  Velocity[Z]                                      0.14982E-29 
c  Pressure     0.18201E-06     264   0.93977E-08   0.18175E+00 0.26571E+03 
c  nu_tilda     0.42002E-05      32   0.11980E-04   0.29025E-06 0.18999E+03 
c  TempC        0.25097E+02      29   0.53936E-03   0.16642E+02 0.45856E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8822          9.8852          4.5729          4.5729
v  Velocity[Y]            -3.6522          7.1085           0.013           0.013
v  Velocity[Z]       -1.9348e-014     4.7706e-015    -1.3865e-017    -1.3865e-017
v  ǁVelocityǁ         0.0031835          9.8973          5.0039          5.0039
v  Pressure                -51.04          20.182         -2.5453         -2.5453
v  nu_tilda           3.8078e-007       0.0042655      0.00078879      0.00078879
v  TempC                       21          73.095          21.452          21.452
v  TurbVisc           1.8529e-014       0.0050273       0.0009173       0.0009173
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              494:        0.22720E+01

===============================================================


 INSTANT    0.495000000E+03   TIME STEP NUMBER             495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16259E-01 0.88328E+00
   Friction velocity        uk    :  0.16259E-01 0.88328E+00
   Dimensionless distance   yplus :  0.13090E+00 0.71110E+01
   Friction thermal sca.    tstar : -0.16085E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97665E-01 0.53056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57667E-02      34   0.56763E-03   0.38928E+01 0.12074E+03 
c  Velocity[X]                                      0.19678E+01 
c  Velocity[Y]                                      0.19249E+01 
c  Velocity[Z]                                      0.14613E-29 
c  Pressure     0.18391E-06     440   0.97453E-08   0.18090E+00 0.51155E+03 
c  nu_tilda     0.42026E-05      32   0.12226E-04   0.28939E-06 0.18959E+03 
c  TempC        0.25111E+02      29   0.34413E-03   0.10040E+02 0.35324E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8884          9.8846          4.5729          4.5729
v  Velocity[Y]            -3.6525          7.1317        0.013059        0.013059
v  Velocity[Z]       -1.7871e-014     4.7784e-015    -1.3921e-017    -1.3921e-017
v  ǁVelocityǁ         0.0023975          9.8964          5.0046          5.0046
v  Pressure               -51.118          20.256         -2.5598         -2.5598
v  nu_tilda           3.8059e-007       0.0042656      0.00078942      0.00078942
v  TempC                       21          73.097          21.453          21.453
v  TurbVisc           1.8496e-014       0.0050274      0.00091807      0.00091807
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              495:        0.26940E+01

===============================================================


 INSTANT    0.496000000E+03   TIME STEP NUMBER             496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17783E-01 0.88424E+00
   Friction velocity        uk    :  0.17783E-01 0.88424E+00
   Dimensionless distance   yplus :  0.14316E+00 0.71187E+01
   Friction thermal sca.    tstar : -0.16939E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10681E+00 0.53114E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57707E-02      34   0.57083E-03   0.39195E+01 0.12077E+03 
c  Velocity[X]                                      0.19839E+01 
c  Velocity[Y]                                      0.19356E+01 
c  Velocity[Z]                                      0.14889E-29 
c  Pressure     0.20339E-06     389   0.98082E-08   0.20233E+00 0.32983E+03 
c  nu_tilda     0.42050E-05      32   0.11982E-04   0.28856E-06 0.18921E+03 
c  TempC        0.25125E+02      29   0.51453E-03   0.89073E+01 0.32447E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8944          9.8842          4.5729          4.5729
v  Velocity[Y]             -3.657          7.0972        0.013116        0.013116
v  Velocity[Z]       -1.6225e-014      4.782e-015    -1.3989e-017    -1.3989e-017
v  ǁVelocityǁ         0.0035063          9.8956          5.0053          5.0053
v  Pressure               -51.123          20.205         -2.5649         -2.5649
v  nu_tilda           3.8043e-007       0.0042656      0.00079008      0.00079008
v  TempC                       21          73.099          21.454          21.454
v  TurbVisc           1.8458e-014       0.0050274      0.00091883      0.00091883
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              496:        0.21120E+01

===============================================================


 INSTANT    0.497000000E+03   TIME STEP NUMBER             497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17836E-01 0.88337E+00
   Friction velocity        uk    :  0.17836E-01 0.88337E+00
   Dimensionless distance   yplus :  0.14359E+00 0.71117E+01
   Friction thermal sca.    tstar : -0.12870E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10714E+00 0.53061E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57748E-02      34   0.49327E-03   0.38897E+01 0.12052E+03 
c  Velocity[X]                                      0.19627E+01 
c  Velocity[Y]                                      0.19271E+01 
c  Velocity[Z]                                      0.12796E-29 
c  Pressure     0.15967E-06     457   0.92399E-08   0.15789E+00 0.42108E+03 
c  nu_tilda     0.42073E-05      32   0.12189E-04   0.28771E-06 0.18882E+03 
c  TempC        0.25138E+02      29   0.51444E-03   0.92407E+01 0.33692E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9013          9.8837          4.5729          4.5729
v  Velocity[Y]            -3.6662          7.1243        0.013175        0.013175
v  Velocity[Z]       -1.6823e-014     4.7871e-015    -1.4064e-017    -1.4064e-017
v  ǁVelocityǁ         0.0036485          9.8944           5.006           5.006
v  Pressure               -51.205          20.257         -2.5876         -2.5876
v  nu_tilda           3.8029e-007       0.0042656      0.00079071      0.00079071
v  TempC                       21          73.451          21.454          21.454
v  TurbVisc           1.8427e-014       0.0050274       0.0009196       0.0009196
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              497:        0.22370E+01

===============================================================


 INSTANT    0.498000000E+03   TIME STEP NUMBER             498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17798E-01 0.88469E+00
   Friction velocity        uk    :  0.17798E-01 0.88469E+00
   Dimensionless distance   yplus :  0.14329E+00 0.71223E+01
   Friction thermal sca.    tstar : -0.81531E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10691E+00 0.53141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57788E-02      33   0.60265E-03   0.38852E+01 0.12041E+03 
c  Velocity[X]                                      0.19809E+01 
c  Velocity[Y]                                      0.19043E+01 
c  Velocity[Z]                                      0.12133E-29 
c  Pressure     0.17184E-06     422   0.92698E-08   0.17109E+00 0.28636E+03 
c  nu_tilda     0.42097E-05      32   0.11985E-04   0.28689E-06 0.18843E+03 
c  TempC        0.25152E+02      29   0.59538E-03   0.98051E+01 0.34782E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.908          9.8828          4.5729          4.5729
v  Velocity[Y]            -3.6759          7.1336        0.013232        0.013232
v  Velocity[Z]       -1.6925e-014     4.8051e-015    -1.4134e-017    -1.4134e-017
v  ǁVelocityǁ         0.0036559          9.8934          5.0068          5.0068
v  Pressure               -51.214          20.282         -2.5789         -2.5789
v  nu_tilda            3.802e-007       0.0042657      0.00079137      0.00079137
v  TempC                       21          73.103          21.455          21.455
v  TurbVisc           1.8399e-014       0.0050275      0.00092037      0.00092037
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              498:        0.27420E+01

===============================================================


 INSTANT    0.499000000E+03   TIME STEP NUMBER             499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11869E-01 0.88424E+00
   Friction velocity        uk    :  0.11869E-01 0.88424E+00
   Dimensionless distance   yplus :  0.95552E-01 0.71187E+01
   Friction thermal sca.    tstar : -0.61609E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71292E-01 0.53114E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57829E-02      33   0.53971E-03   0.39033E+01 0.12046E+03 
c  Velocity[X]                                      0.19888E+01 
c  Velocity[Y]                                      0.19145E+01 
c  Velocity[Z]                                      0.11764E-29 
c  Pressure     0.17848E-06     488   0.96686E-08   0.17882E+00 0.57800E+03 
c  nu_tilda     0.42120E-05      32   0.12158E-04   0.28604E-06 0.18805E+03 
c  TempC        0.25166E+02      29   0.11541E-02   0.10723E+02 0.35514E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9146          9.8817          4.5729          4.5729
v  Velocity[Y]            -3.6861          7.1097        0.013291        0.013291
v  Velocity[Z]       -1.6804e-014     4.8193e-015    -1.4212e-017    -1.4212e-017
v  ǁVelocityǁ         0.0032934          9.8929          5.0075          5.0075
v  Pressure               -51.281          20.194         -2.6246         -2.6246
v  nu_tilda           3.8025e-007       0.0042657        0.000792        0.000792
v  TempC                       21          73.105          21.455          21.455
v  TurbVisc           1.8383e-014       0.0050275      0.00092114      0.00092114
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              499:        0.29760E+01

===============================================================


 INSTANT    0.500000000E+03   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17927E-01 0.88283E+00
   Friction velocity        uk    :  0.17927E-01 0.88283E+00
   Dimensionless distance   yplus :  0.14433E+00 0.71074E+01
   Friction thermal sca.    tstar : -0.54537E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10768E+00 0.53029E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57869E-02      33   0.52943E-03   0.38677E+01 0.11994E+03 
c  Velocity[X]                                      0.19784E+01 
c  Velocity[Y]                                      0.18893E+01 
c  Velocity[Z]                                      0.15088E-29 
c  Pressure     0.16588E-06     425   0.90651E-08   0.16105E+00 0.41253E+03 
c  nu_tilda     0.42144E-05      32   0.12002E-04   0.28522E-06 0.18766E+03 
c  TempC        0.25179E+02      30   0.48892E-03   0.19956E+02 0.46305E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9207          9.8804          4.5729          4.5729
v  Velocity[Y]            -3.6964          7.1225        0.013348        0.013348
v  Velocity[Z]       -1.4275e-014     4.8238e-015    -1.4267e-017    -1.4267e-017
v  ǁVelocityǁ         0.0034356          9.8922          5.0081          5.0081
v  Pressure               -51.295          20.265          -2.611          -2.611
v  nu_tilda            3.803e-007       0.0042657      0.00079266      0.00079266
v  TempC                       21          73.238          21.456          21.456
v  TurbVisc           1.8392e-014       0.0050275      0.00092191      0.00092191
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              500:        0.30510E+01

===============================================================


 INSTANT    0.501000000E+03   TIME STEP NUMBER             501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17859E-01 0.88385E+00
   Friction velocity        uk    :  0.17859E-01 0.88385E+00
   Dimensionless distance   yplus :  0.14378E+00 0.71156E+01
   Friction thermal sca.    tstar : -0.48400E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10727E+00 0.53090E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57910E-02      33   0.55516E-03   0.38704E+01 0.11987E+03 
c  Velocity[X]                                      0.19915E+01 
c  Velocity[Y]                                      0.18789E+01 
c  Velocity[Z]                                      0.12887E-29 
c  Pressure     0.15730E-06     485   0.95626E-08   0.15748E+00 0.63337E+03 
c  nu_tilda     0.42167E-05      32   0.12138E-04   0.28436E-06 0.18728E+03 
c  TempC        0.25193E+02      29   0.57912E-03   0.10124E+02 0.33766E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9268          9.8791          4.5729          4.5729
v  Velocity[Y]            -3.7067          7.1024        0.013407        0.013407
v  Velocity[Z]       -1.5497e-014     4.8291e-015    -1.4348e-017    -1.4348e-017
v  ǁVelocityǁ         0.0030723          9.8912          5.0088          5.0088
v  Pressure               -51.365           20.17         -2.6609         -2.6609
v  nu_tilda           3.8038e-007       0.0042657      0.00079329      0.00079329
v  TempC                       21          73.587          21.457          21.457
v  TurbVisc           1.8402e-014       0.0050276      0.00092268      0.00092268
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              501:        0.47910E+01

===============================================================


 INSTANT    0.502000000E+03   TIME STEP NUMBER             502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17299E-01 0.88290E+00
   Friction velocity        uk    :  0.17299E-01 0.88290E+00
   Dimensionless distance   yplus :  0.13927E+00 0.71080E+01
   Friction thermal sca.    tstar : -0.58556E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10391E+00 0.53033E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57950E-02      33   0.53874E-03   0.38420E+01 0.11966E+03 
c  Velocity[X]                                      0.19538E+01 
c  Velocity[Y]                                      0.18882E+01 
c  Velocity[Z]                                      0.10862E-29 
c  Pressure     0.15393E-06     485   0.98867E-08   0.15226E+00 0.70883E+03 
c  nu_tilda     0.42191E-05      32   0.12002E-04   0.28354E-06 0.18690E+03 
c  TempC        0.25207E+02      29   0.45097E-03   0.10296E+02 0.34562E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9327          9.8773          4.5729          4.5729
v  Velocity[Y]             -3.717          7.1221        0.013464        0.013464
v  Velocity[Z]       -1.5321e-014     4.8311e-015    -1.4413e-017    -1.4413e-017
v  ǁVelocityǁ         0.0034149          9.8902          5.0095          5.0095
v  Pressure               -51.373          20.298          -2.633          -2.633
v  nu_tilda           3.8043e-007       0.0042658      0.00079395      0.00079395
v  TempC                       21          73.109          21.457          21.457
v  TurbVisc           1.8417e-014       0.0050276      0.00092344      0.00092344
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              502:        0.31560E+01

===============================================================


 INSTANT    0.503000000E+03   TIME STEP NUMBER             503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76741E-02 0.88392E+00
   Friction velocity        uk    :  0.76741E-02 0.88392E+00
   Dimensionless distance   yplus :  0.61782E-01 0.71161E+01
   Friction thermal sca.    tstar : -0.95746E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46096E-01 0.53094E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57990E-02      33   0.55066E-03   0.38184E+01 0.11935E+03 
c  Velocity[X]                                      0.19400E+01 
c  Velocity[Y]                                      0.18784E+01 
c  Velocity[Z]                                      0.10682E-29 
c  Pressure     0.15884E-06     473   0.94159E-08   0.15761E+00 0.48523E+03 
c  nu_tilda     0.42214E-05      32   0.12089E-04   0.28269E-06 0.18651E+03 
c  TempC        0.25220E+02      29   0.49291E-03   0.10184E+02 0.33583E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9394          9.8757          4.5729          4.5729
v  Velocity[Y]            -3.7272          7.1221        0.013523        0.013523
v  Velocity[Z]        -1.521e-014     4.8344e-015    -1.4482e-017    -1.4482e-017
v  ǁVelocityǁ         0.0033803          9.8887          5.0102          5.0102
v  Pressure               -51.443          20.244         -2.6759         -2.6759
v  nu_tilda           3.8049e-007       0.0042658      0.00079458      0.00079458
v  TempC                       21           73.11          21.458          21.458
v  TurbVisc           1.8428e-014       0.0050276      0.00092421      0.00092421
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              503:        0.36130E+01

===============================================================


 INSTANT    0.504000000E+03   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16843E-01 0.88326E+00
   Friction velocity        uk    :  0.16843E-01 0.88326E+00
   Dimensionless distance   yplus :  0.13560E+00 0.71108E+01
   Friction thermal sca.    tstar : -0.97496E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10117E+00 0.53055E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58031E-02      33   0.59145E-03   0.38197E+01 0.11928E+03 
c  Velocity[X]                                      0.19630E+01 
c  Velocity[Y]                                      0.18566E+01 
c  Velocity[Z]                                      0.11847E-29 
c  Pressure     0.14572E-06     410   0.97200E-08   0.14746E+00 0.34666E+03 
c  nu_tilda     0.42238E-05      32   0.12011E-04   0.28188E-06 0.18613E+03 
c  TempC        0.25234E+02      29   0.51548E-03   0.87422E+01 0.32650E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9456          9.8735          4.5729          4.5729
v  Velocity[Y]            -3.7376          7.0976         0.01358         0.01358
v  Velocity[Z]       -1.4844e-014     4.8353e-015    -1.4536e-017    -1.4536e-017
v  ǁVelocityǁ         0.0030377           9.887          5.0109          5.0109
v  Pressure               -51.445          20.189         -2.6838         -2.6838
v  nu_tilda           3.8062e-007       0.0042658      0.00079524      0.00079524
v  TempC                       21          73.154          21.459          21.459
v  TurbVisc           1.8439e-014       0.0050277      0.00092498      0.00092498
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              504:        0.33690E+01

===============================================================


 INSTANT    0.505000000E+03   TIME STEP NUMBER             505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14781E-01 0.88232E+00
   Friction velocity        uk    :  0.14781E-01 0.88232E+00
   Dimensionless distance   yplus :  0.11900E+00 0.71032E+01
   Friction thermal sca.    tstar : -0.85633E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88787E-01 0.52998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58071E-02      33   0.53723E-03   0.38402E+01 0.11942E+03 
c  Velocity[X]                                      0.19812E+01 
c  Velocity[Y]                                      0.18590E+01 
c  Velocity[Z]                                      0.13995E-29 
c  Pressure     0.19352E-06     454   0.90623E-08   0.19191E+00 0.41568E+03 
c  nu_tilda     0.42261E-05      32   0.12050E-04   0.28104E-06 0.18575E+03 
c  TempC        0.25247E+02      29   0.49437E-03   0.89163E+01 0.32619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9516          9.8712          4.5729          4.5729
v  Velocity[Y]            -3.7478          7.1193        0.013639        0.013639
v  Velocity[Z]       -1.4686e-014     4.8385e-015     -1.459e-017     -1.459e-017
v  ǁVelocityǁ         0.0031056          9.8854          5.0116          5.0116
v  Pressure               -51.517          20.239          -2.705          -2.705
v  nu_tilda           3.8077e-007       0.0042659      0.00079587      0.00079587
v  TempC                       21          73.545          21.459          21.459
v  TurbVisc           1.8465e-014       0.0050277      0.00092575      0.00092575
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              505:        0.29790E+01

===============================================================


 INSTANT    0.506000000E+03   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12048E-01 0.88346E+00
   Friction velocity        uk    :  0.12048E-01 0.88346E+00
   Dimensionless distance   yplus :  0.96993E-01 0.71125E+01
   Friction thermal sca.    tstar : -0.14868E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72367E-01 0.53067E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58112E-02      33   0.50760E-03   0.37805E+01 0.11882E+03 
c  Velocity[X]                                      0.19408E+01 
c  Velocity[Y]                                      0.18397E+01 
c  Velocity[Z]                                      0.14123E-29 
c  Pressure     0.17691E-06     265   0.96371E-08   0.17782E+00 0.25017E+03 
c  nu_tilda     0.42284E-05      32   0.12014E-04   0.28023E-06 0.18538E+03 
c  TempC        0.25261E+02      29   0.46324E-03   0.99223E+01 0.33290E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9574          9.8687          4.5729          4.5729
v  Velocity[Y]             -3.758          7.0978        0.013696        0.013696
v  Velocity[Z]        -1.412e-014     4.8381e-015    -1.4638e-017    -1.4638e-017
v  ǁVelocityǁ         0.0028975          9.8834          5.0123          5.0123
v  Pressure               -51.514          20.219         -2.7053         -2.7053
v  nu_tilda           3.8097e-007       0.0042659      0.00079653      0.00079653
v  TempC                       21          73.119           21.46           21.46
v  TurbVisc           1.8494e-014       0.0050277      0.00092651      0.00092651
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              506:        0.26410E+01

===============================================================


 INSTANT    0.507000000E+03   TIME STEP NUMBER             507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29831E-02 0.88260E+00
   Friction velocity        uk    :  0.29831E-02 0.88260E+00
   Dimensionless distance   yplus :  0.24016E-01 0.71055E+01
   Friction thermal sca.    tstar : -0.13972E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17919E-01 0.53015E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58152E-02      33   0.59255E-03   0.37533E+01 0.11853E+03 
c  Velocity[X]                                      0.19283E+01 
c  Velocity[Y]                                      0.18250E+01 
c  Velocity[Z]                                      0.13198E-29 
c  Pressure     0.18080E-06     458   0.96620E-08   0.17659E+00 0.36261E+03 
c  nu_tilda     0.42307E-05      32   0.12018E-04   0.27939E-06 0.18500E+03 
c  TempC        0.25274E+02      29   0.80662E-03   0.84748E+01 0.32218E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9628           9.866          4.5729          4.5729
v  Velocity[Y]            -3.7681          7.1188        0.013754        0.013754
v  Velocity[Z]       -1.3546e-014     4.8383e-015    -1.4675e-017    -1.4675e-017
v  ǁVelocityǁ         0.0028985          9.8814          5.0129          5.0129
v  Pressure               -51.584          20.215         -2.7385         -2.7385
v  nu_tilda           3.8115e-007       0.0042659      0.00079716      0.00079716
v  TempC                       21          73.122          21.461          21.461
v  TurbVisc           1.8533e-014       0.0050278      0.00092728      0.00092728
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              507:        0.34130E+01

===============================================================


 INSTANT    0.508000000E+03   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11649E-02 0.88403E+00
   Friction velocity        uk    :  0.11649E-02 0.88403E+00
   Dimensionless distance   yplus :  0.93779E-02 0.71171E+01
   Friction thermal sca.    tstar : -0.84733E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69970E-02 0.53101E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58193E-02      33   0.57655E-03   0.37944E+01 0.11881E+03 
c  Velocity[X]                                      0.19626E+01 
c  Velocity[Y]                                      0.18319E+01 
c  Velocity[Z]                                      0.12113E-29 
c  Pressure     0.20295E-06     377   0.97544E-08   0.20448E+00 0.24749E+03 
c  nu_tilda     0.42331E-05      32   0.12020E-04   0.27858E-06 0.18463E+03 
c  TempC        0.25288E+02      29   0.54176E-03   0.16985E+02 0.44951E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9682          9.8635          4.5729          4.5729
v  Velocity[Y]            -3.7778          7.0945        0.013811        0.013811
v  Velocity[Z]       -1.3643e-014     4.8372e-015    -1.4702e-017    -1.4702e-017
v  ǁVelocityǁ         0.0028455          9.8791          5.0136          5.0136
v  Pressure               -51.576          20.218         -2.7327         -2.7327
v  nu_tilda           3.8141e-007        0.004266      0.00079782      0.00079782
v  TempC                       21          73.124          21.461          21.461
v  TurbVisc           1.8568e-014       0.0050278      0.00092805      0.00092805
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              508:        0.27790E+01

===============================================================


 INSTANT    0.509000000E+03   TIME STEP NUMBER             509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82798E-02 0.88323E+00
   Friction velocity        uk    :  0.82798E-02 0.88323E+00
   Dimensionless distance   yplus :  0.66658E-01 0.71106E+01
   Friction thermal sca.    tstar : -0.66291E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49734E-01 0.53053E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58233E-02      33   0.46190E-03   0.37526E+01 0.11836E+03 
c  Velocity[X]                                      0.19291E+01 
c  Velocity[Y]                                      0.18235E+01 
c  Velocity[Z]                                      0.14044E-29 
c  Pressure     0.21509E-06     378   0.92310E-08   0.21299E+00 0.53841E+03 
c  nu_tilda     0.42354E-05      32   0.11975E-04   0.27776E-06 0.18425E+03 
c  TempC        0.25302E+02      29   0.49704E-03   0.12573E+02 0.37300E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9747          9.8606          4.5729          4.5729
v  Velocity[Y]             -3.788          7.1223        0.013869        0.013869
v  Velocity[Z]       -1.2736e-014     4.8248e-015    -1.4725e-017    -1.4725e-017
v  ǁVelocityǁ         0.0031276          9.8767          5.0143          5.0143
v  Pressure               -51.631          20.296         -2.7418         -2.7418
v  nu_tilda           3.8167e-007        0.004266      0.00079845      0.00079845
v  TempC                       21          73.559          21.462          21.462
v  TurbVisc           1.8618e-014       0.0050279      0.00092882      0.00092882
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              509:        0.26600E+01

===============================================================


 INSTANT    0.510000000E+03   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11815E-01 0.88429E+00
   Friction velocity        uk    :  0.11815E-01 0.88429E+00
   Dimensionless distance   yplus :  0.95116E-01 0.71191E+01
   Friction thermal sca.    tstar : -0.60186E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70967E-01 0.53117E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58274E-02      33   0.54437E-03   0.36975E+01 0.11784E+03 
c  Velocity[X]                                      0.19028E+01 
c  Velocity[Y]                                      0.17947E+01 
c  Velocity[Z]                                      0.11964E-29 
c  Pressure     0.16652E-06     394   0.92354E-08   0.16486E+00 0.27645E+03 
c  nu_tilda     0.42377E-05      32   0.12025E-04   0.27695E-06 0.18388E+03 
c  TempC        0.25315E+02      29   0.46454E-03   0.90406E+01 0.32482E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9807          9.8575          4.5729          4.5729
v  Velocity[Y]            -3.7978          7.1215        0.013925        0.013925
v  Velocity[Z]       -1.1812e-014     4.8113e-015     -1.473e-017     -1.473e-017
v  ǁVelocityǁ          0.003101          9.8743           5.015           5.015
v  Pressure               -51.638          20.271         -2.7508         -2.7508
v  nu_tilda           3.8198e-007        0.004266      0.00079911      0.00079911
v  TempC                       21           73.13          21.463          21.463
v  TurbVisc           1.8669e-014       0.0050279      0.00092958      0.00092958
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              510:        0.26570E+01

===============================================================


 INSTANT    0.511000000E+03   TIME STEP NUMBER             511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65686E-02 0.88371E+00
   Friction velocity        uk    :  0.65686E-02 0.88371E+00
   Dimensionless distance   yplus :  0.52882E-01 0.71145E+01
   Friction thermal sca.    tstar : -0.68611E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39456E-01 0.53082E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58314E-02      33   0.54876E-03   0.37119E+01 0.11786E+03 
c  Velocity[X]                                      0.19150E+01 
c  Velocity[Y]                                      0.17968E+01 
c  Velocity[Z]                                      0.11006E-29 
c  Pressure     0.17463E-06     488   0.96081E-08   0.17744E+00 0.52667E+03 
c  nu_tilda     0.42400E-05      32   0.11950E-04   0.27610E-06 0.18351E+03 
c  TempC        0.25329E+02      29   0.44054E-03   0.82743E+01 0.31545E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9867          9.8543          4.5729          4.5729
v  Velocity[Y]            -3.8075          7.0948        0.013983        0.013983
v  Velocity[Z]       -1.1797e-014       4.81e-015    -1.4737e-017    -1.4737e-017
v  ǁVelocityǁ         0.0027068          9.8715          5.0157          5.0157
v  Pressure               -51.695          20.193          -2.794          -2.794
v  nu_tilda            3.824e-007        0.004266      0.00079974      0.00079974
v  TempC                       21          73.132          21.463          21.463
v  TurbVisc            1.873e-014       0.0050279      0.00093035      0.00093035
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              511:        0.30930E+01

===============================================================


 INSTANT    0.512000000E+03   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15134E-01 0.88234E+00
   Friction velocity        uk    :  0.15134E-01 0.88234E+00
   Dimensionless distance   yplus :  0.12184E+00 0.71034E+01
   Friction thermal sca.    tstar : -0.25510E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90903E-01 0.53000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58354E-02      33   0.54011E-03   0.36975E+01 0.11763E+03 
c  Velocity[X]                                      0.19217E+01 
c  Velocity[Y]                                      0.17758E+01 
c  Velocity[Z]                                      0.14144E-29 
c  Pressure     0.19867E-06     473   0.94475E-08   0.19850E+00 0.72252E+03 
c  nu_tilda     0.42423E-05      32   0.12037E-04   0.27529E-06 0.18314E+03 
c  TempC        0.25342E+02      29   0.53302E-03   0.91368E+01 0.33192E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9928          9.8511          4.5729          4.5729
v  Velocity[Y]            -3.8169          7.1146         0.01404         0.01404
v  Velocity[Z]        -1.118e-014      4.811e-015    -1.4738e-017    -1.4738e-017
v  ǁVelocityǁ          0.002863          9.8688          5.0163          5.0163
v  Pressure               -51.682           20.31         -2.7617         -2.7617
v  nu_tilda           3.8283e-007       0.0042661      0.00080039      0.00080039
v  TempC                       21          73.299          21.464          21.464
v  TurbVisc           1.8813e-014        0.005028      0.00093111      0.00093111
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              512:        0.23210E+01

===============================================================


 INSTANT    0.513000000E+03   TIME STEP NUMBER             513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16759E-01 0.88349E+00
   Friction velocity        uk    :  0.16759E-01 0.88349E+00
   Dimensionless distance   yplus :  0.13492E+00 0.71127E+01
   Friction thermal sca.    tstar : -0.74952E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10066E+00 0.53069E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58395E-02      33   0.55903E-03   0.36841E+01 0.11747E+03 
c  Velocity[X]                                      0.19207E+01 
c  Velocity[Y]                                      0.17634E+01 
c  Velocity[Z]                                      0.12142E-29 
c  Pressure     0.16497E-06     505   0.91875E-08   0.16359E+00 0.90817E+03 
c  nu_tilda     0.42446E-05      32   0.11903E-04   0.27446E-06 0.18277E+03 
c  TempC        0.25355E+02      29   0.83290E-03   0.99209E+01 0.35628E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9983          9.8484          4.5729          4.5729
v  Velocity[Y]            -3.8262          7.0978        0.014098        0.014098
v  Velocity[Z]       -1.0775e-014     4.8104e-015     -1.474e-017     -1.474e-017
v  ǁVelocityǁ         0.0025367          9.8656           5.017           5.017
v  Pressure               -51.747          20.167         -2.8268         -2.8268
v  nu_tilda            3.833e-007       0.0042661      0.00080102      0.00080102
v  TempC                       21          73.591          21.464          21.464
v  TurbVisc           1.8897e-014        0.005028      0.00093188      0.00093188
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              513:        0.22610E+01

===============================================================


 INSTANT    0.514000000E+03   TIME STEP NUMBER             514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14718E-01 0.88293E+00
   Friction velocity        uk    :  0.14718E-01 0.88293E+00
   Dimensionless distance   yplus :  0.11849E+00 0.71082E+01
   Friction thermal sca.    tstar : -0.72690E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88406E-01 0.53035E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58435E-02      33   0.55948E-03   0.36701E+01 0.11724E+03 
c  Velocity[X]                                      0.19047E+01 
c  Velocity[Y]                                      0.17654E+01 
c  Velocity[Z]                                      0.10967E-29 
c  Pressure     0.18774E-06     490   0.97197E-08   0.18629E+00 0.92955E+03 
c  nu_tilda     0.42469E-05      32   0.12053E-04   0.27366E-06 0.18240E+03 
c  TempC        0.25369E+02      29   0.57927E-03   0.16632E+02 0.46236E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0039          9.8454          4.5729          4.5729
v  Velocity[Y]            -3.8356          7.1186        0.014155        0.014155
v  Velocity[Z]       -9.6245e-015     4.8131e-015     -1.473e-017     -1.473e-017
v  ǁVelocityǁ         0.0028944          9.8628          5.0177          5.0177
v  Pressure               -51.736          20.333         -2.7863         -2.7863
v  nu_tilda           3.8376e-007       0.0042661      0.00080168      0.00080168
v  TempC                       21          73.138          21.465          21.465
v  TurbVisc           1.8991e-014        0.005028      0.00093264      0.00093264
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              514:        0.22750E+01

===============================================================


 INSTANT    0.515000000E+03   TIME STEP NUMBER             515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93217E-02 0.88380E+00
   Friction velocity        uk    :  0.93217E-02 0.88380E+00
   Dimensionless distance   yplus :  0.75046E-01 0.71152E+01
   Friction thermal sca.    tstar : -0.75258E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55993E-01 0.53088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58476E-02      33   0.56567E-03   0.36540E+01 0.11704E+03 
c  Velocity[X]                                      0.18977E+01 
c  Velocity[Y]                                      0.17563E+01 
c  Velocity[Z]                                      0.12867E-29 
c  Pressure     0.19058E-06     490   0.97982E-08   0.18702E+00 0.54744E+03 
c  nu_tilda     0.42492E-05      32   0.11868E-04   0.27284E-06 0.18203E+03 
c  TempC        0.25382E+02      29   0.41367E-03   0.10437E+02 0.36379E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0101          9.8428          4.5729          4.5729
v  Velocity[Y]            -3.8448          7.1201        0.014213        0.014213
v  Velocity[Z]       -9.1278e-015     4.8132e-015    -1.4724e-017    -1.4724e-017
v  ǁVelocityǁ         0.0027537          9.8596          5.0183          5.0183
v  Pressure               -51.793          20.262         -2.8329         -2.8329
v  nu_tilda           3.8416e-007       0.0042661      0.00080231      0.00080231
v  TempC                       21          73.239          21.466          21.466
v  TurbVisc           1.9081e-014        0.005028      0.00093341      0.00093341
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              515:        0.25030E+01

===============================================================


 INSTANT    0.516000000E+03   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15904E-01 0.88334E+00
   Friction velocity        uk    :  0.15904E-01 0.88334E+00
   Dimensionless distance   yplus :  0.12804E+00 0.71115E+01
   Friction thermal sca.    tstar : -0.98894E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95533E-01 0.53060E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58516E-02      33   0.55540E-03   0.36767E+01 0.11712E+03 
c  Velocity[X]                                      0.19376E+01 
c  Velocity[Y]                                      0.17392E+01 
c  Velocity[Z]                                      0.12885E-29 
c  Pressure     0.17281E-06     410   0.98950E-08   0.17396E+00 0.37040E+03 
c  nu_tilda     0.42514E-05      32   0.12070E-04   0.27205E-06 0.18167E+03 
c  TempC        0.25396E+02      29   0.56367E-03   0.93669E+01 0.33779E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0161          9.8396          4.5729          4.5729
v  Velocity[Y]            -3.8536          7.0926         0.01427         0.01427
v  Velocity[Z]       -9.3819e-015     4.8766e-015    -1.4719e-017    -1.4719e-017
v  ǁVelocityǁ         0.0024703          9.8563           5.019           5.019
v  Pressure               -51.785          20.204         -2.8435         -2.8435
v  nu_tilda           3.8466e-007       0.0042662      0.00080297      0.00080297
v  TempC                       21          73.799          21.466          21.466
v  TurbVisc           1.9161e-014       0.0050281      0.00093418      0.00093418
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              516:        0.24510E+01

===============================================================


 INSTANT    0.517000000E+03   TIME STEP NUMBER             517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14669E-01 0.88217E+00
   Friction velocity        uk    :  0.14669E-01 0.88217E+00
   Dimensionless distance   yplus :  0.11810E+00 0.71021E+01
   Friction thermal sca.    tstar : -0.35560E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88113E-01 0.52989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58557E-02      33   0.51956E-03   0.36192E+01 0.11669E+03 
c  Velocity[X]                                      0.18787E+01 
c  Velocity[Y]                                      0.17405E+01 
c  Velocity[Z]                                      0.12389E-29 
c  Pressure     0.18602E-06     409   0.93765E-08   0.18463E+00 0.46340E+03 
c  nu_tilda     0.42537E-05      32   0.11845E-04   0.27124E-06 0.18131E+03 
c  TempC        0.25409E+02      29   0.36292E-03   0.10342E+02 0.35429E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0221          9.8363          4.5729          4.5729
v  Velocity[Y]            -3.8625          7.1141        0.014327        0.014327
v  Velocity[Z]       -9.6086e-015     5.0902e-015    -1.4726e-017    -1.4726e-017
v  ǁVelocityǁ         0.0026479           9.853          5.0197          5.0197
v  Pressure               -51.835          20.269         -2.8572         -2.8572
v  nu_tilda           3.8516e-007       0.0042662       0.0008036       0.0008036
v  TempC                       21          73.142          21.467          21.467
v  TurbVisc           1.9261e-014       0.0050281      0.00093494      0.00093494
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              517:        0.20930E+01

===============================================================


 INSTANT    0.518000000E+03   TIME STEP NUMBER             518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15297E-01 0.88337E+00
   Friction velocity        uk    :  0.15297E-01 0.88337E+00
   Dimensionless distance   yplus :  0.12315E+00 0.71118E+01
   Friction thermal sca.    tstar : -0.11162E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91886E-01 0.53062E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58597E-02      33   0.50755E-03   0.35854E+01 0.11625E+03 
c  Velocity[X]                                      0.18703E+01 
c  Velocity[Y]                                      0.17152E+01 
c  Velocity[Z]                                      0.13378E-29 
c  Pressure     0.16457E-06     392   0.96548E-08   0.16440E+00 0.28944E+03 
c  nu_tilda     0.42560E-05      32   0.12086E-04   0.27045E-06 0.18095E+03 
c  TempC        0.25423E+02      29   0.56710E-03   0.77731E+01 0.31420E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0278          9.8331          4.5729          4.5729
v  Velocity[Y]            -3.8711          7.0949        0.014384        0.014384
v  Velocity[Z]       -8.7863e-015     5.2834e-015    -1.4724e-017    -1.4724e-017
v  ǁVelocityǁ         0.0024771          9.8495          5.0203          5.0203
v  Pressure               -51.825          20.233         -2.8627         -2.8627
v  nu_tilda           3.8568e-007       0.0042662      0.00080426      0.00080426
v  TempC                       21          73.144          21.467          21.467
v  TurbVisc           1.9362e-014       0.0050281      0.00093571      0.00093571
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              518:        0.20630E+01

===============================================================


 INSTANT    0.519000000E+03   TIME STEP NUMBER             519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10144E-01 0.88256E+00
   Friction velocity        uk    :  0.10144E-01 0.88256E+00
   Dimensionless distance   yplus :  0.81663E-01 0.71052E+01
   Friction thermal sca.    tstar : -0.92900E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60930E-01 0.53013E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58638E-02      33   0.56747E-03   0.35693E+01 0.11602E+03 
c  Velocity[X]                                      0.18746E+01 
c  Velocity[Y]                                      0.16947E+01 
c  Velocity[Z]                                      0.11942E-29 
c  Pressure     0.18347E-06     472   0.94299E-08   0.17775E+00 0.33343E+03 
c  nu_tilda     0.42583E-05      32   0.11819E-04   0.26965E-06 0.18059E+03 
c  TempC        0.25436E+02      29   0.55986E-03   0.98971E+01 0.34139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0334          9.8296          4.5729          4.5729
v  Velocity[Y]            -3.8797          7.1153        0.014441        0.014441
v  Velocity[Z]       -8.7994e-015     5.3864e-015    -1.4732e-017    -1.4732e-017
v  ǁVelocityǁ         0.0024994          9.8466           5.021           5.021
v  Pressure               -51.876          20.247          -2.888          -2.888
v  nu_tilda           3.8614e-007       0.0042663      0.00080488      0.00080488
v  TempC                       21          73.326          21.468          21.468
v  TurbVisc           1.9466e-014       0.0050282      0.00093648      0.00093648
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              519:        0.22190E+01

===============================================================


 INSTANT    0.520000000E+03   TIME STEP NUMBER             520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14336E-01 0.88407E+00
   Friction velocity        uk    :  0.14336E-01 0.88407E+00
   Dimensionless distance   yplus :  0.11541E+00 0.71173E+01
   Friction thermal sca.    tstar : -0.97860E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86110E-01 0.53103E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58678E-02      33   0.56912E-03   0.36000E+01 0.11621E+03 
c  Velocity[X]                                      0.18982E+01 
c  Velocity[Y]                                      0.17017E+01 
c  Velocity[Z]                                      0.12313E-29 
c  Pressure     0.17527E-06     377   0.92435E-08   0.17646E+00 0.26146E+03 
c  nu_tilda     0.42605E-05      32   0.12104E-04   0.26887E-06 0.18023E+03 
c  TempC        0.25449E+02      29   0.57314E-03   0.95268E+01 0.34078E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0388          9.8262          4.5729          4.5729
v  Velocity[Y]             -3.888          7.0946        0.014497        0.014497
v  Velocity[Z]       -9.1675e-015     5.5015e-015    -1.4736e-017    -1.4736e-017
v  ǁVelocityǁ         0.0022912          9.8434          5.0217          5.0217
v  Pressure               -51.865          20.219          -2.892          -2.892
v  nu_tilda           3.8661e-007       0.0042663      0.00080554      0.00080554
v  TempC                       21          73.665          21.469          21.469
v  TurbVisc           1.9559e-014       0.0050282      0.00093724      0.00093724
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              520:        0.20310E+01

===============================================================


 INSTANT    0.521000000E+03   TIME STEP NUMBER             521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13428E-01 0.88329E+00
   Friction velocity        uk    :  0.13428E-01 0.88329E+00
   Dimensionless distance   yplus :  0.10810E+00 0.71111E+01
   Friction thermal sca.    tstar : -0.10835E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80658E-01 0.53057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58719E-02      33   0.42912E-03   0.35479E+01 0.11575E+03 
c  Velocity[X]                                      0.18697E+01 
c  Velocity[Y]                                      0.16782E+01 
c  Velocity[Z]                                      0.13874E-29 
c  Pressure     0.15924E-06     425   0.92836E-08   0.15655E+00 0.46627E+03 
c  nu_tilda     0.42628E-05      32   0.11781E-04   0.26808E-06 0.17988E+03 
c  TempC        0.25463E+02      29   0.48801E-03   0.11015E+02 0.36345E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0442          9.8225          4.5729          4.5729
v  Velocity[Y]            -3.8963          7.1199        0.014554        0.014554
v  Velocity[Z]       -1.0273e-014     5.5893e-015    -1.4753e-017    -1.4753e-017
v  ǁVelocityǁ         0.0024697            9.84          5.0223          5.0223
v  Pressure               -51.916          20.293         -2.9072         -2.9072
v  nu_tilda           3.8708e-007       0.0042663      0.00080617      0.00080617
v  TempC                       21          73.163          21.469          21.469
v  TurbVisc           1.9655e-014       0.0050282      0.00093801      0.00093801
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              521:        0.23550E+01

===============================================================


 INSTANT    0.522000000E+03   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14007E-01 0.88423E+00
   Friction velocity        uk    :  0.14007E-01 0.88423E+00
   Dimensionless distance   yplus :  0.11277E+00 0.71186E+01
   Friction thermal sca.    tstar : -0.15612E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84138E-01 0.53113E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58759E-02      33   0.57824E-03   0.34804E+01 0.11507E+03 
c  Velocity[X]                                      0.18187E+01 
c  Velocity[Y]                                      0.16617E+01 
c  Velocity[Z]                                      0.10766E-29 
c  Pressure     0.14694E-06     410   0.97029E-08   0.14471E+00 0.27484E+03 
c  nu_tilda     0.42650E-05      32   0.12121E-04   0.26730E-06 0.17953E+03 
c  TempC        0.25476E+02      29   0.74986E-03   0.94168E+01 0.34334E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0501          9.8187          4.5729          4.5729
v  Velocity[Y]            -3.9044           7.126         0.01461         0.01461
v  Velocity[Z]       -1.0542e-014     5.6758e-015    -1.4767e-017    -1.4767e-017
v  ǁVelocityǁ         0.0024819          9.8369           5.023           5.023
v  Pressure               -51.899          20.317         -2.8971         -2.8971
v  nu_tilda            3.876e-007       0.0042663      0.00080683      0.00080683
v  TempC                       21          73.375           21.47           21.47
v  TurbVisc           1.9751e-014       0.0050283      0.00093877      0.00093877
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              522:        0.25440E+01

===============================================================


 INSTANT    0.523000000E+03   TIME STEP NUMBER             523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11032E-01 0.88367E+00
   Friction velocity        uk    :  0.11032E-01 0.88367E+00
   Dimensionless distance   yplus :  0.88818E-01 0.71141E+01
   Friction thermal sca.    tstar : -0.11482E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66268E-01 0.53079E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58800E-02      33   0.56627E-03   0.35199E+01 0.11526E+03 
c  Velocity[X]                                      0.18494E+01 
c  Velocity[Y]                                      0.16704E+01 
c  Velocity[Z]                                      0.10268E-29 
c  Pressure     0.17574E-06     506   0.92505E-08   0.17435E+00 0.74011E+03 
c  nu_tilda     0.42673E-05      32   0.11735E-04   0.26652E-06 0.17918E+03 
c  TempC        0.25489E+02      29   0.47428E-03   0.13830E+02 0.42198E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0562          9.8151          4.5729          4.5729
v  Velocity[Y]            -3.9123          7.0899        0.014667        0.014667
v  Velocity[Z]       -1.0816e-014     5.7577e-015    -1.4782e-017    -1.4782e-017
v  ǁVelocityǁ         0.0022146          9.8333          5.0237          5.0237
v  Pressure               -51.941          20.195         -2.9513         -2.9513
v  nu_tilda           3.8828e-007       0.0042664      0.00080746      0.00080746
v  TempC                       21           73.67           21.47           21.47
v  TurbVisc           1.9856e-014       0.0050283      0.00093954      0.00093954
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              523:        0.24690E+01

===============================================================


 INSTANT    0.524000000E+03   TIME STEP NUMBER             524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12018E-01 0.88223E+00
   Friction velocity        uk    :  0.12018E-01 0.88223E+00
   Dimensionless distance   yplus :  0.96757E-01 0.71025E+01
   Friction thermal sca.    tstar : -0.13521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72192E-01 0.52993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58840E-02      33   0.52912E-03   0.35060E+01 0.11505E+03 
c  Velocity[X]                                      0.18460E+01 
c  Velocity[Y]                                      0.16600E+01 
c  Velocity[Z]                                      0.14287E-29 
c  Pressure     0.16179E-06     488   0.95918E-08   0.15940E+00 0.70045E+03 
c  nu_tilda     0.42695E-05      32   0.12149E-04   0.26574E-06 0.17883E+03 
c  TempC        0.25503E+02      29   0.41543E-03   0.92790E+01 0.33546E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0621          9.8111          4.5729          4.5729
v  Velocity[Y]            -3.9202          7.1117        0.014723        0.014723
v  Velocity[Z]       -1.0642e-014     5.8156e-015    -1.4793e-017    -1.4793e-017
v  ǁVelocityǁ         0.0023682          9.8298          5.0243          5.0243
v  Pressure               -51.929          20.321         -2.9216         -2.9216
v  nu_tilda           3.8896e-007       0.0042664      0.00080811      0.00080811
v  TempC                       21          73.961          21.471          21.471
v  TurbVisc           1.9997e-014       0.0050283       0.0009403       0.0009403
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              524:        0.30100E+01

===============================================================


 INSTANT    0.525000000E+03   TIME STEP NUMBER             525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14012E-01 0.88370E+00
   Friction velocity        uk    :  0.14012E-01 0.88370E+00
   Dimensionless distance   yplus :  0.11280E+00 0.71144E+01
   Friction thermal sca.    tstar : -0.13794E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84163E-01 0.53081E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58881E-02      33   0.54552E-03   0.34787E+01 0.11477E+03 
c  Velocity[X]                                      0.18424E+01 
c  Velocity[Y]                                      0.16363E+01 
c  Velocity[Z]                                      0.12117E-29 
c  Pressure     0.15755E-06     474   0.99472E-08   0.15824E+00 0.74873E+03 
c  nu_tilda     0.42718E-05      32   0.11702E-04   0.26497E-06 0.17848E+03 
c  TempC        0.25516E+02      29   0.52816E-03   0.98710E+01 0.33419E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0676           9.807          4.5729          4.5729
v  Velocity[Y]            -3.9278          7.0973        0.014779        0.014779
v  Velocity[Z]       -1.0631e-014     5.8724e-015    -1.4802e-017    -1.4802e-017
v  ǁVelocityǁ           0.00218          9.8263           5.025           5.025
v  Pressure               -51.978          20.205         -2.9783         -2.9783
v  nu_tilda            3.896e-007       0.0042664      0.00080874      0.00080874
v  TempC                       21          73.149          21.471          21.471
v  TurbVisc           2.0136e-014       0.0050284      0.00094107      0.00094107
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              525:        0.25430E+01

===============================================================


 INSTANT    0.526000000E+03   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11806E-01 0.88285E+00
   Friction velocity        uk    :  0.11806E-01 0.88285E+00
   Dimensionless distance   yplus :  0.95050E-01 0.71075E+01
   Friction thermal sca.    tstar : -0.16731E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70918E-01 0.53030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58921E-02      33   0.51012E-03   0.34692E+01 0.11456E+03 
c  Velocity[X]                                      0.18252E+01 
c  Velocity[Y]                                      0.16439E+01 
c  Velocity[Z]                                      0.10565E-29 
c  Pressure     0.14189E-06     473   0.97611E-08   0.14002E+00 0.59844E+03 
c  nu_tilda     0.42740E-05      32   0.12163E-04   0.26420E-06 0.17813E+03 
c  TempC        0.25529E+02      29   0.50562E-03   0.85944E+01 0.33480E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0728          9.8031          4.5729          4.5729
v  Velocity[Y]            -3.9349          7.1184        0.014835        0.014835
v  Velocity[Z]       -9.9727e-015     5.9082e-015    -1.4801e-017    -1.4801e-017
v  ǁVelocityǁ         0.0023526          9.8224          5.0256          5.0256
v  Pressure               -51.967          20.316         -2.9537         -2.9537
v  nu_tilda           3.9021e-007       0.0042664       0.0008094       0.0008094
v  TempC                       21           73.15          21.472          21.472
v  TurbVisc            2.027e-014       0.0050284      0.00094183      0.00094183
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              526:        0.22190E+01

===============================================================


 INSTANT    0.527000000E+03   TIME STEP NUMBER             527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10185E-01 0.88405E+00
   Friction velocity        uk    :  0.10185E-01 0.88405E+00
   Dimensionless distance   yplus :  0.81995E-01 0.71172E+01
   Friction thermal sca.    tstar : -0.15626E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61178E-01 0.53102E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.58962E-02      33   0.54028E-03   0.34297E+01 0.11404E+03 
c  Velocity[X]                                      0.18126E+01 
c  Velocity[Y]                                      0.16171E+01 
c  Velocity[Z]                                      0.12200E-29 
c  Pressure     0.16400E-06     472   0.99379E-08   0.15938E+00 0.47172E+03 
c  nu_tilda     0.42763E-05      32   0.11661E-04   0.26342E-06 0.17779E+03 
c  TempC        0.25543E+02      29   0.52185E-03   0.75758E+01 0.31770E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0778          9.7989          4.5729          4.5729
v  Velocity[Y]            -3.9423          7.1201        0.014892        0.014892
v  Velocity[Z]       -9.2205e-015     5.9291e-015    -1.4794e-017    -1.4794e-017
v  ǁVelocityǁ         0.0023122          9.8187          5.0263          5.0263
v  Pressure               -52.015          20.264         -2.9963         -2.9963
v  nu_tilda           3.9082e-007       0.0042665      0.00081003      0.00081003
v  TempC                       21           73.15          21.472          21.472
v  TurbVisc           2.0396e-014       0.0050284      0.00094259      0.00094259
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              527:        0.26350E+01

===============================================================


 INSTANT    0.528000000E+03   TIME STEP NUMBER             528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13174E-01 0.88379E+00
   Friction velocity        uk    :  0.13174E-01 0.88379E+00
   Dimensionless distance   yplus :  0.10606E+00 0.71151E+01
   Friction thermal sca.    tstar : -0.17120E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79135E-01 0.53086E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59003E-02      33   0.56297E-03   0.34529E+01 0.11414E+03 
c  Velocity[X]                                      0.18535E+01 
c  Velocity[Y]                                      0.15994E+01 
c  Velocity[Z]                                      0.12272E-29 
c  Pressure     0.16319E-06     362   0.92517E-08   0.16357E+00 0.28245E+03 
c  nu_tilda     0.42785E-05      32   0.12190E-04   0.26266E-06 0.17744E+03 
c  TempC        0.25556E+02      29   0.49852E-03   0.92649E+01 0.33585E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0828          9.7948          4.5729          4.5729
v  Velocity[Y]            -3.9493          7.0951        0.014948        0.014948
v  Velocity[Z]       -8.3066e-015     5.6531e-015    -1.4786e-017    -1.4786e-017
v  ǁVelocityǁ         0.0020504          9.8149          5.0269          5.0269
v  Pressure               -51.995          20.224              -3              -3
v  nu_tilda           3.9154e-007       0.0042665      0.00081068      0.00081068
v  TempC                       21          73.587          21.473          21.473
v  TurbVisc           2.0525e-014       0.0050284      0.00094336      0.00094336
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              528:        0.22220E+01

===============================================================


 INSTANT    0.529000000E+03   TIME STEP NUMBER             529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11522E-01 0.88273E+00
   Friction velocity        uk    :  0.11522E-01 0.88273E+00
   Dimensionless distance   yplus :  0.92760E-01 0.71066E+01
   Friction thermal sca.    tstar : -0.24556E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69209E-01 0.53023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59043E-02      33   0.51594E-03   0.34148E+01 0.11390E+03 
c  Velocity[X]                                      0.18049E+01 
c  Velocity[Y]                                      0.16099E+01 
c  Velocity[Z]                                      0.12437E-29 
c  Pressure     0.14637E-06     470   0.90659E-08   0.14499E+00 0.34911E+03 
c  nu_tilda     0.42807E-05      32   0.11605E-04   0.26189E-06 0.17710E+03 
c  TempC        0.25569E+02      29   0.56707E-03   0.11504E+02 0.37325E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0882          9.7905          4.5729          4.5729
v  Velocity[Y]             -3.956          7.1173        0.015004        0.015004
v  Velocity[Z]        -7.389e-015     5.6067e-015    -1.4776e-017    -1.4776e-017
v  ǁVelocityǁ         0.0021797          9.8109          5.0276          5.0276
v  Pressure               -52.048          20.244         -3.0314         -3.0314
v  nu_tilda           3.9227e-007       0.0042665      0.00081131      0.00081131
v  TempC                       21          73.149          21.474          21.474
v  TurbVisc           2.0676e-014       0.0050285      0.00094412      0.00094412
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              529:        0.31790E+01

===============================================================


 INSTANT    0.530000000E+03   TIME STEP NUMBER             530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11744E-01 0.88386E+00
   Friction velocity        uk    :  0.11744E-01 0.88386E+00
   Dimensionless distance   yplus :  0.94550E-01 0.71157E+01
   Friction thermal sca.    tstar : -0.25276E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70545E-01 0.53091E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59084E-02      33   0.49634E-03   0.33674E+01 0.11326E+03 
c  Velocity[X]                                      0.17837E+01 
c  Velocity[Y]                                      0.15837E+01 
c  Velocity[Z]                                      0.14482E-29 
c  Pressure     0.17080E-06     280   0.92708E-08   0.17221E+00 0.23765E+03 
c  nu_tilda     0.42830E-05      32   0.12207E-04   0.26114E-06 0.17676E+03 
c  TempC        0.25583E+02      29   0.57087E-03   0.89657E+01 0.33731E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0934          9.7864          4.5729          4.5729
v  Velocity[Y]            -3.9631          7.0989        0.015059        0.015059
v  Velocity[Z]       -6.9287e-015     5.5954e-015     -1.476e-017     -1.476e-017
v  ǁVelocityǁ          0.002042           9.807          5.0282          5.0282
v  Pressure               -52.027          20.221         -3.0304         -3.0304
v  nu_tilda           3.9303e-007       0.0042665      0.00081197      0.00081197
v  TempC                       21          73.321          21.474          21.474
v  TurbVisc            2.083e-014       0.0050285      0.00094489      0.00094489
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              530:        0.25560E+01

===============================================================


 INSTANT    0.531000000E+03   TIME STEP NUMBER             531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31407E-02 0.88293E+00
   Friction velocity        uk    :  0.31407E-02 0.88293E+00
   Dimensionless distance   yplus :  0.25285E-01 0.71082E+01
   Friction thermal sca.    tstar : -0.10015E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18865E-01 0.53035E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59124E-02      33   0.56672E-03   0.33641E+01 0.11300E+03 
c  Velocity[X]                                      0.18009E+01 
c  Velocity[Y]                                      0.15632E+01 
c  Velocity[Z]                                      0.11111E-29 
c  Pressure     0.22077E-06     442   0.94808E-08   0.21496E+00 0.35448E+03 
c  nu_tilda     0.42852E-05      32   0.11581E-04   0.26039E-06 0.17642E+03 
c  TempC        0.25596E+02      29   0.54990E-03   0.10254E+02 0.36613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0986          9.7822          4.5729          4.5729
v  Velocity[Y]            -3.9696          7.1176        0.015116        0.015116
v  Velocity[Z]       -6.9287e-015     5.5743e-015    -1.4745e-017    -1.4745e-017
v  ǁVelocityǁ         0.0021787           9.803          5.0289          5.0289
v  Pressure               -52.061          20.258         -3.0491         -3.0491
v  nu_tilda           3.9377e-007       0.0042666      0.00081259      0.00081259
v  TempC                       21          73.416          21.475          21.475
v  TurbVisc           2.0992e-014       0.0050285      0.00094565      0.00094565
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              531:        0.29620E+01

===============================================================


 INSTANT    0.532000000E+03   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39840E-02 0.88414E+00
   Friction velocity        uk    :  0.39840E-02 0.88414E+00
   Dimensionless distance   yplus :  0.32074E-01 0.71179E+01
   Friction thermal sca.    tstar : -0.79298E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23931E-01 0.53108E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59165E-02      33   0.54745E-03   0.33818E+01 0.11318E+03 
c  Velocity[X]                                      0.18094E+01 
c  Velocity[Y]                                      0.15724E+01 
c  Velocity[Z]                                      0.11590E-29 
c  Pressure     0.16384E-06     457   0.94185E-08   0.16552E+00 0.51547E+03 
c  nu_tilda     0.42874E-05      32   0.12233E-04   0.25965E-06 0.17609E+03 
c  TempC        0.25609E+02      29   0.43540E-03   0.87903E+01 0.33297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1029          9.7779          4.5729          4.5729
v  Velocity[Y]            -3.9757          7.0966        0.015171        0.015171
v  Velocity[Z]       -6.9287e-015     5.9043e-015    -1.4733e-017    -1.4733e-017
v  ǁVelocityǁ         0.0019621          9.7988          5.0295          5.0295
v  Pressure               -52.055          20.177         -3.0708         -3.0708
v  nu_tilda           3.9453e-007       0.0042666      0.00081325      0.00081325
v  TempC                       21           73.62          21.475          21.475
v  TurbVisc           2.1151e-014       0.0050286      0.00094641      0.00094641
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              532:        0.28330E+01

===============================================================


 INSTANT    0.533000000E+03   TIME STEP NUMBER             533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10506E-01 0.88339E+00
   Friction velocity        uk    :  0.10506E-01 0.88339E+00
   Dimensionless distance   yplus :  0.84578E-01 0.71119E+01
   Friction thermal sca.    tstar : -0.25927E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63105E-01 0.53063E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59205E-02      33   0.41855E-03   0.33233E+01 0.11261E+03 
c  Velocity[X]                                      0.17732E+01 
c  Velocity[Y]                                      0.15501E+01 
c  Velocity[Z]                                      0.13938E-29 
c  Pressure     0.15567E-06     409   0.99223E-08   0.15370E+00 0.45877E+03 
c  nu_tilda     0.42896E-05      32   0.11551E-04   0.25890E-06 0.17575E+03 
c  TempC        0.25623E+02      29   0.71704E-03   0.80627E+01 0.30967E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1073          9.7735          4.5729          4.5729
v  Velocity[Y]            -3.9818          7.1202        0.015226        0.015226
v  Velocity[Z]       -6.9287e-015     5.5559e-015    -1.4732e-017    -1.4732e-017
v  ǁVelocityǁ         0.0021393          9.7948          5.0301          5.0301
v  Pressure               -52.096          20.251         -3.0845         -3.0845
v  nu_tilda           3.9523e-007       0.0042666      0.00081388      0.00081388
v  TempC                       21          73.148          21.476          21.476
v  TurbVisc           2.1316e-014       0.0050286      0.00094718      0.00094718
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              533:        0.29590E+01

===============================================================


 INSTANT    0.534000000E+03   TIME STEP NUMBER             534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87155E-02 0.88437E+00
   Friction velocity        uk    :  0.87155E-02 0.88437E+00
   Dimensionless distance   yplus :  0.70165E-01 0.71197E+01
   Friction thermal sca.    tstar : -0.35414E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52351E-01 0.53121E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59246E-02      33   0.55975E-03   0.32642E+01 0.11194E+03 
c  Velocity[X]                                      0.17319E+01 
c  Velocity[Y]                                      0.15322E+01 
c  Velocity[Z]                                      0.10686E-29 
c  Pressure     0.18620E-06     456   0.98196E-08   0.18525E+00 0.43640E+03 
c  nu_tilda     0.42918E-05      32   0.12255E-04   0.25817E-06 0.17542E+03 
c  TempC        0.25636E+02      29   0.54678E-03   0.13669E+02 0.41991E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1117          9.7694          4.5729          4.5729
v  Velocity[Y]             -3.988          7.1278        0.015281        0.015281
v  Velocity[Z]       -7.6602e-015     5.4594e-015    -1.4736e-017    -1.4736e-017
v  ǁVelocityǁ         0.0021777          9.7907          5.0308          5.0308
v  Pressure               -52.071          20.315         -3.0642         -3.0642
v  nu_tilda           3.9584e-007       0.0042666      0.00081453      0.00081453
v  TempC                       21            73.2          21.476          21.476
v  TurbVisc           2.1467e-014       0.0050286      0.00094794      0.00094794
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              534:        0.28860E+01

===============================================================


 INSTANT    0.535000000E+03   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54780E-02 0.88383E+00
   Friction velocity        uk    :  0.54780E-02 0.88383E+00
   Dimensionless distance   yplus :  0.44102E-01 0.71155E+01
   Friction thermal sca.    tstar : -0.37170E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32905E-01 0.53089E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59287E-02      33   0.55992E-03   0.32997E+01 0.11207E+03 
c  Velocity[X]                                      0.17594E+01 
c  Velocity[Y]                                      0.15404E+01 
c  Velocity[Z]                                      0.11223E-29 
c  Pressure     0.17359E-06     505   0.99550E-08   0.17529E+00 0.86474E+03 
c  nu_tilda     0.42940E-05      32   0.11484E-04   0.25744E-06 0.17509E+03 
c  TempC        0.25649E+02      29   0.41231E-03   0.90661E+01 0.33678E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1159          9.7651          4.5729          4.5729
v  Velocity[Y]            -3.9936          7.0924        0.015336        0.015336
v  Velocity[Z]       -9.0371e-015     5.4206e-015    -1.4749e-017    -1.4749e-017
v  ǁVelocityǁ         0.0019541          9.7865          5.0314          5.0314
v  Pressure               -52.111          20.167         -3.1244         -3.1244
v  nu_tilda           3.9658e-007       0.0042666      0.00081516      0.00081516
v  TempC                       21          73.527          21.477          21.477
v  TurbVisc           2.1599e-014       0.0050286      0.00094871      0.00094871
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              535:        0.31860E+01

===============================================================


 INSTANT    0.536000000E+03   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78156E-02 0.88239E+00
   Friction velocity        uk    :  0.78156E-02 0.88239E+00
   Dimensionless distance   yplus :  0.62921E-01 0.71038E+01
   Friction thermal sca.    tstar : -0.21735E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46946E-01 0.53002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59327E-02      33   0.51413E-03   0.32831E+01 0.11185E+03 
c  Velocity[X]                                      0.17537E+01 
c  Velocity[Y]                                      0.15294E+01 
c  Velocity[Z]                                      0.14831E-29 
c  Pressure     0.15980E-06     473   0.95545E-08   0.15675E+00 0.62547E+03 
c  nu_tilda     0.42962E-05      32   0.12285E-04   0.25670E-06 0.17476E+03 
c  TempC        0.25662E+02      29   0.51470E-03   0.84252E+01 0.31927E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1204          9.7608          4.5729          4.5729
v  Velocity[Y]             -3.999          7.1136        0.015391        0.015391
v  Velocity[Z]        -1.008e-014     5.3735e-015    -1.4771e-017    -1.4771e-017
v  ǁVelocityǁ         0.0019607          9.7823          5.0321          5.0321
v  Pressure               -52.092          20.277         -3.0975         -3.0975
v  nu_tilda           3.9733e-007       0.0042667      0.00081582      0.00081582
v  TempC                       21          73.147          21.478          21.478
v  TurbVisc           2.1761e-014       0.0050287      0.00094947      0.00094947
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              536:        0.30410E+01

===============================================================


 INSTANT    0.537000000E+03   TIME STEP NUMBER             537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99771E-02 0.88394E+00
   Friction velocity        uk    :  0.99771E-02 0.88394E+00
   Dimensionless distance   yplus :  0.80322E-01 0.71163E+01
   Friction thermal sca.    tstar : -0.22020E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59929E-01 0.53096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59368E-02      33   0.53773E-03   0.32603E+01 0.11145E+03 
c  Velocity[X]                                      0.17547E+01 
c  Velocity[Y]                                      0.15055E+01 
c  Velocity[Z]                                      0.13123E-29 
c  Pressure     0.19665E-06     474   0.95920E-08   0.19809E+00 0.42525E+03 
c  nu_tilda     0.42984E-05      32   0.11454E-04   0.25598E-06 0.17443E+03 
c  TempC        0.25676E+02      29   0.41387E-03   0.84463E+01 0.32203E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1254          9.7566          4.5729          4.5729
v  Velocity[Y]             -4.005          7.0993        0.015446        0.015446
v  Velocity[Z]       -1.0854e-014      5.332e-015    -1.4793e-017    -1.4793e-017
v  ǁVelocityǁ          0.001966          9.7783          5.0327          5.0327
v  Pressure               -52.126          20.221         -3.1347         -3.1347
v  nu_tilda           3.9799e-007       0.0042667      0.00081645      0.00081645
v  TempC                       21          73.146          21.478          21.478
v  TurbVisc           2.1926e-014       0.0050287      0.00095023      0.00095023
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              537:        0.25120E+01

===============================================================


 INSTANT    0.538000000E+03   TIME STEP NUMBER             538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84379E-02 0.88311E+00
   Friction velocity        uk    :  0.84379E-02 0.88311E+00
   Dimensionless distance   yplus :  0.67931E-01 0.71096E+01
   Friction thermal sca.    tstar : -0.19639E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50684E-01 0.53046E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59409E-02      33   0.49544E-03   0.32536E+01 0.11130E+03 
c  Velocity[X]                                      0.17370E+01 
c  Velocity[Y]                                      0.15166E+01 
c  Velocity[Z]                                      0.10939E-29 
c  Pressure     0.15829E-06     440   0.96916E-08   0.15654E+00 0.37030E+03 
c  nu_tilda     0.43006E-05      32   0.12308E-04   0.25526E-06 0.17410E+03 
c  TempC        0.25689E+02      29   0.48253E-03   0.79052E+01 0.31423E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1297          9.7524          4.5729          4.5729
v  Velocity[Y]              -4.01          7.1204          0.0155          0.0155
v  Velocity[Z]       -1.1919e-014     5.3003e-015    -1.4829e-017    -1.4829e-017
v  ǁVelocityǁ         0.0020266          9.7741          5.0333          5.0333
v  Pressure               -52.115          20.296         -3.1224         -3.1224
v  nu_tilda            3.986e-007       0.0042667       0.0008171       0.0008171
v  TempC                       21          73.486          21.479          21.479
v  TurbVisc           2.2072e-014       0.0050287        0.000951        0.000951
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              538:        0.22270E+01

===============================================================


 INSTANT    0.539000000E+03   TIME STEP NUMBER             539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10446E-01 0.88433E+00
   Friction velocity        uk    :  0.10446E-01 0.88433E+00
   Dimensionless distance   yplus :  0.84096E-01 0.71195E+01
   Friction thermal sca.    tstar : -0.22575E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62745E-01 0.53119E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59449E-02      33   0.53084E-03   0.32234E+01 0.11074E+03 
c  Velocity[X]                                      0.17349E+01 
c  Velocity[Y]                                      0.14885E+01 
c  Velocity[Z]                                      0.16566E-29 
c  Pressure     0.19798E-06     458   0.96662E-08   0.19443E+00 0.29509E+03 
c  nu_tilda     0.43028E-05      32   0.11428E-04   0.25454E-06 0.17378E+03 
c  TempC        0.25702E+02      29   0.71782E-03   0.71304E+01 0.30134E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1342          9.7483          4.5729          4.5729
v  Velocity[Y]            -4.0152          7.1226        0.015555        0.015555
v  Velocity[Z]       -1.2039e-014     5.6176e-015    -1.4842e-017    -1.4842e-017
v  ǁVelocityǁ         0.0020723            9.77           5.034           5.034
v  Pressure               -52.139           20.29         -3.1452         -3.1452
v  nu_tilda           3.9924e-007       0.0042667      0.00081773      0.00081773
v  TempC                       21          73.145          21.479          21.479
v  TurbVisc           2.2209e-014       0.0050288      0.00095176      0.00095176
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              539:        0.23180E+01

===============================================================


 INSTANT    0.540000000E+03   TIME STEP NUMBER             540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10385E-01 0.88386E+00
   Friction velocity        uk    :  0.10385E-01 0.88386E+00
   Dimensionless distance   yplus :  0.83609E-01 0.71157E+01
   Friction thermal sca.    tstar : -0.24160E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62382E-01 0.53091E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59490E-02      33   0.55487E-03   0.32520E+01 0.11090E+03 
c  Velocity[X]                                      0.17783E+01 
c  Velocity[Y]                                      0.14737E+01 
c  Velocity[Z]                                      0.12889E-29 
c  Pressure     0.16674E-06     421   0.97106E-08   0.16900E+00 0.39136E+03 
c  nu_tilda     0.43050E-05      32   0.12342E-04   0.25382E-06 0.17345E+03 
c  TempC        0.25715E+02      29   0.39803E-03   0.97443E+01 0.34146E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1385          9.7442          4.5729          4.5729
v  Velocity[Y]            -4.0202          7.0975        0.015608        0.015608
v  Velocity[Z]       -1.2542e-014     5.2261e-015    -1.4865e-017    -1.4865e-017
v  ǁVelocityǁ         0.0018536          9.7658          5.0346          5.0346
v  Pressure               -52.118          20.221         -3.1572         -3.1572
v  nu_tilda           3.9996e-007       0.0042668      0.00081838      0.00081838
v  TempC                       21          73.144           21.48           21.48
v  TurbVisc           2.2352e-014       0.0050288      0.00095252      0.00095252
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              540:        0.30650E+01

===============================================================


 INSTANT    0.541000000E+03   TIME STEP NUMBER             541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83931E-02 0.88283E+00
   Friction velocity        uk    :  0.83931E-02 0.88283E+00
   Dimensionless distance   yplus :  0.67570E-01 0.71074E+01
   Friction thermal sca.    tstar : -0.17852E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50415E-01 0.53029E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59531E-02      33   0.51115E-03   0.32347E+01 0.11069E+03 
c  Velocity[X]                                      0.17495E+01 
c  Velocity[Y]                                      0.14852E+01 
c  Velocity[Z]                                      0.10793E-29 
c  Pressure     0.16107E-06     438   0.93027E-08   0.15877E+00 0.43759E+03 
c  nu_tilda     0.43072E-05      32   0.11365E-04   0.25312E-06 0.17313E+03 
c  TempC        0.25729E+02      29   0.53573E-03   0.73798E+01 0.29838E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1424          9.7402          4.5729          4.5729
v  Velocity[Y]             -4.025          7.1193        0.015662        0.015662
v  Velocity[Z]       -1.2529e-014     5.1021e-015     -1.489e-017     -1.489e-017
v  ǁVelocityǁ         0.0020279          9.7618          5.0352          5.0352
v  Pressure               -52.164          20.294          -3.174          -3.174
v  nu_tilda           4.0062e-007       0.0042668      0.00081901      0.00081901
v  TempC                       21          73.892           21.48           21.48
v  TurbVisc           2.2512e-014       0.0050288      0.00095329      0.00095329
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              541:        0.26440E+01

===============================================================


 INSTANT    0.542000000E+03   TIME STEP NUMBER             542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10166E-01 0.88391E+00
   Friction velocity        uk    :  0.10166E-01 0.88391E+00
   Dimensionless distance   yplus :  0.81846E-01 0.71161E+01
   Friction thermal sca.    tstar : -0.22617E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61066E-01 0.53094E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59572E-02      33   0.48572E-03   0.31853E+01 0.11004E+03 
c  Velocity[X]                                      0.17250E+01 
c  Velocity[Y]                                      0.14603E+01 
c  Velocity[Z]                                      0.16428E-29 
c  Pressure     0.19199E-06     266   0.98210E-08   0.19364E+00 0.26589E+03 
c  nu_tilda     0.43093E-05      32   0.12363E-04   0.25242E-06 0.17281E+03 
c  TempC        0.25742E+02      29   0.47292E-03   0.89186E+01 0.33338E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1465          9.7366          4.5729          4.5729
v  Velocity[Y]            -4.0296          7.1002        0.015716        0.015716
v  Velocity[Z]       -1.3143e-014     5.0622e-015    -1.4915e-017    -1.4915e-017
v  ǁVelocityǁ         0.0018351          9.7577          5.0359          5.0359
v  Pressure                -52.13          20.257         -3.1732         -3.1732
v  nu_tilda           4.0126e-007       0.0042668      0.00081966      0.00081966
v  TempC                       21          73.142          21.481          21.481
v  TurbVisc           2.2663e-014       0.0050288      0.00095405      0.00095405
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              542:        0.22860E+01

===============================================================


 INSTANT    0.543000000E+03   TIME STEP NUMBER             543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87041E-02 0.88311E+00
   Friction velocity        uk    :  0.87041E-02 0.88311E+00
   Dimensionless distance   yplus :  0.70074E-01 0.71096E+01
   Friction thermal sca.    tstar : -0.18832E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52283E-01 0.53046E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59612E-02      33   0.55460E-03   0.31807E+01 0.10982E+03 
c  Velocity[X]                                      0.17353E+01 
c  Velocity[Y]                                      0.14454E+01 
c  Velocity[Z]                                      0.11082E-29 
c  Pressure     0.17177E-06     456   0.97053E-08   0.16727E+00 0.32318E+03 
c  nu_tilda     0.43115E-05      32   0.11320E-04   0.25172E-06 0.17249E+03 
c  TempC        0.25755E+02      29   0.57474E-03   0.81153E+01 0.30695E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1507          9.7331          4.5729          4.5729
v  Velocity[Y]            -4.0339          7.1205        0.015769        0.015769
v  Velocity[Z]       -1.3251e-014     5.0104e-015    -1.4944e-017    -1.4944e-017
v  ǁVelocityǁ         0.0019315          9.7537          5.0365          5.0365
v  Pressure               -52.172          20.277         -3.2015         -3.2015
v  nu_tilda            4.019e-007       0.0042668       0.0008203       0.0008203
v  TempC                       21          73.589          21.482          21.482
v  TurbVisc           2.2808e-014       0.0050289      0.00095482      0.00095482
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              543:        0.27500E+01

===============================================================


 INSTANT    0.544000000E+03   TIME STEP NUMBER             544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81517E-02 0.88444E+00
   Friction velocity        uk    :  0.81517E-02 0.88444E+00
   Dimensionless distance   yplus :  0.65627E-01 0.71203E+01
   Friction thermal sca.    tstar : -0.22172E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48965E-01 0.53126E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59653E-02      33   0.53773E-03   0.31972E+01 0.10994E+03 
c  Velocity[X]                                      0.17466E+01 
c  Velocity[Y]                                      0.14507E+01 
c  Velocity[Z]                                      0.10835E-29 
c  Pressure     0.16867E-06     281   0.98922E-08   0.16844E+00 0.22909E+03 
c  nu_tilda     0.43137E-05      32   0.12386E-04   0.25102E-06 0.17217E+03 
c  TempC        0.25768E+02      29   0.50635E-03   0.77423E+01 0.30988E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1551          9.7295          4.5729          4.5729
v  Velocity[Y]            -4.0382          7.1002        0.015822        0.015822
v  Velocity[Z]       -1.3024e-014     4.9837e-015    -1.4963e-017    -1.4963e-017
v  ǁVelocityǁ         0.0017976          9.7497          5.0371          5.0371
v  Pressure               -52.144          20.251         -3.2009         -3.2009
v  nu_tilda           4.0264e-007       0.0042668      0.00082095      0.00082095
v  TempC                       21           73.14          21.482          21.482
v  TurbVisc           2.2952e-014       0.0050289      0.00095558      0.00095558
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              544:        0.19140E+01

===============================================================


 INSTANT    0.545000000E+03   TIME STEP NUMBER             545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66795E-02 0.88373E+00
   Friction velocity        uk    :  0.66795E-02 0.88373E+00
   Dimensionless distance   yplus :  0.53775E-01 0.71146E+01
   Friction thermal sca.    tstar : -0.19248E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40122E-01 0.53083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59694E-02      33   0.40811E-03   0.31494E+01 0.10945E+03 
c  Velocity[X]                                      0.17152E+01 
c  Velocity[Y]                                      0.14342E+01 
c  Velocity[Z]                                      0.12904E-29 
c  Pressure     0.14535E-06     409   0.94287E-08   0.14297E+00 0.41644E+03 
c  nu_tilda     0.43159E-05      32   0.11286E-04   0.25033E-06 0.17186E+03 
c  TempC        0.25781E+02      29   0.96638E-03   0.90460E+01 0.33022E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1593          9.7262          4.5729          4.5729
v  Velocity[Y]            -4.0423          7.1241        0.015876        0.015876
v  Velocity[Z]       -1.2494e-014     4.9683e-015    -1.4977e-017    -1.4977e-017
v  ǁVelocityǁ           0.00196          9.7458          5.0377          5.0377
v  Pressure                -52.18          20.315         -3.2165         -3.2165
v  nu_tilda           4.0339e-007       0.0042669      0.00082158      0.00082158
v  TempC                       21          73.139          21.483          21.483
v  TurbVisc           2.3122e-014       0.0050289      0.00095634      0.00095634
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              545:        0.23530E+01

===============================================================


 INSTANT    0.546000000E+03   TIME STEP NUMBER             546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87800E-02 0.88467E+00
   Friction velocity        uk    :  0.87800E-02 0.88467E+00
   Dimensionless distance   yplus :  0.70685E-01 0.71222E+01
   Friction thermal sca.    tstar : -0.25469E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52739E-01 0.53139E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59735E-02      33   0.52953E-03   0.31028E+01 0.10887E+03 
c  Velocity[X]                                      0.16806E+01 
c  Velocity[Y]                                      0.14222E+01 
c  Velocity[Z]                                      0.11877E-29 
c  Pressure     0.14778E-06     409   0.95427E-08   0.14600E+00 0.23986E+03 
c  nu_tilda     0.43180E-05      32   0.12412E-04   0.24964E-06 0.17154E+03 
c  TempC        0.25795E+02      30   0.67026E-03   0.19719E+02 0.46978E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1633          9.7229          4.5729          4.5729
v  Velocity[Y]            -4.0462          7.1297        0.015928        0.015928
v  Velocity[Z]       -1.1781e-014     4.9674e-015    -1.4983e-017    -1.4983e-017
v  ǁVelocityǁ         0.0019665           9.742          5.0383          5.0383
v  Pressure               -52.157          20.346         -3.2077         -3.2077
v  nu_tilda           4.0405e-007       0.0042669      0.00082223      0.00082223
v  TempC                       21          73.265          21.483          21.483
v  TurbVisc           2.3295e-014       0.0050289       0.0009571       0.0009571
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              546:        0.22540E+01

===============================================================


 INSTANT    0.547000000E+03   TIME STEP NUMBER             547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94190E-02 0.88401E+00
   Friction velocity        uk    :  0.94190E-02 0.88401E+00
   Dimensionless distance   yplus :  0.75829E-01 0.71169E+01
   Friction thermal sca.    tstar : -0.33626E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56577E-01 0.53100E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59776E-02      33   0.55904E-03   0.31594E+01 0.10915E+03 
c  Velocity[X]                                      0.17277E+01 
c  Velocity[Y]                                      0.14318E+01 
c  Velocity[Z]                                      0.10284E-29 
c  Pressure     0.18276E-06     474   0.98531E-08   0.18087E+00 0.67029E+03 
c  nu_tilda     0.43202E-05      32   0.11242E-04   0.24897E-06 0.17123E+03 
c  TempC        0.25808E+02      29   0.49393E-03   0.99709E+01 0.35193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1672          9.7197          4.5729          4.5729
v  Velocity[Y]            -4.0498          7.0948        0.015982        0.015982
v  Velocity[Z]       -1.1117e-014     4.9702e-015    -1.4996e-017    -1.4996e-017
v  ǁVelocityǁ         0.0018917          9.7382           5.039           5.039
v  Pressure               -52.187          20.224         -3.2568         -3.2568
v  nu_tilda            4.048e-007       0.0042669      0.00082286      0.00082286
v  TempC                       21            73.8          21.484          21.484
v  TurbVisc           2.3448e-014        0.005029      0.00095787      0.00095787
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              547:        0.24370E+01

===============================================================


 INSTANT    0.548000000E+03   TIME STEP NUMBER             548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52744E-02 0.88281E+00
   Friction velocity        uk    :  0.52744E-02 0.88281E+00
   Dimensionless distance   yplus :  0.42463E-01 0.71072E+01
   Friction thermal sca.    tstar : -0.22708E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31682E-01 0.53028E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59817E-02      33   0.50825E-03   0.31390E+01 0.10901E+03 
c  Velocity[X]                                      0.17164E+01 
c  Velocity[Y]                                      0.14226E+01 
c  Velocity[Z]                                      0.12178E-29 
c  Pressure     0.14979E-06     469   0.94968E-08   0.14782E+00 0.57206E+03 
c  nu_tilda     0.43223E-05      32   0.12443E-04   0.24828E-06 0.17092E+03 
c  TempC        0.25821E+02      29   0.54153E-03   0.77664E+01 0.31349E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1708          9.7166          4.5729          4.5729
v  Velocity[Y]            -4.0534          7.1165        0.016033        0.016033
v  Velocity[Z]       -1.0198e-014     4.9643e-015    -1.5009e-017    -1.5009e-017
v  ǁVelocityǁ         0.0019047          9.7346          5.0396          5.0396
v  Pressure                -52.17          20.339          -3.234          -3.234
v  nu_tilda           4.0556e-007       0.0042669      0.00082351      0.00082351
v  TempC                       21          73.135          21.484          21.484
v  TurbVisc           2.3623e-014        0.005029      0.00095863      0.00095863
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              548:        0.33700E+01

===============================================================


 INSTANT    0.549000000E+03   TIME STEP NUMBER             549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87074E-02 0.88417E+00
   Friction velocity        uk    :  0.87074E-02 0.88417E+00
   Dimensionless distance   yplus :  0.70100E-01 0.71182E+01
   Friction thermal sca.    tstar : -0.36531E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52303E-01 0.53110E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59857E-02      33   0.52013E-03   0.30924E+01 0.10843E+03 
c  Velocity[X]                                      0.16940E+01 
c  Velocity[Y]                                      0.13985E+01 
c  Velocity[Z]                                      0.15037E-29 
c  Pressure     0.16286E-06     469   0.92390E-08   0.16225E+00 0.50512E+03 
c  nu_tilda     0.43245E-05      32   0.11195E-04   0.24761E-06 0.17060E+03 
c  TempC        0.25834E+02      29   0.52613E-03   0.77135E+01 0.31765E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1745          9.7136          4.5729          4.5729
v  Velocity[Y]            -4.0568          7.1002        0.016086        0.016086
v  Velocity[Z]       -9.8668e-015     6.2925e-015    -1.4992e-017    -1.4992e-017
v  ǁVelocityǁ         0.0018844           9.731          5.0402          5.0402
v  Pressure               -52.195          20.254         -3.2747         -3.2747
v  nu_tilda           4.0629e-007        0.004267      0.00082414      0.00082414
v  TempC                       21          73.454          21.485          21.485
v  TurbVisc             2.38e-014        0.005029      0.00095939      0.00095939
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              549:        0.39040E+01

===============================================================


 INSTANT    0.550000000E+03   TIME STEP NUMBER             550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60301E-02 0.88374E+00
   Friction velocity        uk    :  0.60301E-02 0.88374E+00
   Dimensionless distance   yplus :  0.48546E-01 0.71147E+01
   Friction thermal sca.    tstar : -0.29254E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36221E-01 0.53084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59898E-02      33   0.48884E-03   0.30723E+01 0.10808E+03 
c  Velocity[X]                                      0.16758E+01 
c  Velocity[Y]                                      0.13965E+01 
c  Velocity[Z]                                      0.12653E-29 
c  Pressure     0.15698E-06     457   0.97312E-08   0.15489E+00 0.71831E+03 
c  nu_tilda     0.43266E-05      32   0.12461E-04   0.24693E-06 0.17029E+03 
c  TempC        0.25847E+02      29   0.51000E-03   0.91823E+01 0.31927E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.178          9.7108          4.5729          4.5729
v  Velocity[Y]            -4.0598          7.1249        0.016137        0.016137
v  Velocity[Z]       -9.8517e-015     6.1419e-015    -1.4998e-017    -1.4998e-017
v  ǁVelocityǁ         0.0019477          9.7276          5.0408          5.0408
v  Pressure               -52.177          20.395         -3.2445         -3.2445
v  nu_tilda           4.0698e-007        0.004267      0.00082479      0.00082479
v  TempC                       21          73.285          21.485          21.485
v  TurbVisc           2.3973e-014        0.005029      0.00096015      0.00096015
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              550:        0.32600E+01

===============================================================


 INSTANT    0.551000000E+03   TIME STEP NUMBER             551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76055E-02 0.88481E+00
   Friction velocity        uk    :  0.76055E-02 0.88481E+00
   Dimensionless distance   yplus :  0.61229E-01 0.71233E+01
   Friction thermal sca.    tstar : -0.41708E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45684E-01 0.53148E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59939E-02      33   0.51108E-03   0.30446E+01 0.10774E+03 
c  Velocity[X]                                      0.16624E+01 
c  Velocity[Y]                                      0.13822E+01 
c  Velocity[Z]                                      0.14314E-29 
c  Pressure     0.16619E-06     469   0.96292E-08   0.16121E+00 0.52710E+03 
c  nu_tilda     0.43288E-05      32   0.11154E-04   0.24626E-06 0.16999E+03 
c  TempC        0.25861E+02      28   0.52598E-03   0.70906E+01 0.29526E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1819          9.7082          4.5729          4.5729
v  Velocity[Y]            -4.0628          7.1258         0.01619         0.01619
v  Velocity[Z]       -8.6124e-015      7.659e-015    -1.4986e-017    -1.4986e-017
v  ǁVelocityǁ          0.001918          9.7246          5.0414          5.0414
v  Pressure               -52.208          20.312         -3.2883         -3.2883
v  nu_tilda           4.0762e-007        0.004267      0.00082542      0.00082542
v  TempC                       21          73.566          21.486          21.486
v  TurbVisc           2.4135e-014       0.0050291      0.00096092      0.00096092
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              551:        0.38380E+01

===============================================================


 INSTANT    0.552000000E+03   TIME STEP NUMBER             552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70104E-02 0.88450E+00
   Friction velocity        uk    :  0.70104E-02 0.88450E+00
   Dimensionless distance   yplus :  0.56438E-01 0.71209E+01
   Friction thermal sca.    tstar : -0.42986E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42109E-01 0.53130E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59980E-02      33   0.54616E-03   0.30728E+01 0.10781E+03 
c  Velocity[X]                                      0.17068E+01 
c  Velocity[Y]                                      0.13660E+01 
c  Velocity[Z]                                      0.13625E-29 
c  Pressure     0.17973E-06     346   0.99072E-08   0.17994E+00 0.23404E+03 
c  nu_tilda     0.43309E-05      32   0.12484E-04   0.24559E-06 0.16968E+03 
c  TempC        0.25874E+02      29   0.49269E-03   0.74562E+01 0.30244E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1855          9.7057          4.5729          4.5729
v  Velocity[Y]            -4.0658          7.1008        0.016241        0.016241
v  Velocity[Z]       -8.6075e-015     7.4785e-015    -1.4998e-017    -1.4998e-017
v  ǁVelocityǁ         0.0017869          9.7217           5.042           5.042
v  Pressure               -52.184          20.282         -3.2915         -3.2915
v  nu_tilda           4.0827e-007        0.004267      0.00082607      0.00082607
v  TempC                       21          73.891          21.487          21.487
v  TurbVisc           2.4287e-014       0.0050291      0.00096168      0.00096168
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              552:        0.30050E+01

===============================================================


 INSTANT    0.553000000E+03   TIME STEP NUMBER             553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44124E-02 0.88343E+00
   Friction velocity        uk    :  0.44124E-02 0.88343E+00
   Dimensionless distance   yplus :  0.35523E-01 0.71122E+01
   Friction thermal sca.    tstar : -0.72236E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26504E-01 0.53065E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60021E-02      33   0.52120E-03   0.30481E+01 0.10760E+03 
c  Velocity[X]                                      0.16720E+01 
c  Velocity[Y]                                      0.13761E+01 
c  Velocity[Z]                                      0.13713E-29 
c  Pressure     0.16580E-06     392   0.93659E-08   0.16351E+00 0.49314E+03 
c  nu_tilda     0.43331E-05      32   0.11120E-04   0.24492E-06 0.16937E+03 
c  TempC        0.25887E+02      28   0.75958E-03   0.79262E+01 0.30162E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1891          9.7033          4.5729          4.5729
v  Velocity[Y]            -4.0681          7.1234        0.016293        0.016293
v  Velocity[Z]       -7.7138e-015     9.8231e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ         0.0019248           9.719          5.0426          5.0426
v  Pressure               -52.217          20.364         -3.3012         -3.3012
v  nu_tilda           4.0887e-007        0.004267       0.0008267       0.0008267
v  TempC                       21          73.128          21.487          21.487
v  TurbVisc           2.4444e-014       0.0050291      0.00096244      0.00096244
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              553:        0.33310E+01

===============================================================


 INSTANT    0.554000000E+03   TIME STEP NUMBER             554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73859E-02 0.88445E+00
   Friction velocity        uk    :  0.73859E-02 0.88445E+00
   Dimensionless distance   yplus :  0.59461E-01 0.71204E+01
   Friction thermal sca.    tstar : -0.24580E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44365E-01 0.53126E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60063E-02      33   0.47867E-03   0.30151E+01 0.10720E+03 
c  Velocity[X]                                      0.16447E+01 
c  Velocity[Y]                                      0.13704E+01 
c  Velocity[Z]                                      0.11647E-29 
c  Pressure     0.14109E-06     425   0.91321E-08   0.14084E+00 0.36311E+03 
c  nu_tilda     0.43352E-05      32   0.12503E-04   0.24426E-06 0.16907E+03 
c  TempC        0.25900E+02      28   0.94253E-03   0.76709E+01 0.30095E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1924          9.7012          4.5729          4.5729
v  Velocity[Y]            -4.0708           7.103        0.016343        0.016343
v  Velocity[Z]       -7.5043e-015     1.1189e-014     -1.495e-017     -1.495e-017
v  ǁVelocityǁ         0.0017873          9.7165          5.0433          5.0433
v  Pressure               -52.191          20.304         -3.3117         -3.3117
v  nu_tilda           4.0944e-007       0.0042671      0.00082735      0.00082735
v  TempC                       21          73.126          21.488          21.488
v  TurbVisc           2.4586e-014       0.0050291       0.0009632       0.0009632
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              554:        0.27320E+01

===============================================================


 INSTANT    0.555000000E+03   TIME STEP NUMBER             555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60626E-02 0.88349E+00
   Friction velocity        uk    :  0.60626E-02 0.88349E+00
   Dimensionless distance   yplus :  0.48808E-01 0.71127E+01
   Friction thermal sca.    tstar : -0.26288E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36416E-01 0.53068E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60104E-02      33   0.54455E-03   0.30176E+01 0.10687E+03 
c  Velocity[X]                                      0.16732E+01 
c  Velocity[Y]                                      0.13444E+01 
c  Velocity[Z]                                      0.10931E-29 
c  Pressure     0.22885E-06     330   0.93566E-08   0.22100E+00 0.44879E+03 
c  nu_tilda     0.43373E-05      32   0.11066E-04   0.24361E-06 0.16876E+03 
c  TempC        0.25913E+02      29   0.51216E-03   0.18643E+02 0.44340E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.196          9.6993          4.5729          4.5729
v  Velocity[Y]             -4.073          7.1236        0.016395        0.016395
v  Velocity[Z]        -7.444e-015     1.0759e-014    -1.4948e-017    -1.4948e-017
v  ǁVelocityǁ         0.0019051          9.7141          5.0439          5.0439
v  Pressure               -52.215          20.364         -3.3195         -3.3195
v  nu_tilda           4.1001e-007       0.0042671      0.00082798      0.00082798
v  TempC                       21          73.212          21.488          21.488
v  TurbVisc           2.4725e-014       0.0050292      0.00096396      0.00096396
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              555:        0.25010E+01

===============================================================


 INSTANT    0.556000000E+03   TIME STEP NUMBER             556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61093E-02 0.88483E+00
   Friction velocity        uk    :  0.61093E-02 0.88483E+00
   Dimensionless distance   yplus :  0.49184E-01 0.71235E+01
   Friction thermal sca.    tstar : -0.20250E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36697E-01 0.53149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60145E-02      33   0.51934E-03   0.30333E+01 0.10709E+03 
c  Velocity[X]                                      0.16761E+01 
c  Velocity[Y]                                      0.13571E+01 
c  Velocity[Z]                                      0.11505E-29 
c  Pressure     0.14235E-06     424   0.98240E-08   0.14204E+00 0.35050E+03 
c  nu_tilda     0.43395E-05      32   0.12532E-04   0.24295E-06 0.16846E+03 
c  TempC        0.25926E+02      29   0.37334E-03   0.76271E+01 0.30032E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.199          9.6976          4.5729          4.5729
v  Velocity[Y]            -4.0754          7.1009        0.016445        0.016445
v  Velocity[Z]       -6.9287e-015     1.1228e-014    -1.4929e-017    -1.4929e-017
v  ǁVelocityǁ         0.0017825          9.7118          5.0445          5.0445
v  Pressure               -52.195           20.31          -3.332          -3.332
v  nu_tilda           4.1054e-007       0.0042671      0.00082862      0.00082862
v  TempC                       21          73.498          21.489          21.489
v  TurbVisc           2.4861e-014       0.0050292      0.00096472      0.00096472
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              556:        0.32320E+01

===============================================================


 INSTANT    0.557000000E+03   TIME STEP NUMBER             557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48788E-02 0.88408E+00
   Friction velocity        uk    :  0.48788E-02 0.88408E+00
   Dimensionless distance   yplus :  0.39277E-01 0.71175E+01
   Friction thermal sca.    tstar : -0.21213E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29305E-01 0.53104E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60186E-02      33   0.39110E-03   0.29757E+01 0.10652E+03 
c  Velocity[X]                                      0.16424E+01 
c  Velocity[Y]                                      0.13333E+01 
c  Velocity[Z]                                      0.13112E-29 
c  Pressure     0.12914E-06     394   0.98467E-08   0.12721E+00 0.47440E+03 
c  nu_tilda     0.43416E-05      32   0.11022E-04   0.24230E-06 0.16816E+03 
c  TempC        0.25940E+02      29   0.54971E-03   0.73060E+01 0.29347E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2021          9.6961          4.5729          4.5729
v  Velocity[Y]            -4.0774          7.1268        0.016496        0.016496
v  Velocity[Z]       -6.9287e-015     1.1902e-014    -1.4901e-017    -1.4901e-017
v  ǁVelocityǁ         0.0019431          9.7097          5.0451          5.0451
v  Pressure                -52.23          20.395         -3.3444         -3.3444
v  nu_tilda           4.1101e-007       0.0042671      0.00082925      0.00082925
v  TempC                       21          73.122          21.489          21.489
v  TurbVisc           2.4991e-014       0.0050292      0.00096548      0.00096548
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              557:        0.30270E+01

===============================================================


 INSTANT    0.558000000E+03   TIME STEP NUMBER             558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82223E-02 0.88498E+00
   Friction velocity        uk    :  0.82223E-02 0.88498E+00
   Dimensionless distance   yplus :  0.66195E-01 0.71247E+01
   Friction thermal sca.    tstar : -0.15313E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49389E-01 0.53158E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60227E-02      33   0.54059E-03   0.29306E+01 0.10577E+03 
c  Velocity[X]                                      0.16209E+01 
c  Velocity[Y]                                      0.13098E+01 
c  Velocity[Z]                                      0.13340E-29 
c  Pressure     0.20547E-06     457   0.97389E-08   0.20374E+00 0.46613E+03 
c  nu_tilda     0.43437E-05      32   0.12561E-04   0.24166E-06 0.16786E+03 
c  TempC        0.25953E+02      29   0.43825E-03   0.88998E+01 0.32408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2053          9.6948          4.5729          4.5729
v  Velocity[Y]            -4.0792          7.1341        0.016546        0.016546
v  Velocity[Z]       -7.4723e-015     1.2855e-014     -1.487e-017     -1.487e-017
v  ǁVelocityǁ         0.0018806          9.7079          5.0457          5.0457
v  Pressure                -52.19          20.448         -3.3193         -3.3193
v  nu_tilda           4.1146e-007       0.0042671       0.0008299       0.0008299
v  TempC                       21          73.296           21.49           21.49
v  TurbVisc           2.5107e-014       0.0050292      0.00096624      0.00096624
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              558:        0.34400E+01

===============================================================


 INSTANT    0.559000000E+03   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92006E-02 0.88448E+00
   Friction velocity        uk    :  0.92006E-02 0.88448E+00
   Dimensionless distance   yplus :  0.74071E-01 0.71206E+01
   Friction thermal sca.    tstar : -0.14395E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55265E-01 0.53128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60268E-02      33   0.52823E-03   0.29621E+01 0.10611E+03 
c  Velocity[X]                                      0.16329E+01 
c  Velocity[Y]                                      0.13292E+01 
c  Velocity[Z]                                      0.12321E-29 
c  Pressure     0.14360E-06     501   0.95722E-08   0.14433E+00 0.92059E+03 
c  nu_tilda     0.43458E-05      32   0.10971E-04   0.24102E-06 0.16756E+03 
c  TempC        0.25966E+02      28   0.48393E-03   0.74990E+01 0.30436E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2085          9.6936          4.5729          4.5729
v  Velocity[Y]             -4.081          7.0989        0.016596        0.016596
v  Velocity[Z]       -6.9287e-015     1.2204e-014     -1.485e-017     -1.485e-017
v  ǁVelocityǁ         0.0018777          9.7062          5.0463          5.0463
v  Pressure               -52.231            20.3         -3.3856         -3.3856
v  nu_tilda             4.12e-007       0.0042672      0.00083053      0.00083053
v  TempC                       21          73.461          21.491          21.491
v  TurbVisc           2.5216e-014       0.0050292        0.000967        0.000967
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              559:        0.31220E+01

===============================================================


 INSTANT    0.560000000E+03   TIME STEP NUMBER             560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14442E-02 0.88305E+00
   Friction velocity        uk    :  0.14442E-02 0.88305E+00
   Dimensionless distance   yplus :  0.11627E-01 0.71091E+01
   Friction thermal sca.    tstar : -0.14690E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86752E-02 0.53042E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60309E-02      33   0.48156E-03   0.29470E+01 0.10585E+03 
c  Velocity[X]                                      0.16295E+01 
c  Velocity[Y]                                      0.13175E+01 
c  Velocity[Z]                                      0.13922E-29 
c  Pressure     0.17569E-06     473   0.96493E-08   0.17200E+00 0.75329E+03 
c  nu_tilda     0.43479E-05      32   0.12594E-04   0.24037E-06 0.16726E+03 
c  TempC        0.25979E+02      28   0.39373E-03   0.67601E+01 0.29185E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2117          9.6928          4.5729          4.5729
v  Velocity[Y]            -4.0826          7.1199        0.016645        0.016645
v  Velocity[Z]       -6.9287e-015     1.3261e-014    -1.4801e-017    -1.4801e-017
v  ǁVelocityǁ         0.0018202          9.7048          5.0469          5.0469
v  Pressure               -52.203          20.434         -3.3507         -3.3507
v  nu_tilda            4.125e-007       0.0042672      0.00083118      0.00083118
v  TempC                       21          73.117          21.491          21.491
v  TurbVisc           2.5348e-014       0.0050293      0.00096776      0.00096776
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              560:        0.29230E+01

===============================================================


 INSTANT    0.561000000E+03   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67941E-02 0.88449E+00
   Friction velocity        uk    :  0.67941E-02 0.88449E+00
   Dimensionless distance   yplus :  0.54697E-01 0.71207E+01
   Friction thermal sca.    tstar : -0.12921E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40810E-01 0.53128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60351E-02      33   0.50950E-03   0.29202E+01 0.10552E+03 
c  Velocity[X]                                      0.16233E+01 
c  Velocity[Y]                                      0.12969E+01 
c  Velocity[Z]                                      0.10328E-29 
c  Pressure     0.15731E-06     488   0.97254E-08   0.15836E+00 0.59031E+03 
c  nu_tilda     0.43501E-05      32   0.10937E-04   0.23973E-06 0.16696E+03 
c  TempC        0.25992E+02      28   0.47258E-03   0.86664E+01 0.30945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2146          9.6922          4.5729          4.5729
v  Velocity[Y]            -4.0837          7.1055        0.016696        0.016696
v  Velocity[Z]       -6.9287e-015      1.325e-014    -1.4786e-017    -1.4786e-017
v  ǁVelocityǁ          0.001878          9.7036          5.0475          5.0475
v  Pressure               -52.238          20.345         -3.3995         -3.3995
v  nu_tilda             4.13e-007       0.0042672      0.00083181      0.00083181
v  TempC                       21          73.148          21.492          21.492
v  TurbVisc           2.5471e-014       0.0050293      0.00096852      0.00096852
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              561:        0.29850E+01

===============================================================


 INSTANT    0.562000000E+03   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36484E-02 0.88358E+00
   Friction velocity        uk    :  0.36484E-02 0.88358E+00
   Dimensionless distance   yplus :  0.29372E-01 0.71134E+01
   Friction thermal sca.    tstar : -0.12533E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21915E-01 0.53074E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60392E-02      33   0.47407E-03   0.29171E+01 0.10533E+03 
c  Velocity[X]                                      0.16091E+01 
c  Velocity[Y]                                      0.13080E+01 
c  Velocity[Z]                                      0.11876E-29 
c  Pressure     0.16468E-06     469   0.96295E-08   0.16212E+00 0.65886E+03 
c  nu_tilda     0.43522E-05      32   0.12614E-04   0.23910E-06 0.16667E+03 
c  TempC        0.26005E+02      29   0.40839E-03   0.72411E+01 0.29844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2175          9.6919          4.5729          4.5729
v  Velocity[Y]            -4.0851          7.1265        0.016744        0.016744
v  Velocity[Z]       -6.9287e-015     1.4651e-014    -1.4753e-017    -1.4753e-017
v  ǁVelocityǁ         0.0018495          9.7026          5.0481          5.0481
v  Pressure                -52.21          20.461         -3.3686         -3.3686
v  nu_tilda           4.1353e-007       0.0042672      0.00083245      0.00083245
v  TempC                       21          73.646          21.493          21.493
v  TurbVisc           2.5596e-014       0.0050293      0.00096928      0.00096928
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              562:        0.29040E+01

===============================================================


 INSTANT    0.563000000E+03   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82607E-02 0.88477E+00
   Friction velocity        uk    :  0.82607E-02 0.88477E+00
   Dimensionless distance   yplus :  0.66504E-01 0.71230E+01
   Friction thermal sca.    tstar : -0.11423E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49620E-01 0.53146E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60433E-02      33   0.50635E-03   0.28770E+01 0.10485E+03 
c  Velocity[X]                                      0.15945E+01 
c  Velocity[Y]                                      0.12825E+01 
c  Velocity[Z]                                      0.12009E-29 
c  Pressure     0.15969E-06     473   0.95411E-08   0.15633E+00 0.35789E+03 
c  nu_tilda     0.43543E-05      32   0.10906E-04   0.23848E-06 0.16637E+03 
c  TempC        0.26018E+02      29   0.56141E-03   0.10009E+02 0.35024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2202          9.6917          4.5729          4.5729
v  Velocity[Y]            -4.0862          7.1259        0.016794        0.016794
v  Velocity[Z]       -6.9287e-015      1.469e-014    -1.4725e-017    -1.4725e-017
v  ǁVelocityǁ         0.0019461          9.7018          5.0487          5.0487
v  Pressure               -52.242          20.431         -3.4042         -3.4042
v  nu_tilda           4.1405e-007       0.0042672      0.00083308      0.00083308
v  TempC                       21          73.112          21.493          21.493
v  TurbVisc           2.5729e-014       0.0050293      0.00097004      0.00097004
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              563:        0.28910E+01

===============================================================


 INSTANT    0.564000000E+03   TIME STEP NUMBER             564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77204E-02 0.88438E+00
   Friction velocity        uk    :  0.77204E-02 0.88438E+00
   Dimensionless distance   yplus :  0.62154E-01 0.71198E+01
   Friction thermal sca.    tstar : -0.22624E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46374E-01 0.53122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60475E-02      33   0.52808E-03   0.29233E+01 0.10501E+03 
c  Velocity[X]                                      0.16572E+01 
c  Velocity[Y]                                      0.12662E+01 
c  Velocity[Z]                                      0.11492E-29 
c  Pressure     0.17608E-06     376   0.96046E-08   0.17799E+00 0.23747E+03 
c  nu_tilda     0.43564E-05      32   0.12642E-04   0.23785E-06 0.16608E+03 
c  TempC        0.26032E+02      28   0.63363E-03   0.80672E+01 0.31804E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2229          9.6918          4.5729          4.5729
v  Velocity[Y]            -4.0868          7.1026        0.016842        0.016842
v  Velocity[Z]       -6.9287e-015     1.3038e-014    -1.4726e-017    -1.4726e-017
v  ǁVelocityǁ          0.001796          9.7014          5.0493          5.0493
v  Pressure               -52.207          20.399            -3.4            -3.4
v  nu_tilda           4.1458e-007       0.0042672      0.00083372      0.00083372
v  TempC                       21           73.11          21.494          21.494
v  TurbVisc           2.5856e-014       0.0050294      0.00097079      0.00097079
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              564:        0.25990E+01

===============================================================


 INSTANT    0.565000000E+03   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57112E-02 0.88344E+00
   Friction velocity        uk    :  0.57112E-02 0.88344E+00
   Dimensionless distance   yplus :  0.45979E-01 0.71123E+01
   Friction thermal sca.    tstar : -0.10779E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34306E-01 0.53066E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60516E-02      33   0.47373E-03   0.28906E+01 0.10485E+03 
c  Velocity[X]                                      0.16089E+01 
c  Velocity[Y]                                      0.12817E+01 
c  Velocity[Z]                                      0.10801E-29 
c  Pressure     0.12459E-06     410   0.98197E-08   0.12322E+00 0.39902E+03 
c  nu_tilda     0.43585E-05      32   0.10855E-04   0.23724E-06 0.16579E+03 
c  TempC        0.26045E+02      29   0.59712E-03   0.80925E+01 0.30508E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2254          9.6922          4.5729          4.5729
v  Velocity[Y]            -4.0876          7.1249         0.01689         0.01689
v  Velocity[Z]       -6.9287e-015      1.251e-014     -1.471e-017     -1.471e-017
v  ǁVelocityǁ         0.0019409          9.7011          5.0499          5.0499
v  Pressure               -52.244          20.465         -3.4174         -3.4174
v  nu_tilda            4.151e-007       0.0042673      0.00083435      0.00083435
v  TempC                       21          73.704          21.494          21.494
v  TurbVisc           2.5991e-014       0.0050294      0.00097155      0.00097155
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              565:        0.27000E+01

===============================================================


 INSTANT    0.566000000E+03   TIME STEP NUMBER             566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80903E-02 0.88445E+00
   Friction velocity        uk    :  0.80903E-02 0.88445E+00
   Dimensionless distance   yplus :  0.65132E-01 0.71204E+01
   Friction thermal sca.    tstar : -0.97444E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48596E-01 0.53126E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60557E-02      33   0.45943E-03   0.28557E+01 0.10423E+03 
c  Velocity[X]                                      0.15981E+01 
c  Velocity[Y]                                      0.12576E+01 
c  Velocity[Z]                                      0.11626E-29 
c  Pressure     0.14574E-06     346   0.95701E-08   0.14731E+00 0.27472E+03 
c  nu_tilda     0.43606E-05      32   0.12663E-04   0.23663E-06 0.16550E+03 
c  TempC        0.26058E+02      29   0.52192E-03   0.91121E+01 0.30807E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2278          9.6928          4.5729          4.5729
v  Velocity[Y]            -4.0883          7.1059        0.016938        0.016938
v  Velocity[Z]       -6.9287e-015     1.1734e-014    -1.4708e-017    -1.4708e-017
v  ǁVelocityǁ         0.0017764          9.7012          5.0505          5.0505
v  Pressure               -52.213          20.417         -3.4196         -3.4196
v  nu_tilda           4.1563e-007       0.0042673        0.000835        0.000835
v  TempC                       21          73.106          21.495          21.495
v  TurbVisc           2.6119e-014       0.0050294      0.00097231      0.00097231
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              566:        0.24930E+01

===============================================================


 INSTANT    0.567000000E+03   TIME STEP NUMBER             567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59746E-02 0.88361E+00
   Friction velocity        uk    :  0.59746E-02 0.88361E+00
   Dimensionless distance   yplus :  0.48100E-01 0.71136E+01
   Friction thermal sca.    tstar : -0.11417E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35888E-01 0.53076E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60599E-02      33   0.53076E-03   0.28520E+01 0.10405E+03 
c  Velocity[X]                                      0.16082E+01 
c  Velocity[Y]                                      0.12438E+01 
c  Velocity[Z]                                      0.11356E-29 
c  Pressure     0.17731E-06     437   0.93441E-08   0.17357E+00 0.32303E+03 
c  nu_tilda     0.43627E-05      32   0.10818E-04   0.23602E-06 0.16521E+03 
c  TempC        0.26071E+02      29   0.49273E-03   0.77896E+01 0.29916E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.23          9.6936          4.5729          4.5729
v  Velocity[Y]            -4.0885          7.1255        0.016986        0.016986
v  Velocity[Z]       -6.9287e-015     1.1389e-014    -1.4707e-017    -1.4707e-017
v  ǁVelocityǁ         0.0018873          9.7015          5.0511          5.0511
v  Pressure               -52.247          20.455         -3.4407         -3.4407
v  nu_tilda           4.1624e-007       0.0042673      0.00083562      0.00083562
v  TempC                       21          73.526          21.496          21.496
v  TurbVisc           2.6255e-014       0.0050294      0.00097307      0.00097307
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              567:        0.28010E+01

===============================================================


 INSTANT    0.568000000E+03   TIME STEP NUMBER             568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60556E-02 0.88486E+00
   Friction velocity        uk    :  0.60556E-02 0.88486E+00
   Dimensionless distance   yplus :  0.48751E-01 0.71237E+01
   Friction thermal sca.    tstar : -0.22648E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36374E-01 0.53151E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60640E-02      33   0.51174E-03   0.28798E+01 0.10424E+03 
c  Velocity[X]                                      0.16280E+01 
c  Velocity[Y]                                      0.12518E+01 
c  Velocity[Z]                                      0.11075E-29 
c  Pressure     0.13816E-06     282   0.98107E-08   0.13913E+00 0.22459E+03 
c  nu_tilda     0.43647E-05      32   0.12684E-04   0.23541E-06 0.16492E+03 
c  TempC        0.26084E+02      28   0.47344E-03   0.73946E+01 0.29862E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2328          9.6947          4.5729          4.5729
v  Velocity[Y]            -4.0889          7.1016        0.017032        0.017032
v  Velocity[Z]       -6.9287e-015     1.1239e-014    -1.4703e-017    -1.4703e-017
v  ǁVelocityǁ         0.0017547          9.7019          5.0517          5.0517
v  Pressure               -52.218          20.423         -3.4415         -3.4415
v  nu_tilda           4.1687e-007       0.0042673      0.00083627      0.00083627
v  TempC                       21          73.102          21.496          21.496
v  TurbVisc           2.6409e-014       0.0050294      0.00097382      0.00097382
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              568:        0.22840E+01

===============================================================


 INSTANT    0.569000000E+03   TIME STEP NUMBER             569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46473E-02 0.88399E+00
   Friction velocity        uk    :  0.46473E-02 0.88399E+00
   Dimensionless distance   yplus :  0.37414E-01 0.71167E+01
   Friction thermal sca.    tstar : -0.16271E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27915E-01 0.53099E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60681E-02      33   0.38148E-03   0.28311E+01 0.10376E+03 
c  Velocity[X]                                      0.15955E+01 
c  Velocity[Y]                                      0.12355E+01 
c  Velocity[Z]                                      0.10486E-29 
c  Pressure     0.12301E-06     409   0.93915E-08   0.12058E+00 0.44493E+03 
c  nu_tilda     0.43668E-05      32   0.10763E-04   0.23481E-06 0.16464E+03 
c  TempC        0.26097E+02      28   0.45893E-03   0.93247E+01 0.31964E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2352          9.6961          4.5729          4.5729
v  Velocity[Y]            -4.0889          7.1271        0.017081        0.017081
v  Velocity[Z]       -6.9287e-015     1.1229e-014    -1.4699e-017    -1.4699e-017
v  ǁVelocityǁ         0.0018885          9.7027          5.0523          5.0523
v  Pressure               -52.254          20.498         -3.4542         -3.4542
v  nu_tilda           4.1736e-007       0.0042673      0.00083689      0.00083689
v  TempC                       21          73.621          21.497          21.497
v  TurbVisc           2.6568e-014       0.0050295      0.00097458      0.00097458
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              569:        0.26590E+01

===============================================================


 INSTANT    0.570000000E+03   TIME STEP NUMBER             570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75447E-02 0.88500E+00
   Friction velocity        uk    :  0.75447E-02 0.88500E+00
   Dimensionless distance   yplus :  0.60740E-01 0.71249E+01
   Friction thermal sca.    tstar : -0.95434E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45319E-01 0.53160E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60723E-02      33   0.51800E-03   0.27808E+01 0.10314E+03 
c  Velocity[X]                                      0.15571E+01 
c  Velocity[Y]                                      0.12237E+01 
c  Velocity[Z]                                      0.12667E-29 
c  Pressure     0.15542E-06     437   0.98184E-08   0.15451E+00 0.31934E+03 
c  nu_tilda     0.43689E-05      32   0.12705E-04   0.23421E-06 0.16435E+03 
c  TempC        0.26110E+02      29   0.81936E-03   0.75667E+01 0.29152E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2375          9.6976          4.5729          4.5729
v  Velocity[Y]             -4.089          7.1291        0.017126        0.017126
v  Velocity[Z]       -6.9287e-015     1.1565e-014    -1.4711e-017    -1.4711e-017
v  ǁVelocityǁ         0.0018596          9.7037          5.0529          5.0529
v  Pressure               -52.221          20.542         -3.4386         -3.4386
v  nu_tilda           4.1771e-007       0.0042674      0.00083753      0.00083753
v  TempC                       21          73.099          21.497          21.497
v  TurbVisc           2.6693e-014       0.0050295      0.00097533      0.00097533
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              570:        0.33090E+01

===============================================================


 INSTANT    0.571000000E+03   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93889E-02 0.88433E+00
   Friction velocity        uk    :  0.93889E-02 0.88433E+00
   Dimensionless distance   yplus :  0.75587E-01 0.71194E+01
   Friction thermal sca.    tstar : -0.83041E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56397E-01 0.53119E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60765E-02      33   0.49005E-03   0.28129E+01 0.10335E+03 
c  Velocity[X]                                      0.15786E+01 
c  Velocity[Y]                                      0.12343E+01 
c  Velocity[Z]                                      0.10638E-29 
c  Pressure     0.14729E-06     488   0.93998E-08   0.14900E+00 0.53716E+03 
c  nu_tilda     0.43710E-05      32   0.10713E-04   0.23363E-06 0.16407E+03 
c  TempC        0.26123E+02      28   0.60222E-03   0.16034E+02 0.44048E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2395          9.6994          4.5729          4.5729
v  Velocity[Y]            -4.0889          7.1058        0.017173        0.017173
v  Velocity[Z]       -6.9287e-015     1.1046e-014    -1.4725e-017    -1.4725e-017
v  ǁVelocityǁ         0.0018606          9.7051          5.0535          5.0535
v  Pressure               -52.254          20.456         -3.4837         -3.4837
v  nu_tilda           4.1812e-007       0.0042674      0.00083816      0.00083816
v  TempC                       21          73.098          21.498          21.498
v  TurbVisc           2.6785e-014       0.0050295      0.00097609      0.00097609
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              571:        0.33580E+01

===============================================================


 INSTANT    0.572000000E+03   TIME STEP NUMBER             572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51960E-02 0.88283E+00
   Friction velocity        uk    :  0.51960E-02 0.88283E+00
   Dimensionless distance   yplus :  0.41831E-01 0.71074E+01
   Friction thermal sca.    tstar : -0.15222E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31211E-01 0.53029E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60806E-02      33   0.51302E-03   0.28015E+01 0.10309E+03 
c  Velocity[X]                                      0.15740E+01 
c  Velocity[Y]                                      0.12275E+01 
c  Velocity[Z]                                      0.12791E-29 
c  Pressure     0.18432E-06     441   0.96987E-08   0.18001E+00 0.44984E+03 
c  nu_tilda     0.43731E-05      32   0.12732E-04   0.23304E-06 0.16379E+03 
c  TempC        0.26136E+02      28   0.47500E-03   0.93513E+01 0.34329E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2415          9.7014          4.5729          4.5729
v  Velocity[Y]            -4.0885          7.1197        0.017219        0.017219
v  Velocity[Z]       -6.9287e-015     1.2319e-014    -1.4738e-017    -1.4738e-017
v  ǁVelocityǁ         0.0018163          9.7066          5.0541          5.0541
v  Pressure               -52.223          20.528         -3.4621         -3.4621
v  nu_tilda           4.1859e-007       0.0042674       0.0008388       0.0008388
v  TempC                       21          73.775          21.499          21.499
v  TurbVisc            2.689e-014       0.0050295      0.00097684      0.00097684
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              572:        0.28130E+01

===============================================================


 INSTANT    0.573000000E+03   TIME STEP NUMBER             573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73287E-02 0.88421E+00
   Friction velocity        uk    :  0.73287E-02 0.88421E+00
   Dimensionless distance   yplus :  0.59001E-01 0.71185E+01
   Friction thermal sca.    tstar : -0.12253E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44021E-01 0.53112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60848E-02      33   0.52871E-03   0.28086E+01 0.10307E+03 
c  Velocity[X]                                      0.15986E+01 
c  Velocity[Y]                                      0.12101E+01 
c  Velocity[Z]                                      0.11302E-29 
c  Pressure     0.14446E-06     473   0.96690E-08   0.14480E+00 0.49338E+03 
c  nu_tilda     0.43751E-05      32   0.10683E-04   0.23246E-06 0.16350E+03 
c  TempC        0.26150E+02      28   0.47438E-03   0.70210E+01 0.29017E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2434          9.7036          4.5729          4.5729
v  Velocity[Y]            -4.0881          7.1029        0.017265        0.017265
v  Velocity[Z]       -6.9287e-015     1.3065e-014    -1.4748e-017    -1.4748e-017
v  ǁVelocityǁ         0.0018693          9.7084          5.0547          5.0547
v  Pressure               -52.251          20.445         -3.5039         -3.5039
v  nu_tilda           4.1906e-007       0.0042674      0.00083943      0.00083943
v  TempC                       21          73.094          21.499          21.499
v  TurbVisc           2.7009e-014       0.0050295       0.0009776       0.0009776
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              573:        0.29480E+01

===============================================================


 INSTANT    0.574000000E+03   TIME STEP NUMBER             574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25715E-02 0.88363E+00
   Friction velocity        uk    :  0.25715E-02 0.88363E+00
   Dimensionless distance   yplus :  0.20702E-01 0.71138E+01
   Friction thermal sca.    tstar : -0.79963E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15446E-01 0.53077E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60889E-02      33   0.44997E-03   0.27916E+01 0.10276E+03 
c  Velocity[X]                                      0.15739E+01 
c  Velocity[Y]                                      0.12176E+01 
c  Velocity[Z]                                      0.10627E-29 
c  Pressure     0.16929E-06     489   0.97966E-08   0.16703E+00 0.94281E+03 
c  nu_tilda     0.43772E-05      32   0.12748E-04   0.23188E-06 0.16322E+03 
c  TempC        0.26163E+02      28   0.49193E-03   0.76369E+01 0.30371E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2456           9.706          4.5729          4.5729
v  Velocity[Y]            -4.0877          7.1235         0.01731         0.01731
v  Velocity[Z]       -6.9287e-015     1.3059e-014    -1.4773e-017    -1.4773e-017
v  ǁVelocityǁ         0.0019203          9.7104          5.0553          5.0553
v  Pressure               -52.219          20.621         -3.4598         -3.4598
v  nu_tilda            4.194e-007       0.0042674      0.00084007      0.00084007
v  TempC                       21          73.697            21.5            21.5
v  TurbVisc            2.713e-014       0.0050296      0.00097835      0.00097835
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              574:        0.29990E+01

===============================================================


 INSTANT    0.575000000E+03   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95613E-02 0.88469E+00
   Friction velocity        uk    :  0.95613E-02 0.88469E+00
   Dimensionless distance   yplus :  0.76975E-01 0.71223E+01
   Friction thermal sca.    tstar : -0.74632E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57432E-01 0.53141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60931E-02      33   0.51667E-03   0.27405E+01 0.10222E+03 
c  Velocity[X]                                      0.15442E+01 
c  Velocity[Y]                                      0.11963E+01 
c  Velocity[Z]                                      0.12948E-29 
c  Pressure     0.14529E-06     473   0.91238E-08   0.14285E+00 0.62879E+03 
c  nu_tilda     0.43793E-05      32   0.10638E-04   0.23132E-06 0.16295E+03 
c  TempC        0.26176E+02      28   0.75709E-03   0.83051E+01 0.29920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2473          9.7086          4.5729          4.5729
v  Velocity[Y]            -4.0869          7.1243        0.017355        0.017355
v  Velocity[Z]       -6.9287e-015     1.1464e-014    -1.4806e-017    -1.4806e-017
v  ǁVelocityǁ         0.0019548          9.7126          5.0559          5.0559
v  Pressure               -52.258          20.524         -3.5115         -3.5115
v  nu_tilda           4.1967e-007       0.0042674      0.00084069      0.00084069
v  TempC                       21          73.092            21.5            21.5
v  TurbVisc           2.7221e-014       0.0050296      0.00097911      0.00097911
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              575:        0.29160E+01

===============================================================


 INSTANT    0.576000000E+03   TIME STEP NUMBER             576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75245E-02 0.88433E+00
   Friction velocity        uk    :  0.75245E-02 0.88433E+00
   Dimensionless distance   yplus :  0.60578E-01 0.71195E+01
   Friction thermal sca.    tstar : -0.72777E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45198E-01 0.53119E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60972E-02      33   0.48254E-03   0.27880E+01 0.10249E+03 
c  Velocity[X]                                      0.16048E+01 
c  Velocity[Y]                                      0.11832E+01 
c  Velocity[Z]                                      0.11163E-29 
c  Pressure     0.15133E-06     362   0.95009E-08   0.15272E+00 0.19738E+03 
c  nu_tilda     0.43813E-05      32   0.12776E-04   0.23074E-06 0.16267E+03 
c  TempC        0.26189E+02      28   0.63950E-03   0.12059E+02 0.36549E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2494          9.7113          4.5729          4.5729
v  Velocity[Y]            -4.0859          7.1003          0.0174          0.0174
v  Velocity[Z]       -6.9287e-015      1.279e-014    -1.4816e-017    -1.4816e-017
v  ǁVelocityǁ         0.0018221          9.7151          5.0565          5.0565
v  Pressure               -52.227          20.509         -3.5074         -3.5074
v  nu_tilda           4.2002e-007       0.0042675      0.00084133      0.00084133
v  TempC                       21          73.089          21.501          21.501
v  TurbVisc            2.729e-014       0.0050296      0.00097986      0.00097986
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              576:        0.25220E+01

===============================================================


 INSTANT    0.577000000E+03   TIME STEP NUMBER             577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61807E-02 0.88327E+00
   Friction velocity        uk    :  0.61807E-02 0.88327E+00
   Dimensionless distance   yplus :  0.49759E-01 0.71109E+01
   Friction thermal sca.    tstar : -0.72381E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37126E-01 0.53056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61014E-02      33   0.46248E-03   0.27476E+01 0.10207E+03 
c  Velocity[X]                                      0.15529E+01 
c  Velocity[Y]                                      0.11947E+01 
c  Velocity[Z]                                      0.96627E-30 
c  Pressure     0.15663E-06     425   0.94000E-08   0.15542E+00 0.65374E+03 
c  nu_tilda     0.43834E-05      32   0.10613E-04   0.23018E-06 0.16239E+03 
c  TempC        0.26202E+02      28   0.66833E-03   0.94052E+01 0.32791E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2519          9.7142          4.5729          4.5729
v  Velocity[Y]            -4.0851          7.1231        0.017445        0.017445
v  Velocity[Z]       -6.9287e-015     1.3667e-014    -1.4829e-017    -1.4829e-017
v  ǁVelocityǁ         0.0019823          9.7177          5.0571          5.0571
v  Pressure               -52.251          20.622         -3.5046         -3.5046
v  nu_tilda            4.204e-007       0.0042675      0.00084196      0.00084196
v  TempC                       21           73.74          21.502          21.502
v  TurbVisc           2.7382e-014       0.0050296      0.00098061      0.00098061
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              577:        0.27290E+01

===============================================================


 INSTANT    0.578000000E+03   TIME STEP NUMBER             578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87087E-02 0.88422E+00
   Friction velocity        uk    :  0.87087E-02 0.88422E+00
   Dimensionless distance   yplus :  0.70111E-01 0.71185E+01
   Friction thermal sca.    tstar : -0.68560E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52310E-01 0.53112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61056E-02      33   0.46519E-03   0.27397E+01 0.10191E+03 
c  Velocity[X]                                      0.15529E+01 
c  Velocity[Y]                                      0.11868E+01 
c  Velocity[Z]                                      0.11895E-29 
c  Pressure     0.12820E-06     437   0.98317E-08   0.12990E+00 0.43865E+03 
c  nu_tilda     0.43854E-05      32   0.12796E-04   0.22962E-06 0.16212E+03 
c  TempC        0.26215E+02      29   0.50829E-03   0.83222E+01 0.30586E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2537          9.7173          4.5729          4.5729
v  Velocity[Y]            -4.0838          7.1034        0.017488        0.017488
v  Velocity[Z]       -6.9287e-015     1.2742e-014    -1.4846e-017    -1.4846e-017
v  ǁVelocityǁ         0.0018203          9.7204          5.0576          5.0576
v  Pressure               -52.231          20.548         -3.5213         -3.5213
v  nu_tilda           4.2076e-007       0.0042675      0.00084259      0.00084259
v  TempC                       21          73.416          21.502          21.502
v  TurbVisc           2.7479e-014       0.0050296      0.00098136      0.00098136
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              578:        0.26940E+01

===============================================================


 INSTANT    0.579000000E+03   TIME STEP NUMBER             579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72506E-02 0.88328E+00
   Friction velocity        uk    :  0.72506E-02 0.88328E+00
   Dimensionless distance   yplus :  0.58372E-01 0.71110E+01
   Friction thermal sca.    tstar : -0.68257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43552E-01 0.53056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61097E-02      33   0.52345E-03   0.27380E+01 0.10156E+03 
c  Velocity[X]                                      0.15753E+01 
c  Velocity[Y]                                      0.11626E+01 
c  Velocity[Z]                                      0.12271E-29 
c  Pressure     0.19726E-06     377   0.98372E-08   0.19146E+00 0.52347E+03 
c  nu_tilda     0.43875E-05      32   0.10556E-04   0.22907E-06 0.16184E+03 
c  TempC        0.26228E+02      28   0.50015E-03   0.91139E+01 0.30499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2557          9.7205          4.5729          4.5729
v  Velocity[Y]            -4.0824          7.1227        0.017532        0.017532
v  Velocity[Z]       -6.9287e-015     1.2581e-014    -1.4875e-017    -1.4875e-017
v  ǁVelocityǁ         0.0019183          9.7234          5.0582          5.0582
v  Pressure               -52.252          20.623         -3.5226         -3.5226
v  nu_tilda           4.2108e-007       0.0042675      0.00084322      0.00084322
v  TempC                       21          73.084          21.503          21.503
v  TurbVisc           2.7574e-014       0.0050297      0.00098212      0.00098212
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              579:        0.23500E+01

===============================================================


 INSTANT    0.580000000E+03   TIME STEP NUMBER             580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64389E-02 0.88457E+00
   Friction velocity        uk    :  0.64389E-02 0.88457E+00
   Dimensionless distance   yplus :  0.51837E-01 0.71214E+01
   Friction thermal sca.    tstar : -0.88704E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38676E-01 0.53134E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61139E-02      33   0.50566E-03   0.27624E+01 0.10180E+03 
c  Velocity[X]                                      0.15924E+01 
c  Velocity[Y]                                      0.11700E+01 
c  Velocity[Z]                                      0.98197E-30 
c  Pressure     0.15149E-06     405   0.94416E-08   0.15225E+00 0.32667E+03 
c  nu_tilda     0.43895E-05      32   0.12821E-04   0.22852E-06 0.16157E+03 
c  TempC        0.26241E+02      28   0.50871E-03   0.83723E+01 0.31324E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2574          9.7237          4.5729          4.5729
v  Velocity[Y]            -4.0811          7.0994        0.017575        0.017575
v  Velocity[Z]       -6.9287e-015     1.1922e-014    -1.4895e-017    -1.4895e-017
v  ǁVelocityǁ         0.0017994          9.7264          5.0588          5.0588
v  Pressure               -52.233          20.572         -3.5344         -3.5344
v  nu_tilda           4.2148e-007       0.0042675      0.00084386      0.00084386
v  TempC                       21          73.696          21.503          21.503
v  TurbVisc           2.7658e-014       0.0050297      0.00098287      0.00098287
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              580:        0.21560E+01

===============================================================


 INSTANT    0.581000000E+03   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49359E-02 0.88375E+00
   Friction velocity        uk    :  0.49359E-02 0.88375E+00
   Dimensionless distance   yplus :  0.39737E-01 0.71148E+01
   Friction thermal sca.    tstar : -0.19631E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29648E-01 0.53084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61180E-02      33   0.37723E-03   0.27112E+01 0.10135E+03 
c  Velocity[X]                                      0.15569E+01 
c  Velocity[Y]                                      0.11544E+01 
c  Velocity[Z]                                      0.11717E-29 
c  Pressure     0.11929E-06     405   0.94773E-08   0.11827E+00 0.41600E+03 
c  nu_tilda     0.43916E-05      32   0.10529E-04   0.22798E-06 0.16130E+03 
c  TempC        0.26254E+02      28   0.42600E-03   0.75331E+01 0.29125E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2589          9.7271          4.5729          4.5729
v  Velocity[Y]            -4.0796          7.1252        0.017619        0.017619
v  Velocity[Z]       -6.9287e-015     1.2865e-014    -1.4899e-017    -1.4899e-017
v  ǁVelocityǁ         0.0019325          9.7297          5.0594          5.0594
v  Pressure               -52.264          20.639         -3.5474         -3.5474
v  nu_tilda           4.2195e-007       0.0042675      0.00084448      0.00084448
v  TempC                       21           73.08          21.504          21.504
v  TurbVisc           2.7765e-014       0.0050297      0.00098362      0.00098362
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              581:        0.20440E+01

===============================================================


 INSTANT    0.582000000E+03   TIME STEP NUMBER             582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75638E-02 0.88480E+00
   Friction velocity        uk    :  0.75638E-02 0.88480E+00
   Dimensionless distance   yplus :  0.60893E-01 0.71233E+01
   Friction thermal sca.    tstar : -0.11774E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45433E-01 0.53147E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61222E-02      33   0.52305E-03   0.26699E+01 0.10077E+03 
c  Velocity[X]                                      0.15312E+01 
c  Velocity[Y]                                      0.11387E+01 
c  Velocity[Z]                                      0.11137E-29 
c  Pressure     0.13357E-06     361   0.98068E-08   0.13057E+00 0.15966E+03 
c  nu_tilda     0.43936E-05      32   0.12841E-04   0.22743E-06 0.16103E+03 
c  TempC        0.26267E+02      28   0.43908E-03   0.69918E+01 0.28826E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2602          9.7307          4.5729          4.5729
v  Velocity[Y]            -4.0779          7.1212        0.017661        0.017661
v  Velocity[Z]       -6.9287e-015     1.3513e-014    -1.4897e-017    -1.4897e-017
v  ǁVelocityǁ         0.0019125           9.733            5.06            5.06
v  Pressure               -52.246          20.655         -3.5443         -3.5443
v  nu_tilda           4.2243e-007       0.0042676      0.00084512      0.00084512
v  TempC                       21          73.077          21.505          21.505
v  TurbVisc           2.7887e-014       0.0050297      0.00098437      0.00098437
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              582:        0.20900E+01

===============================================================


 INSTANT    0.583000000E+03   TIME STEP NUMBER             583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95267E-02 0.88417E+00
   Friction velocity        uk    :  0.95267E-02 0.88417E+00
   Dimensionless distance   yplus :  0.76697E-01 0.71182E+01
   Friction thermal sca.    tstar : -0.73467E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57224E-01 0.53109E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61264E-02      33   0.45599E-03   0.27191E+01 0.10100E+03 
c  Velocity[X]                                      0.15744E+01 
c  Velocity[Y]                                      0.11447E+01 
c  Velocity[Z]                                      0.13389E-29 
c  Pressure     0.17336E-06     456   0.95148E-08   0.17369E+00 0.30798E+03 
c  nu_tilda     0.43957E-05      32   0.10498E-04   0.22690E-06 0.16076E+03 
c  TempC        0.26280E+02      28   0.41619E-03   0.56130E+01 0.26277E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2618          9.7347          4.5729          4.5729
v  Velocity[Y]             -4.076          7.0976        0.017704        0.017704
v  Velocity[Z]       -6.9287e-015     1.4252e-014    -1.4914e-017    -1.4914e-017
v  ǁVelocityǁ         0.0018957          9.7366          5.0606          5.0606
v  Pressure               -52.261          20.598         -3.5696         -3.5696
v  nu_tilda           4.2298e-007       0.0042676      0.00084574      0.00084574
v  TempC                       21          73.303          21.505          21.505
v  TurbVisc           2.8015e-014       0.0050297      0.00098512      0.00098512
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              583:        0.26290E+01

===============================================================


 INSTANT    0.584000000E+03   TIME STEP NUMBER             584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52452E-02 0.88302E+00
   Friction velocity        uk    :  0.52452E-02 0.88302E+00
   Dimensionless distance   yplus :  0.42228E-01 0.71089E+01
   Friction thermal sca.    tstar : -0.61725E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31507E-01 0.53041E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61306E-02      33   0.45431E-03   0.26646E+01 0.10049E+03 
c  Velocity[X]                                      0.15345E+01 
c  Velocity[Y]                                      0.11301E+01 
c  Velocity[Z]                                      0.14723E-29 
c  Pressure     0.14631E-06     458   0.97816E-08   0.14458E+00 0.64307E+03 
c  nu_tilda     0.43977E-05      32   0.12871E-04   0.22636E-06 0.16049E+03 
c  TempC        0.26293E+02      28   0.75858E-03   0.62473E+01 0.27497E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2633          9.7388          4.5729          4.5729
v  Velocity[Y]             -4.074          7.1182        0.017746        0.017746
v  Velocity[Z]       -6.9287e-015     1.3574e-014    -1.4921e-017    -1.4921e-017
v  ǁVelocityǁ         0.0019333          9.7406          5.0612          5.0612
v  Pressure               -52.234          20.723          -3.541          -3.541
v  nu_tilda           4.2349e-007       0.0042676      0.00084637      0.00084637
v  TempC                       21          73.778          21.506          21.506
v  TurbVisc           2.8162e-014       0.0050298      0.00098586      0.00098586
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              584:        0.25100E+01

===============================================================


 INSTANT    0.585000000E+03   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97455E-02 0.88412E+00
   Friction velocity        uk    :  0.97455E-02 0.88412E+00
   Dimensionless distance   yplus :  0.78458E-01 0.71178E+01
   Friction thermal sca.    tstar : -0.59542E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58538E-01 0.53107E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61347E-02      33   0.47550E-03   0.26561E+01 0.10026E+03 
c  Velocity[X]                                      0.15331E+01 
c  Velocity[Y]                                      0.11230E+01 
c  Velocity[Z]                                      0.11214E-29 
c  Pressure     0.14283E-06     501   0.99779E-08   0.14351E+00 0.75877E+03 
c  nu_tilda     0.43997E-05      32   0.10415E-04   0.22584E-06 0.16023E+03 
c  TempC        0.26306E+02      29   0.56193E-03   0.20334E+02 0.46237E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2647           9.743          4.5729          4.5729
v  Velocity[Y]            -4.0721          7.0979        0.017788        0.017788
v  Velocity[Z]       -6.9287e-015     1.2631e-014    -1.4938e-017    -1.4938e-017
v  ǁVelocityǁ          0.001884          9.7448          5.0618          5.0618
v  Pressure               -52.269          20.589         -3.5973         -3.5973
v  nu_tilda           4.2395e-007       0.0042676        0.000847        0.000847
v  TempC                       21          73.072          21.506          21.506
v  TurbVisc           2.8296e-014       0.0050298      0.00098661      0.00098661
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              585:        0.27310E+01

===============================================================


 INSTANT    0.586000000E+03   TIME STEP NUMBER             586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59323E-02 0.88334E+00
   Friction velocity        uk    :  0.59323E-02 0.88334E+00
   Dimensionless distance   yplus :  0.47759E-01 0.71115E+01
   Friction thermal sca.    tstar : -0.59527E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35634E-01 0.53060E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61389E-02      33   0.52954E-03   0.26628E+01 0.10017E+03 
c  Velocity[X]                                      0.15311E+01 
c  Velocity[Y]                                      0.11317E+01 
c  Velocity[Z]                                      0.13927E-29 
c  Pressure     0.15099E-06     505   0.95768E-08   0.15030E+00 0.93690E+03 
c  nu_tilda     0.44018E-05      32   0.12896E-04   0.22531E-06 0.15996E+03 
c  TempC        0.26319E+02      28   0.47671E-03   0.86060E+01 0.30917E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2664          9.7473          4.5729          4.5729
v  Velocity[Y]              -4.07           7.117        0.017828        0.017828
v  Velocity[Z]       -6.9287e-015     1.2724e-014    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ         0.0019439           9.749          5.0624          5.0624
v  Pressure               -52.242          20.759         -3.5528         -3.5528
v  nu_tilda           4.2438e-007       0.0042676      0.00084763      0.00084763
v  TempC                       21           73.07          21.507          21.507
v  TurbVisc           2.8421e-014       0.0050298      0.00098736      0.00098736
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              586:        0.26110E+01

===============================================================


 INSTANT    0.587000000E+03   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10208E-01 0.88446E+00
   Friction velocity        uk    :  0.10208E-01 0.88446E+00
   Dimensionless distance   yplus :  0.82178E-01 0.71205E+01
   Friction thermal sca.    tstar : -0.59859E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61314E-01 0.53127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61431E-02      33   0.50106E-03   0.26663E+01 0.10032E+03 
c  Velocity[X]                                      0.15388E+01 
c  Velocity[Y]                                      0.11275E+01 
c  Velocity[Z]                                      0.13418E-29 
c  Pressure     0.14224E-06     457   0.93754E-08   0.14250E+00 0.40517E+03 
c  nu_tilda     0.44038E-05      32   0.10383E-04   0.22480E-06 0.15970E+03 
c  TempC        0.26332E+02      28   0.40525E-03   0.65667E+01 0.26010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2677          9.7517          4.5729          4.5729
v  Velocity[Y]            -4.0676           7.127        0.017869        0.017869
v  Velocity[Z]       -6.9287e-015     1.2783e-014    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ         0.0019833          9.7532           5.063           5.063
v  Pressure               -52.277          20.713         -3.5923         -3.5923
v  nu_tilda           4.2478e-007       0.0042676      0.00084825      0.00084825
v  TempC                       21          73.579          21.508          21.508
v  TurbVisc           2.8536e-014       0.0050298      0.00098811      0.00098811
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              587:        0.25450E+01

===============================================================


 INSTANT    0.588000000E+03   TIME STEP NUMBER             588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88895E-02 0.88412E+00
   Friction velocity        uk    :  0.88895E-02 0.88412E+00
   Dimensionless distance   yplus :  0.71566E-01 0.71178E+01
   Friction thermal sca.    tstar : -0.67250E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53396E-01 0.53107E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61473E-02      33   0.46932E-03   0.26807E+01 0.10018E+03 
c  Velocity[X]                                      0.15741E+01 
c  Velocity[Y]                                      0.11065E+01 
c  Velocity[Z]                                      0.10784E-29 
c  Pressure     0.16917E-06     393   0.97834E-08   0.16804E+00 0.34659E+03 
c  nu_tilda     0.44058E-05      32   0.12922E-04   0.22427E-06 0.15943E+03 
c  TempC        0.26345E+02      28   0.44096E-03   0.65459E+01 0.27518E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2688          9.7561          4.5729          4.5729
v  Velocity[Y]            -4.0655          7.0965        0.017909        0.017909
v  Velocity[Z]       -6.9287e-015     1.2527e-014    -1.4954e-017    -1.4954e-017
v  ǁVelocityǁ         0.0018129          9.7575          5.0636          5.0636
v  Pressure                -52.25          20.647          -3.601          -3.601
v  nu_tilda           4.2525e-007       0.0042676      0.00084888      0.00084888
v  TempC                       21          73.257          21.508          21.508
v  TurbVisc           2.8645e-014       0.0050298      0.00098886      0.00098886
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              588:        0.23520E+01

===============================================================


 INSTANT    0.589000000E+03   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15718E-02 0.88314E+00
   Friction velocity        uk    :  0.15718E-02 0.88314E+00
   Dimensionless distance   yplus :  0.12654E-01 0.71099E+01
   Friction thermal sca.    tstar : -0.86565E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94414E-02 0.53048E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61514E-02      33   0.43449E-03   0.26197E+01 0.99581E+02 
c  Velocity[X]                                      0.15113E+01 
c  Velocity[Y]                                      0.11084E+01 
c  Velocity[Z]                                      0.97599E-30 
c  Pressure     0.12278E-06     341   0.92110E-08   0.12325E+00 0.49484E+03 
c  nu_tilda     0.44079E-05      32   0.10324E-04   0.22377E-06 0.15917E+03 
c  TempC        0.26358E+02      28   0.81885E-03   0.67586E+01 0.29001E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2698          9.7606          4.5729          4.5729
v  Velocity[Y]            -4.0629          7.1176         0.01795         0.01795
v  Velocity[Z]       -6.9287e-015     1.2528e-014     -1.495e-017     -1.495e-017
v  ǁVelocityǁ          0.001961          9.7618          5.0642          5.0642
v  Pressure               -52.283          20.731         -3.6086         -3.6086
v  nu_tilda           4.2571e-007       0.0042677      0.00084951      0.00084951
v  TempC                       21          73.262          21.509          21.509
v  TurbVisc            2.877e-014       0.0050298       0.0009896       0.0009896
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              589:        0.24340E+01

===============================================================


 INSTANT    0.590000000E+03   TIME STEP NUMBER             590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83994E-02 0.88415E+00
   Friction velocity        uk    :  0.83994E-02 0.88415E+00
   Dimensionless distance   yplus :  0.67621E-01 0.71180E+01
   Friction thermal sca.    tstar : -0.13810E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50453E-01 0.53108E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61556E-02      33   0.47154E-03   0.25994E+01 0.99288E+02 
c  Velocity[X]                                      0.15052E+01 
c  Velocity[Y]                                      0.10942E+01 
c  Velocity[Z]                                      0.11354E-29 
c  Pressure     0.11978E-06     346   0.96932E-08   0.12144E+00 0.23259E+03 
c  nu_tilda     0.44099E-05      32   0.12944E-04   0.22326E-06 0.15891E+03 
c  TempC        0.26371E+02      28   0.53191E-03   0.15243E+02 0.43177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2707           9.765          4.5729          4.5729
v  Velocity[Y]            -4.0601          7.0958        0.017988        0.017988
v  Velocity[Z]       -6.9287e-015     1.2331e-014    -1.4941e-017    -1.4941e-017
v  ǁVelocityǁ         0.0018511          9.7663          5.0648          5.0648
v  Pressure                -52.26          20.697         -3.6125         -3.6125
v  nu_tilda           4.2612e-007       0.0042677      0.00085014      0.00085014
v  TempC                       21           73.77           21.51           21.51
v  TurbVisc           2.8896e-014       0.0050299      0.00099035      0.00099035
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              590:        0.20080E+01

===============================================================


 INSTANT    0.591000000E+03   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82130E-02 0.88316E+00
   Friction velocity        uk    :  0.82130E-02 0.88316E+00
   Dimensionless distance   yplus :  0.66120E-01 0.71100E+01
   Friction thermal sca.    tstar : -0.44311E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49333E-01 0.53049E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61598E-02      33   0.52532E-03   0.26198E+01 0.99328E+02 
c  Velocity[X]                                      0.15380E+01 
c  Velocity[Y]                                      0.10818E+01 
c  Velocity[Z]                                      0.10851E-29 
c  Pressure     0.15832E-06     298   0.96970E-08   0.15762E+00 0.47032E+03 
c  nu_tilda     0.44119E-05      32   0.10286E-04   0.22277E-06 0.15866E+03 
c  TempC        0.26384E+02      28   0.48052E-03   0.79160E+01 0.30222E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2716          9.7695          4.5729          4.5729
v  Velocity[Y]            -4.0577          7.1222        0.018029        0.018029
v  Velocity[Z]       -6.9287e-015     1.2214e-014    -1.4934e-017    -1.4934e-017
v  ǁVelocityǁ         0.0019909          9.7707          5.0654          5.0654
v  Pressure               -52.284          20.766         -3.6178         -3.6178
v  nu_tilda           4.2652e-007       0.0042677      0.00085076      0.00085076
v  TempC                       21          73.165           21.51           21.51
v  TurbVisc           2.9006e-014       0.0050299       0.0009911       0.0009911
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              591:        0.20770E+01

===============================================================


 INSTANT    0.592000000E+03   TIME STEP NUMBER             592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88912E-02 0.88428E+00
   Friction velocity        uk    :  0.88912E-02 0.88428E+00
   Dimensionless distance   yplus :  0.71580E-01 0.71190E+01
   Friction thermal sca.    tstar : -0.11208E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53407E-01 0.53116E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61640E-02      33   0.46392E-03   0.26248E+01 0.99281E+02 
c  Velocity[X]                                      0.15363E+01 
c  Velocity[Y]                                      0.10884E+01 
c  Velocity[Z]                                      0.10980E-29 
c  Pressure     0.13429E-06     346   0.99886E-08   0.13117E+00 0.15547E+03 
c  nu_tilda     0.44139E-05      32   0.12970E-04   0.22225E-06 0.15840E+03 
c  TempC        0.26397E+02      28   0.39744E-03   0.68144E+01 0.27109E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2722          9.7741          4.5729          4.5729
v  Velocity[Y]            -4.0548           7.115        0.018066        0.018066
v  Velocity[Z]       -6.9287e-015     1.1875e-014    -1.4931e-017    -1.4931e-017
v  ǁVelocityǁ         0.0019852          9.7752           5.066           5.066
v  Pressure               -52.267           20.78          -3.615          -3.615
v  nu_tilda           4.2686e-007       0.0042677      0.00085139      0.00085139
v  TempC                       21          73.291          21.511          21.511
v  TurbVisc           2.9114e-014       0.0050299      0.00099184      0.00099184
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              592:        0.20640E+01

===============================================================


 INSTANT    0.593000000E+03   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10444E-01 0.88379E+00
   Friction velocity        uk    :  0.10444E-01 0.88379E+00
   Dimensionless distance   yplus :  0.84080E-01 0.71151E+01
   Friction thermal sca.    tstar : -0.86481E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62733E-01 0.53087E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61681E-02      33   0.40764E-03   0.25930E+01 0.98873E+02 
c  Velocity[X]                                      0.15150E+01 
c  Velocity[Y]                                      0.10780E+01 
c  Velocity[Z]                                      0.10374E-29 
c  Pressure     0.13261E-06     469   0.99889E-08   0.13425E+00 0.38499E+03 
c  nu_tilda     0.44159E-05      32   0.10233E-04   0.22177E-06 0.15814E+03 
c  TempC        0.26410E+02      28   0.46620E-03   0.76903E+01 0.28559E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2729          9.7786          4.5729          4.5729
v  Velocity[Y]            -4.0516          7.0925        0.018105        0.018105
v  Velocity[Z]       -6.9287e-015     1.1991e-014    -1.4921e-017    -1.4921e-017
v  ǁVelocityǁ         0.0019147          9.7797          5.0666          5.0666
v  Pressure               -52.287          20.708         -3.6486         -3.6486
v  nu_tilda           4.2722e-007       0.0042677      0.00085201      0.00085201
v  TempC                       21          73.063          21.511          21.511
v  TurbVisc           2.9208e-014       0.0050299      0.00099259      0.00099259
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              593:        0.29910E+01

===============================================================


 INSTANT    0.594000000E+03   TIME STEP NUMBER             594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73176E-02 0.88266E+00
   Friction velocity        uk    :  0.73176E-02 0.88266E+00
   Dimensionless distance   yplus :  0.58912E-01 0.71060E+01
   Friction thermal sca.    tstar : -0.69565E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43955E-01 0.53019E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61723E-02      33   0.49371E-03   0.25592E+01 0.98445E+02 
c  Velocity[X]                                      0.14958E+01 
c  Velocity[Y]                                      0.10634E+01 
c  Velocity[Z]                                      0.10989E-29 
c  Pressure     0.13554E-06     441   0.97561E-08   0.13501E+00 0.62300E+03 
c  nu_tilda     0.44179E-05      32   0.12997E-04   0.22126E-06 0.15788E+03 
c  TempC        0.26423E+02      28   0.81775E-03   0.78346E+01 0.29479E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2734          9.7831          4.5729          4.5729
v  Velocity[Y]            -4.0488          7.1126        0.018143        0.018143
v  Velocity[Z]       -6.9287e-015      1.198e-014    -1.4917e-017    -1.4917e-017
v  ǁVelocityǁ         0.0020046          9.7842          5.0671          5.0671
v  Pressure               -52.272          20.836         -3.6224         -3.6224
v  nu_tilda           4.2748e-007       0.0042677      0.00085264      0.00085264
v  TempC                       21          73.413          21.512          21.512
v  TurbVisc           2.9306e-014       0.0050299      0.00099333      0.00099333
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              594:        0.29430E+01

===============================================================


 INSTANT    0.595000000E+03   TIME STEP NUMBER             595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10971E-01 0.88363E+00
   Friction velocity        uk    :  0.10971E-01 0.88363E+00
   Dimensionless distance   yplus :  0.88326E-01 0.71138E+01
   Friction thermal sca.    tstar : -0.63281E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65901E-01 0.53077E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61765E-02      33   0.49833E-03   0.26082E+01 0.98857E+02 
c  Velocity[X]                                      0.15337E+01 
c  Velocity[Y]                                      0.10745E+01 
c  Velocity[Z]                                      0.97976E-30 
c  Pressure     0.14648E-06     469   0.96806E-08   0.14725E+00 0.53362E+03 
c  nu_tilda     0.44199E-05      32   0.10195E-04   0.22079E-06 0.15763E+03 
c  TempC        0.26436E+02      28   0.42842E-03   0.15679E+02 0.44210E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2743          9.7876          4.5729          4.5729
v  Velocity[Y]            -4.0456          7.0941         0.01818         0.01818
v  Velocity[Z]       -6.9287e-015     1.2411e-014    -1.4897e-017    -1.4897e-017
v  ǁVelocityǁ         0.0018603          9.7886          5.0677          5.0677
v  Pressure               -52.294           20.73         -3.6639         -3.6639
v  nu_tilda           4.2779e-007       0.0042678      0.00085326      0.00085326
v  TempC                       21          73.062          21.513          21.513
v  TurbVisc            2.938e-014         0.00503      0.00099408      0.00099408
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              595:        0.37290E+01

===============================================================


 INSTANT    0.596000000E+03   TIME STEP NUMBER             596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61284E-02 0.88292E+00
   Friction velocity        uk    :  0.61284E-02 0.88292E+00
   Dimensionless distance   yplus :  0.49338E-01 0.71081E+01
   Friction thermal sca.    tstar : -0.55382E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36812E-01 0.53034E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61807E-02      33   0.43061E-03   0.26024E+01 0.98534E+02 
c  Velocity[X]                                      0.15472E+01 
c  Velocity[Y]                                      0.10551E+01 
c  Velocity[Z]                                      0.12939E-29 
c  Pressure     0.18853E-06     457   0.95814E-08   0.18224E+00 0.74145E+03 
c  nu_tilda     0.44219E-05      32   0.13024E-04   0.22029E-06 0.15738E+03 
c  TempC        0.26449E+02      28   0.45832E-03   0.77568E+01 0.29261E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2755          9.7921          4.5729          4.5729
v  Velocity[Y]            -4.0423          7.1101        0.018217        0.018217
v  Velocity[Z]       -6.9287e-015     1.2151e-014    -1.4885e-017    -1.4885e-017
v  ǁVelocityǁ         0.0014835          9.7931          5.0683          5.0683
v  Pressure               -52.265          20.863         -3.6285         -3.6285
v  nu_tilda           4.2808e-007       0.0042678      0.00085389      0.00085389
v  TempC                       21          73.691          21.513          21.513
v  TurbVisc           2.9463e-014         0.00503      0.00099482      0.00099482
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              596:        0.34710E+01

===============================================================


 INSTANT    0.597000000E+03   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93922E-02 0.88429E+00
   Friction velocity        uk    :  0.93922E-02 0.88429E+00
   Dimensionless distance   yplus :  0.75613E-01 0.71192E+01
   Friction thermal sca.    tstar : -0.56274E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56416E-01 0.53117E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61849E-02      33   0.46984E-03   0.25299E+01 0.97891E+02 
c  Velocity[X]                                      0.14813E+01 
c  Velocity[Y]                                      0.10486E+01 
c  Velocity[Z]                                      0.11056E-29 
c  Pressure     0.12019E-06     458   0.95330E-08   0.12006E+00 0.29863E+03 
c  nu_tilda     0.44239E-05      32   0.10129E-04   0.21983E-06 0.15713E+03 
c  TempC        0.26462E+02      28   0.54533E-03   0.75352E+01 0.27793E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2762          9.7966          4.5729          4.5729
v  Velocity[Y]            -4.0392          7.1197        0.018254        0.018254
v  Velocity[Z]       -6.9287e-015     1.1899e-014    -1.4877e-017    -1.4877e-017
v  ǁVelocityǁ         0.0011079          9.7975          5.0689          5.0689
v  Pressure               -52.304          20.851         -3.6597         -3.6597
v  nu_tilda           4.2839e-007       0.0042678      0.00085451      0.00085451
v  TempC                       21          73.062          21.514          21.514
v  TurbVisc           2.9544e-014         0.00503      0.00099556      0.00099556
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              597:        0.37540E+01

===============================================================


 INSTANT    0.598000000E+03   TIME STEP NUMBER             598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10005E-01 0.88382E+00
   Friction velocity        uk    :  0.10005E-01 0.88382E+00
   Dimensionless distance   yplus :  0.80544E-01 0.71154E+01
   Friction thermal sca.    tstar : -0.70225E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60095E-01 0.53089E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61890E-02      33   0.49697E-03   0.25567E+01 0.97978E+02 
c  Velocity[X]                                      0.14983E+01 
c  Velocity[Y]                                      0.10584E+01 
c  Velocity[Z]                                      0.98912E-30 
c  Pressure     0.17808E-06     344   0.97470E-08   0.17958E+00 0.22709E+03 
c  nu_tilda     0.44259E-05      32   0.13048E-04   0.21935E-06 0.15688E+03 
c  TempC        0.26475E+02      29   0.58594E-03   0.69380E+01 0.28251E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2769           9.801          4.5729          4.5729
v  Velocity[Y]            -4.0356          7.0912        0.018289        0.018289
v  Velocity[Z]       -6.9287e-015     1.1939e-014    -1.4878e-017    -1.4878e-017
v  ǁVelocityǁ         0.0008345          9.8019          5.0695          5.0695
v  Pressure               -52.274          20.817         -3.6576         -3.6576
v  nu_tilda           4.2873e-007       0.0042678      0.00085514      0.00085514
v  TempC                       21          73.061          21.514          21.514
v  TurbVisc           2.9628e-014         0.00503       0.0009963       0.0009963
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              598:        0.30920E+01

===============================================================


 INSTANT    0.599000000E+03   TIME STEP NUMBER             599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89032E-02 0.88254E+00
   Friction velocity        uk    :  0.89032E-02 0.88254E+00
   Dimensionless distance   yplus :  0.71677E-01 0.71051E+01
   Friction thermal sca.    tstar : -0.94061E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53479E-01 0.53012E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61932E-02      33   0.47052E-03   0.25546E+01 0.97991E+02 
c  Velocity[X]                                      0.14979E+01 
c  Velocity[Y]                                      0.10566E+01 
c  Velocity[Z]                                      0.11041E-29 
c  Pressure     0.15352E-06     357   0.98500E-08   0.15211E+00 0.46688E+03 
c  nu_tilda     0.44279E-05      32   0.10113E-04   0.21889E-06 0.15663E+03 
c  TempC        0.26488E+02      28   0.56446E-03   0.88417E+01 0.32536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2776          9.8054          4.5729          4.5729
v  Velocity[Y]            -4.0323          7.1143        0.018325        0.018325
v  Velocity[Z]       -6.9287e-015     1.1917e-014     -1.486e-017     -1.486e-017
v  ǁVelocityǁ        0.00056293          9.8063          5.0701          5.0701
v  Pressure               -52.301          20.895         -3.6647         -3.6647
v  nu_tilda           4.2903e-007       0.0042678      0.00085576      0.00085576
v  TempC                       21          73.929          21.515          21.515
v  TurbVisc           2.9724e-014         0.00503      0.00099705      0.00099705
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              599:        0.31370E+01

===============================================================


 INSTANT    0.600000000E+03   TIME STEP NUMBER             600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99947E-02 0.88355E+00
   Friction velocity        uk    :  0.99947E-02 0.88355E+00
   Dimensionless distance   yplus :  0.80464E-01 0.71131E+01
   Friction thermal sca.    tstar : -0.18854E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60035E-01 0.53072E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61974E-02      33   0.48088E-03   0.25459E+01 0.97764E+02 
c  Velocity[X]                                      0.15098E+01 
c  Velocity[Y]                                      0.10361E+01 
c  Velocity[Z]                                      0.10792E-29 
c  Pressure     0.14576E-06     442   0.96718E-08   0.14542E+00 0.59567E+03 
c  nu_tilda     0.44299E-05      32   0.13075E-04   0.21841E-06 0.15638E+03 
c  TempC        0.26501E+02      28   0.10143E-02   0.67039E+01 0.28063E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2778          9.8097          4.5729          4.5729
v  Velocity[Y]            -4.0287          7.0829        0.018359        0.018359
v  Velocity[Z]       -6.9287e-015     1.1602e-014    -1.4858e-017    -1.4858e-017
v  ǁVelocityǁ        0.00051409          9.8107          5.0707          5.0707
v  Pressure               -52.289          20.787         -3.6904         -3.6904
v  nu_tilda           4.2927e-007       0.0042678      0.00085638      0.00085638
v  TempC                       21          73.062          21.516          21.516
v  TurbVisc           2.9807e-014         0.00503      0.00099779      0.00099779
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              600:        0.34620E+01

===============================================================


 INSTANT    0.601000000E+03   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77472E-02 0.88272E+00
   Friction velocity        uk    :  0.77472E-02 0.88272E+00
   Dimensionless distance   yplus :  0.62370E-01 0.71065E+01
   Friction thermal sca.    tstar : -0.12089E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46535E-01 0.53023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62016E-02      33   0.42266E-03   0.25308E+01 0.97523E+02 
c  Velocity[X]                                      0.14841E+01 
c  Velocity[Y]                                      0.10467E+01 
c  Velocity[Z]                                      0.10572E-29 
c  Pressure     0.13601E-06     425   0.95881E-08   0.13428E+00 0.81225E+03 
c  nu_tilda     0.44319E-05      32   0.10058E-04   0.21796E-06 0.15613E+03 
c  TempC        0.26514E+02      29   0.48351E-03   0.18020E+02 0.41418E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2782          9.8141          4.5729          4.5729
v  Velocity[Y]            -4.0249          7.1068        0.018395        0.018395
v  Velocity[Z]       -6.9287e-015     1.1717e-014    -1.4864e-017    -1.4864e-017
v  ǁVelocityǁ         0.0006273           9.815          5.0713          5.0713
v  Pressure               -52.317          20.931         -3.6787         -3.6787
v  nu_tilda           4.2943e-007       0.0042678        0.000857        0.000857
v  TempC                       21           73.72          21.516          21.516
v  TurbVisc           2.9872e-014       0.0050301      0.00099853      0.00099853
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              601:        0.40010E+01

===============================================================


 INSTANT    0.602000000E+03   TIME STEP NUMBER             602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99519E-02 0.88400E+00
   Friction velocity        uk    :  0.99519E-02 0.88400E+00
   Dimensionless distance   yplus :  0.80119E-01 0.71168E+01
   Friction thermal sca.    tstar : -0.77419E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59778E-01 0.53099E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62057E-02      33   0.42638E-03   0.24906E+01 0.97007E+02 
c  Velocity[X]                                      0.14670E+01 
c  Velocity[Y]                                      0.10236E+01 
c  Velocity[Z]                                      0.11492E-29 
c  Pressure     0.14576E-06     409   0.99725E-08   0.14579E+00 0.23367E+03 
c  nu_tilda     0.44339E-05      32   0.13095E-04   0.21748E-06 0.15589E+03 
c  TempC        0.26527E+02      28   0.48215E-03   0.84093E+01 0.29187E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2785          9.8183          4.5729          4.5729
v  Velocity[Y]            -4.0213          7.1154        0.018429        0.018429
v  Velocity[Z]       -6.9287e-015     1.1518e-014     -1.486e-017     -1.486e-017
v  ǁVelocityǁ        0.00088848          9.8192          5.0719          5.0719
v  Pressure               -52.294          20.963          -3.669          -3.669
v  nu_tilda           4.2958e-007       0.0042678      0.00085762      0.00085762
v  TempC                       21           73.06          21.517          21.517
v  TurbVisc           2.9919e-014       0.0050301      0.00099927      0.00099927
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              602:        0.32980E+01

===============================================================


 INSTANT    0.603000000E+03   TIME STEP NUMBER             603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11483E-01 0.88362E+00
   Friction velocity        uk    :  0.11483E-01 0.88362E+00
   Dimensionless distance   yplus :  0.92446E-01 0.71138E+01
   Friction thermal sca.    tstar : -0.64455E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68975E-01 0.53077E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62099E-02      33   0.51018E-03   0.25076E+01 0.97000E+02 
c  Velocity[X]                                      0.14960E+01 
c  Velocity[Y]                                      0.10116E+01 
c  Velocity[Z]                                      0.11178E-29 
c  Pressure     0.14631E-06     485   0.96320E-08   0.14611E+00 0.68730E+03 
c  nu_tilda     0.44359E-05      32   0.99809E-05   0.21704E-06 0.15565E+03 
c  TempC        0.26540E+02      28   0.55986E-03   0.81285E+01 0.29693E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2786          9.8225          4.5729          4.5729
v  Velocity[Y]            -4.0174          7.0895        0.018462        0.018462
v  Velocity[Z]       -6.9287e-015     1.1089e-014    -1.4864e-017    -1.4864e-017
v  ǁVelocityǁ         0.0011507          9.8234          5.0725          5.0725
v  Pressure               -52.321           20.83         -3.7194         -3.7194
v  nu_tilda           4.2978e-007       0.0042679      0.00085824      0.00085824
v  TempC                       21           73.06          21.517          21.517
v  TurbVisc            2.996e-014       0.0050301           0.001           0.001
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              603:        0.33960E+01

===============================================================


 INSTANT    0.604000000E+03   TIME STEP NUMBER             604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62828E-02 0.88262E+00
   Friction velocity        uk    :  0.62828E-02 0.88262E+00
   Dimensionless distance   yplus :  0.50581E-01 0.71057E+01
   Friction thermal sca.    tstar : -0.55538E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37739E-01 0.53016E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62141E-02      33   0.46483E-03   0.25307E+01 0.97161E+02 
c  Velocity[X]                                      0.15044E+01 
c  Velocity[Y]                                      0.10263E+01 
c  Velocity[Z]                                      0.10152E-29 
c  Pressure     0.15676E-06     488   0.94167E-08   0.15662E+00 0.82275E+03 
c  nu_tilda     0.44378E-05      32   0.13131E-04   0.21658E-06 0.15540E+03 
c  TempC        0.26553E+02      28   0.47564E-03   0.96142E+01 0.31805E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2788          9.8269          4.5729          4.5729
v  Velocity[Y]            -4.0133          7.1063        0.018495        0.018495
v  Velocity[Z]       -6.9287e-015     1.0573e-014    -1.4877e-017    -1.4877e-017
v  ǁVelocityǁ         0.0014547          9.8277          5.0731          5.0731
v  Pressure               -52.299          20.981         -3.6814         -3.6814
v  nu_tilda           4.2993e-007       0.0042679      0.00085887      0.00085887
v  TempC                       21          73.905          21.518          21.518
v  TurbVisc           3.0017e-014       0.0050301       0.0010007       0.0010007
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              604:        0.32780E+01

===============================================================


 INSTANT    0.605000000E+03   TIME STEP NUMBER             605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76810E-02 0.88367E+00
   Friction velocity        uk    :  0.76810E-02 0.88367E+00
   Dimensionless distance   yplus :  0.61837E-01 0.71142E+01
   Friction thermal sca.    tstar : -0.47165E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46137E-01 0.53080E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62183E-02      33   0.40059E-03   0.24842E+01 0.96703E+02 
c  Velocity[X]                                      0.14748E+01 
c  Velocity[Y]                                      0.10094E+01 
c  Velocity[Z]                                      0.11291E-29 
c  Pressure     0.10416E-06     488   0.95839E-08   0.10449E+00 0.64461E+03 
c  nu_tilda     0.44398E-05      32   0.99249E-05   0.21614E-06 0.15516E+03 
c  TempC        0.26566E+02      28   0.41317E-03   0.69109E+01 0.27015E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2791          9.8317          4.5729          4.5729
v  Velocity[Y]            -4.0094          7.0864        0.018529        0.018529
v  Velocity[Z]       -6.9287e-015     1.0468e-014    -1.4884e-017    -1.4884e-017
v  ǁVelocityǁ          0.001732          9.8324          5.0737          5.0737
v  Pressure               -52.332          20.868         -3.7319         -3.7319
v  nu_tilda           4.3017e-007       0.0042679      0.00085948      0.00085948
v  TempC                       21          73.059          21.519          21.519
v  TurbVisc           3.0059e-014       0.0050301       0.0010015       0.0010015
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              605:        0.33440E+01

===============================================================


 INSTANT    0.606000000E+03   TIME STEP NUMBER             606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55584E-02 0.88275E+00
   Friction velocity        uk    :  0.55584E-02 0.88275E+00
   Dimensionless distance   yplus :  0.44749E-01 0.71068E+01
   Friction thermal sca.    tstar : -0.52916E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33388E-01 0.53024E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62224E-02      33   0.49572E-03   0.24508E+01 0.96223E+02 
c  Velocity[X]                                      0.14595E+01 
c  Velocity[Y]                                      0.99129E+00 
c  Velocity[Z]                                      0.13138E-29 
c  Pressure     0.12084E-06     488   0.95911E-08   0.11980E+00 0.76392E+03 
c  nu_tilda     0.44418E-05      32   0.13155E-04   0.21568E-06 0.15492E+03 
c  TempC        0.26579E+02      28   0.45617E-03   0.66785E+01 0.27626E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2795          9.8364          4.5729          4.5729
v  Velocity[Y]            -4.0054          7.1099        0.018561        0.018561
v  Velocity[Z]       -6.9287e-015      1.041e-014    -1.4898e-017    -1.4898e-017
v  ǁVelocityǁ         0.0020465          9.8372          5.0743          5.0743
v  Pressure               -52.312          21.013         -3.6972         -3.6972
v  nu_tilda            4.304e-007       0.0042679      0.00086011      0.00086011
v  TempC                       21          73.059          21.519          21.519
v  TurbVisc           3.0124e-014       0.0050301       0.0010022       0.0010022
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              606:        0.35450E+01

===============================================================


 INSTANT    0.607000000E+03   TIME STEP NUMBER             607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43475E-02 0.88374E+00
   Friction velocity        uk    :  0.43475E-02 0.88374E+00
   Dimensionless distance   yplus :  0.35000E-01 0.71148E+01
   Friction thermal sca.    tstar : -0.58086E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26114E-01 0.53084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62266E-02      33   0.46418E-03   0.24813E+01 0.96497E+02 
c  Velocity[X]                                      0.14742E+01 
c  Velocity[Y]                                      0.10071E+01 
c  Velocity[Z]                                      0.11196E-29 
c  Pressure     0.14537E-06     474   0.92263E-08   0.14352E+00 0.41617E+03 
c  nu_tilda     0.44438E-05      32   0.98928E-05   0.21526E-06 0.15468E+03 
c  TempC        0.26591E+02      28   0.50812E-03   0.77826E+01 0.28663E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2794          9.8411          4.5729          4.5729
v  Velocity[Y]            -4.0011          7.1075        0.018593        0.018593
v  Velocity[Z]       -6.9287e-015     1.0661e-014    -1.4903e-017    -1.4903e-017
v  ǁVelocityǁ         0.0020591          9.8418          5.0749          5.0749
v  Pressure               -52.346          20.951         -3.7363         -3.7363
v  nu_tilda           4.3056e-007       0.0042679      0.00086072      0.00086072
v  TempC                       21          73.813           21.52           21.52
v  TurbVisc           3.0189e-014       0.0050301        0.001003        0.001003
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              607:        0.40140E+01

===============================================================


 INSTANT    0.608000000E+03   TIME STEP NUMBER             608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48261E-02 0.88316E+00
   Friction velocity        uk    :  0.48261E-02 0.88316E+00
   Dimensionless distance   yplus :  0.38854E-01 0.71100E+01
   Friction thermal sca.    tstar : -0.72708E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28989E-01 0.53049E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62308E-02      33   0.41134E-03   0.24730E+01 0.96319E+02 
c  Velocity[X]                                      0.14836E+01 
c  Velocity[Y]                                      0.98943E+00 
c  Velocity[Z]                                      0.11540E-29 
c  Pressure     0.12888E-06     360   0.95746E-08   0.13035E+00 0.23249E+03 
c  nu_tilda     0.44457E-05      32   0.13183E-04   0.21481E-06 0.15445E+03 
c  TempC        0.26604E+02      28   0.73764E-03   0.82245E+01 0.30739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2794          9.8457          4.5729          4.5729
v  Velocity[Y]            -3.9968          7.0808        0.018623        0.018623
v  Velocity[Z]       -6.9287e-015     1.0836e-014    -1.4901e-017    -1.4901e-017
v  ǁVelocityǁ         0.0018729          9.8464          5.0755          5.0755
v  Pressure               -52.322          20.912         -3.7389         -3.7389
v  nu_tilda           4.3077e-007       0.0042679      0.00086135      0.00086135
v  TempC                       21          73.059          21.521          21.521
v  TurbVisc           3.0235e-014       0.0050302       0.0010037       0.0010037
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              608:        0.37900E+01

===============================================================


 INSTANT    0.609000000E+03   TIME STEP NUMBER             609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83920E-02 0.88208E+00
   Friction velocity        uk    :  0.83920E-02 0.88208E+00
   Dimensionless distance   yplus :  0.67562E-01 0.71013E+01
   Friction thermal sca.    tstar : -0.98381E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50408E-01 0.52984E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62350E-02      33   0.46185E-03   0.24277E+01 0.95801E+02 
c  Velocity[X]                                      0.14519E+01 
c  Velocity[Y]                                      0.97585E+00 
c  Velocity[Z]                                      0.10905E-29 
c  Pressure     0.10996E-06     342   0.89924E-08   0.10934E+00 0.56138E+03 
c  nu_tilda     0.44477E-05      32   0.98453E-05   0.21439E-06 0.15421E+03 
c  TempC        0.26617E+02      28   0.46315E-03   0.13596E+02 0.40075E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2792          9.8502          4.5729          4.5729
v  Velocity[Y]            -3.9926          7.1048        0.018654        0.018654
v  Velocity[Z]       -6.9287e-015     1.0941e-014    -1.4901e-017    -1.4901e-017
v  ǁVelocityǁ         0.0020541           9.851          5.0761          5.0761
v  Pressure               -52.356          21.014          -3.742          -3.742
v  nu_tilda           4.3095e-007       0.0042679      0.00086196      0.00086196
v  TempC                       21          73.059          21.521          21.521
v  TurbVisc           3.0295e-014       0.0050302       0.0010044       0.0010044
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              609:        0.43790E+01

===============================================================


 INSTANT    0.610000000E+03   TIME STEP NUMBER             610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81553E-02 0.88295E+00
   Friction velocity        uk    :  0.81553E-02 0.88295E+00
   Dimensionless distance   yplus :  0.65656E-01 0.71083E+01
   Friction thermal sca.    tstar : -0.22308E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48987E-01 0.53036E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62391E-02      33   0.47326E-03   0.24364E+01 0.95741E+02 
c  Velocity[X]                                      0.14537E+01 
c  Velocity[Y]                                      0.98274E+00 
c  Velocity[Z]                                      0.95388E-30 
c  Pressure     0.16972E-06     277   0.90638E-08   0.17199E+00 0.26159E+03 
c  nu_tilda     0.44496E-05      32   0.13206E-04   0.21395E-06 0.15397E+03 
c  TempC        0.26630E+02      28   0.42012E-03   0.10017E+02 0.32743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2792          9.8547          4.5729          4.5729
v  Velocity[Y]            -3.9881          7.0821        0.018684        0.018684
v  Velocity[Z]       -6.9287e-015     1.0833e-014    -1.4893e-017    -1.4893e-017
v  ǁVelocityǁ         0.0018982          9.8553          5.0767          5.0767
v  Pressure                -52.32          20.968         -3.7414         -3.7414
v  nu_tilda           4.3109e-007        0.004268      0.00086258      0.00086258
v  TempC                       21          73.876          21.522          21.522
v  TurbVisc           3.0344e-014       0.0050302       0.0010052       0.0010052
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              610:        0.28580E+01

===============================================================


 INSTANT    0.611000000E+03   TIME STEP NUMBER             611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84765E-02 0.88218E+00
   Friction velocity        uk    :  0.84765E-02 0.88218E+00
   Dimensionless distance   yplus :  0.68241E-01 0.71021E+01
   Friction thermal sca.    tstar : -0.12243E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50916E-01 0.52990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62433E-02      33   0.42891E-03   0.24484E+01 0.95676E+02 
c  Velocity[X]                                      0.14783E+01 
c  Velocity[Y]                                      0.97017E+00 
c  Velocity[Z]                                      0.10392E-29 
c  Pressure     0.15497E-06     393   0.97817E-08   0.15159E+00 0.40472E+03 
c  nu_tilda     0.44516E-05      32   0.97687E-05   0.21354E-06 0.15374E+03 
c  TempC        0.26643E+02      28   0.45487E-03   0.68878E+01 0.27725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2791          9.8591          4.5729          4.5729
v  Velocity[Y]            -3.9835          7.1027        0.018714        0.018714
v  Velocity[Z]       -6.9287e-015     1.0539e-014    -1.4887e-017    -1.4887e-017
v  ǁVelocityǁ         0.0020358          9.8598          5.0773          5.0773
v  Pressure               -52.353          21.028         -3.7515         -3.7515
v  nu_tilda           4.3122e-007        0.004268       0.0008632       0.0008632
v  TempC                       21          73.058          21.522          21.522
v  TurbVisc           3.0383e-014       0.0050302       0.0010059       0.0010059
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              611:        0.34020E+01

===============================================================


 INSTANT    0.612000000E+03   TIME STEP NUMBER             612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96208E-02 0.88352E+00
   Friction velocity        uk    :  0.96208E-02 0.88352E+00
   Dimensionless distance   yplus :  0.77454E-01 0.71130E+01
   Friction thermal sca.    tstar : -0.78354E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57789E-01 0.53071E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62475E-02      33   0.45832E-03   0.24178E+01 0.95332E+02 
c  Velocity[X]                                      0.14580E+01 
c  Velocity[Y]                                      0.95974E+00 
c  Velocity[Z]                                      0.99112E-30 
c  Pressure     0.11916E-06     408   0.96165E-08   0.12128E+00 0.26811E+03 
c  nu_tilda     0.44536E-05      32   0.13231E-04   0.21311E-06 0.15351E+03 
c  TempC        0.26656E+02      28   0.43855E-03   0.60889E+01 0.25953E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2787          9.8634          4.5729          4.5729
v  Velocity[Y]            -3.9792          7.0802        0.018743        0.018743
v  Velocity[Z]       -6.9287e-015     1.0308e-014    -1.4884e-017    -1.4884e-017
v  ǁVelocityǁ         0.0019299          9.8641          5.0779          5.0779
v  Pressure               -52.342          20.987         -3.7616         -3.7616
v  nu_tilda           4.3136e-007        0.004268      0.00086382      0.00086382
v  TempC                       21          73.058          21.523          21.523
v  TurbVisc           3.0421e-014       0.0050302       0.0010066       0.0010066
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              612:        0.34300E+01

===============================================================


 INSTANT    0.613000000E+03   TIME STEP NUMBER             613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95643E-02 0.88246E+00
   Friction velocity        uk    :  0.95643E-02 0.88246E+00
   Dimensionless distance   yplus :  0.76999E-01 0.71044E+01
   Friction thermal sca.    tstar : -0.64884E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57450E-01 0.53007E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62516E-02      33   0.42404E-03   0.24082E+01 0.95250E+02 
c  Velocity[X]                                      0.14392E+01 
c  Velocity[Y]                                      0.96905E+00 
c  Velocity[Z]                                      0.98932E-30 
c  Pressure     0.10475E-06     298   0.94544E-08   0.10361E+00 0.47214E+03 
c  nu_tilda     0.44555E-05      32   0.97607E-05   0.21271E-06 0.15328E+03 
c  TempC        0.26669E+02      28   0.50543E-03   0.77604E+01 0.28409E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2782          9.8676          4.5729          4.5729
v  Velocity[Y]            -3.9745           7.103        0.018772        0.018772
v  Velocity[Z]       -6.9287e-015     1.0474e-014    -1.4876e-017    -1.4876e-017
v  ǁVelocityǁ         0.0020921          9.8684          5.0785          5.0785
v  Pressure               -52.369          21.063         -3.7672         -3.7672
v  nu_tilda           4.3148e-007        0.004268      0.00086443      0.00086443
v  TempC                       21          73.895          21.524          21.524
v  TurbVisc           3.0461e-014       0.0050302       0.0010074       0.0010074
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              613:        0.33670E+01

===============================================================


 INSTANT    0.614000000E+03   TIME STEP NUMBER             614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36798E-02 0.88343E+00
   Friction velocity        uk    :  0.36798E-02 0.88343E+00
   Dimensionless distance   yplus :  0.29625E-01 0.71122E+01
   Friction thermal sca.    tstar : -0.62190E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22104E-01 0.53065E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62558E-02      33   0.45312E-03   0.24067E+01 0.95081E+02 
c  Velocity[X]                                      0.14522E+01 
c  Velocity[Y]                                      0.95455E+00 
c  Velocity[Z]                                      0.10821E-29 
c  Pressure     0.13709E-06     426   0.97903E-08   0.13624E+00 0.31406E+03 
c  nu_tilda     0.44575E-05      32   0.13250E-04   0.21229E-06 0.15305E+03 
c  TempC        0.26681E+02      28   0.46938E-03   0.84343E+01 0.30309E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2783          9.8717          4.5729          4.5729
v  Velocity[Y]            -3.9699          7.0997        0.018799        0.018799
v  Velocity[Z]       -6.9287e-015     1.0452e-014    -1.4858e-017    -1.4858e-017
v  ǁVelocityǁ         0.0021207          9.8726          5.0791          5.0791
v  Pressure               -52.342          21.108         -3.7523         -3.7523
v  nu_tilda            4.316e-007        0.004268      0.00086505      0.00086505
v  TempC                       21          73.457          21.524          21.524
v  TurbVisc           3.0493e-014       0.0050303       0.0010081       0.0010081
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              614:        0.36500E+01

===============================================================


 INSTANT    0.615000000E+03   TIME STEP NUMBER             615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50430E-02 0.88267E+00
   Friction velocity        uk    :  0.50430E-02 0.88267E+00
   Dimensionless distance   yplus :  0.40600E-01 0.71061E+01
   Friction thermal sca.    tstar : -0.88271E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30292E-01 0.53020E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62600E-02      33   0.44063E-03   0.24130E+01 0.94968E+02 
c  Velocity[X]                                      0.14704E+01 
c  Velocity[Y]                                      0.94258E+00 
c  Velocity[Z]                                      0.94899E-30 
c  Pressure     0.14108E-06     472   0.96197E-08   0.14198E+00 0.46249E+03 
c  nu_tilda     0.44594E-05      32   0.97045E-05   0.21189E-06 0.15282E+03 
c  TempC        0.26694E+02      28   0.61156E-03   0.69795E+01 0.27860E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2784          9.8757          4.5729          4.5729
v  Velocity[Y]            -3.9655           7.076        0.018827        0.018827
v  Velocity[Z]       -6.9287e-015      1.027e-014    -1.4842e-017    -1.4842e-017
v  ǁVelocityǁ         0.0019625          9.8766          5.0796          5.0796
v  Pressure               -52.367          21.011         -3.7901         -3.7901
v  nu_tilda           4.3176e-007        0.004268      0.00086567      0.00086567
v  TempC                       21          73.538          21.525          21.525
v  TurbVisc           3.0527e-014       0.0050303       0.0010089       0.0010089
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              615:        0.33350E+01

===============================================================


 INSTANT    0.616000000E+03   TIME STEP NUMBER             616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47981E-02 0.88178E+00
   Friction velocity        uk    :  0.47981E-02 0.88178E+00
   Dimensionless distance   yplus :  0.38628E-01 0.70989E+01
   Friction thermal sca.    tstar : -0.33685E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28821E-01 0.52966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62641E-02      33   0.43426E-03   0.23838E+01 0.94666E+02 
c  Velocity[X]                                      0.14363E+01 
c  Velocity[Y]                                      0.94742E+00 
c  Velocity[Z]                                      0.10785E-29 
c  Pressure     0.14545E-06     473   0.94481E-08   0.14586E+00 0.66003E+03 
c  nu_tilda     0.44614E-05      32   0.13266E-04   0.21148E-06 0.15260E+03 
c  TempC        0.26707E+02      28   0.44684E-03   0.10149E+02 0.32077E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2784          9.8797          4.5729          4.5729
v  Velocity[Y]            -3.9607          7.0947        0.018854        0.018854
v  Velocity[Z]       -6.9287e-015     1.0039e-014     -1.482e-017     -1.482e-017
v  ǁVelocityǁ         0.0020838          9.8806          5.0802          5.0802
v  Pressure               -52.351          21.147         -3.7623         -3.7623
v  nu_tilda           4.3177e-007        0.004268      0.00086628      0.00086628
v  TempC                       21           73.19          21.525          21.525
v  TurbVisc           3.0572e-014       0.0050303       0.0010096       0.0010096
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              616:        0.33720E+01

===============================================================


 INSTANT    0.617000000E+03   TIME STEP NUMBER             617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11284E-01 0.88267E+00
   Friction velocity        uk    :  0.11284E-01 0.88267E+00
   Dimensionless distance   yplus :  0.90847E-01 0.71061E+01
   Friction thermal sca.    tstar : -0.68138E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67782E-01 0.53019E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62683E-02      33   0.39694E-03   0.23686E+01 0.94485E+02 
c  Velocity[X]                                      0.14304E+01 
c  Velocity[Y]                                      0.93823E+00 
c  Velocity[Z]                                      0.10775E-29 
c  Pressure     0.10051E-06     469   0.97506E-08   0.10066E+00 0.56830E+03 
c  nu_tilda     0.44633E-05      32   0.96797E-05   0.21110E-06 0.15237E+03 
c  TempC        0.26720E+02      28   0.53789E-03   0.67943E+01 0.26613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2781          9.8836          4.5729          4.5729
v  Velocity[Y]            -3.9558          7.0778        0.018881        0.018881
v  Velocity[Z]       -6.9287e-015     9.8702e-015     -1.481e-017     -1.481e-017
v  ǁVelocityǁ         0.0019922          9.8843          5.0808          5.0808
v  Pressure                -52.38          21.036         -3.8073         -3.8073
v  nu_tilda            4.318e-007        0.004268       0.0008669       0.0008669
v  TempC                       21          73.535          21.526          21.526
v  TurbVisc           3.0576e-014       0.0050303       0.0010103       0.0010103
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              617:        0.34080E+01

===============================================================


 INSTANT    0.618000000E+03   TIME STEP NUMBER             618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37366E-02 0.88194E+00
   Friction velocity        uk    :  0.37366E-02 0.88194E+00
   Dimensionless distance   yplus :  0.30082E-01 0.71002E+01
   Friction thermal sca.    tstar : -0.44089E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22444E-01 0.52976E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62724E-02      33   0.49577E-03   0.23525E+01 0.94220E+02 
c  Velocity[X]                                      0.14224E+01 
c  Velocity[Y]                                      0.93011E+00 
c  Velocity[Z]                                      0.10001E-29 
c  Pressure     0.11297E-06     472   0.98484E-08   0.11217E+00 0.64813E+03 
c  nu_tilda     0.44652E-05      32   0.13283E-04   0.21069E-06 0.15215E+03 
c  TempC        0.26733E+02      29   0.45072E-03   0.71506E+01 0.27873E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2777          9.8873          4.5729          4.5729
v  Velocity[Y]            -3.9511          7.0992        0.018906        0.018906
v  Velocity[Z]       -6.9287e-015     9.7792e-015    -1.4788e-017    -1.4788e-017
v  ǁVelocityǁ         0.0021213          9.8881          5.0814          5.0814
v  Pressure               -52.364          21.164         -3.7791         -3.7791
v  nu_tilda           4.3177e-007       0.0042681      0.00086751      0.00086751
v  TempC                       21          73.057          21.527          21.527
v  TurbVisc           3.0585e-014       0.0050303       0.0010111       0.0010111
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              618:        0.36080E+01

===============================================================


 INSTANT    0.619000000E+03   TIME STEP NUMBER             619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67656E-02 0.88290E+00
   Friction velocity        uk    :  0.67656E-02 0.88290E+00
   Dimensionless distance   yplus :  0.54468E-01 0.71079E+01
   Friction thermal sca.    tstar : -0.87192E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40639E-01 0.53033E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62766E-02      33   0.50245E-03   0.24016E+01 0.94607E+02 
c  Velocity[X]                                      0.14546E+01 
c  Velocity[Y]                                      0.94696E+00 
c  Velocity[Z]                                      0.10352E-29 
c  Pressure     0.15370E-06     457   0.91230E-08   0.15127E+00 0.30329E+03 
c  nu_tilda     0.44672E-05      32   0.96320E-05   0.21031E-06 0.15193E+03 
c  TempC        0.26745E+02      28   0.50863E-03   0.87392E+01 0.29362E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2771           9.891          4.5729          4.5729
v  Velocity[Y]            -3.9462          7.0974        0.018932        0.018932
v  Velocity[Z]       -6.9287e-015     9.8786e-015    -1.4777e-017    -1.4777e-017
v  ǁVelocityǁ         0.0021094          9.8919           5.082           5.082
v  Pressure               -52.391          21.126         -3.8099         -3.8099
v  nu_tilda            4.318e-007       0.0042681      0.00086813      0.00086813
v  TempC                       21          73.739          21.527          21.527
v  TurbVisc           3.0576e-014       0.0050303       0.0010118       0.0010118
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              619:        0.32400E+01

===============================================================


 INSTANT    0.620000000E+03   TIME STEP NUMBER             620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10686E-01 0.88238E+00
   Friction velocity        uk    :  0.10686E-01 0.88238E+00
   Dimensionless distance   yplus :  0.86028E-01 0.71038E+01
   Friction thermal sca.    tstar : -0.16281E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64187E-01 0.53002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62808E-02      33   0.40431E-03   0.23930E+01 0.94464E+02 
c  Velocity[X]                                      0.14550E+01 
c  Velocity[Y]                                      0.93798E+00 
c  Velocity[Z]                                      0.11430E-29 
c  Pressure     0.14074E-06     248   0.97348E-08   0.14169E+00 0.22570E+03 
c  nu_tilda     0.44691E-05      32   0.13307E-04   0.20991E-06 0.15170E+03 
c  TempC        0.26758E+02      29   0.58881E-03   0.72766E+01 0.26374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2767          9.8946          4.5729          4.5729
v  Velocity[Y]            -3.9412          7.0705        0.018956        0.018956
v  Velocity[Z]       -6.9287e-015     9.9784e-015     -1.476e-017     -1.476e-017
v  ǁVelocityǁ         0.0019383          9.8956          5.0826          5.0826
v  Pressure               -52.366          21.089         -3.8105         -3.8105
v  nu_tilda           4.3189e-007       0.0042681      0.00086874      0.00086874
v  TempC                       21          73.057          21.528          21.528
v  TurbVisc           3.0585e-014       0.0050303       0.0010125       0.0010125
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              620:        0.24740E+01

===============================================================


 INSTANT    0.621000000E+03   TIME STEP NUMBER             621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93441E-02 0.88137E+00
   Friction velocity        uk    :  0.93441E-02 0.88137E+00
   Dimensionless distance   yplus :  0.75226E-01 0.70956E+01
   Friction thermal sca.    tstar : -0.15135E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56127E-01 0.52941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62849E-02      33   0.43197E-03   0.23294E+01 0.93740E+02 
c  Velocity[X]                                      0.14147E+01 
c  Velocity[Y]                                      0.91466E+00 
c  Velocity[Z]                                      0.11061E-29 
c  Pressure     0.10863E-06     394   0.92095E-08   0.10766E+00 0.59693E+03 
c  nu_tilda     0.44710E-05      32   0.95936E-05   0.20954E-06 0.15149E+03 
c  TempC        0.26771E+02      29   0.43410E-03   0.15448E+02 0.37836E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2761          9.8981          4.5729          4.5729
v  Velocity[Y]            -3.9364          7.0946        0.018981        0.018981
v  Velocity[Z]       -6.9287e-015     1.0145e-014    -1.4741e-017    -1.4741e-017
v  ǁVelocityǁ          0.002142          9.8991          5.0832          5.0832
v  Pressure               -52.397          21.193         -3.8099         -3.8099
v  nu_tilda           4.3201e-007       0.0042681      0.00086936      0.00086936
v  TempC                       21          73.058          21.528          21.528
v  TurbVisc            3.061e-014       0.0050304       0.0010132       0.0010132
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              621:        0.30510E+01

===============================================================


 INSTANT    0.622000000E+03   TIME STEP NUMBER             622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11166E-01 0.88227E+00
   Friction velocity        uk    :  0.11166E-01 0.88227E+00
   Dimensionless distance   yplus :  0.89892E-01 0.71029E+01
   Friction thermal sca.    tstar : -0.85862E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67069E-01 0.52996E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62891E-02      33   0.45584E-03   0.23470E+01 0.93841E+02 
c  Velocity[X]                                      0.14161E+01 
c  Velocity[Y]                                      0.93088E+00 
c  Velocity[Z]                                      0.91897E-30 
c  Pressure     0.13271E-06     424   0.96390E-08   0.13422E+00 0.37091E+03 
c  nu_tilda     0.44730E-05      32   0.13325E-04   0.20915E-06 0.15127E+03 
c  TempC        0.26784E+02      28   0.54366E-03   0.78933E+01 0.27465E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2757          9.9021          4.5729          4.5729
v  Velocity[Y]            -3.9314          7.0714        0.019004        0.019004
v  Velocity[Z]       -6.9287e-015     1.0177e-014    -1.4724e-017    -1.4724e-017
v  ǁVelocityǁ         0.0019542           9.903          5.0838          5.0838
v  Pressure               -52.373          21.122         -3.8213         -3.8213
v  nu_tilda           4.3207e-007       0.0042681      0.00086997      0.00086997
v  TempC                       21          73.936          21.529          21.529
v  TurbVisc           3.0643e-014       0.0050304        0.001014        0.001014
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              622:        0.32130E+01

===============================================================


 INSTANT    0.623000000E+03   TIME STEP NUMBER             623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99957E-02 0.88153E+00
   Friction velocity        uk    :  0.99957E-02 0.88153E+00
   Dimensionless distance   yplus :  0.80473E-01 0.70969E+01
   Friction thermal sca.    tstar : -0.68806E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60042E-01 0.52951E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62932E-02      33   0.42291E-03   0.23556E+01 0.93691E+02 
c  Velocity[X]                                      0.14453E+01 
c  Velocity[Y]                                      0.91034E+00 
c  Velocity[Z]                                      0.96294E-30 
c  Pressure     0.15060E-06     312   0.96118E-08   0.14653E+00 0.45367E+03 
c  nu_tilda     0.44749E-05      32   0.95611E-05   0.20879E-06 0.15105E+03 
c  TempC        0.26796E+02      28   0.53406E-03   0.82864E+01 0.29315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2752          9.9062          4.5729          4.5729
v  Velocity[Y]            -3.9263          7.0916        0.019027        0.019027
v  Velocity[Z]       -6.9287e-015     1.0194e-014    -1.4712e-017    -1.4712e-017
v  ǁVelocityǁ         0.0020804          9.9071          5.0844          5.0844
v  Pressure               -52.401          21.192         -3.8271         -3.8271
v  nu_tilda           4.3215e-007       0.0042681      0.00087058      0.00087058
v  TempC                       21          73.057          21.529          21.529
v  TurbVisc           3.0661e-014       0.0050304       0.0010147       0.0010147
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              623:        0.28040E+01

===============================================================


 INSTANT    0.624000000E+03   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10455E-01 0.88285E+00
   Friction velocity        uk    :  0.10455E-01 0.88285E+00
   Dimensionless distance   yplus :  0.84168E-01 0.71075E+01
   Friction thermal sca.    tstar : -0.56303E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62799E-01 0.53030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.62974E-02      33   0.46256E-03   0.23373E+01 0.93523E+02 
c  Velocity[X]                                      0.14379E+01 
c  Velocity[Y]                                      0.89941E+00 
c  Velocity[Z]                                      0.10296E-29 
c  Pressure     0.11416E-06     394   0.99866E-08   0.11591E+00 0.26004E+03 
c  nu_tilda     0.44768E-05      32   0.13340E-04   0.20842E-06 0.15084E+03 
c  TempC        0.26809E+02      28   0.51324E-03   0.92459E+01 0.29259E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.275          9.9102          4.5729          4.5729
v  Velocity[Y]            -3.9213          7.0694        0.019049        0.019049
v  Velocity[Z]       -6.9287e-015     1.0158e-014    -1.4701e-017    -1.4701e-017
v  ǁVelocityǁ          0.001954          9.9111           5.085           5.085
v  Pressure               -52.384          21.152         -3.8357         -3.8357
v  nu_tilda           4.3224e-007       0.0042681       0.0008712       0.0008712
v  TempC                       21          73.793           21.53           21.53
v  TurbVisc           3.0685e-014       0.0050304       0.0010154       0.0010154
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              624:        0.31810E+01

===============================================================


 INSTANT    0.625000000E+03   TIME STEP NUMBER             625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98757E-02 0.88180E+00
   Friction velocity        uk    :  0.98757E-02 0.88180E+00
   Dimensionless distance   yplus :  0.79506E-01 0.70991E+01
   Friction thermal sca.    tstar : -0.53150E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59320E-01 0.52967E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63015E-02      33   0.36767E-03   0.23323E+01 0.93435E+02 
c  Velocity[X]                                      0.14169E+01 
c  Velocity[Y]                                      0.91538E+00 
c  Velocity[Z]                                      0.98107E-30 
c  Pressure     0.14816E-06     373   0.99575E-08   0.14754E+00 0.55741E+03 
c  nu_tilda     0.44787E-05      32   0.95298E-05   0.20806E-06 0.15062E+03 
c  TempC        0.26822E+02      28   0.53076E-03   0.86833E+01 0.27909E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2747           9.914          4.5729          4.5729
v  Velocity[Y]            -3.9163          7.0926        0.019071        0.019071
v  Velocity[Z]       -6.9287e-015     1.0147e-014    -1.4691e-017    -1.4691e-017
v  ǁVelocityǁ         0.0020983          9.9148          5.0856          5.0856
v  Pressure               -52.417          21.243         -3.8361         -3.8361
v  nu_tilda           4.3226e-007       0.0042681      0.00087181      0.00087181
v  TempC                       21          73.058          21.531          21.531
v  TurbVisc            3.071e-014       0.0050304       0.0010162       0.0010162
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              625:        0.30730E+01

===============================================================


 INSTANT    0.626000000E+03   TIME STEP NUMBER             626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10419E-01 0.88277E+00
   Friction velocity        uk    :  0.10419E-01 0.88277E+00
   Dimensionless distance   yplus :  0.83884E-01 0.71069E+01
   Friction thermal sca.    tstar : -0.53459E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62587E-01 0.53026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63057E-02      33   0.43508E-03   0.22971E+01 0.92941E+02 
c  Velocity[X]                                      0.14008E+01 
c  Velocity[Y]                                      0.89632E+00 
c  Velocity[Z]                                      0.12321E-29 
c  Pressure     0.12340E-06     298   0.99382E-08   0.12147E+00 0.14675E+03 
c  nu_tilda     0.44807E-05      32   0.13349E-04   0.20769E-06 0.15041E+03 
c  TempC        0.26834E+02      28   0.67985E-03   0.83585E+01 0.30177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2741          9.9178          4.5729          4.5729
v  Velocity[Y]            -3.9111          7.0882        0.019092        0.019092
v  Velocity[Z]       -6.9287e-015     1.0311e-014    -1.4673e-017    -1.4673e-017
v  ǁVelocityǁ         0.0020971          9.9187          5.0862          5.0862
v  Pressure               -52.401          21.244         -3.8387         -3.8387
v  nu_tilda           4.3216e-007       0.0042681      0.00087242      0.00087242
v  TempC                       21          73.058          21.531          21.531
v  TurbVisc           3.0716e-014       0.0050304       0.0010169       0.0010169
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              626:        0.27290E+01

===============================================================


 INSTANT    0.627000000E+03   TIME STEP NUMBER             627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11251E-01 0.88196E+00
   Friction velocity        uk    :  0.11251E-01 0.88196E+00
   Dimensionless distance   yplus :  0.90577E-01 0.71004E+01
   Friction thermal sca.    tstar : -0.57513E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67581E-01 0.52977E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63098E-02      33   0.46451E-03   0.23185E+01 0.93038E+02 
c  Velocity[X]                                      0.14332E+01 
c  Velocity[Y]                                      0.88533E+00 
c  Velocity[Z]                                      0.97656E-30 
c  Pressure     0.14686E-06     453   0.90064E-08   0.14778E+00 0.39462E+03 
c  nu_tilda     0.44826E-05      32   0.94780E-05   0.20734E-06 0.15020E+03 
c  TempC        0.26847E+02      28   0.50330E-03   0.11664E+02 0.37147E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2737          9.9215          4.5729          4.5729
v  Velocity[Y]            -3.9058          7.0651        0.019113        0.019113
v  Velocity[Z]       -6.9287e-015     1.0219e-014    -1.4662e-017    -1.4662e-017
v  ǁVelocityǁ         0.0019844          9.9225          5.0868          5.0868
v  Pressure               -52.414          21.155         -3.8705         -3.8705
v  nu_tilda           4.3215e-007       0.0042682      0.00087303      0.00087303
v  TempC                       21          73.922          21.532          21.532
v  TurbVisc           3.0685e-014       0.0050304       0.0010176       0.0010176
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              627:        0.35360E+01

===============================================================


 INSTANT    0.628000000E+03   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70342E-02 0.88105E+00
   Friction velocity        uk    :  0.70342E-02 0.88105E+00
   Dimensionless distance   yplus :  0.56630E-01 0.70930E+01
   Friction thermal sca.    tstar : -0.63589E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42252E-01 0.52922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63139E-02      33   0.43456E-03   0.22994E+01 0.92909E+02 
c  Velocity[X]                                      0.13990E+01 
c  Velocity[Y]                                      0.90033E+00 
c  Velocity[Z]                                      0.94946E-30 
c  Pressure     0.13991E-06     457   0.99122E-08   0.14074E+00 0.55383E+03 
c  nu_tilda     0.44845E-05      32   0.13374E-04   0.20698E-06 0.14999E+03 
c  TempC        0.26860E+02      28   0.34073E-03   0.85385E+01 0.29524E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2729           9.925          4.5729          4.5729
v  Velocity[Y]            -3.9008           7.084        0.019132        0.019132
v  Velocity[Z]       -6.9287e-015     9.9127e-015    -1.4651e-017    -1.4651e-017
v  ǁVelocityǁ         0.0021248          9.9261          5.0874          5.0874
v  Pressure               -52.413           21.28         -3.8509         -3.8509
v  nu_tilda           4.3211e-007       0.0042682      0.00087364      0.00087364
v  TempC                       21          73.058          21.532          21.532
v  TurbVisc           3.0682e-014       0.0050305       0.0010183       0.0010183
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              628:        0.33800E+01

===============================================================


 INSTANT    0.629000000E+03   TIME STEP NUMBER             629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11579E-01 0.88198E+00
   Friction velocity        uk    :  0.11579E-01 0.88198E+00
   Dimensionless distance   yplus :  0.93222E-01 0.71006E+01
   Friction thermal sca.    tstar : -0.81847E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69554E-01 0.52978E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63181E-02      33   0.42751E-03   0.22857E+01 0.92707E+02 
c  Velocity[X]                                      0.13906E+01 
c  Velocity[Y]                                      0.89511E+00 
c  Velocity[Z]                                      0.10119E-29 
c  Pressure     0.12351E-06     456   0.98003E-08   0.12454E+00 0.41153E+03 
c  nu_tilda     0.44864E-05      32   0.94244E-05   0.20664E-06 0.14978E+03 
c  TempC        0.26872E+02      28   0.59512E-03   0.61982E+01 0.25009E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2722          9.9285          4.5729          4.5729
v  Velocity[Y]            -3.8956          7.0669        0.019152        0.019152
v  Velocity[Z]       -6.9287e-015     9.6738e-015    -1.4647e-017    -1.4647e-017
v  ǁVelocityǁ         0.0020232          9.9296           5.088           5.088
v  Pressure               -52.434          21.193         -3.8852         -3.8852
v  nu_tilda            4.321e-007       0.0042682      0.00087425      0.00087425
v  TempC                       21          73.058          21.533          21.533
v  TurbVisc           3.0673e-014       0.0050305       0.0010191       0.0010191
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              629:        0.33030E+01

===============================================================


 INSTANT    0.630000000E+03   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93169E-02 0.88115E+00
   Friction velocity        uk    :  0.93169E-02 0.88115E+00
   Dimensionless distance   yplus :  0.75008E-01 0.70939E+01
   Friction thermal sca.    tstar : -0.11996E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55964E-01 0.52928E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63222E-02      33   0.50099E-03   0.22592E+01 0.92279E+02 
c  Velocity[X]                                      0.13888E+01 
c  Velocity[Y]                                      0.87042E+00 
c  Velocity[Z]                                      0.10135E-29 
c  Pressure     0.12473E-06     453   0.91006E-08   0.12328E+00 0.55552E+03 
c  nu_tilda     0.44883E-05      32   0.13392E-04   0.20629E-06 0.14958E+03 
c  TempC        0.26885E+02      29   0.48790E-03   0.89271E+01 0.29527E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2716          9.9319          4.5729          4.5729
v  Velocity[Y]            -3.8902          7.0887        0.019171        0.019171
v  Velocity[Z]       -6.9287e-015     9.4126e-015    -1.4636e-017    -1.4636e-017
v  ǁVelocityǁ         0.0021161          9.9329          5.0886          5.0886
v  Pressure               -52.413          21.302          -3.861          -3.861
v  nu_tilda           4.3207e-007       0.0042682      0.00087486      0.00087486
v  TempC                       21          73.709          21.534          21.534
v  TurbVisc           3.0669e-014       0.0050305       0.0010198       0.0010198
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              630:        0.33530E+01

===============================================================


 INSTANT    0.631000000E+03   TIME STEP NUMBER             631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11935E-01 0.88225E+00
   Friction velocity        uk    :  0.11935E-01 0.88225E+00
   Dimensionless distance   yplus :  0.96081E-01 0.71028E+01
   Friction thermal sca.    tstar : -0.29892E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71687E-01 0.52994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63263E-02      33   0.45928E-03   0.23124E+01 0.92766E+02 
c  Velocity[X]                                      0.14226E+01 
c  Velocity[Y]                                      0.88981E+00 
c  Velocity[Z]                                      0.11720E-29 
c  Pressure     0.13519E-06     437   0.95199E-08   0.13344E+00 0.24289E+03 
c  nu_tilda     0.44902E-05      32   0.93841E-05   0.20595E-06 0.14937E+03 
c  TempC        0.26898E+02      28   0.72905E-03   0.77364E+01 0.28384E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2709          9.9352          4.5729          4.5729
v  Velocity[Y]             -3.885           7.086         0.01919         0.01919
v  Velocity[Z]       -6.9287e-015     9.1429e-015    -1.4637e-017    -1.4637e-017
v  ǁVelocityǁ        0.00097105          9.9362          5.0892          5.0892
v  Pressure               -52.442            21.3          -3.883          -3.883
v  nu_tilda           4.3207e-007       0.0042682      0.00087547      0.00087547
v  TempC                       21          73.408          21.534          21.534
v  TurbVisc           3.0661e-014       0.0050305       0.0010205       0.0010205
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              631:        0.32530E+01

===============================================================


 INSTANT    0.632000000E+03   TIME STEP NUMBER             632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11086E-01 0.88178E+00
   Friction velocity        uk    :  0.11086E-01 0.88178E+00
   Dimensionless distance   yplus :  0.89247E-01 0.70989E+01
   Friction thermal sca.    tstar : -0.10433E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66588E-01 0.52966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63305E-02      33   0.38365E-03   0.22898E+01 0.92499E+02 
c  Velocity[X]                                      0.14189E+01 
c  Velocity[Y]                                      0.87089E+00 
c  Velocity[Z]                                      0.10890E-29 
c  Pressure     0.13477E-06     442   0.94894E-08   0.13561E+00 0.46694E+03 
c  nu_tilda     0.44921E-05      32   0.13401E-04   0.20561E-06 0.14917E+03 
c  TempC        0.26910E+02      28   0.54889E-03   0.13525E+02 0.39384E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2699          9.9384          4.5729          4.5729
v  Velocity[Y]            -3.8798           7.059        0.019206        0.019206
v  Velocity[Z]       -6.9287e-015     9.0489e-015    -1.4631e-017    -1.4631e-017
v  ǁVelocityǁ         0.0019321          9.9394          5.0898          5.0898
v  Pressure                -52.43          21.215         -3.9038         -3.9038
v  nu_tilda            4.321e-007       0.0042682      0.00087608      0.00087608
v  TempC                       21          73.058          21.535          21.535
v  TurbVisc           3.0659e-014       0.0050305       0.0010213       0.0010213
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              632:        0.31910E+01

===============================================================


 INSTANT    0.633000000E+03   TIME STEP NUMBER             633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95789E-02 0.88057E+00
   Friction velocity        uk    :  0.95789E-02 0.88057E+00
   Dimensionless distance   yplus :  0.77117E-01 0.70892E+01
   Friction thermal sca.    tstar : -0.72514E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57538E-01 0.52893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63346E-02      33   0.43985E-03   0.22361E+01 0.91817E+02 
c  Velocity[X]                                      0.13783E+01 
c  Velocity[Y]                                      0.85773E+00 
c  Velocity[Z]                                      0.10846E-29 
c  Pressure     0.12437E-06     410   0.92680E-08   0.12524E+00 0.64211E+03 
c  nu_tilda     0.44940E-05      32   0.93590E-05   0.20528E-06 0.14897E+03 
c  TempC        0.26923E+02      28   0.46419E-03   0.83777E+01 0.32147E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2694          9.9414          4.5729          4.5729
v  Velocity[Y]            -3.8744          7.0826        0.019224        0.019224
v  Velocity[Z]       -6.9287e-015      9.021e-015    -1.4626e-017    -1.4626e-017
v  ǁVelocityǁ           0.00207          9.9426          5.0904          5.0904
v  Pressure               -52.451          21.315         -3.8972         -3.8972
v  nu_tilda           4.3208e-007       0.0042682      0.00087669      0.00087669
v  TempC                       21          73.779          21.535          21.535
v  TurbVisc           3.0669e-014       0.0050305        0.001022        0.001022
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              633:        0.39280E+01

===============================================================


 INSTANT    0.634000000E+03   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10597E-01 0.88171E+00
   Friction velocity        uk    :  0.10597E-01 0.88171E+00
   Dimensionless distance   yplus :  0.85312E-01 0.70984E+01
   Friction thermal sca.    tstar : -0.65927E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63653E-01 0.52962E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63387E-02      33   0.46428E-03   0.22777E+01 0.92151E+02 
c  Velocity[X]                                      0.14009E+01 
c  Velocity[Y]                                      0.87680E+00 
c  Velocity[Z]                                      0.95379E-30 
c  Pressure     0.13632E-06     470   0.93233E-08   0.13527E+00 0.50990E+03 
c  nu_tilda     0.44959E-05      32   0.13415E-04   0.20495E-06 0.14877E+03 
c  TempC        0.26935E+02      28   0.57370E-03   0.75518E+01 0.28378E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2687          9.9444          4.5729          4.5729
v  Velocity[Y]            -3.8691          7.0543         0.01924         0.01924
v  Velocity[Z]       -6.9287e-015     9.0573e-015    -1.4619e-017    -1.4619e-017
v  ǁVelocityǁ         0.0018749          9.9456           5.091           5.091
v  Pressure               -52.433          21.222         -3.9183         -3.9183
v  nu_tilda           4.3209e-007       0.0042682       0.0008773       0.0008773
v  TempC                       21          73.573          21.536          21.536
v  TurbVisc           3.0665e-014       0.0050305       0.0010227       0.0010227
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              634:        0.34650E+01

===============================================================


 INSTANT    0.635000000E+03   TIME STEP NUMBER             635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91612E-02 0.88110E+00
   Friction velocity        uk    :  0.91612E-02 0.88110E+00
   Dimensionless distance   yplus :  0.73754E-01 0.70935E+01
   Friction thermal sca.    tstar : -0.17554E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55029E-01 0.52925E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63428E-02      33   0.42801E-03   0.22860E+01 0.92234E+02 
c  Velocity[X]                                      0.14173E+01 
c  Velocity[Y]                                      0.86871E+00 
c  Velocity[Z]                                      0.84628E-30 
c  Pressure     0.13405E-06     405   0.93921E-08   0.13311E+00 0.64573E+03 
c  nu_tilda     0.44978E-05      32   0.93043E-05   0.20463E-06 0.14857E+03 
c  TempC        0.26948E+02      28   0.36882E-03   0.82962E+01 0.29000E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2681          9.9472          4.5729          4.5729
v  Velocity[Y]            -3.8638          7.0816        0.019256        0.019256
v  Velocity[Z]       -6.9287e-015     9.1232e-015     -1.461e-017     -1.461e-017
v  ǁVelocityǁ         0.0020366          9.9485          5.0915          5.0915
v  Pressure               -52.457          21.328         -3.9124         -3.9124
v  nu_tilda           4.3206e-007       0.0042682      0.00087791      0.00087791
v  TempC                       21          73.058          21.537          21.537
v  TurbVisc           3.0667e-014       0.0050305       0.0010234       0.0010234
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              635:        0.30920E+01

===============================================================


 INSTANT    0.636000000E+03   TIME STEP NUMBER             636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86734E-02 0.88238E+00
   Friction velocity        uk    :  0.86734E-02 0.88238E+00
   Dimensionless distance   yplus :  0.69827E-01 0.71038E+01
   Friction thermal sca.    tstar : -0.93071E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52099E-01 0.53002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63469E-02      33   0.41553E-03   0.22079E+01 0.91362E+02 
c  Velocity[X]                                      0.13627E+01 
c  Velocity[Y]                                      0.84520E+00 
c  Velocity[Z]                                      0.10590E-29 
c  Pressure     0.10166E-06     377   0.96790E-08   0.10170E+00 0.17420E+03 
c  nu_tilda     0.44997E-05      32   0.13431E-04   0.20431E-06 0.14837E+03 
c  TempC        0.26961E+02      28   0.50459E-03   0.61677E+01 0.25141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2673          9.9499          4.5729          4.5729
v  Velocity[Y]            -3.8585          7.0874        0.019271        0.019271
v  Velocity[Z]       -6.9287e-015     9.1154e-015    -1.4602e-017    -1.4602e-017
v  ǁVelocityǁ         0.0021494          9.9513          5.0921          5.0921
v  Pressure               -52.446          21.363         -3.9099         -3.9099
v  nu_tilda           4.3195e-007       0.0042683      0.00087852      0.00087852
v  TempC                       21          73.654          21.537          21.537
v  TurbVisc           3.0658e-014       0.0050306       0.0010242       0.0010242
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              636:        0.29620E+01

===============================================================


 INSTANT    0.637000000E+03   TIME STEP NUMBER             637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12310E-01 0.88166E+00
   Friction velocity        uk    :  0.12310E-01 0.88166E+00
   Dimensionless distance   yplus :  0.99107E-01 0.70979E+01
   Friction thermal sca.    tstar : -0.13788E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73945E-01 0.52959E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63511E-02      33   0.44095E-03   0.22256E+01 0.91416E+02 
c  Velocity[X]                                      0.13739E+01 
c  Velocity[Y]                                      0.85171E+00 
c  Velocity[Z]                                      0.10903E-29 
c  Pressure     0.11912E-06     442   0.99905E-08   0.12122E+00 0.37017E+03 
c  nu_tilda     0.45016E-05      32   0.92967E-05   0.20400E-06 0.14817E+03 
c  TempC        0.26973E+02      28   0.38119E-03   0.76288E+01 0.27472E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2666          9.9527          4.5729          4.5729
v  Velocity[Y]            -3.8531          7.0624        0.019286        0.019286
v  Velocity[Z]       -6.9287e-015     9.1436e-015    -1.4589e-017    -1.4589e-017
v  ǁVelocityǁ          0.001977           9.954          5.0927          5.0927
v  Pressure               -52.465           21.28         -3.9407         -3.9407
v  nu_tilda           4.3186e-007       0.0042683      0.00087913      0.00087913
v  TempC                       21          73.875          21.538          21.538
v  TurbVisc           3.0626e-014       0.0050306       0.0010249       0.0010249
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              637:        0.32330E+01

===============================================================


 INSTANT    0.638000000E+03   TIME STEP NUMBER             638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47067E-02 0.88017E+00
   Friction velocity        uk    :  0.47067E-02 0.88017E+00
   Dimensionless distance   yplus :  0.37892E-01 0.70860E+01
   Friction thermal sca.    tstar : -0.79831E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28272E-01 0.52869E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63552E-02      33   0.44943E-03   0.22398E+01 0.91395E+02 
c  Velocity[X]                                      0.14030E+01 
c  Velocity[Y]                                      0.83681E+00 
c  Velocity[Z]                                      0.93095E-30 
c  Pressure     0.16357E-06     441   0.94073E-08   0.15985E+00 0.49449E+03 
c  nu_tilda     0.45035E-05      32   0.13447E-04   0.20367E-06 0.14798E+03 
c  TempC        0.26986E+02      28   0.53650E-03   0.88115E+01 0.28767E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2661          9.9552          4.5729          4.5729
v  Velocity[Y]            -3.8477           7.074          0.0193          0.0193
v  Velocity[Z]       -6.9287e-015     9.0729e-015    -1.4571e-017    -1.4571e-017
v  ǁVelocityǁ         0.0020198          9.9567          5.0933          5.0933
v  Pressure                -52.44          21.372         -3.9185         -3.9185
v  nu_tilda           4.3182e-007       0.0042683      0.00087973      0.00087973
v  TempC                       21          73.058          21.538          21.538
v  TurbVisc           3.0601e-014       0.0050306       0.0010256       0.0010256
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              638:        0.33250E+01

===============================================================


 INSTANT    0.639000000E+03   TIME STEP NUMBER             639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10536E-01 0.88124E+00
   Friction velocity        uk    :  0.10536E-01 0.88124E+00
   Dimensionless distance   yplus :  0.84822E-01 0.70946E+01
   Friction thermal sca.    tstar : -0.13561E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63287E-01 0.52934E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63593E-02      33   0.44939E-03   0.22425E+01 0.91440E+02 
c  Velocity[X]                                      0.14120E+01 
c  Velocity[Y]                                      0.83043E+00 
c  Velocity[Z]                                      0.11690E-29 
c  Pressure     0.13583E-06     458   0.98459E-08   0.13762E+00 0.53703E+03 
c  nu_tilda     0.45054E-05      32   0.92335E-05   0.20337E-06 0.14778E+03 
c  TempC        0.26998E+02      28   0.72136E-03   0.89023E+01 0.28974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2652          9.9583          4.5729          4.5729
v  Velocity[Y]            -3.8426          7.0553        0.019313        0.019313
v  Velocity[Z]       -6.9287e-015     9.0324e-015    -1.4563e-017    -1.4563e-017
v  ǁVelocityǁ         0.0019547          9.9596          5.0939          5.0939
v  Pressure               -52.472          21.271         -3.9631         -3.9631
v  nu_tilda           4.3186e-007       0.0042683      0.00088034      0.00088034
v  TempC                       21          73.518          21.539          21.539
v  TurbVisc           3.0589e-014       0.0050306       0.0010263       0.0010263
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              639:        0.33630E+01

===============================================================


 INSTANT    0.640000000E+03   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76269E-02 0.88059E+00
   Friction velocity        uk    :  0.76269E-02 0.88059E+00
   Dimensionless distance   yplus :  0.61401E-01 0.70894E+01
   Friction thermal sca.    tstar : -0.89723E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45812E-01 0.52895E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63634E-02      33   0.40831E-03   0.22005E+01 0.91001E+02 
c  Velocity[X]                                      0.13646E+01 
c  Velocity[Y]                                      0.83593E+00 
c  Velocity[Z]                                      0.10911E-29 
c  Pressure     0.94120E-07     442   0.96359E-08   0.93743E-01 0.61554E+03 
c  nu_tilda     0.45072E-05      32   0.13456E-04   0.20306E-06 0.14759E+03 
c  TempC        0.27011E+02      28   0.46710E-03   0.91131E+01 0.30315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2643          9.9614          4.5729          4.5729
v  Velocity[Y]            -3.8372          7.0753        0.019326        0.019326
v  Velocity[Z]       -6.9287e-015     8.9928e-015    -1.4551e-017    -1.4551e-017
v  ǁVelocityǁ         0.0020747          9.9627          5.0945          5.0945
v  Pressure               -52.461          21.401         -3.9382         -3.9382
v  nu_tilda           4.3187e-007       0.0042683      0.00088094      0.00088094
v  TempC                       21          73.264          21.539          21.539
v  TurbVisc           3.0601e-014       0.0050306        0.001027        0.001027
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              640:        0.32050E+01

===============================================================


 INSTANT    0.641000000E+03   TIME STEP NUMBER             641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11398E-01 0.88172E+00
   Friction velocity        uk    :  0.11398E-01 0.88172E+00
   Dimensionless distance   yplus :  0.91760E-01 0.70984E+01
   Friction thermal sca.    tstar : -0.16573E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68464E-01 0.52962E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63675E-02      33   0.39241E-03   0.21596E+01 0.90535E+02 
c  Velocity[X]                                      0.13333E+01 
c  Velocity[Y]                                      0.82626E+00 
c  Velocity[Z]                                      0.10942E-29 
c  Pressure     0.11105E-06     421   0.90167E-08   0.11039E+00 0.23782E+03 
c  nu_tilda     0.45091E-05      32   0.92178E-05   0.20277E-06 0.14740E+03 
c  TempC        0.27023E+02      28   0.46519E-03   0.79001E+01 0.26824E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2633          9.9644          4.5729          4.5729
v  Velocity[Y]            -3.8319          7.0862        0.019338        0.019338
v  Velocity[Z]       -6.9287e-015     9.0428e-015    -1.4532e-017    -1.4532e-017
v  ǁVelocityǁ         0.0021145          9.9658          5.0951          5.0951
v  Pressure               -52.484          21.398         -3.9577         -3.9577
v  nu_tilda           4.3189e-007       0.0042683      0.00088155      0.00088155
v  TempC                       21          73.578           21.54           21.54
v  TurbVisc           3.0604e-014       0.0050306       0.0010278       0.0010278
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              641:        0.31300E+01

===============================================================


 INSTANT    0.642000000E+03   TIME STEP NUMBER             642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10655E-01 0.88117E+00
   Friction velocity        uk    :  0.10655E-01 0.88117E+00
   Dimensionless distance   yplus :  0.85779E-01 0.70940E+01
   Friction thermal sca.    tstar : -0.14790E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64001E-01 0.52929E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63716E-02      33   0.44664E-03   0.21842E+01 0.90597E+02 
c  Velocity[X]                                      0.13657E+01 
c  Velocity[Y]                                      0.81847E+00 
c  Velocity[Z]                                      0.94918E-30 
c  Pressure     0.12560E-06     424   0.96577E-08   0.12731E+00 0.46034E+03 
c  nu_tilda     0.45110E-05      32   0.13478E-04   0.20246E-06 0.14721E+03 
c  TempC        0.27036E+02      28   0.44958E-03   0.76280E+01 0.28241E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2624          9.9673          4.5729          4.5729
v  Velocity[Y]            -3.8265          7.0542        0.019349        0.019349
v  Velocity[Z]       -6.9287e-015     9.1116e-015    -1.4518e-017    -1.4518e-017
v  ǁVelocityǁ         0.0018898          9.9686          5.0957          5.0957
v  Pressure               -52.463          21.305         -3.9751         -3.9751
v  nu_tilda           4.3198e-007       0.0042683      0.00088216      0.00088216
v  TempC                       21          73.336          21.541          21.541
v  TurbVisc            3.061e-014       0.0050306       0.0010285       0.0010285
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              642:        0.35770E+01

===============================================================


 INSTANT    0.643000000E+03   TIME STEP NUMBER             643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81303E-02 0.87986E+00
   Friction velocity        uk    :  0.81303E-02 0.87986E+00
   Dimensionless distance   yplus :  0.65455E-01 0.70835E+01
   Friction thermal sca.    tstar : -0.90862E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48837E-01 0.52851E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63757E-02      33   0.43119E-03   0.21951E+01 0.90711E+02 
c  Velocity[X]                                      0.13649E+01 
c  Velocity[Y]                                      0.83021E+00 
c  Velocity[Z]                                      0.10762E-29 
c  Pressure     0.10736E-06     409   0.94776E-08   0.10621E+00 0.61327E+03 
c  nu_tilda     0.45129E-05      32   0.91835E-05   0.20218E-06 0.14703E+03 
c  TempC        0.27048E+02      28   0.45829E-03   0.64203E+01 0.25867E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2619          9.9702          4.5729          4.5729
v  Velocity[Y]            -3.8213          7.0732         0.01936         0.01936
v  Velocity[Z]       -6.9287e-015     9.2183e-015    -1.4503e-017    -1.4503e-017
v  ǁVelocityǁ         0.0020197          9.9715          5.0963          5.0963
v  Pressure               -52.493          21.408         -3.9721         -3.9721
v  nu_tilda           4.3201e-007       0.0042683      0.00088276      0.00088276
v  TempC                       21          73.647          21.541          21.541
v  TurbVisc           3.0636e-014       0.0050306       0.0010292       0.0010292
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              643:        0.38080E+01

===============================================================


 INSTANT    0.644000000E+03   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93696E-02 0.88105E+00
   Friction velocity        uk    :  0.93696E-02 0.88105E+00
   Dimensionless distance   yplus :  0.75432E-01 0.70931E+01
   Friction thermal sca.    tstar : -0.68562E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56280E-01 0.52922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63798E-02      33   0.41458E-03   0.21862E+01 0.90588E+02 
c  Velocity[X]                                      0.13689E+01 
c  Velocity[Y]                                      0.81727E+00 
c  Velocity[Z]                                      0.11621E-29 
c  Pressure     0.13413E-06     408   0.96857E-08   0.13628E+00 0.28837E+03 
c  nu_tilda     0.45147E-05      32   0.13479E-04   0.20188E-06 0.14684E+03 
c  TempC        0.27061E+02      28   0.43026E-03   0.83742E+01 0.28156E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2612          9.9729          4.5729          4.5729
v  Velocity[Y]             -3.816          7.0528         0.01937         0.01937
v  Velocity[Z]       -6.9287e-015     9.2599e-015    -1.4481e-017    -1.4481e-017
v  ǁVelocityǁ         0.0019199          9.9744          5.0969          5.0969
v  Pressure               -52.475          21.366         -3.9834         -3.9834
v  nu_tilda           4.3195e-007       0.0042683      0.00088337      0.00088337
v  TempC                       21          73.296          21.542          21.542
v  TurbVisc           3.0644e-014       0.0050307       0.0010299       0.0010299
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              644:        0.37280E+01

===============================================================


 INSTANT    0.645000000E+03   TIME STEP NUMBER             645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94489E-02 0.88000E+00
   Friction velocity        uk    :  0.94489E-02 0.88000E+00
   Dimensionless distance   yplus :  0.76070E-01 0.70846E+01
   Friction thermal sca.    tstar : -0.60278E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56757E-01 0.52859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63839E-02      33   0.43441E-03   0.21517E+01 0.90111E+02 
c  Velocity[X]                                      0.13474E+01 
c  Velocity[Y]                                      0.80429E+00 
c  Velocity[Z]                                      0.92470E-30 
c  Pressure     0.11403E-06     376   0.99781E-08   0.11343E+00 0.50030E+03 
c  nu_tilda     0.45166E-05      32   0.91503E-05   0.20161E-06 0.14666E+03 
c  TempC        0.27073E+02      28   0.49479E-03   0.63594E+01 0.24956E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2606          9.9755          4.5729          4.5729
v  Velocity[Y]            -3.8107          7.0772         0.01938         0.01938
v  Velocity[Z]       -6.9287e-015     9.2239e-015    -1.4463e-017    -1.4463e-017
v  ǁVelocityǁ         0.0020336          9.9771          5.0975          5.0975
v  Pressure               -52.493          21.439         -3.9837         -3.9837
v  nu_tilda           4.3186e-007       0.0042683      0.00088398      0.00088398
v  TempC                       21          73.761          21.542          21.542
v  TurbVisc           3.0626e-014       0.0050307       0.0010307       0.0010307
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              645:        0.34240E+01

===============================================================


 INSTANT    0.646000000E+03   TIME STEP NUMBER             646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98063E-02 0.88115E+00
   Friction velocity        uk    :  0.98063E-02 0.88115E+00
   Dimensionless distance   yplus :  0.78947E-01 0.70939E+01
   Friction thermal sca.    tstar : -0.56854E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58903E-01 0.52928E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63880E-02      33   0.44948E-03   0.21572E+01 0.90120E+02 
c  Velocity[X]                                      0.13438E+01 
c  Velocity[Y]                                      0.81340E+00 
c  Velocity[Z]                                      0.87712E-30 
c  Pressure     0.14551E-06     362   0.93698E-08   0.14423E+00 0.14979E+03 
c  nu_tilda     0.45185E-05      32   0.13498E-04   0.20132E-06 0.14647E+03 
c  TempC        0.27086E+02      28   0.74812E-03   0.83884E+01 0.28357E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2597           9.978          4.5729          4.5729
v  Velocity[Y]            -3.8054          7.0712        0.019388        0.019388
v  Velocity[Z]       -6.9287e-015     9.2072e-015    -1.4446e-017    -1.4446e-017
v  ǁVelocityǁ         0.0020357          9.9795          5.0981          5.0981
v  Pressure               -52.489          21.442         -3.9898         -3.9898
v  nu_tilda           4.3172e-007       0.0042684      0.00088458      0.00088458
v  TempC                       21          73.076          21.543          21.543
v  TurbVisc             3.06e-014       0.0050307       0.0010314       0.0010314
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              646:        0.29550E+01

===============================================================


 INSTANT    0.647000000E+03   TIME STEP NUMBER             647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11021E-01 0.88056E+00
   Friction velocity        uk    :  0.11021E-01 0.88056E+00
   Dimensionless distance   yplus :  0.88726E-01 0.70891E+01
   Friction thermal sca.    tstar : -0.57262E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66199E-01 0.52893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63920E-02      33   0.41844E-03   0.21921E+01 0.90406E+02 
c  Velocity[X]                                      0.13865E+01 
c  Velocity[Y]                                      0.80557E+00 
c  Velocity[Z]                                      0.94052E-30 
c  Pressure     0.12165E-06     488   0.97310E-08   0.12318E+00 0.49394E+03 
c  nu_tilda     0.45203E-05      32   0.91163E-05   0.20104E-06 0.14629E+03 
c  TempC        0.27098E+02      29   0.49325E-03   0.20960E+02 0.45391E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2588          9.9804          4.5729          4.5729
v  Velocity[Y]            -3.8002          7.0483        0.019397        0.019397
v  Velocity[Z]       -6.9287e-015     9.2597e-015    -1.4428e-017    -1.4428e-017
v  ǁVelocityǁ         0.0019138           9.982          5.0987          5.0987
v  Pressure               -52.506          21.335         -4.0288         -4.0288
v  nu_tilda           4.3164e-007       0.0042684      0.00088518      0.00088518
v  TempC                       21          73.059          21.544          21.544
v  TurbVisc           3.0562e-014       0.0050307       0.0010321       0.0010321
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              647:        0.35030E+01

===============================================================


 INSTANT    0.648000000E+03   TIME STEP NUMBER             648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54437E-02 0.87946E+00
   Friction velocity        uk    :  0.54437E-02 0.87946E+00
   Dimensionless distance   yplus :  0.43825E-01 0.70803E+01
   Friction thermal sca.    tstar : -0.56567E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32699E-01 0.52827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63961E-02      33   0.41346E-03   0.21318E+01 0.89713E+02 
c  Velocity[X]                                      0.13390E+01 
c  Velocity[Y]                                      0.79282E+00 
c  Velocity[Z]                                      0.11117E-29 
c  Pressure     0.11203E-06     472   0.98522E-08   0.11124E+00 0.75613E+03 
c  nu_tilda     0.45222E-05      32   0.13514E-04   0.20076E-06 0.14611E+03 
c  TempC        0.27111E+02      28   0.32705E-03   0.79565E+01 0.27303E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2579          9.9827          4.5729          4.5729
v  Velocity[Y]            -3.7948          7.0678        0.019404        0.019404
v  Velocity[Z]       -6.9287e-015     9.2351e-015    -1.4402e-017    -1.4402e-017
v  ǁVelocityǁ         0.0019804          9.9845          5.0993          5.0993
v  Pressure                -52.49          21.486         -3.9958         -3.9958
v  nu_tilda            4.315e-007       0.0042684      0.00088579      0.00088579
v  TempC                       21          73.786          21.544          21.544
v  TurbVisc            3.054e-014       0.0050307       0.0010328       0.0010328
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              648:        0.36960E+01

===============================================================


 INSTANT    0.649000000E+03   TIME STEP NUMBER             649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97611E-02 0.88048E+00
   Friction velocity        uk    :  0.97611E-02 0.88048E+00
   Dimensionless distance   yplus :  0.78583E-01 0.70884E+01
   Friction thermal sca.    tstar : -0.63109E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58632E-01 0.52888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64002E-02      33   0.41806E-03   0.21355E+01 0.89694E+02 
c  Velocity[X]                                      0.13314E+01 
c  Velocity[Y]                                      0.80405E+00 
c  Velocity[Z]                                      0.98857E-30 
c  Pressure     0.11235E-06     457   0.98727E-08   0.11430E+00 0.42521E+03 
c  nu_tilda     0.45241E-05      32   0.90741E-05   0.20050E-06 0.14593E+03 
c  TempC        0.27123E+02      28   0.48988E-03   0.61494E+01 0.23987E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2571          9.9851          4.5729          4.5729
v  Velocity[Y]            -3.7895          7.0505        0.019412        0.019412
v  Velocity[Z]       -6.9287e-015     9.1522e-015    -1.4391e-017    -1.4391e-017
v  ǁVelocityǁ         0.0019289          9.9868          5.0999          5.0999
v  Pressure               -52.515          21.395         -4.0318         -4.0318
v  nu_tilda           4.3132e-007       0.0042684      0.00088639      0.00088639
v  TempC                       21           73.06          21.545          21.545
v  TurbVisc           3.0499e-014       0.0050307       0.0010335       0.0010335
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              649:        0.36460E+01

===============================================================


 INSTANT    0.650000000E+03   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69356E-02 0.87968E+00
   Friction velocity        uk    :  0.69356E-02 0.87968E+00
   Dimensionless distance   yplus :  0.55837E-01 0.70821E+01
   Friction thermal sca.    tstar : -0.70930E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41660E-01 0.52840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64043E-02      33   0.43636E-03   0.21451E+01 0.89628E+02 
c  Velocity[X]                                      0.13550E+01 
c  Velocity[Y]                                      0.79010E+00 
c  Velocity[Z]                                      0.95274E-30 
c  Pressure     0.13856E-06     425   0.90716E-08   0.13644E+00 0.40251E+03 
c  nu_tilda     0.45259E-05      32   0.13517E-04   0.20022E-06 0.14575E+03 
c  TempC        0.27136E+02      28   0.52233E-03   0.84776E+01 0.28103E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2562          9.9872          4.5729          4.5729
v  Velocity[Y]            -3.7845           7.066        0.019418        0.019418
v  Velocity[Z]       -6.9287e-015     8.9429e-015    -1.4371e-017    -1.4371e-017
v  ǁVelocityǁ         0.0019539           9.989          5.1005          5.1005
v  Pressure               -52.497           21.48         -4.0162         -4.0162
v  nu_tilda           4.3112e-007       0.0042684      0.00088699      0.00088699
v  TempC                       21          73.775          21.545          21.545
v  TurbVisc           3.0448e-014       0.0050307       0.0010342       0.0010342
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              650:        0.34870E+01

===============================================================


 INSTANT    0.651000000E+03   TIME STEP NUMBER             651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10004E-01 0.88091E+00
   Friction velocity        uk    :  0.10004E-01 0.88091E+00
   Dimensionless distance   yplus :  0.80535E-01 0.70919E+01
   Friction thermal sca.    tstar : -0.96231E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60088E-01 0.52914E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64083E-02      33   0.45835E-03   0.21343E+01 0.89580E+02 
c  Velocity[X]                                      0.13479E+01 
c  Velocity[Y]                                      0.78642E+00 
c  Velocity[Z]                                      0.11517E-29 
c  Pressure     0.11364E-06     457   0.92245E-08   0.11351E+00 0.23922E+03 
c  nu_tilda     0.45278E-05      32   0.90392E-05   0.19996E-06 0.14558E+03 
c  TempC        0.27148E+02      28   0.63556E-03   0.85414E+01 0.28637E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2557          9.9893          4.5729          4.5729
v  Velocity[Y]            -3.7792          7.0743        0.019424        0.019424
v  Velocity[Z]       -6.9287e-015     8.7643e-015    -1.4361e-017    -1.4361e-017
v  ǁVelocityǁ         0.0019948           9.991           5.101           5.101
v  Pressure               -52.524          21.474         -4.0382         -4.0382
v  nu_tilda           4.3094e-007       0.0042684       0.0008876       0.0008876
v  TempC                       21           73.06          21.546          21.546
v  TurbVisc           3.0391e-014       0.0050307        0.001035        0.001035
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              651:        0.37560E+01

===============================================================


 INSTANT    0.652000000E+03   TIME STEP NUMBER             652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88468E-02 0.88050E+00
   Friction velocity        uk    :  0.88468E-02 0.88050E+00
   Dimensionless distance   yplus :  0.71223E-01 0.70886E+01
   Friction thermal sca.    tstar : -0.16774E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53140E-01 0.52889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64124E-02      33   0.42499E-03   0.21436E+01 0.89666E+02 
c  Velocity[X]                                      0.13454E+01 
c  Velocity[Y]                                      0.79823E+00 
c  Velocity[Z]                                      0.10449E-29 
c  Pressure     0.11554E-06     405   0.94357E-08   0.11750E+00 0.34673E+03 
c  nu_tilda     0.45296E-05      32   0.13536E-04   0.19969E-06 0.14540E+03 
c  TempC        0.27160E+02      28   0.53902E-03   0.10953E+02 0.35233E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2552          9.9912          4.5729          4.5729
v  Velocity[Y]             -3.774          7.0451        0.019429        0.019429
v  Velocity[Z]       -6.9287e-015     8.5929e-015    -1.4346e-017    -1.4346e-017
v  ǁVelocityǁ         0.0018466          9.9931          5.1016          5.1016
v  Pressure               -52.505           21.41         -4.0509         -4.0509
v  nu_tilda           4.3082e-007       0.0042684       0.0008882       0.0008882
v  TempC                       21           73.06          21.546          21.546
v  TurbVisc           3.0342e-014       0.0050307       0.0010357       0.0010357
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              652:        0.38280E+01

===============================================================


 INSTANT    0.653000000E+03   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70506E-02 0.87925E+00
   Friction velocity        uk    :  0.70506E-02 0.87925E+00
   Dimensionless distance   yplus :  0.56762E-01 0.70786E+01
   Friction thermal sca.    tstar : -0.15180E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42351E-01 0.52814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64165E-02      32   0.39688E-03   0.21034E+01 0.89241E+02 
c  Velocity[X]                                      0.13076E+01 
c  Velocity[Y]                                      0.79586E+00 
c  Velocity[Z]                                      0.95980E-30 
c  Pressure     0.10399E-06     311   0.99811E-08   0.10319E+00 0.47179E+03 
c  nu_tilda     0.45315E-05      32   0.90372E-05   0.19944E-06 0.14523E+03 
c  TempC        0.27173E+02      28   0.45874E-03   0.96423E+01 0.30974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2545          9.9932          4.5729          4.5729
v  Velocity[Y]            -3.7688          7.0676        0.019434        0.019434
v  Velocity[Z]       -6.9287e-015     8.4796e-015    -1.4337e-017    -1.4337e-017
v  ǁVelocityǁ         0.0019799          9.9951          5.1022          5.1022
v  Pressure               -52.533          21.489         -4.0562         -4.0562
v  nu_tilda           4.3069e-007       0.0042684      0.00088881      0.00088881
v  TempC                       21          74.162          21.547          21.547
v  TurbVisc           3.0308e-014       0.0050308       0.0010364       0.0010364
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              653:        0.28860E+01

===============================================================


 INSTANT    0.654000000E+03   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86554E-02 0.88023E+00
   Friction velocity        uk    :  0.86554E-02 0.88023E+00
   Dimensionless distance   yplus :  0.69682E-01 0.70865E+01
   Friction thermal sca.    tstar : -0.87946E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51990E-01 0.52873E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64205E-02      32   0.47567E-03   0.21042E+01 0.89049E+02 
c  Velocity[X]                                      0.13262E+01 
c  Velocity[Y]                                      0.77805E+00 
c  Velocity[Z]                                      0.10463E-29 
c  Pressure     0.12136E-06     424   0.96404E-08   0.12193E+00 0.34555E+03 
c  nu_tilda     0.45333E-05      32   0.13540E-04   0.19918E-06 0.14506E+03 
c  TempC        0.27185E+02      28   0.47085E-03   0.83836E+01 0.29243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2538          9.9949          4.5729          4.5729
v  Velocity[Y]            -3.7638          7.0364        0.019437        0.019437
v  Velocity[Z]       -6.9287e-015     8.3986e-015    -1.4325e-017    -1.4325e-017
v  ǁVelocityǁ         0.0018129           9.997          5.1028          5.1028
v  Pressure               -52.515          21.419         -4.0676         -4.0676
v  nu_tilda           4.3057e-007       0.0042684      0.00088941      0.00088941
v  TempC                       21           73.06          21.548          21.548
v  TurbVisc           3.0271e-014       0.0050308       0.0010371       0.0010371
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              654:        0.30500E+01

===============================================================


 INSTANT    0.655000000E+03   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67168E-02 0.87933E+00
   Friction velocity        uk    :  0.67168E-02 0.87933E+00
   Dimensionless distance   yplus :  0.54075E-01 0.70792E+01
   Friction thermal sca.    tstar : -0.72554E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40346E-01 0.52819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64246E-02      32   0.43544E-03   0.21473E+01 0.89499E+02 
c  Velocity[X]                                      0.13550E+01 
c  Velocity[Y]                                      0.79237E+00 
c  Velocity[Z]                                      0.95828E-30 
c  Pressure     0.15670E-06     425   0.93744E-08   0.15642E+00 0.66620E+03 
c  nu_tilda     0.45352E-05      32   0.89841E-05   0.19894E-06 0.14488E+03 
c  TempC        0.27198E+02      27   0.47633E-03   0.71892E+01 0.26623E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2534          9.9967          4.5729          4.5729
v  Velocity[Y]            -3.7587          7.0605        0.019441        0.019441
v  Velocity[Z]       -6.9287e-015     8.2534e-015     -1.432e-017     -1.432e-017
v  ǁVelocityǁ         0.0019578          9.9987          5.1034          5.1034
v  Pressure               -52.526          21.535         -4.0592         -4.0592
v  nu_tilda           4.3047e-007       0.0042684      0.00089001      0.00089001
v  TempC                       21          73.172          21.548          21.548
v  TurbVisc           3.0238e-014       0.0050308       0.0010378       0.0010378
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              655:        0.31490E+01

===============================================================


 INSTANT    0.656000000E+03   TIME STEP NUMBER             656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82693E-02 0.88068E+00
   Friction velocity        uk    :  0.82693E-02 0.88068E+00
   Dimensionless distance   yplus :  0.66574E-01 0.70901E+01
   Friction thermal sca.    tstar : -0.59159E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49672E-01 0.52900E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64287E-02      32   0.38045E-03   0.20898E+01 0.88883E+02 
c  Velocity[X]                                      0.13183E+01 
c  Velocity[Y]                                      0.77148E+00 
c  Velocity[Z]                                      0.91700E-30 
c  Pressure     0.10124E-06     377   0.94541E-08   0.10146E+00 0.17958E+03 
c  nu_tilda     0.45370E-05      32   0.13554E-04   0.19868E-06 0.14472E+03 
c  TempC        0.27210E+02      28   0.49229E-03   0.72687E+01 0.25089E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2526          9.9983          4.5729          4.5729
v  Velocity[Y]            -3.7536          7.0687        0.019443        0.019443
v  Velocity[Z]       -6.9287e-015     8.1562e-015     -1.431e-017     -1.431e-017
v  ǁVelocityǁ         0.0019399              10           5.104           5.104
v  Pressure               -52.521          21.527         -4.0682         -4.0682
v  nu_tilda           4.3038e-007       0.0042685      0.00089061      0.00089061
v  TempC                       21          74.123          21.549          21.549
v  TurbVisc           3.0208e-014       0.0050308       0.0010386       0.0010386
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              656:        0.31310E+01

===============================================================


 INSTANT    0.657000000E+03   TIME STEP NUMBER             657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96757E-02 0.88032E+00
   Friction velocity        uk    :  0.96757E-02 0.88032E+00
   Dimensionless distance   yplus :  0.77896E-01 0.70872E+01
   Friction thermal sca.    tstar : -0.58314E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58119E-01 0.52878E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64327E-02      32   0.41828E-03   0.20744E+01 0.88569E+02 
c  Velocity[X]                                      0.13085E+01 
c  Velocity[Y]                                      0.76594E+00 
c  Velocity[Z]                                      0.11686E-29 
c  Pressure     0.12742E-06     458   0.96510E-08   0.12821E+00 0.48282E+03 
c  nu_tilda     0.45389E-05      32   0.89483E-05   0.19845E-06 0.14455E+03 
c  TempC        0.27222E+02      28   0.66685E-03   0.84044E+01 0.28375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2519              10          4.5729          4.5729
v  Velocity[Y]            -3.7485          7.0459        0.019445        0.019445
v  Velocity[Z]       -6.9287e-015     8.0668e-015    -1.4303e-017    -1.4303e-017
v  ǁVelocityǁ         0.0019028          10.002          5.1046          5.1046
v  Pressure               -52.536          21.422         -4.1065         -4.1065
v  nu_tilda           4.3043e-007       0.0042685      0.00089122      0.00089122
v  TempC                       21           73.06          21.549          21.549
v  TurbVisc           3.0184e-014       0.0050308       0.0010393       0.0010393
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              657:        0.35330E+01

===============================================================


 INSTANT    0.658000000E+03   TIME STEP NUMBER             658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16757E-02 0.87916E+00
   Friction velocity        uk    :  0.16757E-02 0.87916E+00
   Dimensionless distance   yplus :  0.13490E-01 0.70779E+01
   Friction thermal sca.    tstar : -0.56712E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10065E-01 0.52809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64367E-02      32   0.45343E-03   0.20827E+01 0.88613E+02 
c  Velocity[X]                                      0.13021E+01 
c  Velocity[Y]                                      0.78063E+00 
c  Velocity[Z]                                      0.10771E-29 
c  Pressure     0.13041E-06     458   0.95746E-08   0.12971E+00 0.55520E+03 
c  nu_tilda     0.45407E-05      32   0.13574E-04   0.19820E-06 0.14438E+03 
c  TempC        0.27235E+02      28   0.45565E-03   0.11661E+02 0.35999E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2512          10.002          4.5729          4.5729
v  Velocity[Y]            -3.7435          7.0579        0.019446        0.019446
v  Velocity[Z]       -6.9287e-015     8.0282e-015    -1.4292e-017    -1.4292e-017
v  ǁVelocityǁ         0.0018788          10.004          5.1052          5.1052
v  Pressure               -52.527          21.539         -4.0849         -4.0849
v  nu_tilda           4.3043e-007       0.0042685      0.00089181      0.00089181
v  TempC                       21          73.127           21.55           21.55
v  TurbVisc           3.0197e-014       0.0050308         0.00104         0.00104
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              658:        0.32410E+01

===============================================================


 INSTANT    0.659000000E+03   TIME STEP NUMBER             659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78435E-02 0.88011E+00
   Friction velocity        uk    :  0.78435E-02 0.88011E+00
   Dimensionless distance   yplus :  0.63146E-01 0.70855E+01
   Friction thermal sca.    tstar : -0.57309E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47114E-01 0.52866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64408E-02      32   0.41452E-03   0.20972E+01 0.88752E+02 
c  Velocity[X]                                      0.13197E+01 
c  Velocity[Y]                                      0.77749E+00 
c  Velocity[Z]                                      0.10754E-29 
c  Pressure     0.13250E-06     472   0.98521E-08   0.13410E+00 0.42601E+03 
c  nu_tilda     0.45425E-05      32   0.89379E-05   0.19797E-06 0.14421E+03 
c  TempC        0.27247E+02      27   0.36932E-03   0.79142E+01 0.27543E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2506          10.004          4.5729          4.5729
v  Velocity[Y]            -3.7388          7.0387        0.019447        0.019447
v  Velocity[Z]       -6.9287e-015     7.9805e-015    -1.4285e-017    -1.4285e-017
v  ǁVelocityǁ         0.0018908          10.006          5.1058          5.1058
v  Pressure               -52.536          21.444         -4.1182         -4.1182
v  nu_tilda           4.3049e-007       0.0042685      0.00089242      0.00089242
v  TempC                       21          73.867           21.55           21.55
v  TurbVisc           3.0199e-014       0.0050308       0.0010407       0.0010407
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              659:        0.33270E+01

===============================================================


 INSTANT    0.660000000E+03   TIME STEP NUMBER             660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12976E-02 0.87954E+00
   Friction velocity        uk    :  0.12976E-02 0.87954E+00
   Dimensionless distance   yplus :  0.10447E-01 0.70809E+01
   Friction thermal sca.    tstar : -0.59881E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77943E-02 0.52831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64448E-02      32   0.44142E-03   0.20573E+01 0.88264E+02 
c  Velocity[X]                                      0.13027E+01 
c  Velocity[Y]                                      0.75458E+00 
c  Velocity[Z]                                      0.10484E-29 
c  Pressure     0.11556E-06     441   0.97768E-08   0.11634E+00 0.49840E+03 
c  nu_tilda     0.45444E-05      32   0.13573E-04   0.19772E-06 0.14405E+03 
c  TempC        0.27259E+02      28   0.51669E-03   0.55250E+01 0.22182E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2503          10.006          4.5729          4.5729
v  Velocity[Y]            -3.7338          7.0609        0.019446        0.019446
v  Velocity[Z]       -6.9287e-015      8.124e-015    -1.4276e-017    -1.4276e-017
v  ǁVelocityǁ         0.0018753          10.008          5.1064          5.1064
v  Pressure               -52.537           21.56         -4.1022         -4.1022
v  nu_tilda           4.3049e-007       0.0042685      0.00089302      0.00089302
v  TempC                       21          73.061          21.551          21.551
v  TurbVisc           3.0214e-014       0.0050308       0.0010414       0.0010414
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              660:        0.31580E+01

===============================================================


 INSTANT    0.661000000E+03   TIME STEP NUMBER             661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85113E-02 0.88048E+00
   Friction velocity        uk    :  0.85113E-02 0.88048E+00
   Dimensionless distance   yplus :  0.68521E-01 0.70885E+01
   Friction thermal sca.    tstar : -0.71989E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51125E-01 0.52888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64489E-02      32   0.42965E-03   0.20842E+01 0.88473E+02 
c  Velocity[X]                                      0.13059E+01 
c  Velocity[Y]                                      0.77836E+00 
c  Velocity[Z]                                      0.91590E-30 
c  Pressure     0.12621E-06     458   0.96125E-08   0.12399E+00 0.25632E+03 
c  nu_tilda     0.45462E-05      32   0.89154E-05   0.19750E-06 0.14389E+03 
c  TempC        0.27272E+02      29   0.46860E-03   0.59060E+01 0.23421E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2499          10.008          4.5729          4.5729
v  Velocity[Y]             -3.729          7.0585        0.019447        0.019447
v  Velocity[Z]       -6.9287e-015     8.0465e-015    -1.4268e-017    -1.4268e-017
v  ǁVelocityǁ         0.0019114           10.01           5.107           5.107
v  Pressure               -52.556          21.523         -4.1271         -4.1271
v  nu_tilda           4.3042e-007       0.0042685      0.00089362      0.00089362
v  TempC                       21          73.089          21.552          21.552
v  TurbVisc           3.0216e-014       0.0050308       0.0010421       0.0010421
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              661:        0.33890E+01

===============================================================


 INSTANT    0.662000000E+03   TIME STEP NUMBER             662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41633E-02 0.88011E+00
   Friction velocity        uk    :  0.41633E-02 0.88011E+00
   Dimensionless distance   yplus :  0.33517E-01 0.70855E+01
   Friction thermal sca.    tstar : -0.85558E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25008E-01 0.52866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64529E-02      32   0.36877E-03   0.20727E+01 0.88249E+02 
c  Velocity[X]                                      0.13169E+01 
c  Velocity[Y]                                      0.75582E+00 
c  Velocity[Z]                                      0.11790E-29 
c  Pressure     0.13760E-06     298   0.93202E-08   0.14046E+00 0.20070E+03 
c  nu_tilda     0.45480E-05      32   0.13594E-04   0.19726E-06 0.14372E+03 
c  TempC        0.27284E+02      28   0.65140E-03   0.71439E+01 0.25738E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2496           10.01          4.5729          4.5729
v  Velocity[Y]            -3.7241          7.0333        0.019445        0.019445
v  Velocity[Z]       -6.9287e-015     8.0507e-015    -1.4251e-017    -1.4251e-017
v  ǁVelocityǁ         0.0017885          10.012          5.1075          5.1075
v  Pressure               -52.536          21.497         -4.1287         -4.1287
v  nu_tilda           4.3036e-007       0.0042685      0.00089422      0.00089422
v  TempC                       21          73.815          21.552          21.552
v  TurbVisc           3.0194e-014       0.0050308       0.0010429       0.0010429
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              662:        0.28010E+01

===============================================================


 INSTANT    0.663000000E+03   TIME STEP NUMBER             663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40320E-02 0.87896E+00
   Friction velocity        uk    :  0.40320E-02 0.87896E+00
   Dimensionless distance   yplus :  0.32461E-01 0.70762E+01
   Friction thermal sca.    tstar : -0.12965E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24219E-01 0.52797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64569E-02      32   0.44794E-03   0.20202E+01 0.87729E+02 
c  Velocity[X]                                      0.12791E+01 
c  Velocity[Y]                                      0.74113E+00 
c  Velocity[Z]                                      0.96851E-30 
c  Pressure     0.92084E-07     344   0.97699E-08   0.92392E-01 0.43539E+03 
c  nu_tilda     0.45499E-05      32   0.88774E-05   0.19704E-06 0.14356E+03 
c  TempC        0.27296E+02      28   0.48343E-03   0.10882E+02 0.33259E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2492          10.012          4.5729          4.5729
v  Velocity[Y]            -3.7193          7.0578        0.019444        0.019444
v  Velocity[Z]       -6.9287e-015     8.0903e-015    -1.4242e-017    -1.4242e-017
v  ǁVelocityǁ         0.0019034          10.014          5.1081          5.1081
v  Pressure                -52.56          21.568          -4.135          -4.135
v  nu_tilda           4.3024e-007       0.0042685      0.00089482      0.00089482
v  TempC                       21          73.063          21.553          21.553
v  TurbVisc           3.0178e-014       0.0050309       0.0010436       0.0010436
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              663:        0.34400E+01

===============================================================


 INSTANT    0.664000000E+03   TIME STEP NUMBER             664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43181E-02 0.88007E+00
   Friction velocity        uk    :  0.43181E-02 0.88007E+00
   Dimensionless distance   yplus :  0.34764E-01 0.70852E+01
   Friction thermal sca.    tstar : -0.27131E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25938E-01 0.52863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64610E-02      32   0.41260E-03   0.20621E+01 0.88085E+02 
c  Velocity[X]                                      0.13036E+01 
c  Velocity[Y]                                      0.75850E+00 
c  Velocity[Z]                                      0.10646E-29 
c  Pressure     0.13733E-06     405   0.93846E-08   0.13910E+00 0.33551E+03 
c  nu_tilda     0.45517E-05      32   0.13589E-04   0.19680E-06 0.14340E+03 
c  TempC        0.27309E+02      28   0.49031E-03   0.67297E+01 0.25165E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2488          10.013          4.5729          4.5729
v  Velocity[Y]            -3.7145          7.0355        0.019441        0.019441
v  Velocity[Z]       -6.9287e-015     8.0608e-015     -1.423e-017     -1.423e-017
v  ǁVelocityǁ         0.0018059          10.016          5.1087          5.1087
v  Pressure               -52.541          21.506         -4.1473         -4.1473
v  nu_tilda            4.301e-007       0.0042685      0.00089542      0.00089542
v  TempC                       21          73.216          21.553          21.553
v  TurbVisc           3.0143e-014       0.0050309       0.0010443       0.0010443
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              664:        0.43620E+01

===============================================================


 INSTANT    0.665000000E+03   TIME STEP NUMBER             665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13533E-02 0.87923E+00
   Friction velocity        uk    :  0.13533E-02 0.87923E+00
   Dimensionless distance   yplus :  0.10895E-01 0.70784E+01
   Friction thermal sca.    tstar : -0.10958E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81288E-02 0.52813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64650E-02      32   0.36142E-03   0.20567E+01 0.87845E+02 
c  Velocity[X]                                      0.13054E+01 
c  Velocity[Y]                                      0.75131E+00 
c  Velocity[Z]                                      0.10212E-29 
c  Pressure     0.15182E-06     421   0.97653E-08   0.14768E+00 0.28578E+03 
c  nu_tilda     0.45535E-05      32   0.88457E-05   0.19659E-06 0.14325E+03 
c  TempC        0.27321E+02      28   0.49493E-03   0.68667E+01 0.25487E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2483          10.015          4.5729          4.5729
v  Velocity[Y]            -3.7101          7.0548        0.019439        0.019439
v  Velocity[Z]       -6.9287e-015     8.0553e-015    -1.4214e-017    -1.4214e-017
v  ǁVelocityǁ         0.0018892          10.017          5.1093          5.1093
v  Pressure               -52.563          21.538         -4.1639         -4.1639
v  nu_tilda           4.2996e-007       0.0042685      0.00089603      0.00089603
v  TempC                       21           73.11          21.554          21.554
v  TurbVisc           3.0106e-014       0.0050309        0.001045        0.001045
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              665:        0.36220E+01

===============================================================


 INSTANT    0.666000000E+03   TIME STEP NUMBER             666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27312E-02 0.88049E+00
   Friction velocity        uk    :  0.27312E-02 0.88049E+00
   Dimensionless distance   yplus :  0.21988E-01 0.70886E+01
   Friction thermal sca.    tstar : -0.13632E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16406E-01 0.52889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64690E-02      32   0.41629E-03   0.19937E+01 0.87246E+02 
c  Velocity[X]                                      0.12616E+01 
c  Velocity[Y]                                      0.73215E+00 
c  Velocity[Z]                                      0.97981E-30 
c  Pressure     0.10078E-06     421   0.94303E-08   0.10106E+00 0.32671E+03 
c  nu_tilda     0.45553E-05      32   0.13609E-04   0.19636E-06 0.14309E+03 
c  TempC        0.27333E+02      28   0.42682E-03   0.67230E+01 0.25722E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2479          10.016          4.5729          4.5729
v  Velocity[Y]            -3.7055          7.0619        0.019434        0.019434
v  Velocity[Z]       -6.9287e-015      8.185e-015    -1.4202e-017    -1.4202e-017
v  ǁVelocityǁ         0.0008883          10.019          5.1099          5.1099
v  Pressure               -52.551          21.595         -4.1517         -4.1517
v  nu_tilda           4.2979e-007       0.0042685      0.00089662      0.00089662
v  TempC                       21          73.517          21.554          21.554
v  TurbVisc           3.0067e-014       0.0050309       0.0010457       0.0010457
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              666:        0.34420E+01

===============================================================


 INSTANT    0.667000000E+03   TIME STEP NUMBER             667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69608E-02 0.88008E+00
   Friction velocity        uk    :  0.69608E-02 0.88008E+00
   Dimensionless distance   yplus :  0.56039E-01 0.70852E+01
   Friction thermal sca.    tstar : -0.24177E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41811E-01 0.52864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64730E-02      32   0.45933E-03   0.20253E+01 0.87648E+02 
c  Velocity[X]                                      0.12729E+01 
c  Velocity[Y]                                      0.75246E+00 
c  Velocity[Z]                                      0.10094E-29 
c  Pressure     0.11227E-06     458   0.97664E-08   0.11398E+00 0.54052E+03 
c  nu_tilda     0.45572E-05      32   0.88359E-05   0.19615E-06 0.14293E+03 
c  TempC        0.27346E+02      27   0.52657E-03   0.72468E+01 0.25903E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2479          10.018          4.5729          4.5729
v  Velocity[Y]            -3.7009          7.0358        0.019431        0.019431
v  Velocity[Z]       -6.9287e-015     8.0167e-015    -1.4194e-017    -1.4194e-017
v  ǁVelocityǁ         0.0018888           10.02          5.1105          5.1105
v  Pressure                -52.57          21.487         -4.1946         -4.1946
v  nu_tilda           4.2968e-007       0.0042685      0.00089723      0.00089723
v  TempC                       21          73.266          21.555          21.555
v  TurbVisc           3.0018e-014       0.0050309       0.0010464       0.0010464
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              667:        0.36960E+01

===============================================================


 INSTANT    0.668000000E+03   TIME STEP NUMBER             668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46435E-02 0.87874E+00
   Friction velocity        uk    :  0.46435E-02 0.87874E+00
   Dimensionless distance   yplus :  0.37384E-01 0.70745E+01
   Friction thermal sca.    tstar : -0.18478E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27892E-01 0.52784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64770E-02      32   0.41648E-03   0.20323E+01 0.87700E+02 
c  Velocity[X]                                      0.12822E+01 
c  Velocity[Y]                                      0.75006E+00 
c  Velocity[Z]                                      0.10614E-29 
c  Pressure     0.12858E-06     437   0.91371E-08   0.12766E+00 0.52016E+03 
c  nu_tilda     0.45590E-05      32   0.13610E-04   0.19593E-06 0.14278E+03 
c  TempC        0.27358E+02      27   0.46686E-03   0.89773E+01 0.27749E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2478          10.019          4.5729          4.5729
v  Velocity[Y]            -3.6964           7.056        0.019425        0.019425
v  Velocity[Z]       -6.9287e-015     7.9576e-015    -1.4178e-017    -1.4178e-017
v  ǁVelocityǁ          0.001794          10.022          5.1111          5.1111
v  Pressure               -52.558          21.594          -4.174          -4.174
v  nu_tilda           4.2955e-007       0.0042686      0.00089782      0.00089782
v  TempC                       21          73.655          21.555          21.555
v  TurbVisc           2.9988e-014       0.0050309       0.0010471       0.0010471
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              668:        0.33830E+01

===============================================================


 INSTANT    0.669000000E+03   TIME STEP NUMBER             669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59534E-02 0.87985E+00
   Friction velocity        uk    :  0.59534E-02 0.87985E+00
   Dimensionless distance   yplus :  0.47929E-01 0.70834E+01
   Friction thermal sca.    tstar : -0.13424E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35760E-01 0.52850E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64811E-02      32   0.43427E-03   0.20165E+01 0.87314E+02 
c  Velocity[X]                                      0.12897E+01 
c  Velocity[Y]                                      0.72681E+00 
c  Velocity[Z]                                      0.13587E-29 
c  Pressure     0.14508E-06     440   0.95763E-08   0.14579E+00 0.31536E+03 
c  nu_tilda     0.45608E-05      32   0.88068E-05   0.19572E-06 0.14262E+03 
c  TempC        0.27370E+02      27   0.45793E-03   0.79529E+01 0.27099E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2479          10.021          4.5729          4.5729
v  Velocity[Y]            -3.6919          7.0323         0.01942         0.01942
v  Velocity[Z]       -6.9287e-015     7.8567e-015    -1.4183e-017    -1.4183e-017
v  ǁVelocityǁ         0.0018548          10.023          5.1117          5.1117
v  Pressure               -52.565          21.523         -4.1993         -4.1993
v  nu_tilda           4.2947e-007       0.0042686      0.00089843      0.00089843
v  TempC                       21          73.064          21.556          21.556
v  TurbVisc           2.9951e-014       0.0050309       0.0010479       0.0010479
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              669:        0.34050E+01

===============================================================


 INSTANT    0.670000000E+03   TIME STEP NUMBER             670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50877E-02 0.87904E+00
   Friction velocity        uk    :  0.50877E-02 0.87904E+00
   Dimensionless distance   yplus :  0.40960E-01 0.70769E+01
   Friction thermal sca.    tstar : -0.10199E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30560E-01 0.52802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64851E-02      32   0.38114E-03   0.20148E+01 0.87373E+02 
c  Velocity[X]                                      0.12648E+01 
c  Velocity[Y]                                      0.75001E+00 
c  Velocity[Z]                                      0.10295E-29 
c  Pressure     0.11019E-06     393   0.92029E-08   0.10946E+00 0.34949E+03 
c  nu_tilda     0.45626E-05      32   0.13628E-04   0.19551E-06 0.14247E+03 
c  TempC        0.27382E+02      27   0.44157E-03   0.70926E+01 0.26012E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2478          10.022          4.5729          4.5729
v  Velocity[Y]            -3.6876          7.0511        0.019414        0.019414
v  Velocity[Z]       -6.9287e-015     7.7803e-015    -1.4171e-017    -1.4171e-017
v  ǁVelocityǁ         0.0017569          10.024          5.1123          5.1123
v  Pressure               -52.562          21.612         -4.1913         -4.1913
v  nu_tilda           4.2939e-007       0.0042686      0.00089902      0.00089902
v  TempC                       21          73.578          21.557          21.557
v  TurbVisc           2.9929e-014       0.0050309       0.0010486       0.0010486
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              670:        0.35410E+01

===============================================================


 INSTANT    0.671000000E+03   TIME STEP NUMBER             671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60305E-02 0.88022E+00
   Friction velocity        uk    :  0.60305E-02 0.88022E+00
   Dimensionless distance   yplus :  0.48549E-01 0.70863E+01
   Friction thermal sca.    tstar : -0.89593E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36223E-01 0.52872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64891E-02      32   0.36731E-03   0.19701E+01 0.86850E+02 
c  Velocity[X]                                      0.12399E+01 
c  Velocity[Y]                                      0.73019E+00 
c  Velocity[Z]                                      0.11922E-29 
c  Pressure     0.10565E-06     394   0.95438E-08   0.10717E+00 0.27851E+03 
c  nu_tilda     0.45644E-05      32   0.87803E-05   0.19530E-06 0.14232E+03 
c  TempC        0.27395E+02      28   0.68180E-03   0.54001E+01 0.21987E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2476          10.023          4.5729          4.5729
v  Velocity[Y]            -3.6833          7.0611        0.019407        0.019407
v  Velocity[Z]       -6.9287e-015     7.8148e-015    -1.4168e-017    -1.4168e-017
v  ǁVelocityǁ         0.0018585          10.025          5.1129          5.1129
v  Pressure               -52.583          21.633         -4.2046         -4.2046
v  nu_tilda           4.2924e-007       0.0042686      0.00089963      0.00089963
v  TempC                       21          73.065          21.557          21.557
v  TurbVisc           2.9908e-014       0.0050309       0.0010493       0.0010493
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              671:        0.37720E+01

===============================================================


 INSTANT    0.672000000E+03   TIME STEP NUMBER             672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49111E-02 0.87943E+00
   Friction velocity        uk    :  0.49111E-02 0.87943E+00
   Dimensionless distance   yplus :  0.39537E-01 0.70800E+01
   Friction thermal sca.    tstar : -0.78591E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29499E-01 0.52825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64931E-02      32   0.43730E-03   0.19821E+01 0.86847E+02 
c  Velocity[X]                                      0.12656E+01 
c  Velocity[Y]                                      0.71647E+00 
c  Velocity[Z]                                      0.10983E-29 
c  Pressure     0.12670E-06     442   0.91287E-08   0.12696E+00 0.72207E+03 
c  nu_tilda     0.45662E-05      32   0.13626E-04   0.19509E-06 0.14217E+03 
c  TempC        0.27407E+02      29   0.46233E-03   0.72376E+01 0.26762E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2474          10.024          4.5729          4.5729
v  Velocity[Y]             -3.679          7.0294          0.0194          0.0194
v  Velocity[Z]       -6.9287e-015     7.5942e-015    -1.4159e-017    -1.4159e-017
v  ǁVelocityǁ         0.0017972          10.027          5.1134          5.1134
v  Pressure               -52.566          21.486         -4.2367         -4.2367
v  nu_tilda           4.2919e-007       0.0042686      0.00090022      0.00090022
v  TempC                       21          73.772          21.558          21.558
v  TurbVisc           2.9865e-014       0.0050309         0.00105         0.00105
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              672:        0.34860E+01

===============================================================


 INSTANT    0.673000000E+03   TIME STEP NUMBER             673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66051E-02 0.87845E+00
   Friction velocity        uk    :  0.66051E-02 0.87845E+00
   Dimensionless distance   yplus :  0.53176E-01 0.70721E+01
   Friction thermal sca.    tstar : -0.77393E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39675E-01 0.52766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64971E-02      32   0.39348E-03   0.20053E+01 0.87098E+02 
c  Velocity[X]                                      0.12725E+01 
c  Velocity[Y]                                      0.73285E+00 
c  Velocity[Z]                                      0.92506E-30 
c  Pressure     0.13570E-06     409   0.91183E-08   0.13658E+00 0.70520E+03 
c  nu_tilda     0.45680E-05      32   0.87650E-05   0.19489E-06 0.14202E+03 
c  TempC        0.27419E+02      28   0.48727E-03   0.71584E+01 0.24139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2472          10.025          4.5729          4.5729
v  Velocity[Y]            -3.6748          7.0481        0.019392        0.019392
v  Velocity[Z]       -6.9287e-015     7.4937e-015    -1.4157e-017    -1.4157e-017
v  ǁVelocityǁ         0.0018553          10.028           5.114           5.114
v  Pressure               -52.588          21.614         -4.2278         -4.2278
v  nu_tilda           4.2918e-007       0.0042686      0.00090083      0.00090083
v  TempC                       21          73.065          21.558          21.558
v  TurbVisc           2.9852e-014        0.005031       0.0010507       0.0010507
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              673:        0.31680E+01

===============================================================


 INSTANT    0.674000000E+03   TIME STEP NUMBER             674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31026E-02 0.87949E+00
   Friction velocity        uk    :  0.31026E-02 0.87949E+00
   Dimensionless distance   yplus :  0.24978E-01 0.70805E+01
   Friction thermal sca.    tstar : -0.94973E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18637E-01 0.52829E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65011E-02      32   0.37963E-03   0.19746E+01 0.86727E+02 
c  Velocity[X]                                      0.12542E+01 
c  Velocity[Y]                                      0.72036E+00 
c  Velocity[Z]                                      0.11355E-29 
c  Pressure     0.11546E-06     421   0.94733E-08   0.11635E+00 0.46257E+03 
c  nu_tilda     0.45699E-05      32   0.13639E-04   0.19468E-06 0.14187E+03 
c  TempC        0.27431E+02      27   0.44435E-03   0.78092E+01 0.27507E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.247          10.026          4.5729          4.5729
v  Velocity[Y]            -3.6706          7.0262        0.019383        0.019383
v  Velocity[Z]       -6.9287e-015     7.4508e-015    -1.4149e-017    -1.4149e-017
v  ǁVelocityǁ         0.0017703          10.029          5.1146          5.1146
v  Pressure               -52.573           21.53         -4.2493         -4.2493
v  nu_tilda           4.2918e-007       0.0042686      0.00090142      0.00090142
v  TempC                       21          73.066          21.559          21.559
v  TurbVisc           2.9849e-014        0.005031       0.0010514       0.0010514
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              674:        0.32170E+01

===============================================================


 INSTANT    0.675000000E+03   TIME STEP NUMBER             675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51829E-02 0.87871E+00
   Friction velocity        uk    :  0.51829E-02 0.87871E+00
   Dimensionless distance   yplus :  0.41726E-01 0.70742E+01
   Friction thermal sca.    tstar : -0.18223E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31132E-01 0.52782E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65050E-02      32   0.45241E-03   0.19463E+01 0.86411E+02 
c  Velocity[X]                                      0.12389E+01 
c  Velocity[Y]                                      0.70743E+00 
c  Velocity[Z]                                      0.99839E-30 
c  Pressure     0.10031E-06     393   0.99443E-08   0.10021E+00 0.53530E+03 
c  nu_tilda     0.45717E-05      32   0.87374E-05   0.19449E-06 0.14173E+03 
c  TempC        0.27443E+02      27   0.47451E-03   0.67431E+01 0.25859E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2474          10.027          4.5729          4.5729
v  Velocity[Y]            -3.6665          7.0527        0.019374        0.019374
v  Velocity[Z]       -6.9287e-015     7.5428e-015     -1.414e-017     -1.414e-017
v  ǁVelocityǁ         0.0018756           10.03          5.1152          5.1152
v  Pressure               -52.595           21.62         -4.2486         -4.2486
v  nu_tilda           4.2909e-007       0.0042686      0.00090203      0.00090203
v  TempC                       21           74.27          21.559          21.559
v  TurbVisc           2.9848e-014        0.005031       0.0010521       0.0010521
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              675:        0.30810E+01

===============================================================


 INSTANT    0.676000000E+03   TIME STEP NUMBER             676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31674E-02 0.87998E+00
   Friction velocity        uk    :  0.31674E-02 0.87998E+00
   Dimensionless distance   yplus :  0.25500E-01 0.70845E+01
   Friction thermal sca.    tstar : -0.15669E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19026E-01 0.52858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65090E-02      32   0.41823E-03   0.19526E+01 0.86362E+02 
c  Velocity[X]                                      0.12340E+01 
c  Velocity[Y]                                      0.71861E+00 
c  Velocity[Z]                                      0.13269E-29 
c  Pressure     0.12532E-06     329   0.90702E-08   0.12495E+00 0.16217E+03 
c  nu_tilda     0.45735E-05      32   0.13644E-04   0.19428E-06 0.14158E+03 
c  TempC        0.27456E+02      27   0.69934E-03   0.81359E+01 0.28212E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2478          10.028          4.5729          4.5729
v  Velocity[Y]            -3.6626          7.0492        0.019364        0.019364
v  Velocity[Z]       -6.9287e-015     7.3654e-015    -1.4138e-017    -1.4138e-017
v  ǁVelocityǁ         0.0017894          10.031          5.1158          5.1158
v  Pressure               -52.577          21.633         -4.2486         -4.2486
v  nu_tilda            4.289e-007       0.0042686      0.00090262      0.00090262
v  TempC                       21          73.067           21.56           21.56
v  TurbVisc           2.9824e-014        0.005031       0.0010529       0.0010529
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              676:        0.28290E+01

===============================================================


 INSTANT    0.677000000E+03   TIME STEP NUMBER             677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48023E-02 0.87936E+00
   Friction velocity        uk    :  0.48023E-02 0.87936E+00
   Dimensionless distance   yplus :  0.38662E-01 0.70794E+01
   Friction thermal sca.    tstar : -0.96369E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28846E-01 0.52820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65130E-02      32   0.44384E-03   0.19467E+01 0.86292E+02 
c  Velocity[X]                                      0.12362E+01 
c  Velocity[Y]                                      0.71050E+00 
c  Velocity[Z]                                      0.12714E-29 
c  Pressure     0.98968E-07     456   0.97091E-08   0.10093E+00 0.45581E+03 
c  nu_tilda     0.45753E-05      32   0.87089E-05   0.19409E-06 0.14144E+03 
c  TempC        0.27468E+02      28   0.46648E-03   0.14046E+02 0.37656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2481          10.028          4.5729          4.5729
v  Velocity[Y]            -3.6587          7.0256        0.019354        0.019354
v  Velocity[Z]       -6.9287e-015     7.2964e-015    -1.4133e-017    -1.4133e-017
v  ǁVelocityǁ         0.0019098          10.031          5.1164          5.1164
v  Pressure               -52.597          21.532         -4.2858         -4.2858
v  nu_tilda            4.288e-007       0.0042686      0.00090323      0.00090323
v  TempC                       21          73.177          21.561          21.561
v  TurbVisc           2.9771e-014        0.005031       0.0010536       0.0010536
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              677:        0.34500E+01

===============================================================


 INSTANT    0.678000000E+03   TIME STEP NUMBER             678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72452E-02 0.87830E+00
   Friction velocity        uk    :  0.72452E-02 0.87830E+00
   Dimensionless distance   yplus :  0.58329E-01 0.70709E+01
   Friction thermal sca.    tstar : -0.72563E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43520E-01 0.52757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65170E-02      32   0.46358E-03   0.19598E+01 0.86412E+02 
c  Velocity[X]                                      0.12609E+01 
c  Velocity[Y]                                      0.69890E+00 
c  Velocity[Z]                                      0.96180E-30 
c  Pressure     0.13111E-06     440   0.97677E-08   0.13117E+00 0.47004E+03 
c  nu_tilda     0.45771E-05      32   0.13660E-04   0.19389E-06 0.14129E+03 
c  TempC        0.27480E+02      27   0.52966E-03   0.73530E+01 0.27035E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2484           10.03          4.5729          4.5729
v  Velocity[Y]            -3.6548          7.0466        0.019343        0.019343
v  Velocity[Z]       -6.9287e-015     7.2115e-015    -1.4134e-017    -1.4134e-017
v  ǁVelocityǁ         0.0017571          10.032           5.117           5.117
v  Pressure               -52.584          21.634         -4.2684         -4.2684
v  nu_tilda            4.288e-007       0.0042686      0.00090382      0.00090382
v  TempC                       21          74.299          21.561          21.561
v  TurbVisc           2.9744e-014        0.005031       0.0010543       0.0010543
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              678:        0.33530E+01

===============================================================


 INSTANT    0.679000000E+03   TIME STEP NUMBER             679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23035E-02 0.87944E+00
   Friction velocity        uk    :  0.23035E-02 0.87944E+00
   Dimensionless distance   yplus :  0.18545E-01 0.70801E+01
   Friction thermal sca.    tstar : -0.64320E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13836E-01 0.52825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65210E-02      32   0.39830E-03   0.19802E+01 0.86510E+02 
c  Velocity[X]                                      0.12645E+01 
c  Velocity[Y]                                      0.71569E+00 
c  Velocity[Z]                                      0.10108E-29 
c  Pressure     0.14081E-06     473   0.93233E-08   0.14096E+00 0.52055E+03 
c  nu_tilda     0.45788E-05      32   0.86860E-05   0.19370E-06 0.14115E+03 
c  TempC        0.27492E+02      28   0.40724E-03   0.73272E+01 0.25080E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2485          10.031          4.5729          4.5729
v  Velocity[Y]             -3.651          7.0224        0.019331        0.019331
v  Velocity[Z]       -6.9287e-015     7.3065e-015    -1.4135e-017    -1.4135e-017
v  ǁVelocityǁ         0.0020102          10.034          5.1176          5.1176
v  Pressure               -52.604          21.527         -4.3098         -4.3098
v  nu_tilda           4.2885e-007       0.0042686      0.00090442      0.00090442
v  TempC                       21          73.068          21.562          21.562
v  TurbVisc           2.9742e-014        0.005031        0.001055        0.001055
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              679:        0.36680E+01

===============================================================


 INSTANT    0.680000000E+03   TIME STEP NUMBER             680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95736E-02 0.87883E+00
   Friction velocity        uk    :  0.95736E-02 0.87883E+00
   Dimensionless distance   yplus :  0.77074E-01 0.70752E+01
   Friction thermal sca.    tstar : -0.54407E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57506E-01 0.52789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65250E-02      32   0.39143E-03   0.19285E+01 0.85972E+02 
c  Velocity[X]                                      0.12284E+01 
c  Velocity[Y]                                      0.70013E+00 
c  Velocity[Z]                                      0.97290E-30 
c  Pressure     0.99351E-07     469   0.99567E-08   0.10030E+00 0.57726E+03 
c  nu_tilda     0.45806E-05      32   0.13668E-04   0.19350E-06 0.14101E+03 
c  TempC        0.27504E+02      27   0.34589E-03   0.62197E+01 0.24174E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2488          10.032          4.5729          4.5729
v  Velocity[Y]            -3.6472          7.0454        0.019318        0.019318
v  Velocity[Z]       -6.9287e-015     7.1262e-015    -1.4132e-017    -1.4132e-017
v  ǁVelocityǁ         0.0018037          10.035          5.1181          5.1181
v  Pressure               -52.595          21.649         -4.2875         -4.2875
v  nu_tilda           4.2886e-007       0.0042686      0.00090502      0.00090502
v  TempC                       21          73.215          21.562          21.562
v  TurbVisc           2.9757e-014        0.005031       0.0010557       0.0010557
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              680:        0.35180E+01

===============================================================


 INSTANT    0.681000000E+03   TIME STEP NUMBER             681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57404E-02 0.87998E+00
   Friction velocity        uk    :  0.57404E-02 0.87998E+00
   Dimensionless distance   yplus :  0.46214E-01 0.70845E+01
   Friction thermal sca.    tstar : -0.55441E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34481E-01 0.52858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65289E-02      32   0.43867E-03   0.18991E+01 0.85702E+02 
c  Velocity[X]                                      0.12015E+01 
c  Velocity[Y]                                      0.69756E+00 
c  Velocity[Z]                                      0.90857E-30 
c  Pressure     0.90662E-07     441   0.94753E-08   0.90861E-01 0.24579E+03 
c  nu_tilda     0.45824E-05      32   0.86680E-05   0.19332E-06 0.14087E+03 
c  TempC        0.27517E+02      28   0.73683E-03   0.43126E+01 0.19412E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2492          10.033          4.5729          4.5729
v  Velocity[Y]            -3.6436          7.0547        0.019307        0.019307
v  Velocity[Z]       -6.9287e-015     7.0527e-015    -1.4121e-017    -1.4121e-017
v  ǁVelocityǁ         0.0018983          10.036          5.1187          5.1187
v  Pressure               -52.617          21.628         -4.3123         -4.3123
v  nu_tilda           4.2882e-007       0.0042687      0.00090562      0.00090562
v  TempC                       21           74.18          21.563          21.563
v  TurbVisc            2.976e-014        0.005031       0.0010564       0.0010564
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              681:        0.35640E+01

===============================================================


 INSTANT    0.682000000E+03   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63480E-02 0.87949E+00
   Friction velocity        uk    :  0.63480E-02 0.87949E+00
   Dimensionless distance   yplus :  0.51106E-01 0.70805E+01
   Friction thermal sca.    tstar : -0.54868E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38131E-01 0.52828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65329E-02      32   0.43787E-03   0.19640E+01 0.86339E+02 
c  Velocity[X]                                      0.12557E+01 
c  Velocity[Y]                                      0.70838E+00 
c  Velocity[Z]                                      0.99354E-30 
c  Pressure     0.13570E-06     394   0.91442E-08   0.13876E+00 0.29844E+03 
c  nu_tilda     0.45842E-05      32   0.13676E-04   0.19312E-06 0.14072E+03 
c  TempC        0.27529E+02      28   0.74479E-03   0.10667E+02 0.31739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2498          10.034          4.5729          4.5729
v  Velocity[Y]              -3.64          7.0282        0.019292        0.019292
v  Velocity[Z]       -6.9287e-015     6.9939e-015     -1.412e-017     -1.412e-017
v  ǁVelocityǁ        0.00090055          10.037          5.1193          5.1193
v  Pressure               -52.602          21.576         -4.3244         -4.3244
v  nu_tilda           4.2878e-007       0.0042687      0.00090622      0.00090622
v  TempC                       21           73.07          21.563          21.563
v  TurbVisc           2.9749e-014        0.005031       0.0010571       0.0010571
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              682:        0.32480E+01

===============================================================


 INSTANT    0.683000000E+03   TIME STEP NUMBER             683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76509E-02 0.87807E+00
   Friction velocity        uk    :  0.76509E-02 0.87807E+00
   Dimensionless distance   yplus :  0.61595E-01 0.70691E+01
   Friction thermal sca.    tstar : -0.59285E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45957E-01 0.52743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65369E-02      32   0.37256E-03   0.19524E+01 0.86204E+02 
c  Velocity[X]                                      0.12538E+01 
c  Velocity[Y]                                      0.69860E+00 
c  Velocity[Z]                                      0.10726E-29 
c  Pressure     0.13973E-06     410   0.92207E-08   0.13767E+00 0.26125E+03 
c  nu_tilda     0.45860E-05      32   0.86417E-05   0.19295E-06 0.14059E+03 
c  TempC        0.27541E+02      27   0.49157E-03   0.14949E+02 0.40971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2503          10.035          4.5729          4.5729
v  Velocity[Y]            -3.6366          7.0425         0.01928         0.01928
v  Velocity[Z]       -6.9287e-015      7.098e-015    -1.4109e-017    -1.4109e-017
v  ǁVelocityǁ          0.001964          10.038          5.1199          5.1199
v  Pressure               -52.623          21.596         -4.3414         -4.3414
v  nu_tilda           4.2867e-007       0.0042687      0.00090682      0.00090682
v  TempC                       21          73.414          21.564          21.564
v  TurbVisc           2.9737e-014        0.005031       0.0010578       0.0010578
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              683:        0.33940E+01

===============================================================


 INSTANT    0.684000000E+03   TIME STEP NUMBER             684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84865E-02 0.87926E+00
   Friction velocity        uk    :  0.84865E-02 0.87926E+00
   Dimensionless distance   yplus :  0.68322E-01 0.70786E+01
   Friction thermal sca.    tstar : -0.64748E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50976E-01 0.52814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65408E-02      32   0.41062E-03   0.19089E+01 0.85652E+02 
c  Velocity[X]                                      0.12187E+01 
c  Velocity[Y]                                      0.69021E+00 
c  Velocity[Z]                                      0.97508E-30 
c  Pressure     0.10269E-06     325   0.98994E-08   0.10506E+00 0.17620E+03 
c  nu_tilda     0.45878E-05      32   0.13689E-04   0.19275E-06 0.14045E+03 
c  TempC        0.27553E+02      27   0.46281E-03   0.80123E+01 0.27192E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2509          10.036          4.5729          4.5729
v  Velocity[Y]            -3.6332          7.0203        0.019265        0.019265
v  Velocity[Z]       -6.9287e-015     6.9533e-015    -1.4112e-017    -1.4112e-017
v  ǁVelocityǁ         0.0018704          10.039          5.1205          5.1205
v  Pressure               -52.611          21.581         -4.3445         -4.3445
v  nu_tilda           4.2857e-007       0.0042687      0.00090742      0.00090742
v  TempC                       21           73.07          21.564          21.564
v  TurbVisc           2.9707e-014       0.0050311       0.0010586       0.0010586
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              684:        0.28290E+01

===============================================================


 INSTANT    0.685000000E+03   TIME STEP NUMBER             685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85440E-02 0.87847E+00
   Friction velocity        uk    :  0.85440E-02 0.87847E+00
   Dimensionless distance   yplus :  0.68785E-01 0.70723E+01
   Friction thermal sca.    tstar : -0.77971E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51321E-01 0.52767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65448E-02      32   0.43476E-03   0.19141E+01 0.85718E+02 
c  Velocity[X]                                      0.12095E+01 
c  Velocity[Y]                                      0.70463E+00 
c  Velocity[Z]                                      0.12713E-29 
c  Pressure     0.14207E-06     408   0.99787E-08   0.14270E+00 0.56425E+03 
c  nu_tilda     0.45896E-05      32   0.86187E-05   0.19257E-06 0.14031E+03 
c  TempC        0.27565E+02      28   0.40192E-03   0.79294E+01 0.25830E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2517          10.037          4.5729          4.5729
v  Velocity[Y]              -3.63          7.0437         0.01925         0.01925
v  Velocity[Z]       -6.9287e-015     6.8594e-015     -1.412e-017     -1.412e-017
v  ǁVelocityǁ         0.0018932           10.04           5.121           5.121
v  Pressure               -52.621          21.679         -4.3401         -4.3401
v  nu_tilda           4.2846e-007       0.0042687      0.00090802      0.00090802
v  TempC                       21          73.071          21.565          21.565
v  TurbVisc            2.968e-014       0.0050311       0.0010593       0.0010593
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              685:        0.32810E+01

===============================================================


 INSTANT    0.686000000E+03   TIME STEP NUMBER             686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61858E-02 0.87955E+00
   Friction velocity        uk    :  0.61858E-02 0.87955E+00
   Dimensionless distance   yplus :  0.49800E-01 0.70810E+01
   Friction thermal sca.    tstar : -0.97456E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37156E-01 0.52832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65488E-02      32   0.40820E-03   0.19112E+01 0.85732E+02 
c  Velocity[X]                                      0.12082E+01 
c  Velocity[Y]                                      0.70295E+00 
c  Velocity[Z]                                      0.13814E-29 
c  Pressure     0.12557E-06     394   0.92540E-08   0.12644E+00 0.23323E+03 
c  nu_tilda     0.45914E-05      32   0.13692E-04   0.19238E-06 0.14017E+03 
c  TempC        0.27577E+02      28   0.51565E-03   0.53065E+01 0.21107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2522          10.038          4.5729          4.5729
v  Velocity[Y]            -3.6268          7.0514        0.019233        0.019233
v  Velocity[Z]       -6.9287e-015     6.8398e-015    -1.4107e-017    -1.4107e-017
v  ǁVelocityǁ         0.0017754          10.041          5.1216          5.1216
v  Pressure                -52.62          21.652          -4.353          -4.353
v  nu_tilda           4.2835e-007       0.0042687      0.00090862      0.00090862
v  TempC                       21          74.425          21.566          21.566
v  TurbVisc           2.9649e-014       0.0050311         0.00106         0.00106
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              686:        0.31620E+01

===============================================================


 INSTANT    0.687000000E+03   TIME STEP NUMBER             687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57517E-02 0.87932E+00
   Friction velocity        uk    :  0.57517E-02 0.87932E+00
   Dimensionless distance   yplus :  0.46305E-01 0.70791E+01
   Friction thermal sca.    tstar : -0.17389E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34549E-01 0.52818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65527E-02      32   0.39581E-03   0.19094E+01 0.85489E+02 
c  Velocity[X]                                      0.12187E+01 
c  Velocity[Y]                                      0.69065E+00 
c  Velocity[Z]                                      0.11045E-29 
c  Pressure     0.13321E-06     456   0.95185E-08   0.13439E+00 0.45100E+03 
c  nu_tilda     0.45931E-05      32   0.85868E-05   0.19221E-06 0.14004E+03 
c  TempC        0.27590E+02      27   0.50795E-03   0.81778E+01 0.26273E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2528          10.039          4.5729          4.5729
v  Velocity[Y]            -3.6236          7.0223        0.019218        0.019218
v  Velocity[Z]       -6.9287e-015     6.9264e-015    -1.4106e-017    -1.4106e-017
v  ǁVelocityǁ         0.0021141          10.042          5.1222          5.1222
v  Pressure               -52.633          21.559         -4.3896         -4.3896
v  nu_tilda            4.283e-007       0.0042687      0.00090922      0.00090922
v  TempC                       21          73.071          21.566          21.566
v  TurbVisc           2.9618e-014       0.0050311       0.0010607       0.0010607
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              687:        0.34070E+01

===============================================================


 INSTANT    0.688000000E+03   TIME STEP NUMBER             688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11057E-01 0.87788E+00
   Friction velocity        uk    :  0.11057E-01 0.87788E+00
   Dimensionless distance   yplus :  0.89018E-01 0.70676E+01
   Friction thermal sca.    tstar : -0.15827E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66418E-01 0.52732E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65567E-02      32   0.37496E-03   0.18987E+01 0.85481E+02 
c  Velocity[X]                                      0.11928E+01 
c  Velocity[Y]                                      0.70587E+00 
c  Velocity[Z]                                      0.11032E-29 
c  Pressure     0.11117E-06     426   0.95164E-08   0.11240E+00 0.48925E+03 
c  nu_tilda     0.45949E-05      32   0.13713E-04   0.19202E-06 0.13990E+03 
c  TempC        0.27602E+02      27   0.46112E-03   0.68063E+01 0.25886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2536          10.039          4.5729          4.5729
v  Velocity[Y]            -3.6205          7.0382          0.0192          0.0192
v  Velocity[Z]       -6.9866e-015     6.7436e-015    -1.4112e-017    -1.4112e-017
v  ǁVelocityǁ         0.0018895          10.043          5.1228          5.1228
v  Pressure                -52.62           21.66         -4.3711         -4.3711
v  nu_tilda           4.2821e-007       0.0042687      0.00090982      0.00090982
v  TempC                       21          73.206          21.567          21.567
v  TurbVisc           2.9604e-014       0.0050311       0.0010614       0.0010614
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              688:        0.34640E+01

===============================================================


 INSTANT    0.689000000E+03   TIME STEP NUMBER             689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87678E-02 0.87906E+00
   Friction velocity        uk    :  0.87678E-02 0.87906E+00
   Dimensionless distance   yplus :  0.70587E-01 0.70770E+01
   Friction thermal sca.    tstar : -0.98958E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52666E-01 0.52803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65606E-02      32   0.38212E-03   0.19001E+01 0.85469E+02 
c  Velocity[X]                                      0.12105E+01 
c  Velocity[Y]                                      0.68962E+00 
c  Velocity[Z]                                      0.10329E-29 
c  Pressure     0.12165E-06     456   0.94675E-08   0.12531E+00 0.35769E+03 
c  nu_tilda     0.45967E-05      32   0.85649E-05   0.19185E-06 0.13977E+03 
c  TempC        0.27614E+02      27   0.66199E-03   0.66096E+01 0.24855E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2548           10.04          4.5729          4.5729
v  Velocity[Y]            -3.6175          7.0212        0.019184        0.019184
v  Velocity[Z]       -6.9287e-015     6.6462e-015    -1.4109e-017    -1.4109e-017
v  ǁVelocityǁ         0.0021057          10.043          5.1234          5.1234
v  Pressure                -52.64          21.591         -4.4035         -4.4035
v  nu_tilda           4.2811e-007       0.0042687      0.00091043      0.00091043
v  TempC                       21          73.279          21.567          21.567
v  TurbVisc           2.9578e-014       0.0050311       0.0010621       0.0010621
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              689:        0.37980E+01

===============================================================


 INSTANT    0.690000000E+03   TIME STEP NUMBER             690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68031E-02 0.87811E+00
   Friction velocity        uk    :  0.68031E-02 0.87811E+00
   Dimensionless distance   yplus :  0.54770E-01 0.70694E+01
   Friction thermal sca.    tstar : -0.74062E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40864E-01 0.52746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65646E-02      32   0.44694E-03   0.18715E+01 0.85131E+02 
c  Velocity[X]                                      0.11925E+01 
c  Velocity[Y]                                      0.67902E+00 
c  Velocity[Z]                                      0.98568E-30 
c  Pressure     0.11642E-06     377   0.98869E-08   0.11768E+00 0.22957E+03 
c  nu_tilda     0.45985E-05      32   0.13712E-04   0.19166E-06 0.13964E+03 
c  TempC        0.27626E+02      27   0.48768E-03   0.11583E+02 0.35624E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2558          10.041          4.5729          4.5729
v  Velocity[Y]            -3.6145          7.0424        0.019165        0.019165
v  Velocity[Z]       -6.9287e-015     6.5816e-015    -1.4098e-017    -1.4098e-017
v  ǁVelocityǁ         0.0018591          10.044          5.1239          5.1239
v  Pressure               -52.639          21.647         -4.4017         -4.4017
v  nu_tilda           4.2796e-007       0.0042687      0.00091102      0.00091102
v  TempC                       21          73.848          21.568          21.568
v  TurbVisc           2.9551e-014       0.0050311       0.0010628       0.0010628
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              690:        0.37380E+01

===============================================================


 INSTANT    0.691000000E+03   TIME STEP NUMBER             691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84091E-02 0.87929E+00
   Friction velocity        uk    :  0.84091E-02 0.87929E+00
   Dimensionless distance   yplus :  0.67699E-01 0.70789E+01
   Friction thermal sca.    tstar : -0.65103E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50511E-01 0.52816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65685E-02      32   0.38817E-03   0.19040E+01 0.85340E+02 
c  Velocity[X]                                      0.12022E+01 
c  Velocity[Y]                                      0.70183E+00 
c  Velocity[Z]                                      0.12948E-29 
c  Pressure     0.15626E-06     408   0.97427E-08   0.15362E+00 0.23342E+03 
c  nu_tilda     0.46002E-05      32   0.85493E-05   0.19150E-06 0.13951E+03 
c  TempC        0.27638E+02      27   0.46725E-03   0.71383E+01 0.25477E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2569          10.042          4.5729          4.5729
v  Velocity[Y]            -3.6118            7.04        0.019148        0.019148
v  Velocity[Z]       -7.4939e-015     6.5836e-015    -1.4111e-017    -1.4111e-017
v  ǁVelocityǁ         0.0020477          10.045          5.1245          5.1245
v  Pressure                -52.65          21.636         -4.4168         -4.4168
v  nu_tilda           4.2781e-007       0.0042687      0.00091163      0.00091163
v  TempC                       21          73.073          21.568          21.568
v  TurbVisc            2.951e-014       0.0050311       0.0010636       0.0010636
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              691:        0.33290E+01

===============================================================


 INSTANT    0.692000000E+03   TIME STEP NUMBER             692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58998E-02 0.87901E+00
   Friction velocity        uk    :  0.58998E-02 0.87901E+00
   Dimensionless distance   yplus :  0.47497E-01 0.70767E+01
   Friction thermal sca.    tstar : -0.55514E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35438E-01 0.52800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65725E-02      32   0.34285E-03   0.18834E+01 0.85127E+02 
c  Velocity[X]                                      0.12001E+01 
c  Velocity[Y]                                      0.68336E+00 
c  Velocity[Z]                                      0.11665E-29 
c  Pressure     0.11427E-06     425   0.93364E-08   0.11787E+00 0.37777E+03 
c  nu_tilda     0.46020E-05      32   0.13733E-04   0.19132E-06 0.13938E+03 
c  TempC        0.27650E+02      28   0.40705E-03   0.59337E+01 0.23118E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2579          10.042          4.5729          4.5729
v  Velocity[Y]             -3.609          7.0154        0.019127        0.019127
v  Velocity[Z]       -6.9287e-015     6.3922e-015    -1.4105e-017    -1.4105e-017
v  ǁVelocityǁ         0.0020208          10.045          5.1251          5.1251
v  Pressure               -52.642          21.572         -4.4361         -4.4361
v  nu_tilda           4.2775e-007       0.0042687      0.00091222      0.00091222
v  TempC                       21           73.55          21.569          21.569
v  TurbVisc           2.9469e-014       0.0050311       0.0010643       0.0010643
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              692:        0.35570E+01

===============================================================


 INSTANT    0.693000000E+03   TIME STEP NUMBER             693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10898E-01 0.87795E+00
   Friction velocity        uk    :  0.10898E-01 0.87795E+00
   Dimensionless distance   yplus :  0.87737E-01 0.70681E+01
   Friction thermal sca.    tstar : -0.57152E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65462E-01 0.52736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65764E-02      32   0.43229E-03   0.18514E+01 0.84818E+02 
c  Velocity[X]                                      0.11789E+01 
c  Velocity[Y]                                      0.67249E+00 
c  Velocity[Z]                                      0.12141E-29 
c  Pressure     0.96187E-07     409   0.99700E-08   0.97415E-01 0.63792E+03 
c  nu_tilda     0.46038E-05      32   0.85160E-05   0.19115E-06 0.13925E+03 
c  TempC        0.27662E+02      27   0.37831E-03   0.64907E+01 0.25088E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.259          10.043          4.5729          4.5729
v  Velocity[Y]            -3.6064           7.039        0.019108        0.019108
v  Velocity[Z]       -8.0311e-015      6.247e-015    -1.4114e-017    -1.4114e-017
v  ǁVelocityǁ          0.002009          10.046          5.1257          5.1257
v  Pressure                -52.66          21.682         -4.4281         -4.4281
v  nu_tilda           4.2763e-007       0.0042687      0.00091283      0.00091283
v  TempC                       21          73.161          21.569          21.569
v  TurbVisc           2.9452e-014       0.0050311        0.001065        0.001065
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              693:        0.32250E+01

===============================================================


 INSTANT    0.694000000E+03   TIME STEP NUMBER             694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96452E-02 0.87891E+00
   Friction velocity        uk    :  0.96452E-02 0.87891E+00
   Dimensionless distance   yplus :  0.77651E-01 0.70758E+01
   Friction thermal sca.    tstar : -0.56845E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57936E-01 0.52793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65803E-02      32   0.42514E-03   0.18790E+01 0.85124E+02 
c  Velocity[X]                                      0.11822E+01 
c  Velocity[Y]                                      0.69683E+00 
c  Velocity[Z]                                      0.12392E-29 
c  Pressure     0.11349E-06     441   0.94499E-08   0.11660E+00 0.59909E+03 
c  nu_tilda     0.46055E-05      32   0.13733E-04   0.19097E-06 0.13912E+03 
c  TempC        0.27674E+02      27   0.92517E-03   0.59762E+01 0.24746E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.26          10.043          4.5729          4.5729
v  Velocity[Y]            -3.6039          7.0177        0.019088        0.019088
v  Velocity[Z]       -7.0866e-015     6.1703e-015    -1.4109e-017    -1.4109e-017
v  ǁVelocityǁ         0.0020261          10.047          5.1262          5.1262
v  Pressure                -52.65          21.574         -4.4581         -4.4581
v  nu_tilda           4.2758e-007       0.0042687      0.00091342      0.00091342
v  TempC                       21          74.045           21.57           21.57
v  TurbVisc           2.9419e-014       0.0050311       0.0010657       0.0010657
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              694:        0.32630E+01

===============================================================


 INSTANT    0.695000000E+03   TIME STEP NUMBER             695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11191E-01 0.87810E+00
   Friction velocity        uk    :  0.11191E-01 0.87810E+00
   Dimensionless distance   yplus :  0.90095E-01 0.70693E+01
   Friction thermal sca.    tstar : -0.60262E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67221E-01 0.52745E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65843E-02      32   0.41389E-03   0.18909E+01 0.85144E+02 
c  Velocity[X]                                      0.11990E+01 
c  Velocity[Y]                                      0.69187E+00 
c  Velocity[Z]                                      0.99958E-30 
c  Pressure     0.13252E-06     342   0.91933E-08   0.13073E+00 0.47479E+03 
c  nu_tilda     0.46073E-05      32   0.84919E-05   0.19082E-06 0.13899E+03 
c  TempC        0.27686E+02      27   0.46905E-03   0.20348E+02 0.43940E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2615          10.044          4.5729          4.5729
v  Velocity[Y]            -3.6015          7.0369        0.019068        0.019068
v  Velocity[Z]       -8.5355e-015     6.1958e-015    -1.4116e-017    -1.4116e-017
v  ǁVelocityǁ         0.0021493          10.047          5.1268          5.1268
v  Pressure               -52.669          21.646         -4.4585         -4.4585
v  nu_tilda           4.2756e-007       0.0042688      0.00091403      0.00091403
v  TempC                       21          73.073           21.57           21.57
v  TurbVisc           2.9405e-014       0.0050311       0.0010664       0.0010664
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              695:        0.29580E+01

===============================================================


 INSTANT    0.696000000E+03   TIME STEP NUMBER             696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11553E-01 0.87946E+00
   Friction velocity        uk    :  0.11553E-01 0.87946E+00
   Dimensionless distance   yplus :  0.93008E-01 0.70803E+01
   Friction thermal sca.    tstar : -0.66655E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69394E-01 0.52827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65882E-02      32   0.45713E-03   0.18702E+01 0.84981E+02 
c  Velocity[X]                                      0.11988E+01 
c  Velocity[Y]                                      0.67133E+00 
c  Velocity[Z]                                      0.99532E-30 
c  Pressure     0.11550E-06     377   0.94118E-08   0.11666E+00 0.17062E+03 
c  nu_tilda     0.46091E-05      32   0.13753E-04   0.19064E-06 0.13886E+03 
c  TempC        0.27699E+02      28   0.46984E-03   0.66952E+01 0.23602E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2629          10.045          4.5729          4.5729
v  Velocity[Y]            -3.5992          7.0445        0.019046        0.019046
v  Velocity[Z]       -7.5471e-015     6.0655e-015    -1.4113e-017    -1.4113e-017
v  ǁVelocityǁ         0.0019489          10.048          5.1274          5.1274
v  Pressure               -52.664          21.644         -4.4677         -4.4677
v  nu_tilda           4.2751e-007       0.0042688      0.00091462      0.00091462
v  TempC                       21          73.075          21.571          21.571
v  TurbVisc           2.9401e-014       0.0050311       0.0010671       0.0010671
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              696:        0.32620E+01

===============================================================


 INSTANT    0.697000000E+03   TIME STEP NUMBER             697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10286E-01 0.87926E+00
   Friction velocity        uk    :  0.10286E-01 0.87926E+00
   Dimensionless distance   yplus :  0.82809E-01 0.70786E+01
   Friction thermal sca.    tstar : -0.74257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61784E-01 0.52814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65921E-02      32   0.37660E-03   0.18912E+01 0.85261E+02 
c  Velocity[X]                                      0.12000E+01 
c  Velocity[Y]                                      0.69119E+00 
c  Velocity[Z]                                      0.11072E-29 
c  Pressure     0.12691E-06     442   0.96067E-08   0.13046E+00 0.27905E+03 
c  nu_tilda     0.46108E-05      32   0.84842E-05   0.19048E-06 0.13874E+03 
c  TempC        0.27711E+02      28   0.56137E-03   0.62951E+01 0.23287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2644          10.045          4.5729          4.5729
v  Velocity[Y]            -3.5969           7.019        0.019024        0.019024
v  Velocity[Z]       -9.1307e-015     6.0055e-015    -1.4123e-017    -1.4123e-017
v  ǁVelocityǁ          0.002229          10.048           5.128           5.128
v  Pressure               -52.678           21.59         -4.4929         -4.4929
v  nu_tilda           4.2744e-007       0.0042688      0.00091523      0.00091523
v  TempC                       21          74.461          21.572          21.572
v  TurbVisc           2.9387e-014       0.0050312       0.0010678       0.0010678
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              697:        0.33660E+01

===============================================================


 INSTANT    0.698000000E+03   TIME STEP NUMBER             698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12575E-01 0.87791E+00
   Friction velocity        uk    :  0.12575E-01 0.87791E+00
   Dimensionless distance   yplus :  0.10124E+00 0.70678E+01
   Friction thermal sca.    tstar : -0.94933E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75534E-01 0.52734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65960E-02      32   0.37029E-03   0.18350E+01 0.84482E+02 
c  Velocity[X]                                      0.11624E+01 
c  Velocity[Y]                                      0.67260E+00 
c  Velocity[Z]                                      0.93008E-30 
c  Pressure     0.13928E-06     441   0.96402E-08   0.14029E+00 0.38835E+03 
c  nu_tilda     0.46126E-05      32   0.13756E-04   0.19030E-06 0.13861E+03 
c  TempC        0.27723E+02      27   0.40493E-03   0.74219E+01 0.26524E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.266          10.046          4.5729          4.5729
v  Velocity[Y]            -3.5947          7.0385        0.019002        0.019002
v  Velocity[Z]       -9.7578e-015     6.0626e-015    -1.4118e-017    -1.4118e-017
v  ǁVelocityǁ         0.0019388          10.049          5.1285          5.1285
v  Pressure               -52.662          21.674         -4.4788         -4.4788
v  nu_tilda           4.2729e-007       0.0042688      0.00091583      0.00091583
v  TempC                       21          73.102          21.572          21.572
v  TurbVisc           2.9367e-014       0.0050312       0.0010686       0.0010686
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              698:        0.35250E+01

===============================================================


 INSTANT    0.699000000E+03   TIME STEP NUMBER             699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10506E-01 0.87893E+00
   Friction velocity        uk    :  0.10506E-01 0.87893E+00
   Dimensionless distance   yplus :  0.84581E-01 0.70760E+01
   Friction thermal sca.    tstar : -0.13994E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63107E-01 0.52795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66000E-02      32   0.44047E-03   0.18394E+01 0.84454E+02 
c  Velocity[X]                                      0.11727E+01 
c  Velocity[Y]                                      0.66667E+00 
c  Velocity[Z]                                      0.10332E-29 
c  Pressure     0.11984E-06     472   0.99635E-08   0.12218E+00 0.49281E+03 
c  nu_tilda     0.46144E-05      32   0.84217E-05   0.19016E-06 0.13849E+03 
c  TempC        0.27735E+02      27   0.45749E-03   0.61822E+01 0.23685E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2675          10.046          4.5729          4.5729
v  Velocity[Y]            -3.5925          7.0158        0.018979        0.018979
v  Velocity[Z]       -7.4237e-015     5.9588e-015    -1.4106e-017    -1.4106e-017
v  ǁVelocityǁ         0.0023512          10.049          5.1291          5.1291
v  Pressure               -52.688          21.571         -4.5193         -4.5193
v  nu_tilda            4.272e-007       0.0042688      0.00091644      0.00091644
v  TempC                       21          73.516          21.573          21.573
v  TurbVisc           2.9325e-014       0.0050312       0.0010693       0.0010693
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              699:        0.35650E+01

===============================================================


 INSTANT    0.700000000E+03   TIME STEP NUMBER             700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13536E-01 0.87805E+00
   Friction velocity        uk    :  0.13536E-01 0.87805E+00
   Dimensionless distance   yplus :  0.10898E+00 0.70689E+01
   Friction thermal sca.    tstar : -0.24942E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81310E-01 0.52742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66039E-02      32   0.40440E-03   0.18648E+01 0.84847E+02 
c  Velocity[X]                                      0.11780E+01 
c  Velocity[Y]                                      0.68687E+00 
c  Velocity[Z]                                      0.12167E-29 
c  Pressure     0.11900E-06     405   0.96838E-08   0.11946E+00 0.30659E+03 
c  nu_tilda     0.46161E-05      32   0.13777E-04   0.18998E-06 0.13836E+03 
c  TempC        0.27747E+02      27   0.45056E-03   0.71116E+01 0.26200E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2689          10.046          4.5729          4.5729
v  Velocity[Y]            -3.5904          7.0353        0.018955        0.018955
v  Velocity[Z]       -8.5215e-015     5.9045e-015    -1.4111e-017    -1.4111e-017
v  ǁVelocityǁ          0.002023           10.05          5.1297          5.1297
v  Pressure               -52.682          21.644         -4.5123         -4.5123
v  nu_tilda           4.2715e-007       0.0042688      0.00091703      0.00091703
v  TempC                       21          73.075          21.573          21.573
v  TurbVisc           2.9302e-014       0.0050312         0.00107         0.00107
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              700:        0.32320E+01

===============================================================


 INSTANT    0.701000000E+03   TIME STEP NUMBER             701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11393E-01 0.87944E+00
   Friction velocity        uk    :  0.11393E-01 0.87944E+00
   Dimensionless distance   yplus :  0.91718E-01 0.70801E+01
   Friction thermal sca.    tstar : -0.10494E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68432E-01 0.52826E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66078E-02      32   0.37886E-03   0.18185E+01 0.84333E+02 
c  Velocity[X]                                      0.11485E+01 
c  Velocity[Y]                                      0.67001E+00 
c  Velocity[Z]                                      0.98281E-30 
c  Pressure     0.11400E-06     346   0.92595E-08   0.11678E+00 0.40118E+03 
c  nu_tilda     0.46179E-05      32   0.84289E-05   0.18983E-06 0.13824E+03 
c  TempC        0.27759E+02      27   0.75163E-03   0.66978E+01 0.26208E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2708          10.047          4.5729          4.5729
v  Velocity[Y]            -3.5886          7.0451        0.018932        0.018932
v  Velocity[Z]        -9.754e-015     5.8243e-015     -1.412e-017     -1.412e-017
v  ǁVelocityǁ         0.0020574           10.05          5.1302          5.1302
v  Pressure               -52.698          21.695         -4.5149         -4.5149
v  nu_tilda           4.2706e-007       0.0042688      0.00091764      0.00091764
v  TempC                       21          73.961          21.574          21.574
v  TurbVisc           2.9287e-014       0.0050312       0.0010707       0.0010707
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              701:        0.29740E+01

===============================================================


 INSTANT    0.702000000E+03   TIME STEP NUMBER             702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10860E-01 0.87877E+00
   Friction velocity        uk    :  0.10860E-01 0.87877E+00
   Dimensionless distance   yplus :  0.87434E-01 0.70747E+01
   Friction thermal sca.    tstar : -0.10747E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65235E-01 0.52785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66117E-02      32   0.41640E-03   0.18394E+01 0.84390E+02 
c  Velocity[X]                                      0.11784E+01 
c  Velocity[Y]                                      0.66107E+00 
c  Velocity[Z]                                      0.87435E-30 
c  Pressure     0.13091E-06     470   0.91684E-08   0.13298E+00 0.77921E+03 
c  nu_tilda     0.46196E-05      32   0.13775E-04   0.18966E-06 0.13812E+03 
c  TempC        0.27771E+02      27   0.52341E-03   0.13030E+02 0.37423E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2729          10.047          4.5729          4.5729
v  Velocity[Y]            -3.5868          7.0145        0.018907        0.018907
v  Velocity[Z]       -8.8283e-015     5.8828e-015    -1.4109e-017    -1.4109e-017
v  ǁVelocityǁ         0.0022052          10.051          5.1308          5.1308
v  Pressure               -52.689          21.548         -4.5535         -4.5535
v  nu_tilda           4.2709e-007       0.0042688      0.00091824      0.00091824
v  TempC                       21          73.075          21.574          21.574
v  TurbVisc           2.9263e-014       0.0050312       0.0010714       0.0010714
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              702:        0.34810E+01

===============================================================


 INSTANT    0.703000000E+03   TIME STEP NUMBER             703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13044E-01 0.87767E+00
   Friction velocity        uk    :  0.13044E-01 0.87767E+00
   Dimensionless distance   yplus :  0.10501E+00 0.70658E+01
   Friction thermal sca.    tstar : -0.11770E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78349E-01 0.52719E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66156E-02      32   0.39796E-03   0.18287E+01 0.84390E+02 
c  Velocity[X]                                      0.11503E+01 
c  Velocity[Y]                                      0.67838E+00 
c  Velocity[Z]                                      0.10830E-29 
c  Pressure     0.11350E-06     426   0.95954E-08   0.11627E+00 0.75398E+03 
c  nu_tilda     0.46214E-05      32   0.83822E-05   0.18952E-06 0.13800E+03 
c  TempC        0.27783E+02      27   0.31829E-03   0.80984E+01 0.27322E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.275          10.048          4.5729          4.5729
v  Velocity[Y]            -3.5851          7.0327        0.018882        0.018882
v  Velocity[Z]       -9.4761e-015     5.8121e-015    -1.4117e-017    -1.4117e-017
v  ǁVelocityǁ         0.0022049          10.051          5.1314          5.1314
v  Pressure               -52.711          21.684         -4.5403         -4.5403
v  nu_tilda           4.2713e-007       0.0042688      0.00091885      0.00091885
v  TempC                       21          73.395          21.575          21.575
v  TurbVisc           2.9272e-014       0.0050312       0.0010721       0.0010721
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              703:        0.34500E+01

===============================================================


 INSTANT    0.704000000E+03   TIME STEP NUMBER             704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57890E-02 0.87850E+00
   Friction velocity        uk    :  0.57890E-02 0.87850E+00
   Dimensionless distance   yplus :  0.46605E-01 0.70725E+01
   Friction thermal sca.    tstar : -0.21117E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34773E-01 0.52769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66196E-02      32   0.39885E-03   0.18228E+01 0.84392E+02 
c  Velocity[X]                                      0.11439E+01 
c  Velocity[Y]                                      0.67893E+00 
c  Velocity[Z]                                      0.89966E-30 
c  Pressure     0.99697E-07     453   0.95338E-08   0.10197E+00 0.69007E+03 
c  nu_tilda     0.46231E-05      32   0.13797E-04   0.18936E-06 0.13788E+03 
c  TempC        0.27795E+02      27   0.54307E-03   0.50618E+01 0.21587E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2768          10.049          4.5729          4.5729
v  Velocity[Y]            -3.5834          7.0115        0.018856        0.018856
v  Velocity[Z]       -8.9251e-015     5.8529e-015    -1.4114e-017    -1.4114e-017
v  ǁVelocityǁ         0.0022747          10.052          5.1319          5.1319
v  Pressure               -52.704          21.556         -4.5754         -4.5754
v  nu_tilda           4.2715e-007       0.0042688      0.00091944      0.00091944
v  TempC                       21          73.639          21.575          21.575
v  TurbVisc           2.9281e-014       0.0050312       0.0010729       0.0010729
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              704:        0.33410E+01

===============================================================


 INSTANT    0.705000000E+03   TIME STEP NUMBER             705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67076E-02 0.87794E+00
   Friction velocity        uk    :  0.67076E-02 0.87794E+00
   Dimensionless distance   yplus :  0.54001E-01 0.70680E+01
   Friction thermal sca.    tstar : -0.28023E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40291E-01 0.52735E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66235E-02      32   0.45077E-03   0.18169E+01 0.84193E+02 
c  Velocity[X]                                      0.11570E+01 
c  Velocity[Y]                                      0.65983E+00 
c  Velocity[Z]                                      0.99610E-30 
c  Pressure     0.11255E-06     406   0.90980E-08   0.11378E+00 0.63550E+03 
c  nu_tilda     0.46249E-05      32   0.83894E-05   0.18921E-06 0.13776E+03 
c  TempC        0.27807E+02      28   0.52475E-03   0.67839E+01 0.25371E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2788          10.049          4.5729          4.5729
v  Velocity[Y]            -3.5817          7.0388        0.018831        0.018831
v  Velocity[Z]       -9.7972e-015     5.9122e-015    -1.4118e-017    -1.4118e-017
v  ǁVelocityǁ         0.0022343          10.053          5.1325          5.1325
v  Pressure               -52.724           21.67         -4.5681         -4.5681
v  nu_tilda           4.2707e-007       0.0042688      0.00092005      0.00092005
v  TempC                       21          73.279          21.576          21.576
v  TurbVisc           2.9288e-014       0.0050312       0.0010736       0.0010736
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              705:        0.37220E+01

===============================================================


 INSTANT    0.706000000E+03   TIME STEP NUMBER             706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88510E-02 0.87920E+00
   Friction velocity        uk    :  0.88510E-02 0.87920E+00
   Dimensionless distance   yplus :  0.71257E-01 0.70782E+01
   Friction thermal sca.    tstar : -0.12723E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53165E-01 0.52811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66274E-02      32   0.40413E-03   0.18193E+01 0.84290E+02 
c  Velocity[X]                                      0.11354E+01 
c  Velocity[Y]                                      0.68385E+00 
c  Velocity[Z]                                      0.11048E-29 
c  Pressure     0.12341E-06     408   0.94476E-08   0.12441E+00 0.29215E+03 
c  nu_tilda     0.46266E-05      32   0.13795E-04   0.18905E-06 0.13764E+03 
c  TempC        0.27819E+02      27   0.41404E-03   0.77491E+01 0.27401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2806           10.05          4.5729          4.5729
v  Velocity[Y]            -3.5803           7.035        0.018804        0.018804
v  Velocity[Z]       -9.3862e-015     5.9535e-015    -1.4112e-017    -1.4112e-017
v  ǁVelocityǁ         0.0019585          10.053          5.1331          5.1331
v  Pressure                -52.72          21.636         -4.5849         -4.5849
v  nu_tilda           4.2696e-007       0.0042688      0.00092065      0.00092065
v  TempC                       21          73.077          21.576          21.576
v  TurbVisc           2.9267e-014       0.0050312       0.0010743       0.0010743
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              706:        0.36170E+01

===============================================================


 INSTANT    0.707000000E+03   TIME STEP NUMBER             707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85110E-03 0.87876E+00
   Friction velocity        uk    :  0.85110E-03 0.87876E+00
   Dimensionless distance   yplus :  0.68519E-02 0.70746E+01
   Friction thermal sca.    tstar : -0.10354E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51123E-02 0.52785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66313E-02      32   0.35089E-03   0.18211E+01 0.84278E+02 
c  Velocity[X]                                      0.11569E+01 
c  Velocity[Y]                                      0.66424E+00 
c  Velocity[Z]                                      0.91904E-30 
c  Pressure     0.10340E-06     453   0.94556E-08   0.10690E+00 0.33019E+03 
c  nu_tilda     0.46284E-05      32   0.83530E-05   0.18892E-06 0.13753E+03 
c  TempC        0.27831E+02      27   0.76121E-03   0.56716E+01 0.23062E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2827          10.051          4.5729          4.5729
v  Velocity[Y]            -3.5789          7.0112        0.018777        0.018777
v  Velocity[Z]       -1.0415e-014     5.9993e-015    -1.4118e-017    -1.4118e-017
v  ǁVelocityǁ          0.001888          10.054          5.1336          5.1336
v  Pressure               -52.734          21.565         -4.6131         -4.6131
v  nu_tilda           4.2692e-007       0.0042688      0.00092126      0.00092126
v  TempC                       21          73.881          21.577          21.577
v  TurbVisc           2.9237e-014       0.0050312        0.001075        0.001075
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              707:        0.32940E+01

===============================================================


 INSTANT    0.708000000E+03   TIME STEP NUMBER             708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80532E-03 0.87760E+00
   Friction velocity        uk    :  0.80532E-03 0.87760E+00
   Dimensionless distance   yplus :  0.64833E-02 0.70653E+01
   Friction thermal sca.    tstar : -0.83636E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48373E-02 0.52715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66352E-02      32   0.40018E-03   0.17850E+01 0.83875E+02 
c  Velocity[X]                                      0.11311E+01 
c  Velocity[Y]                                      0.65384E+00 
c  Velocity[Z]                                      0.93146E-30 
c  Pressure     0.10096E-06     394   0.99269E-08   0.10252E+00 0.35685E+03 
c  nu_tilda     0.46301E-05      32   0.13825E-04   0.18876E-06 0.13741E+03 
c  TempC        0.27844E+02      27   0.54757E-03   0.10298E+02 0.31757E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2852          10.052          4.5729          4.5729
v  Velocity[Y]            -3.5775          7.0334        0.018749        0.018749
v  Velocity[Z]        -1.004e-014     6.0513e-015    -1.4111e-017    -1.4111e-017
v  ǁVelocityǁ          0.001695          10.055          5.1342          5.1342
v  Pressure               -52.736          21.651         -4.6047         -4.6047
v  nu_tilda           4.2685e-007       0.0042688      0.00092186      0.00092186
v  TempC                       21          73.078          21.578          21.578
v  TurbVisc           2.9226e-014       0.0050312       0.0010757       0.0010757
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              708:        0.37840E+01

===============================================================


 INSTANT    0.709000000E+03   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19603E-02 0.87863E+00
   Friction velocity        uk    :  0.19603E-02 0.87863E+00
   Dimensionless distance   yplus :  0.15782E-01 0.70736E+01
   Friction thermal sca.    tstar : -0.69620E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11775E-01 0.52777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66391E-02      32   0.42972E-03   0.18261E+01 0.84262E+02 
c  Velocity[X]                                      0.11500E+01 
c  Velocity[Y]                                      0.67604E+00 
c  Velocity[Z]                                      0.10295E-29 
c  Pressure     0.15433E-06     456   0.98842E-08   0.15722E+00 0.37668E+03 
c  nu_tilda     0.46319E-05      32   0.83386E-05   0.18862E-06 0.13730E+03 
c  TempC        0.27856E+02      27   0.36599E-03   0.80128E+01 0.26573E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2877          10.053          4.5729          4.5729
v  Velocity[Y]            -3.5763           7.009        0.018721        0.018721
v  Velocity[Z]       -1.1081e-014     6.0949e-015    -1.4115e-017    -1.4115e-017
v  ǁVelocityǁ         0.0016451          10.056          5.1347          5.1347
v  Pressure               -52.742          21.562         -4.6322         -4.6322
v  nu_tilda            4.268e-007       0.0042688      0.00092247      0.00092247
v  TempC                       21          73.331          21.578          21.578
v  TurbVisc           2.9204e-014       0.0050312       0.0010765       0.0010765
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              709:        0.38840E+01

===============================================================


 INSTANT    0.710000000E+03   TIME STEP NUMBER             710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27871E-02 0.87806E+00
   Friction velocity        uk    :  0.27871E-02 0.87806E+00
   Dimensionless distance   yplus :  0.22438E-01 0.70690E+01
   Friction thermal sca.    tstar : -0.86130E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16741E-01 0.52743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66430E-02      32   0.38510E-03   0.18320E+01 0.84351E+02 
c  Velocity[X]                                      0.11719E+01 
c  Velocity[Y]                                      0.66006E+00 
c  Velocity[Z]                                      0.92308E-30 
c  Pressure     0.11432E-06     410   0.92180E-08   0.11619E+00 0.33688E+03 
c  nu_tilda     0.46336E-05      32   0.13819E-04   0.18846E-06 0.13718E+03 
c  TempC        0.27868E+02      27   0.41223E-03   0.55292E+01 0.22613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.29          10.053          4.5729          4.5729
v  Velocity[Y]            -3.5751          7.0315        0.018692        0.018692
v  Velocity[Z]        -9.588e-015      6.137e-015    -1.4103e-017    -1.4103e-017
v  ǁVelocityǁ         0.0015273          10.056          5.1353          5.1353
v  Pressure               -52.748           21.65         -4.6268         -4.6268
v  nu_tilda           4.2674e-007       0.0042688      0.00092306      0.00092306
v  TempC                       21          73.918          21.579          21.579
v  TurbVisc           2.9193e-014       0.0050312       0.0010772       0.0010772
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              710:        0.33480E+01

===============================================================


 INSTANT    0.711000000E+03   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14924E-02 0.87927E+00
   Friction velocity        uk    :  0.14924E-02 0.87927E+00
   Dimensionless distance   yplus :  0.12015E-01 0.70787E+01
   Friction thermal sca.    tstar : -0.11318E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89646E-02 0.52815E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66469E-02      32   0.39130E-03   0.17663E+01 0.83652E+02 
c  Velocity[X]                                      0.11167E+01 
c  Velocity[Y]                                      0.64965E+00 
c  Velocity[Z]                                      0.97763E-30 
c  Pressure     0.89733E-07     392   0.96017E-08   0.91454E-01 0.26910E+03 
c  nu_tilda     0.46353E-05      32   0.82943E-05   0.18833E-06 0.13707E+03 
c  TempC        0.27880E+02      27   0.68949E-03   0.70091E+01 0.24806E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2924          10.054          4.5729          4.5729
v  Velocity[Y]            -3.5741           7.041        0.018663        0.018663
v  Velocity[Z]       -1.0506e-014     6.1901e-015    -1.4106e-017    -1.4106e-017
v  ǁVelocityǁ         0.0014806          10.057          5.1359          5.1359
v  Pressure               -52.768          21.668         -4.6388         -4.6388
v  nu_tilda           4.2668e-007       0.0042688      0.00092368      0.00092368
v  TempC                       21          73.283          21.579          21.579
v  TurbVisc           2.9177e-014       0.0050313       0.0010779       0.0010779
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              711:        0.34260E+01

===============================================================


 INSTANT    0.712000000E+03   TIME STEP NUMBER             712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32407E-02 0.87873E+00
   Friction velocity        uk    :  0.32407E-02 0.87873E+00
   Dimensionless distance   yplus :  0.26090E-01 0.70744E+01
   Friction thermal sca.    tstar : -0.28408E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19466E-01 0.52783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66508E-02      32   0.36965E-03   0.17918E+01 0.83880E+02 
c  Velocity[X]                                      0.11253E+01 
c  Velocity[Y]                                      0.66646E+00 
c  Velocity[Z]                                      0.10051E-29 
c  Pressure     0.12251E-06     469   0.97526E-08   0.12678E+00 0.66055E+03 
c  nu_tilda     0.46371E-05      32   0.13844E-04   0.18819E-06 0.13696E+03 
c  TempC        0.27892E+02      28   0.39314E-03   0.13472E+02 0.38881E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2947          10.055          4.5729          4.5729
v  Velocity[Y]            -3.5731          7.0144        0.018633        0.018633
v  Velocity[Z]       -1.0525e-014      6.228e-015    -1.4099e-017    -1.4099e-017
v  ǁVelocityǁ         0.0014116          10.058          5.1364          5.1364
v  Pressure               -52.758          21.547          -4.672          -4.672
v  nu_tilda           4.2663e-007       0.0042689      0.00092427      0.00092427
v  TempC                       21          73.079           21.58           21.58
v  TurbVisc           2.9158e-014       0.0050313       0.0010786       0.0010786
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              712:        0.36810E+01

===============================================================


 INSTANT    0.713000000E+03   TIME STEP NUMBER             713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25806E-02 0.87750E+00
   Friction velocity        uk    :  0.25806E-02 0.87750E+00
   Dimensionless distance   yplus :  0.20776E-01 0.70645E+01
   Friction thermal sca.    tstar : -0.12463E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15501E-01 0.52709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66546E-02      32   0.39527E-03   0.17841E+01 0.83716E+02 
c  Velocity[X]                                      0.11288E+01 
c  Velocity[Y]                                      0.65530E+00 
c  Velocity[Z]                                      0.10087E-29 
c  Pressure     0.11809E-06     425   0.92655E-08   0.11937E+00 0.62103E+03 
c  nu_tilda     0.46388E-05      32   0.83024E-05   0.18805E-06 0.13684E+03 
c  TempC        0.27904E+02      27   0.44081E-03   0.62947E+01 0.24805E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2973          10.056          4.5729          4.5729
v  Velocity[Y]            -3.5722           7.031        0.018603        0.018603
v  Velocity[Z]        -1.093e-014     6.2711e-015    -1.4097e-017    -1.4097e-017
v  ǁVelocityǁ         0.0013775          10.059           5.137           5.137
v  Pressure               -52.777           21.65         -4.6637         -4.6637
v  nu_tilda           4.2649e-007       0.0042689      0.00092489      0.00092489
v  TempC                       21          73.078           21.58           21.58
v  TurbVisc           2.9146e-014       0.0050313       0.0010793       0.0010793
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              713:        0.34150E+01

===============================================================


 INSTANT    0.714000000E+03   TIME STEP NUMBER             714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39211E-02 0.87840E+00
   Friction velocity        uk    :  0.39211E-02 0.87840E+00
   Dimensionless distance   yplus :  0.31567E-01 0.70717E+01
   Friction thermal sca.    tstar : -0.91807E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23553E-01 0.52763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66585E-02      32   0.43769E-03   0.17866E+01 0.83770E+02 
c  Velocity[X]                                      0.11394E+01 
c  Velocity[Y]                                      0.64723E+00 
c  Velocity[Z]                                      0.11017E-29 
c  Pressure     0.11599E-06     469   0.94014E-08   0.11889E+00 0.61671E+03 
c  nu_tilda     0.46405E-05      32   0.13840E-04   0.18791E-06 0.13673E+03 
c  TempC        0.27916E+02      28   0.48077E-03   0.76268E+01 0.25151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3002          10.056          4.5729          4.5729
v  Velocity[Y]            -3.5713          7.0089        0.018572        0.018572
v  Velocity[Z]       -1.0134e-014       6.32e-015    -1.4085e-017    -1.4085e-017
v  ǁVelocityǁ          0.001334          10.059          5.1375          5.1375
v  Pressure               -52.773          21.538         -4.6955         -4.6955
v  nu_tilda           4.2642e-007       0.0042689      0.00092548      0.00092548
v  TempC                       21          74.143          21.581          21.581
v  TurbVisc           2.9107e-014       0.0050313       0.0010801       0.0010801
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              714:        0.35100E+01

===============================================================


 INSTANT    0.715000000E+03   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50082E-02 0.87792E+00
   Friction velocity        uk    :  0.50082E-02 0.87792E+00
   Dimensionless distance   yplus :  0.40319E-01 0.70679E+01
   Friction thermal sca.    tstar : -0.70996E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30083E-01 0.52734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66624E-02      32   0.38698E-03   0.17918E+01 0.83919E+02 
c  Velocity[X]                                      0.11339E+01 
c  Velocity[Y]                                      0.65785E+00 
c  Velocity[Z]                                      0.12707E-29 
c  Pressure     0.12255E-06     425   0.95400E-08   0.12585E+00 0.73841E+03 
c  nu_tilda     0.46423E-05      32   0.82820E-05   0.18778E-06 0.13662E+03 
c  TempC        0.27928E+02      28   0.34632E-03   0.67696E+01 0.23186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3031          10.057          4.5729          4.5729
v  Velocity[Y]            -3.5704          7.0327        0.018542        0.018542
v  Velocity[Z]       -1.0524e-014     6.3596e-015    -1.4087e-017    -1.4087e-017
v  ǁVelocityǁ         0.0013042           10.06          5.1381          5.1381
v  Pressure               -52.794          21.677         -4.6832         -4.6832
v  nu_tilda           4.2631e-007       0.0042689       0.0009261       0.0009261
v  TempC                       21          73.846          21.581          21.581
v  TurbVisc           2.9087e-014       0.0050313       0.0010808       0.0010808
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              715:        0.34010E+01

===============================================================


 INSTANT    0.716000000E+03   TIME STEP NUMBER             716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39142E-02 0.87889E+00
   Friction velocity        uk    :  0.39142E-02 0.87889E+00
   Dimensionless distance   yplus :  0.31512E-01 0.70756E+01
   Friction thermal sca.    tstar : -0.64087E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23511E-01 0.52792E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66663E-02      32   0.39127E-03   0.17696E+01 0.83585E+02 
c  Velocity[X]                                      0.11188E+01 
c  Velocity[Y]                                      0.65088E+00 
c  Velocity[Z]                                      0.10563E-29 
c  Pressure     0.12474E-06     440   0.97712E-08   0.12593E+00 0.42411E+03 
c  nu_tilda     0.46440E-05      32   0.13848E-04   0.18764E-06 0.13651E+03 
c  TempC        0.27940E+02      27   0.48335E-03   0.51461E+01 0.20175E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3058          10.058          4.5729          4.5729
v  Velocity[Y]            -3.5696          7.0354         0.01851         0.01851
v  Velocity[Z]       -1.0184e-014     6.3953e-015    -1.4077e-017    -1.4077e-017
v  ǁVelocityǁ         0.0012696          10.061          5.1386          5.1386
v  Pressure               -52.793          21.612         -4.7071         -4.7071
v  nu_tilda            4.262e-007       0.0042689       0.0009267       0.0009267
v  TempC                       21          73.528          21.582          21.582
v  TurbVisc           2.9058e-014       0.0050313       0.0010815       0.0010815
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              716:        0.34360E+01

===============================================================


 INSTANT    0.717000000E+03   TIME STEP NUMBER             717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26236E-02 0.87870E+00
   Friction velocity        uk    :  0.26236E-02 0.87870E+00
   Dimensionless distance   yplus :  0.21122E-01 0.70741E+01
   Friction thermal sca.    tstar : -0.54810E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15759E-01 0.52781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66702E-02      32   0.37949E-03   0.17739E+01 0.83620E+02 
c  Velocity[X]                                      0.11264E+01 
c  Velocity[Y]                                      0.64752E+00 
c  Velocity[Z]                                      0.92491E-30 
c  Pressure     0.10167E-06     442   0.93660E-08   0.10672E+00 0.28656E+03 
c  nu_tilda     0.46457E-05      32   0.82706E-05   0.18752E-06 0.13641E+03 
c  TempC        0.27952E+02      28   0.44404E-03   0.54917E+01 0.22393E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3086          10.059          4.5729          4.5729
v  Velocity[Y]             -3.569          7.0112        0.018478        0.018478
v  Velocity[Z]       -1.0965e-014     6.4475e-015    -1.4076e-017    -1.4076e-017
v  ǁVelocityǁ          0.001259          10.062          5.1392          5.1392
v  Pressure                -52.81          21.553         -4.7324         -4.7324
v  nu_tilda            4.262e-007       0.0042689      0.00092731      0.00092731
v  TempC                       21          73.079          21.582          21.582
v  TurbVisc           2.9028e-014       0.0050313       0.0010822       0.0010822
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              717:        0.34440E+01

===============================================================


 INSTANT    0.718000000E+03   TIME STEP NUMBER             718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42781E-02 0.87738E+00
   Friction velocity        uk    :  0.42781E-02 0.87738E+00
   Dimensionless distance   yplus :  0.34441E-01 0.70635E+01
   Friction thermal sca.    tstar : -0.50090E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25697E-01 0.52701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66741E-02      32   0.40659E-03   0.17587E+01 0.83540E+02 
c  Velocity[X]                                      0.10998E+01 
c  Velocity[Y]                                      0.65890E+00 
c  Velocity[Z]                                      0.97615E-30 
c  Pressure     0.84253E-07     376   0.95040E-08   0.85379E-01 0.25678E+03 
c  nu_tilda     0.46475E-05      32   0.13866E-04   0.18738E-06 0.13630E+03 
c  TempC        0.27964E+02      27   0.66260E-03   0.59326E+01 0.23196E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3113           10.06          4.5729          4.5729
v  Velocity[Y]            -3.5684          7.0279        0.018445        0.018445
v  Velocity[Z]       -1.0945e-014     6.4845e-015    -1.4066e-017    -1.4066e-017
v  ǁVelocityǁ         0.0012328          10.062          5.1397          5.1397
v  Pressure               -52.813          21.619         -4.7296         -4.7296
v  nu_tilda           4.2622e-007       0.0042689      0.00092791      0.00092791
v  TempC                       21          74.222          21.583          21.583
v  TurbVisc           2.9027e-014       0.0050313       0.0010829       0.0010829
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              718:        0.31460E+01

===============================================================


 INSTANT    0.719000000E+03   TIME STEP NUMBER             719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43948E-02 0.87850E+00
   Friction velocity        uk    :  0.43948E-02 0.87850E+00
   Dimensionless distance   yplus :  0.35381E-01 0.70725E+01
   Friction thermal sca.    tstar : -0.52854E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26398E-01 0.52769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66780E-02      32   0.36815E-03   0.17764E+01 0.83675E+02 
c  Velocity[X]                                      0.11218E+01 
c  Velocity[Y]                                      0.65459E+00 
c  Velocity[Z]                                      0.88697E-30 
c  Pressure     0.12932E-06     457   0.95222E-08   0.13370E+00 0.34681E+03 
c  nu_tilda     0.46492E-05      32   0.82705E-05   0.18726E-06 0.13619E+03 
c  TempC        0.27976E+02      27   0.40057E-03   0.10542E+02 0.33146E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3141          10.061          4.5729          4.5729
v  Velocity[Y]            -3.5678          7.0111        0.018412        0.018412
v  Velocity[Z]       -1.1868e-014     6.5217e-015    -1.4067e-017    -1.4067e-017
v  ǁVelocityǁ         0.0012224          10.063          5.1403          5.1403
v  Pressure               -52.828          21.546          -4.759          -4.759
v  nu_tilda           4.2623e-007       0.0042689      0.00092853      0.00092853
v  TempC                       21          73.079          21.583          21.583
v  TurbVisc           2.9033e-014       0.0050313       0.0010837       0.0010837
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              719:        0.35510E+01

===============================================================


 INSTANT    0.720000000E+03   TIME STEP NUMBER             720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32189E-02 0.87773E+00
   Friction velocity        uk    :  0.32189E-02 0.87773E+00
   Dimensionless distance   yplus :  0.25914E-01 0.70663E+01
   Friction thermal sca.    tstar : -0.57861E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19335E-01 0.52723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66818E-02      32   0.38300E-03   0.17555E+01 0.83365E+02 
c  Velocity[X]                                      0.11124E+01 
c  Velocity[Y]                                      0.64313E+00 
c  Velocity[Z]                                      0.11829E-29 
c  Pressure     0.12153E-06     425   0.99225E-08   0.12329E+00 0.41766E+03 
c  nu_tilda     0.46509E-05      32   0.13866E-04   0.18712E-06 0.13609E+03 
c  TempC        0.27988E+02      27   0.43070E-03   0.55499E+01 0.22408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3176          10.061          4.5729          4.5729
v  Velocity[Y]            -3.5673          7.0285        0.018379        0.018379
v  Velocity[Z]       -1.1522e-014     6.5687e-015    -1.4055e-017    -1.4055e-017
v  ǁVelocityǁ         0.0011824          10.064          5.1408          5.1408
v  Pressure               -52.821          21.635          -4.744          -4.744
v  nu_tilda           4.2619e-007       0.0042689      0.00092912      0.00092912
v  TempC                       21          73.333          21.584          21.584
v  TurbVisc           2.9037e-014       0.0050313       0.0010844       0.0010844
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              720:        0.33890E+01

===============================================================


 INSTANT    0.721000000E+03   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22696E-02 0.87895E+00
   Friction velocity        uk    :  0.22696E-02 0.87895E+00
   Dimensionless distance   yplus :  0.18272E-01 0.70762E+01
   Friction thermal sca.    tstar : -0.68912E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13633E-01 0.52796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66857E-02      32   0.40036E-03   0.17386E+01 0.83328E+02 
c  Velocity[X]                                      0.10827E+01 
c  Velocity[Y]                                      0.65591E+00 
c  Velocity[Z]                                      0.11245E-29 
c  Pressure     0.85273E-07     426   0.97521E-08   0.87737E-01 0.23110E+03 
c  nu_tilda     0.46526E-05      32   0.82138E-05   0.18701E-06 0.13598E+03 
c  TempC        0.28000E+02      27   0.51851E-03   0.54747E+01 0.21484E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3208          10.062          4.5729          4.5729
v  Velocity[Y]            -3.5668          7.0354        0.018345        0.018345
v  Velocity[Z]       -1.0731e-014      6.603e-015    -1.4046e-017    -1.4046e-017
v  ǁVelocityǁ         0.0011678          10.065          5.1414          5.1414
v  Pressure                -52.85           21.63         -4.7649         -4.7649
v  nu_tilda           4.2613e-007       0.0042689      0.00092974      0.00092974
v  TempC                       21          73.079          21.585          21.585
v  TurbVisc           2.9026e-014       0.0050313       0.0010851       0.0010851
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              721:        0.33610E+01

===============================================================


 INSTANT    0.722000000E+03   TIME STEP NUMBER             722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81148E-03 0.87858E+00
   Friction velocity        uk    :  0.81148E-03 0.87858E+00
   Dimensionless distance   yplus :  0.65330E-02 0.70732E+01
   Friction thermal sca.    tstar : -0.75595E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48743E-02 0.52774E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66896E-02      32   0.35211E-03   0.17553E+01 0.83455E+02 
c  Velocity[X]                                      0.11051E+01 
c  Velocity[Y]                                      0.65019E+00 
c  Velocity[Z]                                      0.83606E-30 
c  Pressure     0.12075E-06     456   0.95993E-08   0.12588E+00 0.54118E+03 
c  nu_tilda     0.46544E-05      32   0.13893E-04   0.18688E-06 0.13588E+03 
c  TempC        0.28012E+02      27   0.38417E-03   0.88834E+01 0.27374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.324          10.063          4.5729          4.5729
v  Velocity[Y]            -3.5665          7.0106         0.01831         0.01831
v  Velocity[Z]       -1.1071e-014     6.6372e-015    -1.4036e-017    -1.4036e-017
v  ǁVelocityǁ         0.0011809          10.066          5.1419          5.1419
v  Pressure               -52.844          21.536         -4.7931         -4.7931
v  nu_tilda           4.2612e-007       0.0042689      0.00093034      0.00093034
v  TempC                       21          73.568          21.585          21.585
v  TurbVisc           2.9008e-014       0.0050313       0.0010858       0.0010858
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              722:        0.36300E+01

===============================================================


 INSTANT    0.723000000E+03   TIME STEP NUMBER             723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43419E-02 0.87717E+00
   Friction velocity        uk    :  0.43419E-02 0.87717E+00
   Dimensionless distance   yplus :  0.34955E-01 0.70618E+01
   Friction thermal sca.    tstar : -0.10107E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26081E-01 0.52689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66934E-02      32   0.46530E-03   0.17266E+01 0.83129E+02 
c  Velocity[X]                                      0.10864E+01 
c  Velocity[Y]                                      0.64024E+00 
c  Velocity[Z]                                      0.10560E-29 
c  Pressure     0.10030E-06     424   0.99129E-08   0.10266E+00 0.59995E+03 
c  nu_tilda     0.46561E-05      32   0.82269E-05   0.18676E-06 0.13578E+03 
c  TempC        0.28024E+02      27   0.44818E-03   0.57952E+01 0.23252E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3272          10.064          4.5729          4.5729
v  Velocity[Y]            -3.5661          7.0321        0.018275        0.018275
v  Velocity[Z]       -1.1237e-014     6.6842e-015    -1.4032e-017    -1.4032e-017
v  ǁVelocityǁ         0.0012006          10.067          5.1424          5.1424
v  Pressure               -52.864          21.635          -4.785          -4.785
v  nu_tilda            4.261e-007       0.0042689      0.00093096      0.00093096
v  TempC                       21          73.555          21.586          21.586
v  TurbVisc           2.9007e-014       0.0050313       0.0010865       0.0010865
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              723:        0.37370E+01

===============================================================


 INSTANT    0.724000000E+03   TIME STEP NUMBER             724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60364E-02 0.87822E+00
   Friction velocity        uk    :  0.60364E-02 0.87822E+00
   Dimensionless distance   yplus :  0.48597E-01 0.70702E+01
   Friction thermal sca.    tstar : -0.14445E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36259E-01 0.52752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66973E-02      32   0.41585E-03   0.17883E+01 0.83718E+02 
c  Velocity[X]                                      0.11281E+01 
c  Velocity[Y]                                      0.66023E+00 
c  Velocity[Z]                                      0.95669E-30 
c  Pressure     0.14533E-06     488   0.97917E-08   0.14841E+00 0.77231E+03 
c  nu_tilda     0.46578E-05      32   0.13886E-04   0.18664E-06 0.13568E+03 
c  TempC        0.28036E+02      27   0.42416E-03   0.60956E+01 0.22971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3303          10.065          4.5729          4.5729
v  Velocity[Y]            -3.5657          7.0047         0.01824         0.01824
v  Velocity[Z]       -1.0708e-014     6.7159e-015    -1.4021e-017    -1.4021e-017
v  ǁVelocityǁ         0.0011265          10.067           5.143           5.143
v  Pressure               -52.862          21.493         -4.8254         -4.8254
v  nu_tilda            4.261e-007       0.0042689      0.00093155      0.00093155
v  TempC                       21          73.696          21.586          21.586
v  TurbVisc              2.9e-014       0.0050313       0.0010873       0.0010873
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              724:        0.40280E+01

===============================================================


 INSTANT    0.725000000E+03   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11026E-02 0.87778E+00
   Friction velocity        uk    :  0.11026E-02 0.87778E+00
   Dimensionless distance   yplus :  0.88770E-02 0.70667E+01
   Friction thermal sca.    tstar : -0.19003E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66232E-02 0.52725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67012E-02      32   0.33264E-03   0.17551E+01 0.83418E+02 
c  Velocity[X]                                      0.11071E+01 
c  Velocity[Y]                                      0.64804E+00 
c  Velocity[Z]                                      0.11601E-29 
c  Pressure     0.99569E-07     441   0.97666E-08   0.10269E+00 0.81814E+03 
c  nu_tilda     0.46595E-05      32   0.81944E-05   0.18653E-06 0.13558E+03 
c  TempC        0.28048E+02      28   0.47170E-03   0.95580E+01 0.29502E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3338          10.066          4.5729          4.5729
v  Velocity[Y]            -3.5655           7.029        0.018204        0.018204
v  Velocity[Z]       -1.0885e-014     6.7512e-015    -1.4017e-017    -1.4017e-017
v  ǁVelocityǁ         0.0011254          10.068          5.1435          5.1435
v  Pressure               -52.887          21.647         -4.8079         -4.8079
v  nu_tilda           4.2604e-007       0.0042689      0.00093217      0.00093217
v  TempC                       21          73.079          21.587          21.587
v  TurbVisc           2.9001e-014       0.0050313        0.001088        0.001088
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              725:        0.37750E+01

===============================================================


 INSTANT    0.726000000E+03   TIME STEP NUMBER             726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44369E-02 0.87875E+00
   Friction velocity        uk    :  0.44369E-02 0.87875E+00
   Dimensionless distance   yplus :  0.35720E-01 0.70745E+01
   Friction thermal sca.    tstar : -0.11181E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26651E-01 0.52784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67051E-02      32   0.39095E-03   0.17080E+01 0.83010E+02 
c  Velocity[X]                                      0.10674E+01 
c  Velocity[Y]                                      0.64054E+00 
c  Velocity[Z]                                      0.11698E-29 
c  Pressure     0.83302E-07     425   0.97137E-08   0.85797E-01 0.34530E+03 
c  nu_tilda     0.46612E-05      31   0.13905E-04   0.18640E-06 0.13547E+03 
c  TempC        0.28060E+02      27   0.69644E-03   0.52900E+01 0.22239E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3374          10.067          4.5729          4.5729
v  Velocity[Y]            -3.5653          7.0371        0.018167        0.018167
v  Velocity[Z]       -1.0688e-014     6.7913e-015    -1.4005e-017    -1.4005e-017
v  ǁVelocityǁ         0.0011231          10.069          5.1441          5.1441
v  Pressure                -52.89          21.604          -4.829          -4.829
v  nu_tilda           4.2595e-007       0.0042689      0.00093277      0.00093277
v  TempC                       21          74.002          21.587          21.587
v  TurbVisc           2.8985e-014       0.0050314       0.0010887       0.0010887
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              726:        0.42640E+01

===============================================================


 INSTANT    0.727000000E+03   TIME STEP NUMBER             727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48247E-02 0.87833E+00
   Friction velocity        uk    :  0.48247E-02 0.87833E+00
   Dimensionless distance   yplus :  0.38842E-01 0.70711E+01
   Friction thermal sca.    tstar : -0.12090E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28980E-01 0.52758E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67089E-02      32   0.39270E-03   0.17489E+01 0.83380E+02 
c  Velocity[X]                                      0.10951E+01 
c  Velocity[Y]                                      0.65374E+00 
c  Velocity[Z]                                      0.95724E-30 
c  Pressure     0.11521E-06     458   0.93304E-08   0.11905E+00 0.43597E+03 
c  nu_tilda     0.46630E-05      31   0.82015E-05   0.18630E-06 0.13538E+03 
c  TempC        0.28072E+02      28   0.46725E-03   0.93670E+01 0.29114E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3409          10.068          4.5729          4.5729
v  Velocity[Y]            -3.5652          7.0068        0.018131        0.018131
v  Velocity[Z]       -1.1171e-014     6.8235e-015    -1.4005e-017    -1.4005e-017
v  ǁVelocityǁ         0.0010978           10.07          5.1446          5.1446
v  Pressure               -52.908          21.502         -4.8626         -4.8626
v  nu_tilda           4.2609e-007       0.0042689      0.00093339      0.00093339
v  TempC                       21          73.079          21.588          21.588
v  TurbVisc            2.896e-014       0.0050314       0.0010894       0.0010894
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              727:        0.36280E+01

===============================================================


 INSTANT    0.728000000E+03   TIME STEP NUMBER             728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23195E-02 0.87715E+00
   Friction velocity        uk    :  0.23195E-02 0.87715E+00
   Dimensionless distance   yplus :  0.18674E-01 0.70616E+01
   Friction thermal sca.    tstar : -0.21708E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13933E-01 0.52688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67128E-02      32   0.40836E-03   0.17400E+01 0.83404E+02 
c  Velocity[X]                                      0.10926E+01 
c  Velocity[Y]                                      0.64748E+00 
c  Velocity[Z]                                      0.96424E-30 
c  Pressure     0.89674E-07     421   0.99372E-08   0.92098E-01 0.34747E+03 
c  nu_tilda     0.46647E-05      31   0.13916E-04   0.18618E-06 0.13528E+03 
c  TempC        0.28084E+02      27   0.43946E-03   0.73020E+01 0.25549E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3444          10.069          4.5729          4.5729
v  Velocity[Y]            -3.5651          7.0243        0.018093        0.018093
v  Velocity[Z]       -1.1135e-014     6.8527e-015    -1.3996e-017    -1.3996e-017
v  ǁVelocityǁ         0.0011334          10.071          5.1451          5.1451
v  Pressure               -52.915          21.593          -4.856          -4.856
v  nu_tilda           4.2617e-007       0.0042689      0.00093399      0.00093399
v  TempC                       21           73.08          21.588          21.588
v  TurbVisc           2.8997e-014       0.0050314       0.0010902       0.0010902
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              728:        0.34000E+01

===============================================================


 INSTANT    0.729000000E+03   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56200E-02 0.87828E+00
   Friction velocity        uk    :  0.56200E-02 0.87828E+00
   Dimensionless distance   yplus :  0.45245E-01 0.70707E+01
   Friction thermal sca.    tstar : -0.89979E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33758E-01 0.52756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67166E-02      32   0.40783E-03   0.17659E+01 0.83588E+02 
c  Velocity[X]                                      0.11264E+01 
c  Velocity[Y]                                      0.63946E+00 
c  Velocity[Z]                                      0.95601E-30 
c  Pressure     0.13301E-06     457   0.99879E-08   0.13807E+00 0.35903E+03 
c  nu_tilda     0.46664E-05      31   0.81917E-05   0.18607E-06 0.13518E+03 
c  TempC        0.28096E+02      28   0.42613E-03   0.48622E+01 0.20306E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3478           10.07          4.5729          4.5729
v  Velocity[Y]             -3.565          7.0072        0.018056        0.018056
v  Velocity[Z]       -1.1559e-014     6.8915e-015    -1.3992e-017    -1.3992e-017
v  ǁVelocityǁ          0.001086          10.072          5.1457          5.1457
v  Pressure               -52.931          21.511         -4.8851         -4.8851
v  nu_tilda           4.2625e-007       0.0042689      0.00093461      0.00093461
v  TempC                       21          74.589          21.589          21.589
v  TurbVisc           2.9021e-014       0.0050314       0.0010909       0.0010909
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              729:        0.34520E+01

===============================================================


 INSTANT    0.730000000E+03   TIME STEP NUMBER             730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35779E-02 0.87758E+00
   Friction velocity        uk    :  0.35779E-02 0.87758E+00
   Dimensionless distance   yplus :  0.28805E-01 0.70651E+01
   Friction thermal sca.    tstar : -0.71793E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21491E-01 0.52714E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67205E-02      32   0.37275E-03   0.17407E+01 0.83287E+02 
c  Velocity[X]                                      0.10910E+01 
c  Velocity[Y]                                      0.64976E+00 
c  Velocity[Z]                                      0.11678E-29 
c  Pressure     0.12386E-06     441   0.94929E-08   0.12577E+00 0.48523E+03 
c  nu_tilda     0.46681E-05      31   0.13915E-04   0.18595E-06 0.13508E+03 
c  TempC        0.28108E+02      27   0.49880E-03   0.48436E+01 0.21257E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3514          10.071          4.5729          4.5729
v  Velocity[Y]            -3.5649          7.0279        0.018018        0.018018
v  Velocity[Z]       -1.0993e-014     6.9224e-015    -1.3983e-017    -1.3983e-017
v  ǁVelocityǁ          0.001098          10.073          5.1462          5.1462
v  Pressure               -52.928          21.625         -4.8681         -4.8681
v  nu_tilda            4.262e-007       0.0042689      0.00093521      0.00093521
v  TempC                       21           73.08          21.589          21.589
v  TurbVisc           2.9042e-014       0.0050314       0.0010916       0.0010916
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              730:        0.39650E+01

===============================================================


 INSTANT    0.731000000E+03   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52771E-02 0.87871E+00
   Friction velocity        uk    :  0.52771E-02 0.87871E+00
   Dimensionless distance   yplus :  0.42484E-01 0.70742E+01
   Friction thermal sca.    tstar : -0.56412E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31698E-01 0.52781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67244E-02      32   0.38849E-03   0.17124E+01 0.83030E+02 
c  Velocity[X]                                      0.10691E+01 
c  Velocity[Y]                                      0.64324E+00 
c  Velocity[Z]                                      0.10094E-29 
c  Pressure     0.11570E-06     470   0.90701E-08   0.11690E+00 0.34197E+03 
c  nu_tilda     0.46698E-05      31   0.81375E-05   0.18586E-06 0.13499E+03 
c  TempC        0.28120E+02      28   0.42583E-03   0.49202E+01 0.21647E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3549          10.073          4.5729          4.5729
v  Velocity[Y]            -3.5648          7.0271        0.017979        0.017979
v  Velocity[Z]       -1.0624e-014     6.9515e-015    -1.3971e-017    -1.3971e-017
v  ǁVelocityǁ         0.0010683          10.075          5.1467          5.1467
v  Pressure               -52.955          21.565         -4.9005         -4.9005
v  nu_tilda           4.2614e-007        0.004269      0.00093583      0.00093583
v  TempC                       21          74.381           21.59           21.59
v  TurbVisc           2.9028e-014       0.0050314       0.0010924       0.0010924
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              731:        0.36620E+01

===============================================================


 INSTANT    0.732000000E+03   TIME STEP NUMBER             732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22351E-02 0.87837E+00
   Friction velocity        uk    :  0.22351E-02 0.87837E+00
   Dimensionless distance   yplus :  0.17994E-01 0.70715E+01
   Friction thermal sca.    tstar : -0.53028E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13425E-01 0.52761E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67282E-02      32   0.38294E-03   0.17345E+01 0.83254E+02 
c  Velocity[X]                                      0.10914E+01 
c  Velocity[Y]                                      0.64302E+00 
c  Velocity[Z]                                      0.90385E-30 
c  Pressure     0.10076E-06     438   0.90175E-08   0.10544E+00 0.38204E+03 
c  nu_tilda     0.46715E-05      31   0.13943E-04   0.18575E-06 0.13489E+03 
c  TempC        0.28132E+02      27   0.64540E-03   0.57277E+01 0.21735E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3589          10.074          4.5729          4.5729
v  Velocity[Y]            -3.5647          7.0021        0.017939        0.017939
v  Velocity[Z]       -1.0692e-014     6.9902e-015    -1.3964e-017    -1.3964e-017
v  ǁVelocityǁ         0.0010779          10.076          5.1473          5.1473
v  Pressure               -52.955          21.504         -4.9214         -4.9214
v  nu_tilda            4.261e-007        0.004269      0.00093643      0.00093643
v  TempC                       21           73.31           21.59           21.59
v  TurbVisc           2.9012e-014       0.0050314       0.0010931       0.0010931
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              732:        0.34040E+01

===============================================================


 INSTANT    0.733000000E+03   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13425E-02 0.87715E+00
   Friction velocity        uk    :  0.13425E-02 0.87715E+00
   Dimensionless distance   yplus :  0.10808E-01 0.70616E+01
   Friction thermal sca.    tstar : -0.62132E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80641E-02 0.52688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67321E-02      32   0.42995E-03   0.17249E+01 0.83222E+02 
c  Velocity[X]                                      0.10667E+01 
c  Velocity[Y]                                      0.65824E+00 
c  Velocity[Z]                                      0.96793E-30 
c  Pressure     0.10384E-06     425   0.96263E-08   0.10629E+00 0.58195E+03 
c  nu_tilda     0.46732E-05      31   0.81514E-05   0.18565E-06 0.13480E+03 
c  TempC        0.28144E+02      27   0.43765E-03   0.10964E+02 0.32895E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3629          10.075          4.5729          4.5729
v  Velocity[Y]            -3.5647          7.0247          0.0179          0.0179
v  Velocity[Z]       -1.0626e-014     7.0205e-015    -1.3958e-017    -1.3958e-017
v  ǁVelocityǁ         0.0010714          10.077          5.1478          5.1478
v  Pressure               -52.976            21.6         -4.9135         -4.9135
v  nu_tilda           4.2612e-007        0.004269      0.00093706      0.00093706
v  TempC                       21          73.498          21.591          21.591
v  TurbVisc           2.9002e-014       0.0050314       0.0010938       0.0010938
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              733:        0.33720E+01

===============================================================


 INSTANT    0.734000000E+03   TIME STEP NUMBER             734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47377E-02 0.87829E+00
   Friction velocity        uk    :  0.47377E-02 0.87829E+00
   Dimensionless distance   yplus :  0.38142E-01 0.70708E+01
   Friction thermal sca.    tstar : -0.67076E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28458E-01 0.52756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67359E-02      32   0.40509E-03   0.17505E+01 0.83480E+02 
c  Velocity[X]                                      0.10939E+01 
c  Velocity[Y]                                      0.65656E+00 
c  Velocity[Z]                                      0.93729E-30 
c  Pressure     0.11200E-06     456   0.98955E-08   0.11531E+00 0.68364E+03 
c  nu_tilda     0.46749E-05      31   0.13933E-04   0.18554E-06 0.13471E+03 
c  TempC        0.28156E+02      27   0.51057E-03   0.59225E+01 0.23905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3667          10.076          4.5729          4.5729
v  Velocity[Y]            -3.5647          7.0052         0.01786         0.01786
v  Velocity[Z]       -1.0261e-014     7.0482e-015    -1.3953e-017    -1.3953e-017
v  ǁVelocityǁ         0.0010563          10.078          5.1483          5.1483
v  Pressure               -52.979          21.477         -4.9503         -4.9503
v  nu_tilda           4.2612e-007        0.004269      0.00093766      0.00093766
v  TempC                       21           73.08          21.591          21.591
v  TurbVisc           2.9007e-014       0.0050314       0.0010945       0.0010945
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              734:        0.34920E+01

===============================================================


 INSTANT    0.735000000E+03   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29311E-02 0.87760E+00
   Friction velocity        uk    :  0.29311E-02 0.87760E+00
   Dimensionless distance   yplus :  0.23597E-01 0.70653E+01
   Friction thermal sca.    tstar : -0.81315E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17606E-01 0.52715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67398E-02      32   0.38966E-03   0.17379E+01 0.83217E+02 
c  Velocity[X]                                      0.10948E+01 
c  Velocity[Y]                                      0.64308E+00 
c  Velocity[Z]                                      0.11093E-29 
c  Pressure     0.13553E-06     409   0.94160E-08   0.13610E+00 0.54315E+03 
c  nu_tilda     0.46766E-05      31   0.81186E-05   0.18544E-06 0.13461E+03 
c  TempC        0.28168E+02      27   0.40350E-03   0.66389E+01 0.25801E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3705          10.078          4.5729          4.5729
v  Velocity[Y]            -3.5648          7.0257         0.01782         0.01782
v  Velocity[Z]       -1.0279e-014     7.0864e-015    -1.3945e-017    -1.3945e-017
v  ǁVelocityǁ         0.0011445           10.08          5.1488          5.1488
v  Pressure               -53.002          21.569         -4.9456         -4.9456
v  nu_tilda           4.2615e-007        0.004269      0.00093828      0.00093828
v  TempC                       21          74.182          21.592          21.592
v  TurbVisc           2.9007e-014       0.0050314       0.0010953       0.0010953
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              735:        0.32960E+01

===============================================================


 INSTANT    0.736000000E+03   TIME STEP NUMBER             736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75274E-02 0.87894E+00
   Friction velocity        uk    :  0.75274E-02 0.87894E+00
   Dimensionless distance   yplus :  0.60600E-01 0.70761E+01
   Friction thermal sca.    tstar : -0.95236E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45215E-01 0.52795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67436E-02      32   0.36762E-03   0.17169E+01 0.83206E+02 
c  Velocity[X]                                      0.10565E+01 
c  Velocity[Y]                                      0.66038E+00 
c  Velocity[Z]                                      0.98678E-30 
c  Pressure     0.98065E-07     394   0.96750E-08   0.10069E+00 0.22210E+03 
c  nu_tilda     0.46783E-05      31   0.13955E-04   0.18534E-06 0.13452E+03 
c  TempC        0.28180E+02      27   0.37559E-03   0.65121E+01 0.24128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3744           10.08          4.5729          4.5729
v  Velocity[Y]            -3.5648          7.0302        0.017778        0.017778
v  Velocity[Z]       -1.0169e-014     7.1111e-015    -1.3935e-017    -1.3935e-017
v  ǁVelocityǁ         0.0011319          10.081          5.1494          5.1494
v  Pressure               -53.009          21.561         -4.9604         -4.9604
v  nu_tilda           4.2611e-007        0.004269      0.00093888      0.00093888
v  TempC                       21           73.08          21.592          21.592
v  TurbVisc           2.9015e-014       0.0050314        0.001096        0.001096
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              736:        0.32300E+01

===============================================================


 INSTANT    0.737000000E+03   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21466E-02 0.87849E+00
   Friction velocity        uk    :  0.21466E-02 0.87849E+00
   Dimensionless distance   yplus :  0.17282E-01 0.70724E+01
   Friction thermal sca.    tstar : -0.14813E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12894E-01 0.52768E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67475E-02      32   0.39095E-03   0.17129E+01 0.83109E+02 
c  Velocity[X]                                      0.10677E+01 
c  Velocity[Y]                                      0.64521E+00 
c  Velocity[Z]                                      0.90892E-30 
c  Pressure     0.10868E-06     442   0.92457E-08   0.11341E+00 0.35957E+03 
c  nu_tilda     0.46800E-05      31   0.81131E-05   0.18525E-06 0.13443E+03 
c  TempC        0.28192E+02      27   0.82529E-03   0.58947E+01 0.23688E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3784          10.081          4.5729          4.5729
v  Velocity[Y]            -3.5649          7.0071        0.017737        0.017737
v  Velocity[Z]       -1.0385e-014     7.1429e-015    -1.3932e-017    -1.3932e-017
v  ǁVelocityǁ         0.0011258          10.083          5.1499          5.1499
v  Pressure               -53.028          21.479         -4.9897         -4.9897
v  nu_tilda           4.2611e-007        0.004269       0.0009395       0.0009395
v  TempC                       21          73.499          21.593          21.593
v  TurbVisc           2.9003e-014       0.0050314       0.0010967       0.0010967
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              737:        0.34500E+01

===============================================================


 INSTANT    0.738000000E+03   TIME STEP NUMBER             738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71920E-02 0.87719E+00
   Friction velocity        uk    :  0.71920E-02 0.87719E+00
   Dimensionless distance   yplus :  0.57901E-01 0.70620E+01
   Friction thermal sca.    tstar : -0.26140E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43201E-01 0.52690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67513E-02      32   0.41375E-03   0.17194E+01 0.83207E+02 
c  Velocity[X]                                      0.10788E+01 
c  Velocity[Y]                                      0.64061E+00 
c  Velocity[Z]                                      0.11703E-29 
c  Pressure     0.10390E-06     309   0.96748E-08   0.10558E+00 0.17145E+03 
c  nu_tilda     0.46817E-05      31   0.13963E-04   0.18515E-06 0.13434E+03 
c  TempC        0.28205E+02      27   0.36435E-03   0.12328E+02 0.37952E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3826          10.083          4.5729          4.5729
v  Velocity[Y]            -3.5651           7.027        0.017695        0.017695
v  Velocity[Z]       -1.0233e-014     7.1771e-015    -1.3922e-017    -1.3922e-017
v  ǁVelocityǁ         0.0011169          10.085          5.1504          5.1504
v  Pressure               -53.036           21.52         -4.9942         -4.9942
v  nu_tilda           4.2609e-007        0.004269      0.00094011      0.00094011
v  TempC                       21          73.324          21.593          21.593
v  TurbVisc           2.9003e-014       0.0050314       0.0010974       0.0010974
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              738:        0.30380E+01

===============================================================


 INSTANT    0.739000000E+03   TIME STEP NUMBER             739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69956E-02 0.87838E+00
   Friction velocity        uk    :  0.69956E-02 0.87838E+00
   Dimensionless distance   yplus :  0.56319E-01 0.70715E+01
   Friction thermal sca.    tstar : -0.10924E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42020E-01 0.52762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67552E-02      32   0.37449E-03   0.17388E+01 0.83376E+02 
c  Velocity[X]                                      0.10775E+01 
c  Velocity[Y]                                      0.66125E+00 
c  Velocity[Z]                                      0.95535E-30 
c  Pressure     0.11280E-06     437   0.96689E-08   0.11573E+00 0.29879E+03 
c  nu_tilda     0.46834E-05      31   0.81088E-05   0.18505E-06 0.13425E+03 
c  TempC        0.28217E+02      27   0.42284E-03   0.66744E+01 0.23711E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3868          10.085          4.5729          4.5729
v  Velocity[Y]            -3.5652          7.0025        0.017653        0.017653
v  Velocity[Z]       -1.0224e-014      7.202e-015    -1.3918e-017    -1.3918e-017
v  ǁVelocityǁ         0.0010432          10.086          5.1509          5.1509
v  Pressure               -53.055          21.457         -5.0197         -5.0197
v  nu_tilda           4.2615e-007        0.004269      0.00094073      0.00094073
v  TempC                       21           73.38          21.594          21.594
v  TurbVisc           2.8998e-014       0.0050314       0.0010982       0.0010982
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              739:        0.36020E+01

===============================================================


 INSTANT    0.740000000E+03   TIME STEP NUMBER             740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27617E-02 0.87760E+00
   Friction velocity        uk    :  0.27617E-02 0.87760E+00
   Dimensionless distance   yplus :  0.22233E-01 0.70653E+01
   Friction thermal sca.    tstar : -0.82391E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16588E-01 0.52715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67590E-02      32   0.32744E-03   0.17078E+01 0.83029E+02 
c  Velocity[X]                                      0.10636E+01 
c  Velocity[Y]                                      0.64416E+00 
c  Velocity[Z]                                      0.98792E-30 
c  Pressure     0.11682E-06     425   0.92757E-08   0.11894E+00 0.41523E+03 
c  nu_tilda     0.46851E-05      31   0.13965E-04   0.18495E-06 0.13417E+03 
c  TempC        0.28229E+02      27   0.54365E-03   0.66307E+01 0.25096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3912          10.087          4.5729          4.5729
v  Velocity[Y]            -3.5653          7.0238         0.01761         0.01761
v  Velocity[Z]       -9.6985e-015     7.2284e-015    -1.3906e-017    -1.3906e-017
v  ǁVelocityǁ         0.0010642          10.088          5.1514          5.1514
v  Pressure               -53.054          21.554          -5.006          -5.006
v  nu_tilda           4.2609e-007        0.004269      0.00094133      0.00094133
v  TempC                       21          73.315          21.594          21.594
v  TurbVisc           2.9014e-014       0.0050314       0.0010989       0.0010989
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              740:        0.33660E+01

===============================================================


 INSTANT    0.741000000E+03   TIME STEP NUMBER             741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53205E-02 0.87884E+00
   Friction velocity        uk    :  0.53205E-02 0.87884E+00
   Dimensionless distance   yplus :  0.42834E-01 0.70752E+01
   Friction thermal sca.    tstar : -0.80945E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31959E-01 0.52789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67629E-02      32   0.38986E-03   0.16775E+01 0.82759E+02 
c  Velocity[X]                                      0.10392E+01 
c  Velocity[Y]                                      0.63831E+00 
c  Velocity[Z]                                      0.10202E-29 
c  Pressure     0.10210E-06     410   0.91570E-08   0.10581E+00 0.23595E+03 
c  nu_tilda     0.46868E-05      31   0.80557E-05   0.18487E-06 0.13408E+03 
c  TempC        0.28241E+02      28   0.44911E-03   0.66692E+01 0.26032E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3954          10.088          4.5729          4.5729
v  Velocity[Y]            -3.5654          7.0347        0.017567        0.017567
v  Velocity[Z]       -9.3127e-015     7.2518e-015    -1.3897e-017    -1.3897e-017
v  ǁVelocityǁ         0.0012369           10.09          5.1519          5.1519
v  Pressure               -53.084          21.564         -5.0231         -5.0231
v  nu_tilda           4.2597e-007        0.004269      0.00094196      0.00094196
v  TempC                       21          73.989          21.595          21.595
v  TurbVisc           2.8998e-014       0.0050314       0.0010996       0.0010996
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              741:        0.33200E+01

===============================================================


 INSTANT    0.742000000E+03   TIME STEP NUMBER             742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53629E-02 0.87813E+00
   Friction velocity        uk    :  0.53629E-02 0.87813E+00
   Dimensionless distance   yplus :  0.43175E-01 0.70696E+01
   Friction thermal sca.    tstar : -0.20862E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32213E-01 0.52747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67667E-02      32   0.41035E-03   0.17310E+01 0.83365E+02 
c  Velocity[X]                                      0.10711E+01 
c  Velocity[Y]                                      0.65984E+00 
c  Velocity[Z]                                      0.90651E-30 
c  Pressure     0.12597E-06     474   0.92427E-08   0.12956E+00 0.79345E+03 
c  nu_tilda     0.46885E-05      31   0.13989E-04   0.18478E-06 0.13399E+03 
c  TempC        0.28253E+02      27   0.40725E-03   0.73101E+01 0.25750E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3995           10.09          4.5729          4.5729
v  Velocity[Y]            -3.5655          7.0008        0.017523        0.017523
v  Velocity[Z]       -9.1359e-015     7.2813e-015    -1.3885e-017    -1.3885e-017
v  ǁVelocityǁ          0.001176          10.092          5.1524          5.1524
v  Pressure               -53.085          21.409         -5.0633         -5.0633
v  nu_tilda           4.2592e-007        0.004269      0.00094256      0.00094256
v  TempC                       21          73.081          21.595          21.595
v  TurbVisc           2.8964e-014       0.0050314       0.0011004       0.0011004
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              742:        0.35140E+01

===============================================================


 INSTANT    0.743000000E+03   TIME STEP NUMBER             743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83029E-02 0.87707E+00
   Friction velocity        uk    :  0.83029E-02 0.87707E+00
   Dimensionless distance   yplus :  0.66844E-01 0.70611E+01
   Friction thermal sca.    tstar : -0.10422E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49873E-01 0.52683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67705E-02      32   0.39532E-03   0.17499E+01 0.83634E+02 
c  Velocity[X]                                      0.10915E+01 
c  Velocity[Y]                                      0.65833E+00 
c  Velocity[Z]                                      0.10462E-29 
c  Pressure     0.12773E-06     426   0.93490E-08   0.13153E+00 0.65585E+03 
c  nu_tilda     0.46902E-05      31   0.80704E-05   0.18469E-06 0.13391E+03 
c  TempC        0.28265E+02      27   0.96630E-03   0.52191E+01 0.22103E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4038          10.092          4.5729          4.5729
v  Velocity[Y]            -3.5656          7.0229        0.017479        0.017479
v  Velocity[Z]        -9.059e-015     7.3093e-015    -1.3877e-017    -1.3877e-017
v  ǁVelocityǁ         0.0010325          10.093           5.153           5.153
v  Pressure               -53.108          21.526         -5.0522         -5.0522
v  nu_tilda           4.2594e-007        0.004269      0.00094319      0.00094319
v  TempC                       21          73.644          21.596          21.596
v  TurbVisc           2.8951e-014       0.0050314       0.0011011       0.0011011
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              743:        0.33960E+01

===============================================================


 INSTANT    0.744000000E+03   TIME STEP NUMBER             744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17197E-02 0.87831E+00
   Friction velocity        uk    :  0.17197E-02 0.87831E+00
   Dimensionless distance   yplus :  0.13845E-01 0.70710E+01
   Friction thermal sca.    tstar : -0.66640E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10330E-01 0.52757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67744E-02      32   0.38307E-03   0.17067E+01 0.83118E+02 
c  Velocity[X]                                      0.10653E+01 
c  Velocity[Y]                                      0.64139E+00 
c  Velocity[Z]                                      0.10336E-29 
c  Pressure     0.11958E-06     440   0.94718E-08   0.12343E+00 0.55709E+03 
c  nu_tilda     0.46919E-05      31   0.13981E-04   0.18460E-06 0.13382E+03 
c  TempC        0.28277E+02      28   0.47922E-03   0.15475E+02 0.37058E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.408          10.094          4.5729          4.5729
v  Velocity[Y]            -3.5657          7.0018        0.017435        0.017435
v  Velocity[Z]        -8.759e-015     7.3342e-015    -1.3866e-017    -1.3866e-017
v  ǁVelocityǁ         0.0010465          10.095          5.1535          5.1535
v  Pressure               -53.114          21.433         -5.0833         -5.0833
v  nu_tilda           4.2591e-007        0.004269      0.00094379      0.00094379
v  TempC                       21          73.082          21.596          21.596
v  TurbVisc           2.8956e-014       0.0050314       0.0011018       0.0011018
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              744:        0.34130E+01

===============================================================


 INSTANT    0.745000000E+03   TIME STEP NUMBER             745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49870E-02 0.87757E+00
   Friction velocity        uk    :  0.49870E-02 0.87757E+00
   Dimensionless distance   yplus :  0.40149E-01 0.70650E+01
   Friction thermal sca.    tstar : -0.53684E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29955E-01 0.52713E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67782E-02      32   0.40279E-03   0.16994E+01 0.83048E+02 
c  Velocity[X]                                      0.10501E+01 
c  Velocity[Y]                                      0.64926E+00 
c  Velocity[Z]                                      0.10719E-29 
c  Pressure     0.10169E-06     425   0.92238E-08   0.10476E+00 0.57973E+03 
c  nu_tilda     0.46936E-05      31   0.80363E-05   0.18452E-06 0.13374E+03 
c  TempC        0.28289E+02      27   0.53898E-03   0.83419E+01 0.26496E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4126          10.096          4.5729          4.5729
v  Velocity[Y]            -3.5658          7.0275         0.01739         0.01739
v  Velocity[Z]       -8.6641e-015     7.3589e-015    -1.3859e-017    -1.3859e-017
v  ǁVelocityǁ         0.0012132          10.097           5.154           5.154
v  Pressure               -53.139          21.534         -5.0763         -5.0763
v  nu_tilda           4.2586e-007        0.004269      0.00094442      0.00094442
v  TempC                       21          73.362          21.597          21.597
v  TurbVisc           2.8951e-014       0.0050315       0.0011026       0.0011026
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              745:        0.36850E+01

===============================================================


 INSTANT    0.746000000E+03   TIME STEP NUMBER             746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89841E-02 0.87870E+00
   Friction velocity        uk    :  0.89841E-02 0.87870E+00
   Dimensionless distance   yplus :  0.72328E-01 0.70741E+01
   Friction thermal sca.    tstar : -0.54829E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53965E-01 0.52781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67821E-02      32   0.40396E-03   0.17165E+01 0.83235E+02 
c  Velocity[X]                                      0.10748E+01 
c  Velocity[Y]                                      0.64170E+00 
c  Velocity[Z]                                      0.95769E-30 
c  Pressure     0.12026E-06     425   0.98975E-08   0.12188E+00 0.37686E+03 
c  nu_tilda     0.46953E-05      31   0.13996E-04   0.18443E-06 0.13366E+03 
c  TempC        0.28301E+02      27   0.47005E-03   0.79444E+01 0.27861E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4169          10.098          4.5729          4.5729
v  Velocity[Y]             -3.566          7.0252        0.017345        0.017345
v  Velocity[Z]       -8.5717e-015      7.381e-015    -1.3846e-017    -1.3846e-017
v  ǁVelocityǁ         0.0011115          10.099          5.1545          5.1545
v  Pressure               -53.148          21.483         -5.0993         -5.0993
v  nu_tilda           4.2576e-007        0.004269      0.00094502      0.00094502
v  TempC                       21          73.262          21.597          21.597
v  TurbVisc           2.8936e-014       0.0050315       0.0011033       0.0011033
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              746:        0.33910E+01

===============================================================


 INSTANT    0.747000000E+03   TIME STEP NUMBER             747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73228E-02 0.87835E+00
   Friction velocity        uk    :  0.73228E-02 0.87835E+00
   Dimensionless distance   yplus :  0.58953E-01 0.70714E+01
   Friction thermal sca.    tstar : -0.63690E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43986E-01 0.52760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67859E-02      32   0.38838E-03   0.17351E+01 0.83422E+02 
c  Velocity[X]                                      0.10979E+01 
c  Velocity[Y]                                      0.63720E+00 
c  Velocity[Z]                                      0.90500E-30 
c  Pressure     0.11783E-06     426   0.93699E-08   0.12270E+00 0.33320E+03 
c  nu_tilda     0.46970E-05      31   0.80247E-05   0.18435E-06 0.13357E+03 
c  TempC        0.28313E+02      27   0.45541E-03   0.63429E+01 0.24785E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4213            10.1          4.5729          4.5729
v  Velocity[Y]             -3.566          7.0022        0.017299        0.017299
v  Velocity[Z]       -8.6353e-015     7.4025e-015    -1.3836e-017    -1.3836e-017
v  ǁVelocityǁ         0.0010528          10.101           5.155           5.155
v  Pressure               -53.168          21.409         -5.1273         -5.1273
v  nu_tilda           4.2573e-007        0.004269      0.00094565      0.00094565
v  TempC                       21          73.213          21.598          21.598
v  TurbVisc           2.8909e-014       0.0050315        0.001104        0.001104
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              747:        0.33220E+01

===============================================================


 INSTANT    0.748000000E+03   TIME STEP NUMBER             748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52132E-02 0.87731E+00
   Friction velocity        uk    :  0.52132E-02 0.87731E+00
   Dimensionless distance   yplus :  0.41970E-01 0.70630E+01
   Friction thermal sca.    tstar : -0.68921E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31314E-01 0.52698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67897E-02      32   0.36010E-03   0.16979E+01 0.83065E+02 
c  Velocity[X]                                      0.10505E+01 
c  Velocity[Y]                                      0.64734E+00 
c  Velocity[Z]                                      0.10945E-29 
c  Pressure     0.10980E-06     420   0.96340E-08   0.11179E+00 0.43225E+03 
c  nu_tilda     0.46987E-05      31   0.14013E-04   0.18427E-06 0.13349E+03 
c  TempC        0.28325E+02      27   0.48431E-03   0.67738E+01 0.24013E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4258          10.102          4.5729          4.5729
v  Velocity[Y]            -3.5661          7.0217        0.017253        0.017253
v  Velocity[Z]        -8.415e-015     7.4276e-015    -1.3824e-017    -1.3824e-017
v  ǁVelocityǁ         0.0011956          10.103          5.1555          5.1555
v  Pressure                -53.17          21.511         -5.1131         -5.1131
v  nu_tilda           4.2567e-007        0.004269      0.00094625      0.00094625
v  TempC                       21          73.082          21.598          21.598
v  TurbVisc           2.8901e-014       0.0050315       0.0011048       0.0011048
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              748:        0.33220E+01

===============================================================


 INSTANT    0.749000000E+03   TIME STEP NUMBER             749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86617E-02 0.87844E+00
   Friction velocity        uk    :  0.86617E-02 0.87844E+00
   Dimensionless distance   yplus :  0.69733E-01 0.70720E+01
   Friction thermal sca.    tstar : -0.77377E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52029E-01 0.52765E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67935E-02      32   0.36214E-03   0.16912E+01 0.83000E+02 
c  Velocity[X]                                      0.10449E+01 
c  Velocity[Y]                                      0.64627E+00 
c  Velocity[Z]                                      0.11894E-29 
c  Pressure     0.10996E-06     458   0.98142E-08   0.11519E+00 0.52523E+03 
c  nu_tilda     0.47004E-05      31   0.80003E-05   0.18419E-06 0.13341E+03 
c  TempC        0.28337E+02      27   0.35021E-03   0.64698E+01 0.23355E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4301          10.104          4.5729          4.5729
v  Velocity[Y]            -3.5661          7.0061        0.017207        0.017207
v  Velocity[Z]       -8.3131e-015     7.4475e-015    -1.3814e-017    -1.3814e-017
v  ǁVelocityǁ         0.0010918          10.105           5.156           5.156
v  Pressure               -53.198          21.404         -5.1549         -5.1549
v  nu_tilda           4.2569e-007        0.004269      0.00094688      0.00094688
v  TempC                       21          73.256          21.599          21.599
v  TurbVisc           2.8885e-014       0.0050315       0.0011055       0.0011055
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              749:        0.34630E+01

===============================================================


 INSTANT    0.750000000E+03   TIME STEP NUMBER             750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66930E-02 0.87756E+00
   Friction velocity        uk    :  0.66930E-02 0.87756E+00
   Dimensionless distance   yplus :  0.53883E-01 0.70650E+01
   Friction thermal sca.    tstar : -0.98686E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40203E-01 0.52713E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        750, Physical time    0.75000E+03


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.52900E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67974E-02      32   0.42466E-03   0.17053E+01 0.83079E+02 
c  Velocity[X]                                      0.10669E+01 
c  Velocity[Y]                                      0.63844E+00 
c  Velocity[Z]                                      0.12712E-29 
c  Pressure     0.12168E-06     362   0.99463E-08   0.12290E+00 0.23502E+03 
c  nu_tilda     0.47021E-05      31   0.14009E-04   0.18411E-06 0.13333E+03 
c  TempC        0.28349E+02      27   0.40596E-03   0.53643E+01 0.21664E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4343          10.106          4.5729          4.5729
v  Velocity[Y]            -3.5662          7.0227        0.017159        0.017159
v  Velocity[Z]       -8.1946e-015     7.4694e-015      -1.38e-017      -1.38e-017
v  ǁVelocityǁ         0.0010313          10.107          5.1565          5.1565
v  Pressure               -53.208          21.462         -5.1529         -5.1529
v  nu_tilda           4.2567e-007        0.004269      0.00094749      0.00094749
v  TempC                       21          73.082            21.6            21.6
v  TurbVisc           2.8891e-014       0.0050315       0.0011062       0.0011062
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              750:        0.36260E+01

===============================================================


 INSTANT    0.751000000E+03   TIME STEP NUMBER             751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13241E-02 0.87882E+00
   Friction velocity        uk    :  0.13241E-02 0.87882E+00
   Dimensionless distance   yplus :  0.10660E-01 0.70751E+01
   Friction thermal sca.    tstar : -0.13420E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79533E-02 0.52788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68012E-02      32   0.41046E-03   0.17195E+01 0.83372E+02 
c  Velocity[X]                                      0.10676E+01 
c  Velocity[Y]                                      0.65187E+00 
c  Velocity[Z]                                      0.10238E-29 
c  Pressure     0.11938E-06     313   0.99875E-08   0.12311E+00 0.32011E+03 
c  nu_tilda     0.47037E-05      31   0.79994E-05   0.18403E-06 0.13325E+03 
c  TempC        0.28361E+02      27   0.66300E-03   0.49419E+01 0.21646E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4387          10.108          4.5729          4.5729
v  Velocity[Y]            -3.5663          7.0303        0.017112        0.017112
v  Velocity[Z]       -8.0754e-015     7.4922e-015    -1.3791e-017    -1.3791e-017
v  ǁVelocityǁ         0.0012992          10.109           5.157           5.157
v  Pressure               -53.231          21.492         -5.1577         -5.1577
v  nu_tilda           4.2561e-007        0.004269      0.00094812      0.00094812
v  TempC                       21           73.94            21.6            21.6
v  TurbVisc           2.8883e-014       0.0050315        0.001107        0.001107
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              751:        0.29320E+01

===============================================================


 INSTANT    0.752000000E+03   TIME STEP NUMBER             752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10025E-01 0.87846E+00
   Friction velocity        uk    :  0.10025E-01 0.87846E+00
   Dimensionless distance   yplus :  0.80706E-01 0.70722E+01
   Friction thermal sca.    tstar : -0.35099E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60216E-01 0.52766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68050E-02      32   0.32873E-03   0.17143E+01 0.83376E+02 
c  Velocity[X]                                      0.10684E+01 
c  Velocity[Y]                                      0.64592E+00 
c  Velocity[Z]                                      0.90024E-30 
c  Pressure     0.11096E-06     457   0.96676E-08   0.11482E+00 0.76086E+03 
c  nu_tilda     0.47054E-05      31   0.14031E-04   0.18396E-06 0.13317E+03 
c  TempC        0.28373E+02      27   0.42684E-03   0.83546E+01 0.28354E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4432          10.111          4.5729          4.5729
v  Velocity[Y]            -3.5664          7.0032        0.017065        0.017065
v  Velocity[Z]       -8.0153e-015      7.512e-015    -1.3778e-017    -1.3778e-017
v  ǁVelocityǁ         0.0011315          10.111          5.1574          5.1574
v  Pressure               -53.241           21.36         -5.2006         -5.2006
v  nu_tilda           4.2562e-007        0.004269      0.00094872      0.00094872
v  TempC                       21          73.082            21.6            21.6
v  TurbVisc           2.8867e-014       0.0050315       0.0011077       0.0011077
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              752:        0.35290E+01

===============================================================


 INSTANT    0.753000000E+03   TIME STEP NUMBER             753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58580E-02 0.87719E+00
   Friction velocity        uk    :  0.58580E-02 0.87719E+00
   Dimensionless distance   yplus :  0.47161E-01 0.70620E+01
   Friction thermal sca.    tstar : -0.13347E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35187E-01 0.52690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68088E-02      32   0.38767E-03   0.16687E+01 0.82862E+02 
c  Velocity[X]                                      0.10298E+01 
c  Velocity[Y]                                      0.63889E+00 
c  Velocity[Z]                                      0.10059E-29 
c  Pressure     0.10298E-06     409   0.94351E-08   0.10531E+00 0.56641E+03 
c  nu_tilda     0.47071E-05      31   0.79927E-05   0.18388E-06 0.13309E+03 
c  TempC        0.28385E+02      27   0.46521E-03   0.48853E+01 0.20565E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4476          10.113          4.5729          4.5729
v  Velocity[Y]            -3.5665          7.0267        0.017017        0.017017
v  Velocity[Z]       -8.0527e-015     7.5316e-015    -1.3765e-017    -1.3765e-017
v  ǁVelocityǁ         0.0010579          10.114          5.1579          5.1579
v  Pressure               -53.269          21.463         -5.1946         -5.1946
v  nu_tilda           4.2563e-007        0.004269      0.00094935      0.00094935
v  TempC                       21          73.628          21.601          21.601
v  TurbVisc            2.887e-014       0.0050315       0.0011084       0.0011084
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              753:        0.33560E+01

===============================================================


 INSTANT    0.754000000E+03   TIME STEP NUMBER             754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52314E-02 0.87823E+00
   Friction velocity        uk    :  0.52314E-02 0.87823E+00
   Dimensionless distance   yplus :  0.42116E-01 0.70703E+01
   Friction thermal sca.    tstar : -0.23003E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31423E-01 0.52753E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68127E-02      32   0.39182E-03   0.16891E+01 0.83040E+02 
c  Velocity[X]                                      0.10408E+01 
c  Velocity[Y]                                      0.64834E+00 
c  Velocity[Z]                                      0.90587E-30 
c  Pressure     0.12018E-06     453   0.98504E-08   0.12470E+00 0.56776E+03 
c  nu_tilda     0.47088E-05      31   0.14035E-04   0.18380E-06 0.13302E+03 
c  TempC        0.28397E+02      28   0.36680E-03   0.48398E+01 0.19930E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.452          10.115          4.5729          4.5729
v  Velocity[Y]            -3.5665          6.9992        0.016967        0.016967
v  Velocity[Z]       -7.9403e-015     7.5528e-015    -1.3754e-017    -1.3754e-017
v  ǁVelocityǁ         0.0012993          10.116          5.1584          5.1584
v  Pressure                -53.27          21.353         -5.2224         -5.2224
v  nu_tilda            4.256e-007       0.0042691      0.00094996      0.00094996
v  TempC                       21          73.083          21.601          21.601
v  TurbVisc           2.8872e-014       0.0050315       0.0011092       0.0011092
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              754:        0.35120E+01

===============================================================


 INSTANT    0.755000000E+03   TIME STEP NUMBER             755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41658E-02 0.87748E+00
   Friction velocity        uk    :  0.41658E-02 0.87748E+00
   Dimensionless distance   yplus :  0.33537E-01 0.70643E+01
   Friction thermal sca.    tstar : -0.80832E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25023E-01 0.52708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68165E-02      32   0.38689E-03   0.16725E+01 0.82925E+02 
c  Velocity[X]                                      0.10283E+01 
c  Velocity[Y]                                      0.64423E+00 
c  Velocity[Z]                                      0.11770E-29 
c  Pressure     0.79041E-07     389   0.96544E-08   0.80858E-01 0.51311E+03 
c  nu_tilda     0.47105E-05      31   0.79812E-05   0.18373E-06 0.13294E+03 
c  TempC        0.28409E+02      27   0.50884E-03   0.52305E+01 0.21480E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4564          10.117          4.5729          4.5729
v  Velocity[Y]            -3.5665          7.0238        0.016919        0.016919
v  Velocity[Z]       -7.8237e-015     7.5717e-015    -1.3746e-017    -1.3746e-017
v  ǁVelocityǁ         0.0010208          10.118          5.1589          5.1589
v  Pressure               -53.299          21.447         -5.2201         -5.2201
v  nu_tilda           4.2557e-007       0.0042691      0.00095059      0.00095059
v  TempC                       21          73.345          21.602          21.602
v  TurbVisc           2.8865e-014       0.0050315       0.0011099       0.0011099
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              755:        0.32920E+01

===============================================================


 INSTANT    0.756000000E+03   TIME STEP NUMBER             756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34874E-02 0.87875E+00
   Friction velocity        uk    :  0.34874E-02 0.87875E+00
   Dimensionless distance   yplus :  0.28076E-01 0.70746E+01
   Friction thermal sca.    tstar : -0.67608E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20948E-01 0.52784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68203E-02      32   0.40785E-03   0.16810E+01 0.83041E+02 
c  Velocity[X]                                      0.10433E+01 
c  Velocity[Y]                                      0.63763E+00 
c  Velocity[Z]                                      0.11056E-29 
c  Pressure     0.11873E-06     362   0.96421E-08   0.12184E+00 0.16776E+03 
c  nu_tilda     0.47121E-05      31   0.14034E-04   0.18365E-06 0.13286E+03 
c  TempC        0.28421E+02      27   0.47037E-03   0.67541E+01 0.25186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4607           10.12          4.5729          4.5729
v  Velocity[Y]            -3.5665          7.0324        0.016869        0.016869
v  Velocity[Z]       -7.5682e-015     7.5906e-015    -1.3728e-017    -1.3728e-017
v  ǁVelocityǁ         0.0011074           10.12          5.1594          5.1594
v  Pressure               -53.306          21.448         -5.2287         -5.2287
v  nu_tilda           4.2549e-007       0.0042691      0.00095119      0.00095119
v  TempC                       21          73.083          21.602          21.602
v  TurbVisc           2.8857e-014       0.0050315       0.0011106       0.0011106
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              756:        0.31400E+01

===============================================================


 INSTANT    0.757000000E+03   TIME STEP NUMBER             757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12536E-02 0.87831E+00
   Friction velocity        uk    :  0.12536E-02 0.87831E+00
   Dimensionless distance   yplus :  0.10092E-01 0.70710E+01
   Friction thermal sca.    tstar : -0.59877E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75298E-02 0.52758E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68241E-02      32   0.35948E-03   0.17181E+01 0.83379E+02 
c  Velocity[X]                                      0.10639E+01 
c  Velocity[Y]                                      0.65420E+00 
c  Velocity[Z]                                      0.84162E-30 
c  Pressure     0.14411E-06     457   0.93588E-08   0.14839E+00 0.46590E+03 
c  nu_tilda     0.47138E-05      31   0.79414E-05   0.18359E-06 0.13279E+03 
c  TempC        0.28433E+02      27   0.45252E-03   0.65952E+01 0.23814E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4652          10.122          4.5729          4.5729
v  Velocity[Y]            -3.5665           7.001         0.01682         0.01682
v  Velocity[Z]       -7.2939e-015     7.6098e-015    -1.3713e-017    -1.3713e-017
v  ǁVelocityǁ          0.001105          10.123          5.1599          5.1599
v  Pressure                -53.32          21.338         -5.2617         -5.2617
v  nu_tilda           4.2549e-007       0.0042691      0.00095183      0.00095183
v  TempC                       21          73.482          21.603          21.603
v  TurbVisc           2.8835e-014       0.0050315       0.0011114       0.0011114
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              757:        0.34900E+01

===============================================================


 INSTANT    0.758000000E+03   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74283E-02 0.87719E+00
   Friction velocity        uk    :  0.74283E-02 0.87719E+00
   Dimensionless distance   yplus :  0.59803E-01 0.70620E+01
   Friction thermal sca.    tstar : -0.57685E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44620E-01 0.52690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68279E-02      32   0.36457E-03   0.16753E+01 0.82984E+02 
c  Velocity[X]                                      0.10321E+01 
c  Velocity[Y]                                      0.64323E+00 
c  Velocity[Z]                                      0.10431E-29 
c  Pressure     0.88776E-07     394   0.91991E-08   0.92162E-01 0.35468E+03 
c  nu_tilda     0.47155E-05      31   0.14071E-04   0.18352E-06 0.13271E+03 
c  TempC        0.28445E+02      27   0.37106E-03   0.64902E+01 0.23778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4694          10.124          4.5729          4.5729
v  Velocity[Y]            -3.5664          7.0202        0.016769        0.016769
v  Velocity[Z]       -7.1018e-015     7.6287e-015    -1.3696e-017    -1.3696e-017
v  ǁVelocityǁ         0.0010173          10.125          5.1604          5.1604
v  Pressure               -53.342          21.434         -5.2566         -5.2566
v  nu_tilda           4.2556e-007       0.0042691      0.00095243      0.00095243
v  TempC                       21          73.083          21.603          21.603
v  TurbVisc           2.8836e-014       0.0050315       0.0011121       0.0011121
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              758:        0.32570E+01

===============================================================


 INSTANT    0.759000000E+03   TIME STEP NUMBER             759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35729E-02 0.87822E+00
   Friction velocity        uk    :  0.35729E-02 0.87822E+00
   Dimensionless distance   yplus :  0.28764E-01 0.70702E+01
   Friction thermal sca.    tstar : -0.51828E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21461E-01 0.52752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68317E-02      32   0.42083E-03   0.16689E+01 0.82963E+02 
c  Velocity[X]                                      0.10290E+01 
c  Velocity[Y]                                      0.63988E+00 
c  Velocity[Z]                                      0.10357E-29 
c  Pressure     0.90928E-07     457   0.92387E-08   0.94940E-01 0.45657E+03 
c  nu_tilda     0.47172E-05      31   0.79407E-05   0.18345E-06 0.13264E+03 
c  TempC        0.28457E+02      27   0.43557E-03   0.47249E+01 0.20678E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4739          10.127          4.5729          4.5729
v  Velocity[Y]            -3.5664          7.0032        0.016719        0.016719
v  Velocity[Z]       -6.9894e-015     7.6457e-015    -1.3687e-017    -1.3687e-017
v  ǁVelocityǁ         0.0013026          10.127          5.1608          5.1608
v  Pressure               -53.364          21.332         -5.2919         -5.2919
v  nu_tilda           4.2569e-007       0.0042691      0.00095306      0.00095306
v  TempC                       21           73.34          21.604          21.604
v  TurbVisc           2.8855e-014       0.0050315       0.0011129       0.0011129
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              759:        0.35860E+01

===============================================================


 INSTANT    0.760000000E+03   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53619E-02 0.87747E+00
   Friction velocity        uk    :  0.53619E-02 0.87747E+00
   Dimensionless distance   yplus :  0.43167E-01 0.70643E+01
   Friction thermal sca.    tstar : -0.49355E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32207E-01 0.52707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68356E-02      32   0.41361E-03   0.17203E+01 0.83532E+02 
c  Velocity[X]                                      0.10635E+01 
c  Velocity[Y]                                      0.65683E+00 
c  Velocity[Z]                                      0.11596E-29 
c  Pressure     0.12847E-06     409   0.94926E-08   0.13176E+00 0.37465E+03 
c  nu_tilda     0.47189E-05      31   0.14057E-04   0.18337E-06 0.13257E+03 
c  TempC        0.28469E+02      27   0.50622E-03   0.58228E+01 0.23679E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4785          10.129          4.5729          4.5729
v  Velocity[Y]            -3.5664          7.0246        0.016667        0.016667
v  Velocity[Z]       -6.9287e-015     7.6659e-015    -1.3673e-017    -1.3673e-017
v  ǁVelocityǁ         0.0010288          10.129          5.1613          5.1613
v  Pressure               -53.373          21.426         -5.2818         -5.2818
v  nu_tilda            4.257e-007       0.0042691      0.00095367      0.00095367
v  TempC                       21          73.894          21.604          21.604
v  TurbVisc           2.8889e-014       0.0050315       0.0011136       0.0011136
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              760:        0.33210E+01

===============================================================


 INSTANT    0.761000000E+03   TIME STEP NUMBER             761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45051E-02 0.87861E+00
   Friction velocity        uk    :  0.45051E-02 0.87861E+00
   Dimensionless distance   yplus :  0.36269E-01 0.70734E+01
   Friction thermal sca.    tstar : -0.55304E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27061E-01 0.52776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68394E-02      32   0.34886E-03   0.17140E+01 0.83438E+02 
c  Velocity[X]                                      0.10661E+01 
c  Velocity[Y]                                      0.64787E+00 
c  Velocity[Z]                                      0.12162E-29 
c  Pressure     0.12421E-06     441   0.91819E-08   0.12539E+00 0.24664E+03 
c  nu_tilda     0.47205E-05      31   0.79300E-05   0.18331E-06 0.13249E+03 
c  TempC        0.28481E+02      28   0.48310E-03   0.59140E+01 0.23664E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4829          10.131          4.5729          4.5729
v  Velocity[Y]            -3.5663           7.024        0.016616        0.016616
v  Velocity[Z]       -6.9287e-015     7.6819e-015    -1.3658e-017    -1.3658e-017
v  ǁVelocityǁ         0.0012904          10.132          5.1618          5.1618
v  Pressure               -53.401          21.388         -5.3055         -5.3055
v  nu_tilda           4.2564e-007       0.0042691       0.0009543       0.0009543
v  TempC                       21          73.267          21.605          21.605
v  TurbVisc           2.8893e-014       0.0050315       0.0011143       0.0011143
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              761:        0.34360E+01

===============================================================


 INSTANT    0.762000000E+03   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17276E-02 0.87827E+00
   Friction velocity        uk    :  0.17276E-02 0.87827E+00
   Dimensionless distance   yplus :  0.13908E-01 0.70707E+01
   Friction thermal sca.    tstar : -0.57602E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10377E-01 0.52755E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68432E-02      32   0.36366E-03   0.16847E+01 0.83133E+02 
c  Velocity[X]                                      0.10409E+01 
c  Velocity[Y]                                      0.64387E+00 
c  Velocity[Z]                                      0.98673E-30 
c  Pressure     0.10495E-06     425   0.93518E-08   0.10940E+00 0.41038E+03 
c  nu_tilda     0.47222E-05      31   0.14071E-04   0.18325E-06 0.13242E+03 
c  TempC        0.28493E+02      27   0.59079E-03   0.51415E+01 0.20845E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4872          10.134          4.5729          4.5729
v  Velocity[Y]            -3.5661          6.9985        0.016564        0.016564
v  Velocity[Z]       -6.9287e-015     7.6991e-015    -1.3645e-017    -1.3645e-017
v  ǁVelocityǁ         0.0011048          10.134          5.1623          5.1623
v  Pressure               -53.408           21.32          -5.328          -5.328
v  nu_tilda           4.2565e-007       0.0042691      0.00095491      0.00095491
v  TempC                       21          73.166          21.605          21.605
v  TurbVisc           2.8875e-014       0.0050315       0.0011151       0.0011151
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              762:        0.33550E+01

===============================================================


 INSTANT    0.763000000E+03   TIME STEP NUMBER             763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65641E-02 0.87711E+00
   Friction velocity        uk    :  0.65641E-02 0.87711E+00
   Dimensionless distance   yplus :  0.52845E-01 0.70614E+01
   Friction thermal sca.    tstar : -0.84557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39428E-01 0.52686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68470E-02      32   0.38848E-03   0.16770E+01 0.83205E+02 
c  Velocity[X]                                      0.10168E+01 
c  Velocity[Y]                                      0.66017E+00 
c  Velocity[Z]                                      0.10346E-29 
c  Pressure     0.96349E-07     346   0.95032E-08   0.98919E-01 0.40198E+03 
c  nu_tilda     0.47239E-05      31   0.79080E-05   0.18319E-06 0.13235E+03 
c  TempC        0.28505E+02      28   0.39323E-03   0.66100E+01 0.24008E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4915          10.136          4.5729          4.5729
v  Velocity[Y]            -3.5659          7.0207        0.016512        0.016512
v  Velocity[Z]       -6.9287e-015     7.7162e-015    -1.3628e-017    -1.3628e-017
v  ǁVelocityǁ         0.0011635          10.137          5.1627          5.1627
v  Pressure               -53.438          21.391         -5.3319         -5.3319
v  nu_tilda           4.2567e-007       0.0042691      0.00095554      0.00095554
v  TempC                       21          74.269          21.606          21.606
v  TurbVisc           2.8879e-014       0.0050315       0.0011158       0.0011158
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              763:        0.30670E+01

===============================================================


 INSTANT    0.764000000E+03   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59821E-02 0.87821E+00
   Friction velocity        uk    :  0.59821E-02 0.87821E+00
   Dimensionless distance   yplus :  0.48160E-01 0.70702E+01
   Friction thermal sca.    tstar : -0.18441E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35933E-01 0.52752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68508E-02      32   0.39248E-03   0.17081E+01 0.83562E+02 
c  Velocity[X]                                      0.10433E+01 
c  Velocity[Y]                                      0.66472E+00 
c  Velocity[Z]                                      0.90337E-30 
c  Pressure     0.11632E-06     456   0.95775E-08   0.11988E+00 0.58536E+03 
c  nu_tilda     0.47255E-05      31   0.14088E-04   0.18312E-06 0.13228E+03 
c  TempC        0.28517E+02      27   0.46078E-03   0.47861E+01 0.20411E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4956          10.139          4.5729          4.5729
v  Velocity[Y]            -3.5659          7.0015        0.016459        0.016459
v  Velocity[Z]       -6.9287e-015     7.7343e-015    -1.3612e-017    -1.3612e-017
v  ǁVelocityǁ         0.0012038          10.139          5.1632          5.1632
v  Pressure               -53.445          21.279         -5.3623         -5.3623
v  nu_tilda           4.2569e-007       0.0042691      0.00095615      0.00095615
v  TempC                       21          73.083          21.606          21.606
v  TurbVisc           2.8884e-014       0.0050315       0.0011165       0.0011165
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              764:        0.39200E+01

===============================================================


 INSTANT    0.765000000E+03   TIME STEP NUMBER             765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15707E-02 0.87771E+00
   Friction velocity        uk    :  0.15707E-02 0.87771E+00
   Dimensionless distance   yplus :  0.12646E-01 0.70662E+01
   Friction thermal sca.    tstar : -0.11585E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94350E-02 0.52722E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68546E-02      32   0.38410E-03   0.16848E+01 0.83201E+02 
c  Velocity[X]                                      0.10383E+01 
c  Velocity[Y]                                      0.64653E+00 
c  Velocity[Z]                                      0.12435E-29 
c  Pressure     0.10438E-06     377   0.91251E-08   0.10542E+00 0.48082E+03 
c  nu_tilda     0.47272E-05      31   0.79191E-05   0.18306E-06 0.13221E+03 
c  TempC        0.28529E+02      27   0.41026E-03   0.60242E+01 0.22368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4998          10.141          4.5729          4.5729
v  Velocity[Y]            -3.5657          7.0228        0.016406        0.016406
v  Velocity[Z]       -6.9287e-015     7.7484e-015      -1.36e-017      -1.36e-017
v  ǁVelocityǁ         0.0010948          10.142          5.1637          5.1637
v  Pressure               -53.476          21.368         -5.3614         -5.3614
v  nu_tilda           4.2564e-007       0.0042691      0.00095679      0.00095679
v  TempC                       21          73.701          21.607          21.607
v  TurbVisc           2.8888e-014       0.0050315       0.0011173       0.0011173
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              765:        0.31430E+01

===============================================================


 INSTANT    0.766000000E+03   TIME STEP NUMBER             766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49052E-02 0.87883E+00
   Friction velocity        uk    :  0.49052E-02 0.87883E+00
   Dimensionless distance   yplus :  0.39490E-01 0.70752E+01
   Friction thermal sca.    tstar : -0.88546E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29464E-01 0.52789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68584E-02      32   0.35051E-03   0.16755E+01 0.83287E+02 
c  Velocity[X]                                      0.10082E+01 
c  Velocity[Y]                                      0.66737E+00 
c  Velocity[Z]                                      0.10712E-29 
c  Pressure     0.90937E-07     377   0.90803E-08   0.92999E-01 0.18571E+03 
c  nu_tilda     0.47289E-05      31   0.14083E-04   0.18299E-06 0.13214E+03 
c  TempC        0.28541E+02      27   0.44135E-03   0.58495E+01 0.23304E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5038          10.144          4.5729          4.5729
v  Velocity[Y]            -3.5655          7.0275        0.016353        0.016353
v  Velocity[Z]       -6.9287e-015     7.7667e-015     -1.358e-017     -1.358e-017
v  ǁVelocityǁ         0.0012913          10.145          5.1641          5.1641
v  Pressure               -53.484          21.363         -5.3717         -5.3717
v  nu_tilda           4.2563e-007       0.0042691      0.00095739      0.00095739
v  TempC                       21          73.083          21.607          21.607
v  TurbVisc           2.8877e-014       0.0050316        0.001118        0.001118
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              766:        0.31520E+01

===============================================================


 INSTANT    0.767000000E+03   TIME STEP NUMBER             767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72201E-02 0.87853E+00
   Friction velocity        uk    :  0.72201E-02 0.87853E+00
   Dimensionless distance   yplus :  0.58127E-01 0.70728E+01
   Friction thermal sca.    tstar : -0.11752E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43369E-01 0.52771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68622E-02      32   0.32281E-03   0.16832E+01 0.83253E+02 
c  Velocity[X]                                      0.10307E+01 
c  Velocity[Y]                                      0.65251E+00 
c  Velocity[Z]                                      0.88989E-30 
c  Pressure     0.13149E-06     437   0.98652E-08   0.13771E+00 0.27835E+03 
c  nu_tilda     0.47306E-05      31   0.79012E-05   0.18293E-06 0.13207E+03 
c  TempC        0.28552E+02      28   0.36545E-03   0.48308E+01 0.20464E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5081          10.147          4.5729          4.5729
v  Velocity[Y]            -3.5652          7.0051        0.016299        0.016299
v  Velocity[Z]       -6.9287e-015     7.7839e-015    -1.3567e-017    -1.3567e-017
v  ǁVelocityǁ         0.0010718          10.147          5.1646          5.1646
v  Pressure               -53.501          21.303         -5.3934         -5.3934
v  nu_tilda           4.2565e-007       0.0042691      0.00095803      0.00095803
v  TempC                       21          73.656          21.608          21.608
v  TurbVisc           2.8874e-014       0.0050316       0.0011188       0.0011188
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              767:        0.34130E+01

===============================================================


 INSTANT    0.768000000E+03   TIME STEP NUMBER             768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53747E-02 0.87700E+00
   Friction velocity        uk    :  0.53747E-02 0.87700E+00
   Dimensionless distance   yplus :  0.43270E-01 0.70604E+01
   Friction thermal sca.    tstar : -0.19329E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32284E-01 0.52679E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68660E-02      32   0.45270E-03   0.16517E+01 0.82970E+02 
c  Velocity[X]                                      0.10098E+01 
c  Velocity[Y]                                      0.64195E+00 
c  Velocity[Z]                                      0.10600E-29 
c  Pressure     0.99204E-07     378   0.93380E-08   0.10217E+00 0.15664E+03 
c  nu_tilda     0.47322E-05      31   0.14099E-04   0.18287E-06 0.13200E+03 
c  TempC        0.28564E+02      27   0.33279E-03   0.48856E+01 0.21832E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5124           10.15          4.5729          4.5729
v  Velocity[Y]            -3.5649          7.0238        0.016244        0.016244
v  Velocity[Z]       -6.9287e-015     7.7982e-015    -1.3547e-017    -1.3547e-017
v  ǁVelocityǁ         0.0013579           10.15          5.1651          5.1651
v  Pressure               -53.521          21.332         -5.4024         -5.4024
v  nu_tilda           4.2565e-007       0.0042691      0.00095864      0.00095864
v  TempC                       21          73.879          21.608          21.608
v  TurbVisc           2.8879e-014       0.0050316       0.0011195       0.0011195
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              768:        0.31940E+01

===============================================================


 INSTANT    0.769000000E+03   TIME STEP NUMBER             769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59480E-02 0.87807E+00
   Friction velocity        uk    :  0.59480E-02 0.87807E+00
   Dimensionless distance   yplus :  0.47886E-01 0.70690E+01
   Friction thermal sca.    tstar : -0.21805E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35728E-01 0.52743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68698E-02      32   0.36731E-03   0.17158E+01 0.83611E+02 
c  Velocity[X]                                      0.10474E+01 
c  Velocity[Y]                                      0.66841E+00 
c  Velocity[Z]                                      0.10235E-29 
c  Pressure     0.13754E-06     457   0.92391E-08   0.13975E+00 0.40856E+03 
c  nu_tilda     0.47339E-05      31   0.78776E-05   0.18281E-06 0.13194E+03 
c  TempC        0.28576E+02      27   0.66767E-03   0.51400E+01 0.19979E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5166          10.153          4.5729          4.5729
v  Velocity[Y]            -3.5646          6.9986         0.01619         0.01619
v  Velocity[Z]       -6.9287e-015     7.8152e-015    -1.3537e-017    -1.3537e-017
v  ǁVelocityǁ         0.0010451          10.153          5.1655          5.1655
v  Pressure               -53.544          21.238         -5.4341         -5.4341
v  nu_tilda            4.257e-007       0.0042691      0.00095927      0.00095927
v  TempC                       21          73.627          21.609          21.609
v  TurbVisc            2.888e-014       0.0050316       0.0011202       0.0011202
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              769:        0.34340E+01

===============================================================


 INSTANT    0.770000000E+03   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15364E-02 0.87760E+00
   Friction velocity        uk    :  0.15364E-02 0.87760E+00
   Dimensionless distance   yplus :  0.12369E-01 0.70653E+01
   Friction thermal sca.    tstar : -0.12867E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92288E-02 0.52715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68736E-02      32   0.32424E-03   0.16926E+01 0.83447E+02 
c  Velocity[X]                                      0.10403E+01 
c  Velocity[Y]                                      0.65233E+00 
c  Velocity[Z]                                      0.11430E-29 
c  Pressure     0.11582E-06     424   0.99329E-08   0.11901E+00 0.45916E+03 
c  nu_tilda     0.47355E-05      31   0.14116E-04   0.18275E-06 0.13187E+03 
c  TempC        0.28588E+02      27   0.41524E-03   0.13133E+02 0.37747E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5208          10.155          4.5729          4.5729
v  Velocity[Y]            -3.5644           7.021        0.016135        0.016135
v  Velocity[Z]       -6.9287e-015     7.8325e-015    -1.3515e-017    -1.3515e-017
v  ǁVelocityǁ         0.0013408          10.156           5.166           5.166
v  Pressure               -53.555          21.352         -5.4197         -5.4197
v  nu_tilda           4.2571e-007       0.0042691      0.00095988      0.00095988
v  TempC                       21          73.126          21.609          21.609
v  TurbVisc           2.8893e-014       0.0050316        0.001121        0.001121
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              770:        0.33620E+01

===============================================================


 INSTANT    0.771000000E+03   TIME STEP NUMBER             771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63883E-02 0.87877E+00
   Friction velocity        uk    :  0.63883E-02 0.87877E+00
   Dimensionless distance   yplus :  0.51430E-01 0.70747E+01
   Friction thermal sca.    tstar : -0.95821E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38373E-01 0.52785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68774E-02      32   0.37270E-03   0.16455E+01 0.83003E+02 
c  Velocity[X]                                      0.99928E+00 
c  Velocity[Y]                                      0.64625E+00 
c  Velocity[Z]                                      0.10688E-29 
c  Pressure     0.90289E-07     409   0.98295E-08   0.92834E-01 0.20974E+03 
c  nu_tilda     0.47372E-05      31   0.78735E-05   0.18268E-06 0.13180E+03 
c  TempC        0.28600E+02      27   0.40931E-03   0.59714E+01 0.23968E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5249          10.158          4.5729          4.5729
v  Velocity[Y]            -3.5641          7.0315         0.01608         0.01608
v  Velocity[Z]       -6.9287e-015      7.845e-015    -1.3498e-017    -1.3498e-017
v  ǁVelocityǁ          0.001052          10.159          5.1664          5.1664
v  Pressure               -53.583          21.347         -5.4368         -5.4368
v  nu_tilda           4.2565e-007       0.0042691      0.00096052      0.00096052
v  TempC                       21          73.926           21.61           21.61
v  TurbVisc           2.8896e-014       0.0050316       0.0011217       0.0011217
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              771:        0.32690E+01

===============================================================


 INSTANT    0.772000000E+03   TIME STEP NUMBER             772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42854E-02 0.87822E+00
   Friction velocity        uk    :  0.42854E-02 0.87822E+00
   Dimensionless distance   yplus :  0.34501E-01 0.70703E+01
   Friction thermal sca.    tstar : -0.13414E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25741E-01 0.52752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68812E-02      32   0.33893E-03   0.16957E+01 0.83559E+02 
c  Velocity[X]                                      0.10260E+01 
c  Velocity[Y]                                      0.66967E+00 
c  Velocity[Z]                                      0.93447E-30 
c  Pressure     0.11200E-06     469   0.98800E-08   0.11630E+00 0.71598E+03 
c  nu_tilda     0.47389E-05      31   0.14109E-04   0.18262E-06 0.13174E+03 
c  TempC        0.28612E+02      27   0.44719E-03   0.55555E+01 0.24411E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5289          10.161          4.5729          4.5729
v  Velocity[Y]            -3.5636           6.999        0.016024        0.016024
v  Velocity[Z]       -6.9287e-015     7.8614e-015    -1.3482e-017    -1.3482e-017
v  ǁVelocityǁ         0.0013386          10.161          5.1669          5.1669
v  Pressure               -53.589          21.211         -5.4741         -5.4741
v  nu_tilda            4.257e-007       0.0042691      0.00096113      0.00096113
v  TempC                       21          73.877           21.61           21.61
v  TurbVisc           2.8879e-014       0.0050316       0.0011225       0.0011225
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              772:        0.35020E+01

===============================================================


 INSTANT    0.773000000E+03   TIME STEP NUMBER             773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70037E-02 0.87705E+00
   Friction velocity        uk    :  0.70037E-02 0.87705E+00
   Dimensionless distance   yplus :  0.56385E-01 0.70609E+01
   Friction thermal sca.    tstar : -0.72451E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42069E-01 0.52682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68849E-02      32   0.37458E-03   0.16623E+01 0.83233E+02 
c  Velocity[X]                                      0.10074E+01 
c  Velocity[Y]                                      0.65493E+00 
c  Velocity[Z]                                      0.11116E-29 
c  Pressure     0.76863E-07     393   0.94927E-08   0.79266E-01 0.48854E+03 
c  nu_tilda     0.47405E-05      31   0.78596E-05   0.18257E-06 0.13167E+03 
c  TempC        0.28624E+02      27   0.34827E-03   0.54238E+01 0.23544E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5328          10.164          4.5729          4.5729
v  Velocity[Y]            -3.5632            7.02        0.015968        0.015968
v  Velocity[Z]       -6.9287e-015     7.8755e-015    -1.3462e-017    -1.3462e-017
v  ǁVelocityǁ         0.0010567          10.164          5.1673          5.1673
v  Pressure               -53.621          21.299         -5.4721         -5.4721
v  nu_tilda           4.2572e-007       0.0042691      0.00096176      0.00096176
v  TempC                       21          73.251          21.611          21.611
v  TurbVisc           2.8892e-014       0.0050316       0.0011232       0.0011232
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              773:        0.31850E+01

===============================================================


 INSTANT    0.774000000E+03   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24435E-02 0.87821E+00
   Friction velocity        uk    :  0.24435E-02 0.87821E+00
   Dimensionless distance   yplus :  0.19671E-01 0.70702E+01
   Friction thermal sca.    tstar : -0.63390E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14677E-01 0.52751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68887E-02      32   0.43365E-03   0.17044E+01 0.83672E+02 
c  Velocity[X]                                      0.10554E+01 
c  Velocity[Y]                                      0.64908E+00 
c  Velocity[Z]                                      0.10586E-29 
c  Pressure     0.12658E-06     425   0.97577E-08   0.13130E+00 0.50489E+03 
c  nu_tilda     0.47422E-05      31   0.14122E-04   0.18251E-06 0.13160E+03 
c  TempC        0.28636E+02      27   0.46081E-03   0.48053E+01 0.21253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5366          10.167          4.5729          4.5729
v  Velocity[Y]            -3.5627          7.0005        0.015911        0.015911
v  Velocity[Z]       -6.9287e-015     7.8936e-015    -1.3441e-017    -1.3441e-017
v  ǁVelocityǁ         0.0013035          10.167          5.1678          5.1678
v  Pressure               -53.629           21.21         -5.4994         -5.4994
v  nu_tilda           4.2575e-007       0.0042691      0.00096237      0.00096237
v  TempC                       21          73.862          21.611          21.611
v  TurbVisc           2.8899e-014       0.0050316        0.001124        0.001124
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              774:        0.33190E+01

===============================================================


 INSTANT    0.775000000E+03   TIME STEP NUMBER             775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51727E-02 0.87750E+00
   Friction velocity        uk    :  0.51727E-02 0.87750E+00
   Dimensionless distance   yplus :  0.41643E-01 0.70645E+01
   Friction thermal sca.    tstar : -0.57562E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31071E-01 0.52709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68925E-02      32   0.35613E-03   0.16913E+01 0.83590E+02 
c  Velocity[X]                                      0.10236E+01 
c  Velocity[Y]                                      0.66771E+00 
c  Velocity[Z]                                      0.12205E-29 
c  Pressure     0.11627E-06     410   0.93927E-08   0.11908E+00 0.59051E+03 
c  nu_tilda     0.47439E-05      31   0.78473E-05   0.18246E-06 0.13154E+03 
c  TempC        0.28648E+02      27   0.69905E-03   0.67827E+01 0.25815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5406          10.169          4.5729          4.5729
v  Velocity[Y]            -3.5623          7.0247        0.015854        0.015854
v  Velocity[Z]       -6.9287e-015     7.9078e-015    -1.3424e-017    -1.3424e-017
v  ǁVelocityǁ         0.0010478           10.17          5.1682          5.1682
v  Pressure               -53.652          21.312         -5.4882         -5.4882
v  nu_tilda           4.2573e-007       0.0042691      0.00096301      0.00096301
v  TempC                       21          73.082          21.612          21.612
v  TurbVisc           2.8906e-014       0.0050316       0.0011247       0.0011247
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              775:        0.32720E+01

===============================================================


 INSTANT    0.776000000E+03   TIME STEP NUMBER             776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28971E-02 0.87880E+00
   Friction velocity        uk    :  0.28971E-02 0.87880E+00
   Dimensionless distance   yplus :  0.23324E-01 0.70749E+01
   Friction thermal sca.    tstar : -0.56835E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17402E-01 0.52787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68963E-02      32   0.39350E-03   0.16621E+01 0.83228E+02 
c  Velocity[X]                                      0.10082E+01 
c  Velocity[Y]                                      0.65389E+00 
c  Velocity[Z]                                      0.11117E-29 
c  Pressure     0.12380E-06     409   0.97952E-08   0.12574E+00 0.31778E+03 
c  nu_tilda     0.47455E-05      31   0.14138E-04   0.18240E-06 0.13148E+03 
c  TempC        0.28660E+02      27   0.85080E-03   0.53099E+01 0.24295E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5445          10.172          4.5729          4.5729
v  Velocity[Y]            -3.5619          7.0274        0.015796        0.015796
v  Velocity[Z]       -6.9287e-015      7.917e-015    -1.3408e-017    -1.3408e-017
v  ǁVelocityǁ         0.0011798          10.172          5.1687          5.1687
v  Pressure               -53.672           21.28         -5.5101         -5.5101
v  nu_tilda           4.2574e-007       0.0042691      0.00096362      0.00096362
v  TempC                       21          74.015          21.612          21.612
v  TurbVisc           2.8901e-014       0.0050316       0.0011254       0.0011254
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              776:        0.32850E+01

===============================================================


 INSTANT    0.777000000E+03   TIME STEP NUMBER             777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12619E-02 0.87853E+00
   Friction velocity        uk    :  0.12619E-02 0.87853E+00
   Dimensionless distance   yplus :  0.10160E-01 0.70727E+01
   Friction thermal sca.    tstar : -0.51703E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75802E-02 0.52771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69001E-02      32   0.36402E-03   0.16809E+01 0.83447E+02 
c  Velocity[X]                                      0.10288E+01 
c  Velocity[Y]                                      0.65208E+00 
c  Velocity[Z]                                      0.97954E-30 
c  Pressure     0.10329E-06     437   0.95400E-08   0.10904E+00 0.43603E+03 
c  nu_tilda     0.47472E-05      31   0.78478E-05   0.18235E-06 0.13142E+03 
c  TempC        0.28672E+02      27   0.39841E-03   0.16302E+02 0.39851E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5485          10.175          4.5729          4.5729
v  Velocity[Y]            -3.5614           7.004        0.015739        0.015739
v  Velocity[Z]       -6.9287e-015     7.9288e-015    -1.3394e-017    -1.3394e-017
v  ǁVelocityǁ         0.0010106          10.175          5.1691          5.1691
v  Pressure               -53.694          21.183         -5.5441         -5.5441
v  nu_tilda           4.2579e-007       0.0042691      0.00096426      0.00096426
v  TempC                       21           73.48          21.613          21.613
v  TurbVisc           2.8903e-014       0.0050316       0.0011262       0.0011262
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              777:        0.33880E+01

===============================================================


 INSTANT    0.778000000E+03   TIME STEP NUMBER             778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51582E-02 0.87716E+00
   Friction velocity        uk    :  0.51582E-02 0.87716E+00
   Dimensionless distance   yplus :  0.41527E-01 0.70617E+01
   Friction thermal sca.    tstar : -0.53226E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30984E-01 0.52688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69038E-02      32   0.42853E-03   0.16769E+01 0.83551E+02 
c  Velocity[X]                                      0.10064E+01 
c  Velocity[Y]                                      0.67053E+00 
c  Velocity[Z]                                      0.10244E-29 
c  Pressure     0.10129E-06     422   0.89575E-08   0.10474E+00 0.44993E+03 
c  nu_tilda     0.47488E-05      31   0.14137E-04   0.18229E-06 0.13135E+03 
c  TempC        0.28684E+02      27   0.37958E-03   0.75218E+01 0.25910E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5523          10.178          4.5729          4.5729
v  Velocity[Y]            -3.5608          7.0217         0.01568         0.01568
v  Velocity[Z]       -6.9287e-015     7.9421e-015    -1.3369e-017    -1.3369e-017
v  ǁVelocityǁ         0.0010775          10.178          5.1696          5.1696
v  Pressure               -53.707           21.29         -5.5292         -5.5292
v  nu_tilda           4.2573e-007       0.0042691      0.00096487      0.00096487
v  TempC                       21          73.166          21.613          21.613
v  TurbVisc           2.8918e-014       0.0050316       0.0011269       0.0011269
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              778:        0.33420E+01

===============================================================


 INSTANT    0.779000000E+03   TIME STEP NUMBER             779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24604E-02 0.87814E+00
   Friction velocity        uk    :  0.24604E-02 0.87814E+00
   Dimensionless distance   yplus :  0.19808E-01 0.70696E+01
   Friction thermal sca.    tstar : -0.81942E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14779E-01 0.52747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69076E-02      32   0.36516E-03   0.17162E+01 0.84011E+02 
c  Velocity[X]                                      0.10442E+01 
c  Velocity[Y]                                      0.67202E+00 
c  Velocity[Z]                                      0.97958E-30 
c  Pressure     0.12333E-06     469   0.95399E-08   0.12835E+00 0.54965E+03 
c  nu_tilda     0.47505E-05      31   0.78339E-05   0.18224E-06 0.13129E+03 
c  TempC        0.28696E+02      27   0.47296E-03   0.58009E+01 0.24238E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5561           10.18          4.5729          4.5729
v  Velocity[Y]            -3.5601          7.0047        0.015622        0.015622
v  Velocity[Z]       -6.9287e-015     7.9532e-015    -1.3351e-017    -1.3351e-017
v  ǁVelocityǁ         0.0010532          10.181            5.17            5.17
v  Pressure               -53.732          21.169         -5.5698         -5.5698
v  nu_tilda           4.2571e-007       0.0042691      0.00096551      0.00096551
v  TempC                       21          73.082          21.614          21.614
v  TurbVisc           2.8901e-014       0.0050316       0.0011277       0.0011277
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              779:        0.35520E+01

===============================================================


 INSTANT    0.780000000E+03   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32613E-02 0.87737E+00
   Friction velocity        uk    :  0.32613E-02 0.87737E+00
   Dimensionless distance   yplus :  0.26256E-01 0.70634E+01
   Friction thermal sca.    tstar : -0.17453E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19590E-01 0.52701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69114E-02      32   0.36704E-03   0.16943E+01 0.83596E+02 
c  Velocity[X]                                      0.10422E+01 
c  Velocity[Y]                                      0.65211E+00 
c  Velocity[Z]                                      0.12637E-29 
c  Pressure     0.13035E-06     394   0.95105E-08   0.13165E+00 0.33597E+03 
c  nu_tilda     0.47521E-05      31   0.14150E-04   0.18219E-06 0.13123E+03 
c  TempC        0.28708E+02      27   0.41764E-03   0.62927E+01 0.25723E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5598          10.183          4.5729          4.5729
v  Velocity[Y]            -3.5597          7.0213        0.015563        0.015563
v  Velocity[Z]       -6.9287e-015     7.9671e-015    -1.3333e-017    -1.3333e-017
v  ǁVelocityǁ         0.0010285          10.183          5.1704          5.1704
v  Pressure               -53.746          21.252         -5.5617         -5.5617
v  nu_tilda           4.2571e-007       0.0042691      0.00096612      0.00096612
v  TempC                       21          74.138          21.614          21.614
v  TurbVisc           2.8894e-014       0.0050316       0.0011284       0.0011284
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              780:        0.32960E+01

===============================================================


 INSTANT    0.781000000E+03   TIME STEP NUMBER             781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31708E-02 0.87872E+00
   Friction velocity        uk    :  0.31708E-02 0.87872E+00
   Dimensionless distance   yplus :  0.25527E-01 0.70743E+01
   Friction thermal sca.    tstar : -0.65643E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19046E-01 0.52782E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69151E-02      32   0.38177E-03   0.16625E+01 0.83429E+02 
c  Velocity[X]                                      0.99841E+00 
c  Velocity[Y]                                      0.66410E+00 
c  Velocity[Z]                                      0.11219E-29 
c  Pressure     0.90123E-07     394   0.95725E-08   0.93471E-01 0.21161E+03 
c  nu_tilda     0.47538E-05      31   0.78146E-05   0.18214E-06 0.13117E+03 
c  TempC        0.28720E+02      27   0.37998E-03   0.76987E+01 0.27001E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5634          10.186          4.5729          4.5729
v  Velocity[Y]             -3.559          7.0285        0.015504        0.015504
v  Velocity[Z]       -6.9287e-015     7.9735e-015    -1.3308e-017    -1.3308e-017
v  ǁVelocityǁ         0.0010891          10.186          5.1709          5.1709
v  Pressure               -53.775          21.258         -5.5772         -5.5772
v  nu_tilda           4.2571e-007       0.0042691      0.00096676      0.00096676
v  TempC                       21          73.597          21.615          21.615
v  TurbVisc           2.8895e-014       0.0050316       0.0011292       0.0011292
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              781:        0.35100E+01

===============================================================


 INSTANT    0.782000000E+03   TIME STEP NUMBER             782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49906E-02 0.87822E+00
   Friction velocity        uk    :  0.49906E-02 0.87822E+00
   Dimensionless distance   yplus :  0.40177E-01 0.70702E+01
   Friction thermal sca.    tstar : -0.60030E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29977E-01 0.52752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69189E-02      32   0.35946E-03   0.16850E+01 0.83728E+02 
c  Velocity[X]                                      0.10262E+01 
c  Velocity[Y]                                      0.65876E+00 
c  Velocity[Z]                                      0.87788E-30 
c  Pressure     0.10709E-06     426   0.95209E-08   0.11254E+00 0.58962E+03 
c  nu_tilda     0.47554E-05      31   0.14166E-04   0.18209E-06 0.13111E+03 
c  TempC        0.28732E+02      27   0.52016E-03   0.50739E+01 0.21994E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5669          10.188          4.5729          4.5729
v  Velocity[Y]            -3.5584          7.0036        0.015444        0.015444
v  Velocity[Z]       -6.9287e-015     7.9849e-015     -1.329e-017     -1.329e-017
v  ǁVelocityǁ        0.00098532          10.189          5.1713          5.1713
v  Pressure               -53.785          21.146         -5.6089         -5.6089
v  nu_tilda           4.2574e-007       0.0042691      0.00096737      0.00096737
v  TempC                       21          73.255          21.615          21.615
v  TurbVisc           2.8895e-014       0.0050316       0.0011299       0.0011299
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              782:        0.34440E+01

===============================================================


 INSTANT    0.783000000E+03   TIME STEP NUMBER             783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29346E-02 0.87700E+00
   Friction velocity        uk    :  0.29346E-02 0.87700E+00
   Dimensionless distance   yplus :  0.23626E-01 0.70604E+01
   Friction thermal sca.    tstar : -0.63152E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17627E-01 0.52679E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69227E-02      32   0.39456E-03   0.16854E+01 0.83699E+02 
c  Velocity[X]                                      0.10339E+01 
c  Velocity[Y]                                      0.65156E+00 
c  Velocity[Z]                                      0.10076E-29 
c  Pressure     0.11621E-06     393   0.90734E-08   0.11958E+00 0.45067E+03 
c  nu_tilda     0.47571E-05      31   0.78231E-05   0.18203E-06 0.13105E+03 
c  TempC        0.28744E+02      28   0.37755E-03   0.51582E+01 0.22311E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5703          10.191          4.5729          4.5729
v  Velocity[Y]            -3.5576          7.0264        0.015384        0.015384
v  Velocity[Z]       -6.9287e-015     7.9947e-015    -1.3265e-017    -1.3265e-017
v  ǁVelocityǁ         0.0011965          10.191          5.1717          5.1717
v  Pressure               -53.816          21.226         -5.6077         -5.6077
v  nu_tilda           4.2568e-007       0.0042692      0.00096801      0.00096801
v  TempC                       21          73.223          21.615          21.615
v  TurbVisc           2.8904e-014       0.0050316       0.0011306       0.0011306
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              783:        0.35660E+01

===============================================================


 INSTANT    0.784000000E+03   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52873E-02 0.87808E+00
   Friction velocity        uk    :  0.52873E-02 0.87808E+00
   Dimensionless distance   yplus :  0.42566E-01 0.70692E+01
   Friction thermal sca.    tstar : -0.72055E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31759E-01 0.52744E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69264E-02      32   0.35451E-03   0.17130E+01 0.83879E+02 
c  Velocity[X]                                      0.10456E+01 
c  Velocity[Y]                                      0.66741E+00 
c  Velocity[Z]                                      0.97789E-30 
c  Pressure     0.14366E-06     426   0.93993E-08   0.14735E+00 0.47145E+03 
c  nu_tilda     0.47587E-05      31   0.14161E-04   0.18198E-06 0.13099E+03 
c  TempC        0.28756E+02      27   0.41352E-03   0.42034E+01 0.19295E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5738          10.194          4.5729          4.5729
v  Velocity[Y]            -3.5568          6.9969        0.015324        0.015324
v  Velocity[Z]       -6.9287e-015     8.0091e-015     -1.325e-017     -1.325e-017
v  ǁVelocityǁ        0.00096622          10.194          5.1722          5.1722
v  Pressure               -53.819          21.139         -5.6306         -5.6306
v  nu_tilda           4.2554e-007       0.0042692      0.00096862      0.00096862
v  TempC                       21          73.196          21.616          21.616
v  TurbVisc           2.8887e-014       0.0050316       0.0011314       0.0011314
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              784:        0.33750E+01

===============================================================


 INSTANT    0.785000000E+03   TIME STEP NUMBER             785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24619E-03 0.87745E+00
   Friction velocity        uk    :  0.24619E-03 0.87745E+00
   Dimensionless distance   yplus :  0.19820E-02 0.70641E+01
   Friction thermal sca.    tstar : -0.76269E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14788E-02 0.52706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69302E-02      32   0.31894E-03   0.16705E+01 0.83534E+02 
c  Velocity[X]                                      0.10125E+01 
c  Velocity[Y]                                      0.65795E+00 
c  Velocity[Z]                                      0.11970E-29 
c  Pressure     0.91805E-07     378   0.93732E-08   0.94779E-01 0.49379E+03 
c  nu_tilda     0.47604E-05      31   0.77928E-05   0.18193E-06 0.13093E+03 
c  TempC        0.28768E+02      27   0.48976E-03   0.40660E+01 0.19123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5772          10.196          4.5729          4.5729
v  Velocity[Y]            -3.5562           7.023        0.015263        0.015263
v  Velocity[Z]       -6.9287e-015     8.0182e-015    -1.3231e-017    -1.3231e-017
v  ǁVelocityǁ         0.0013373          10.197          5.1726          5.1726
v  Pressure               -53.849          21.229         -5.6268         -5.6268
v  nu_tilda           4.2535e-007       0.0042692      0.00096926      0.00096926
v  TempC                       21          73.463          21.616          21.616
v  TurbVisc           2.8849e-014       0.0050316       0.0011321       0.0011321
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              785:        0.32050E+01

===============================================================


 INSTANT    0.786000000E+03   TIME STEP NUMBER             786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69642E-02 0.87874E+00
   Friction velocity        uk    :  0.69642E-02 0.87874E+00
   Dimensionless distance   yplus :  0.56067E-01 0.70745E+01
   Friction thermal sca.    tstar : -0.11581E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41832E-01 0.52784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69340E-02      32   0.40468E-03   0.16431E+01 0.83354E+02 
c  Velocity[X]                                      0.98964E+00 
c  Velocity[Y]                                      0.65344E+00 
c  Velocity[Z]                                      0.10187E-29 
c  Pressure     0.86114E-07     410   0.95139E-08   0.89153E-01 0.20626E+03 
c  nu_tilda     0.47620E-05      31   0.14169E-04   0.18188E-06 0.13087E+03 
c  TempC        0.28780E+02      27   0.38183E-03   0.61520E+01 0.24016E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5807          10.199          4.5729          4.5729
v  Velocity[Y]            -3.5554          7.0304        0.015202        0.015202
v  Velocity[Z]       -6.9287e-015     8.0246e-015    -1.3217e-017    -1.3217e-017
v  ǁVelocityǁ        0.00095665          10.199           5.173           5.173
v  Pressure               -53.869          21.226         -5.6419         -5.6419
v  nu_tilda           4.2509e-007       0.0042692      0.00096987      0.00096987
v  TempC                       21          73.979          21.617          21.617
v  TurbVisc           2.8798e-014       0.0050316       0.0011329       0.0011329
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              786:        0.33300E+01

===============================================================


 INSTANT    0.787000000E+03   TIME STEP NUMBER             787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60184E-02 0.87827E+00
   Friction velocity        uk    :  0.60184E-02 0.87827E+00
   Dimensionless distance   yplus :  0.48452E-01 0.70707E+01
   Friction thermal sca.    tstar : -0.10392E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36151E-01 0.52755E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69377E-02      32   0.39826E-03   0.17069E+01 0.84054E+02 
c  Velocity[X]                                      0.10347E+01 
c  Velocity[Y]                                      0.67226E+00 
c  Velocity[Z]                                      0.10310E-29 
c  Pressure     0.11749E-06     472   0.94899E-08   0.12225E+00 0.53705E+03 
c  nu_tilda     0.47637E-05      31   0.77882E-05   0.18184E-06 0.13082E+03 
c  TempC        0.28791E+02      27   0.31194E-03   0.48525E+01 0.21207E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5841          10.202          4.5729          4.5729
v  Velocity[Y]            -3.5546          7.0058        0.015141        0.015141
v  Velocity[Z]       -6.9287e-015     8.0343e-015    -1.3194e-017    -1.3194e-017
v  ǁVelocityǁ         0.0012068          10.202          5.1735          5.1735
v  Pressure               -53.891          21.099         -5.6799         -5.6799
v  nu_tilda           4.2484e-007       0.0042692      0.00097051      0.00097051
v  TempC                       21          73.373          21.617          21.617
v  TurbVisc           2.8728e-014       0.0050316       0.0011336       0.0011336
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              787:        0.35050E+01

===============================================================


 INSTANT    0.788000000E+03   TIME STEP NUMBER             788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82972E-02 0.87717E+00
   Friction velocity        uk    :  0.82972E-02 0.87717E+00
   Dimensionless distance   yplus :  0.66799E-01 0.70618E+01
   Friction thermal sca.    tstar : -0.13584E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49839E-01 0.52689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69415E-02      32   0.32708E-03   0.16825E+01 0.83746E+02 
c  Velocity[X]                                      0.10204E+01 
c  Velocity[Y]                                      0.66204E+00 
c  Velocity[Z]                                      0.11042E-29 
c  Pressure     0.10975E-06     409   0.94747E-08   0.11174E+00 0.38947E+03 
c  nu_tilda     0.47653E-05      31   0.14197E-04   0.18179E-06 0.13076E+03 
c  TempC        0.28803E+02      27   0.59296E-03   0.36571E+01 0.17591E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5874          10.204          4.5729          4.5729
v  Velocity[Y]            -3.5538          7.0194        0.015079        0.015079
v  Velocity[Z]       -6.9287e-015     8.0446e-015    -1.3172e-017    -1.3172e-017
v  ǁVelocityǁ         0.0010413          10.204          5.1739          5.1739
v  Pressure               -53.904          21.196         -5.6684         -5.6684
v  nu_tilda           4.2452e-007       0.0042692      0.00097112      0.00097112
v  TempC                       21          73.582          21.618          21.618
v  TurbVisc            2.866e-014       0.0050316       0.0011344       0.0011344
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              788:        0.32950E+01

===============================================================


 INSTANT    0.789000000E+03   TIME STEP NUMBER             789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85416E-02 0.87814E+00
   Friction velocity        uk    :  0.85416E-02 0.87814E+00
   Dimensionless distance   yplus :  0.68766E-01 0.70696E+01
   Friction thermal sca.    tstar : -0.19677E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51307E-01 0.52747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69452E-02      32   0.37550E-03   0.16620E+01 0.83581E+02 
c  Velocity[X]                                      0.10056E+01 
c  Velocity[Y]                                      0.65649E+00 
c  Velocity[Z]                                      0.96761E-30 
c  Pressure     0.92574E-07     470   0.90444E-08   0.96267E-01 0.46393E+03 
c  nu_tilda     0.47670E-05      31   0.77791E-05   0.18174E-06 0.13070E+03 
c  TempC        0.28815E+02      27   0.35381E-03   0.71175E+01 0.25518E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5907          10.207          4.5729          4.5729
v  Velocity[Y]            -3.5528          7.0006        0.015017        0.015017
v  Velocity[Z]       -6.9287e-015     8.0546e-015    -1.3159e-017    -1.3159e-017
v  ǁVelocityǁ         0.0010772          10.207          5.1743          5.1743
v  Pressure               -53.929          21.091         -5.7039         -5.7039
v  nu_tilda           4.2414e-007       0.0042692      0.00097176      0.00097176
v  TempC                       21          73.091          21.618          21.618
v  TurbVisc           2.8573e-014       0.0050316       0.0011351       0.0011351
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              789:        0.35030E+01

===============================================================


 INSTANT    0.790000000E+03   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53400E-02 0.87756E+00
   Friction velocity        uk    :  0.53400E-02 0.87756E+00
   Dimensionless distance   yplus :  0.42991E-01 0.70649E+01
   Friction thermal sca.    tstar : -0.23822E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32076E-01 0.52712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69490E-02      32   0.35547E-03   0.16718E+01 0.83744E+02 
c  Velocity[X]                                      0.10067E+01 
c  Velocity[Y]                                      0.66506E+00 
c  Velocity[Z]                                      0.11216E-29 
c  Pressure     0.10752E-06     426   0.99622E-08   0.11130E+00 0.45842E+03 
c  nu_tilda     0.47686E-05      31   0.14186E-04   0.18169E-06 0.13065E+03 
c  TempC        0.28827E+02      27   0.45948E-03   0.48161E+01 0.20339E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5939           10.21          4.5729          4.5729
v  Velocity[Y]            -3.5519          7.0221        0.014954        0.014954
v  Velocity[Z]       -6.9287e-015     8.0659e-015     -1.314e-017     -1.314e-017
v  ǁVelocityǁ         0.0011869           10.21          5.1747          5.1747
v  Pressure               -53.944          21.207         -5.6897         -5.6897
v  nu_tilda           4.2367e-007       0.0042692      0.00097237      0.00097237
v  TempC                       21          73.209          21.619          21.619
v  TurbVisc           2.8471e-014       0.0050316       0.0011359       0.0011359
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              790:        0.32670E+01

===============================================================


 INSTANT    0.791000000E+03   TIME STEP NUMBER             791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10351E-01 0.87861E+00
   Friction velocity        uk    :  0.10351E-01 0.87861E+00
   Dimensionless distance   yplus :  0.83335E-01 0.70734E+01
   Friction thermal sca.    tstar : -0.14555E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62177E-01 0.52776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69527E-02      32   0.39951E-03   0.16658E+01 0.83677E+02 
c  Velocity[X]                                      0.10040E+01 
c  Velocity[Y]                                      0.66180E+00 
c  Velocity[Z]                                      0.12506E-29 
c  Pressure     0.11188E-06     442   0.94724E-08   0.11375E+00 0.30834E+03 
c  nu_tilda     0.47703E-05      31   0.77684E-05   0.18165E-06 0.13059E+03 
c  TempC        0.28839E+02      27   0.51087E-03   0.54395E+01 0.24181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5969          10.213          4.5729          4.5729
v  Velocity[Y]            -3.5511           7.027        0.014891        0.014891
v  Velocity[Z]       -6.9287e-015     8.0702e-015    -1.3118e-017    -1.3118e-017
v  ǁVelocityǁ         0.0010693          10.213          5.1751          5.1751
v  Pressure                -53.97          21.148         -5.7173         -5.7173
v  nu_tilda           4.2323e-007       0.0042692      0.00097302      0.00097302
v  TempC                       21          73.676          21.619          21.619
v  TurbVisc           2.8346e-014       0.0050316       0.0011366       0.0011366
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              791:        0.33320E+01

===============================================================


 INSTANT    0.792000000E+03   TIME STEP NUMBER             792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45386E-02 0.87838E+00
   Friction velocity        uk    :  0.45386E-02 0.87838E+00
   Dimensionless distance   yplus :  0.36539E-01 0.70716E+01
   Friction thermal sca.    tstar : -0.10373E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27262E-01 0.52762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69565E-02      32   0.36551E-03   0.16997E+01 0.84023E+02 
c  Velocity[X]                                      0.10419E+01 
c  Velocity[Y]                                      0.65779E+00 
c  Velocity[Z]                                      0.98424E-30 
c  Pressure     0.10963E-06     441   0.94464E-08   0.11492E+00 0.47140E+03 
c  nu_tilda     0.47719E-05      31   0.14200E-04   0.18160E-06 0.13054E+03 
c  TempC        0.28851E+02      27   0.59371E-03   0.58722E+01 0.25381E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5999          10.216          4.5729          4.5729
v  Velocity[Y]            -3.5501          7.0013        0.014828        0.014828
v  Velocity[Z]       -6.9287e-015     8.0787e-015      -1.31e-017      -1.31e-017
v  ǁVelocityǁ         0.0013959          10.216          5.1756          5.1756
v  Pressure               -53.983          21.062         -5.7432         -5.7432
v  nu_tilda           4.2293e-007       0.0042692      0.00097363      0.00097363
v  TempC                       21          73.256           21.62           21.62
v  TurbVisc           2.8229e-014       0.0050316       0.0011374       0.0011374
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              792:        0.33670E+01

===============================================================


 INSTANT    0.793000000E+03   TIME STEP NUMBER             793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10755E-01 0.87732E+00
   Friction velocity        uk    :  0.10755E-01 0.87732E+00
   Dimensionless distance   yplus :  0.86586E-01 0.70630E+01
   Friction thermal sca.    tstar : -0.94231E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64603E-01 0.52698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69602E-02      32   0.34668E-03   0.16737E+01 0.83831E+02 
c  Velocity[X]                                      0.10034E+01 
c  Velocity[Y]                                      0.67036E+00 
c  Velocity[Z]                                      0.10268E-29 
c  Pressure     0.11493E-06     441   0.94714E-08   0.11761E+00 0.69301E+03 
c  nu_tilda     0.47736E-05      31   0.77517E-05   0.18156E-06 0.13048E+03 
c  TempC        0.28863E+02      28   0.37209E-03   0.68117E+01 0.25850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6029          10.218          4.5729          4.5729
v  Velocity[Y]            -3.5491          7.0215        0.014765        0.014765
v  Velocity[Z]       -6.9287e-015     8.0879e-015    -1.3092e-017    -1.3092e-017
v  ǁVelocityǁ         0.0012475          10.219           5.176           5.176
v  Pressure               -54.005          21.191         -5.7257         -5.7257
v  nu_tilda            4.227e-007       0.0042692      0.00097427      0.00097427
v  TempC                       21          73.092           21.62           21.62
v  TurbVisc           2.8148e-014       0.0050317       0.0011381       0.0011381
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              793:        0.33940E+01

===============================================================


 INSTANT    0.794000000E+03   TIME STEP NUMBER             794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90419E-02 0.87830E+00
   Friction velocity        uk    :  0.90419E-02 0.87830E+00
   Dimensionless distance   yplus :  0.72794E-01 0.70710E+01
   Friction thermal sca.    tstar : -0.82241E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54312E-01 0.52757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69640E-02      32   0.38759E-03   0.16646E+01 0.83784E+02 
c  Velocity[X]                                      0.10009E+01 
c  Velocity[Y]                                      0.66368E+00 
c  Velocity[Z]                                      0.99167E-30 
c  Pressure     0.10137E-06     486   0.90347E-08   0.10545E+00 0.81968E+03 
c  nu_tilda     0.47752E-05      31   0.14218E-04   0.18151E-06 0.13043E+03 
c  TempC        0.28875E+02      27   0.46493E-03   0.50457E+01 0.21882E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6057          10.221          4.5729          4.5729
v  Velocity[Y]            -3.5481          7.0014          0.0147          0.0147
v  Velocity[Z]       -6.9287e-015     8.0978e-015    -1.3083e-017    -1.3083e-017
v  ǁVelocityǁ         0.0011758          10.221          5.1764          5.1764
v  Pressure               -54.022          21.044         -5.7726         -5.7726
v  nu_tilda           4.2259e-007       0.0042692      0.00097488      0.00097488
v  TempC                       21          73.311          21.621          21.621
v  TurbVisc           2.8085e-014       0.0050317       0.0011389       0.0011389
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              794:        0.35920E+01

===============================================================


 INSTANT    0.795000000E+03   TIME STEP NUMBER             795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79626E-02 0.87763E+00
   Friction velocity        uk    :  0.79626E-02 0.87763E+00
   Dimensionless distance   yplus :  0.64104E-01 0.70655E+01
   Friction thermal sca.    tstar : -0.70923E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47829E-01 0.52716E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69677E-02      32   0.37240E-03   0.16743E+01 0.83830E+02 
c  Velocity[X]                                      0.10123E+01 
c  Velocity[Y]                                      0.66198E+00 
c  Velocity[Z]                                      0.13030E-29 
c  Pressure     0.11803E-06     425   0.91493E-08   0.12081E+00 0.51209E+03 
c  nu_tilda     0.47769E-05      31   0.77543E-05   0.18147E-06 0.13037E+03 
c  TempC        0.28887E+02      27   0.55563E-03   0.67827E+01 0.24659E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6085          10.224          4.5729          4.5729
v  Velocity[Y]             -3.547          7.0233        0.014636        0.014636
v  Velocity[Z]       -6.9287e-015     8.1066e-015    -1.3063e-017    -1.3063e-017
v  ǁVelocityǁ         0.0015058          10.224          5.1768          5.1768
v  Pressure               -54.049          21.135         -5.7658         -5.7658
v  nu_tilda           4.2255e-007       0.0042692      0.00097552      0.00097552
v  TempC                       21          73.209          21.621          21.621
v  TurbVisc           2.8057e-014       0.0050317       0.0011396       0.0011396
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              795:        0.33200E+01

===============================================================


 INSTANT    0.796000000E+03   TIME STEP NUMBER             796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11520E-01 0.87887E+00
   Friction velocity        uk    :  0.11520E-01 0.87887E+00
   Dimensionless distance   yplus :  0.92743E-01 0.70755E+01
   Friction thermal sca.    tstar : -0.68773E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69197E-01 0.52791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69714E-02      32   0.38199E-03   0.16583E+01 0.83805E+02 
c  Velocity[X]                                      0.98498E+00 
c  Velocity[Y]                                      0.67332E+00 
c  Velocity[Z]                                      0.11669E-29 
c  Pressure     0.89587E-07     378   0.97118E-08   0.92461E-01 0.17998E+03 
c  nu_tilda     0.47785E-05      31   0.14212E-04   0.18143E-06 0.13032E+03 
c  TempC        0.28899E+02      27   0.44806E-03   0.70528E+01 0.27179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6115          10.227          4.5729          4.5729
v  Velocity[Y]             -3.546          7.0283        0.014571        0.014571
v  Velocity[Z]       -6.9287e-015     8.1121e-015    -1.3054e-017    -1.3054e-017
v  ǁVelocityǁ         0.0010609          10.227          5.1772          5.1772
v  Pressure               -54.059          21.133         -5.7753         -5.7753
v  nu_tilda            4.225e-007       0.0042692      0.00097614      0.00097614
v  TempC                       21          73.794          21.622          21.622
v  TurbVisc           2.8045e-014       0.0050317       0.0011403       0.0011403
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              796:        0.31380E+01

===============================================================


 INSTANT    0.797000000E+03   TIME STEP NUMBER             797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66082E-03 0.87860E+00
   Friction velocity        uk    :  0.66082E-03 0.87860E+00
   Dimensionless distance   yplus :  0.53201E-02 0.70733E+01
   Friction thermal sca.    tstar : -0.61898E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39694E-02 0.52775E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69752E-02      32   0.37784E-03   0.17066E+01 0.84295E+02 
c  Velocity[X]                                      0.10361E+01 
c  Velocity[Y]                                      0.67049E+00 
c  Velocity[Z]                                      0.98405E-30 
c  Pressure     0.12830E-06     472   0.97527E-08   0.13365E+00 0.34903E+03 
c  nu_tilda     0.47801E-05      31   0.77473E-05   0.18139E-06 0.13027E+03 
c  TempC        0.28910E+02      27   0.52173E-03   0.67974E+01 0.25445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6143          10.229          4.5729          4.5729
v  Velocity[Y]            -3.5449          7.0063        0.014507        0.014507
v  Velocity[Z]       -6.9287e-015     8.1187e-015    -1.3038e-017    -1.3038e-017
v  ǁVelocityǁ         0.0013749           10.23          5.1776          5.1776
v  Pressure               -54.086           21.05         -5.8036         -5.8036
v  nu_tilda           4.2257e-007       0.0042692      0.00097678      0.00097678
v  TempC                       21          73.088          21.622          21.622
v  TurbVisc           2.8033e-014       0.0050317       0.0011411       0.0011411
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              797:        0.35800E+01

===============================================================


 INSTANT    0.798000000E+03   TIME STEP NUMBER             798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10409E-01 0.87729E+00
   Friction velocity        uk    :  0.10409E-01 0.87729E+00
   Dimensionless distance   yplus :  0.83797E-01 0.70628E+01
   Friction thermal sca.    tstar : -0.57736E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62522E-01 0.52696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69789E-02      32   0.38415E-03   0.16830E+01 0.84162E+02 
c  Velocity[X]                                      0.10207E+01 
c  Velocity[Y]                                      0.66236E+00 
c  Velocity[Z]                                      0.93190E-30 
c  Pressure     0.90438E-07     326   0.89843E-08   0.92914E-01 0.20886E+03 
c  nu_tilda     0.47818E-05      31   0.14224E-04   0.18135E-06 0.13022E+03 
c  TempC        0.28922E+02      27   0.48789E-03   0.58932E+01 0.25919E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.617          10.232          4.5729          4.5729
v  Velocity[Y]            -3.5438          7.0253        0.014441        0.014441
v  Velocity[Z]       -6.9287e-015      8.126e-015    -1.3026e-017    -1.3026e-017
v  ǁVelocityǁ         0.0011655          10.232           5.178           5.178
v  Pressure               -54.102          21.112         -5.8052         -5.8052
v  nu_tilda           4.2272e-007       0.0042692      0.00097739      0.00097739
v  TempC                       21          73.235          21.622          21.622
v  TurbVisc           2.8052e-014       0.0050317       0.0011418       0.0011418
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              798:        0.29120E+01

===============================================================


 INSTANT    0.799000000E+03   TIME STEP NUMBER             799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76990E-02 0.87839E+00
   Friction velocity        uk    :  0.76990E-02 0.87839E+00
   Dimensionless distance   yplus :  0.61982E-01 0.70716E+01
   Friction thermal sca.    tstar : -0.56973E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46246E-01 0.52762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69826E-02      32   0.39756E-03   0.16981E+01 0.84251E+02 
c  Velocity[X]                                      0.10206E+01 
c  Velocity[Y]                                      0.67749E+00 
c  Velocity[Z]                                      0.10085E-29 
c  Pressure     0.11294E-06     458   0.97801E-08   0.11613E+00 0.41685E+03 
c  nu_tilda     0.47834E-05      31   0.77275E-05   0.18131E-06 0.13017E+03 
c  TempC        0.28934E+02      27   0.47632E-03   0.52800E+01 0.22214E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6196          10.235          4.5729          4.5729
v  Velocity[Y]            -3.5426          7.0006        0.014376        0.014376
v  Velocity[Z]       -6.9287e-015     8.1342e-015    -1.3005e-017    -1.3005e-017
v  ǁVelocityǁ          0.001133          10.235          5.1784          5.1784
v  Pressure               -54.126          21.013         -5.8366         -5.8366
v  nu_tilda           4.2301e-007       0.0042692      0.00097804      0.00097804
v  TempC                       21          73.087          21.623          21.623
v  TurbVisc           2.8093e-014       0.0050317       0.0011426       0.0011426
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              799:        0.34660E+01

===============================================================


 INSTANT    0.800000000E+03   TIME STEP NUMBER             800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69761E-02 0.87778E+00
   Friction velocity        uk    :  0.69761E-02 0.87778E+00
   Dimensionless distance   yplus :  0.56162E-01 0.70667E+01
   Friction thermal sca.    tstar : -0.52947E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41903E-01 0.52726E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69863E-02      32   0.32229E-03   0.16987E+01 0.84281E+02 
c  Velocity[X]                                      0.10295E+01 
c  Velocity[Y]                                      0.66924E+00 
c  Velocity[Z]                                      0.12751E-29 
c  Pressure     0.99472E-07     422   0.89353E-08   0.10218E+00 0.34043E+03 
c  nu_tilda     0.47850E-05      31   0.14247E-04   0.18127E-06 0.13012E+03 
c  TempC        0.28946E+02      27   0.53334E-03   0.55373E+01 0.22492E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6222          10.237          4.5729          4.5729
v  Velocity[Y]            -3.5413           7.023         0.01431         0.01431
v  Velocity[Z]       -6.9287e-015     8.1418e-015    -1.2991e-017    -1.2991e-017
v  ǁVelocityǁ         0.0014684          10.238          5.1788          5.1788
v  Pressure               -54.139          21.105         -5.8287         -5.8287
v  nu_tilda           4.2331e-007       0.0042692      0.00097865      0.00097865
v  TempC                       21          73.321          21.623          21.623
v  TurbVisc           2.8168e-014       0.0050317       0.0011433       0.0011433
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              800:        0.33570E+01

===============================================================


 INSTANT    0.801000000E+03   TIME STEP NUMBER             801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11209E-01 0.87894E+00
   Friction velocity        uk    :  0.11209E-01 0.87894E+00
   Dimensionless distance   yplus :  0.90237E-01 0.70761E+01
   Friction thermal sca.    tstar : -0.51369E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67327E-01 0.52796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69901E-02      32   0.37594E-03   0.16517E+01 0.83870E+02 
c  Velocity[X]                                      0.98644E+00 
c  Velocity[Y]                                      0.66530E+00 
c  Velocity[Z]                                      0.10406E-29 
c  Pressure     0.92508E-07     405   0.99738E-08   0.95531E-01 0.21031E+03 
c  nu_tilda     0.47867E-05      31   0.77231E-05   0.18123E-06 0.13007E+03 
c  TempC        0.28958E+02      27   0.43472E-03   0.66825E+01 0.27057E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6246           10.24          4.5729          4.5729
v  Velocity[Y]            -3.5402          7.0332        0.014244        0.014244
v  Velocity[Z]       -6.9287e-015     8.1442e-015    -1.2973e-017    -1.2973e-017
v  ǁVelocityǁ         0.0010745           10.24          5.1792          5.1792
v  Pressure               -54.166          21.109         -5.8406         -5.8406
v  nu_tilda           4.2351e-007       0.0042692      0.00097929      0.00097929
v  TempC                       21          73.156          21.624          21.624
v  TurbVisc           2.8249e-014       0.0050317       0.0011441       0.0011441
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              801:        0.31830E+01

===============================================================


 INSTANT    0.802000000E+03   TIME STEP NUMBER             802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42790E-02 0.87841E+00
   Friction velocity        uk    :  0.42790E-02 0.87841E+00
   Dimensionless distance   yplus :  0.34449E-01 0.70718E+01
   Friction thermal sca.    tstar : -0.51197E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25703E-01 0.52763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69938E-02      32   0.33001E-03   0.16900E+01 0.84254E+02 
c  Velocity[X]                                      0.10113E+01 
c  Velocity[Y]                                      0.67877E+00 
c  Velocity[Z]                                      0.89755E-30 
c  Pressure     0.10573E-06     458   0.93043E-08   0.10962E+00 0.65840E+03 
c  nu_tilda     0.47883E-05      31   0.14240E-04   0.18119E-06 0.13002E+03 
c  TempC        0.28970E+02      27   0.42998E-03   0.49249E+01 0.21588E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.627          10.242          4.5729          4.5729
v  Velocity[Y]             -3.539          7.0012        0.014177        0.014177
v  Velocity[Z]       -6.9287e-015     8.1512e-015    -1.2964e-017    -1.2964e-017
v  ǁVelocityǁ         0.0014077          10.243          5.1796          5.1796
v  Pressure               -54.177           20.98         -5.8754         -5.8754
v  nu_tilda           4.2377e-007       0.0042692       0.0009799       0.0009799
v  TempC                       21          73.361          21.624          21.624
v  TurbVisc           2.8303e-014       0.0050317       0.0011448       0.0011448
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              802:        0.40570E+01

===============================================================


 INSTANT    0.803000000E+03   TIME STEP NUMBER             803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10692E-01 0.87728E+00
   Friction velocity        uk    :  0.10692E-01 0.87728E+00
   Dimensionless distance   yplus :  0.86080E-01 0.70627E+01
   Friction thermal sca.    tstar : -0.53585E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64225E-01 0.52696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69975E-02      32   0.36318E-03   0.16692E+01 0.84046E+02 
c  Velocity[X]                                      0.99646E+00 
c  Velocity[Y]                                      0.67278E+00 
c  Velocity[Z]                                      0.12618E-29 
c  Pressure     0.11255E-06     453   0.97105E-08   0.11602E+00 0.69253E+03 
c  nu_tilda     0.47900E-05      31   0.77143E-05   0.18114E-06 0.12997E+03 
c  TempC        0.28982E+02      27   0.48293E-03   0.49016E+01 0.21253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6295          10.245          4.5729          4.5729
v  Velocity[Y]            -3.5377          7.0219         0.01411         0.01411
v  Velocity[Z]       -7.1848e-015     8.1582e-015    -1.2966e-017    -1.2966e-017
v  ǁVelocityǁ         0.0012006          10.245            5.18            5.18
v  Pressure               -54.197          21.109         -5.8571         -5.8571
v  nu_tilda           4.2403e-007       0.0042692      0.00098055      0.00098055
v  TempC                       21          74.382          21.625          21.625
v  TurbVisc           2.8371e-014       0.0050317       0.0011456       0.0011456
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              803:        0.35130E+01

===============================================================


 INSTANT    0.804000000E+03   TIME STEP NUMBER             804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97126E-02 0.87837E+00
   Friction velocity        uk    :  0.97126E-02 0.87837E+00
   Dimensionless distance   yplus :  0.78193E-01 0.70715E+01
   Friction thermal sca.    tstar : -0.53813E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58341E-01 0.52761E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70012E-02      32   0.42312E-03   0.16976E+01 0.84392E+02 
c  Velocity[X]                                      0.10313E+01 
c  Velocity[Y]                                      0.66622E+00 
c  Velocity[Z]                                      0.12508E-29 
c  Pressure     0.12659E-06     458   0.98721E-08   0.13261E+00 0.66402E+03 
c  nu_tilda     0.47916E-05      31   0.14245E-04   0.18111E-06 0.12992E+03 
c  TempC        0.28994E+02      27   0.45097E-03   0.49903E+01 0.22483E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6317          10.247          4.5729          4.5729
v  Velocity[Y]            -3.5364          7.0022        0.014043        0.014043
v  Velocity[Z]       -6.9287e-015     8.1647e-015    -1.2952e-017    -1.2952e-017
v  ǁVelocityǁ         0.0011264          10.247          5.1804          5.1804
v  Pressure               -54.216          20.992         -5.8963         -5.8963
v  nu_tilda           4.2429e-007       0.0042692      0.00098116      0.00098116
v  TempC                       21          73.085          21.625          21.625
v  TurbVisc           2.8441e-014       0.0050317       0.0011463       0.0011463
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              804:        0.32620E+01

===============================================================


 INSTANT    0.805000000E+03   TIME STEP NUMBER             805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67416E-02 0.87760E+00
   Friction velocity        uk    :  0.67416E-02 0.87760E+00
   Dimensionless distance   yplus :  0.54275E-01 0.70652E+01
   Friction thermal sca.    tstar : -0.57519E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40495E-01 0.52715E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70049E-02      32   0.36718E-03   0.17035E+01 0.84582E+02 
c  Velocity[X]                                      0.10246E+01 
c  Velocity[Y]                                      0.67895E+00 
c  Velocity[Z]                                      0.12151E-29 
c  Pressure     0.10333E-06     421   0.94166E-08   0.10596E+00 0.49390E+03 
c  nu_tilda     0.47932E-05      31   0.76891E-05   0.18107E-06 0.12987E+03 
c  TempC        0.29005E+02      26   0.39967E-03   0.57852E+01 0.25228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6339           10.25          4.5729          4.5729
v  Velocity[Y]             -3.535          7.0255        0.013975        0.013975
v  Velocity[Z]       -6.9287e-015     8.1699e-015    -1.2942e-017    -1.2942e-017
v  ǁVelocityǁ        0.00094782           10.25          5.1808          5.1808
v  Pressure               -54.241          21.084         -5.8902         -5.8902
v  nu_tilda           4.2446e-007       0.0042692      0.00098181      0.00098181
v  TempC                       21          73.645          21.626          21.626
v  TurbVisc           2.8512e-014       0.0050317       0.0011471       0.0011471
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              805:        0.32640E+01

===============================================================


 INSTANT    0.806000000E+03   TIME STEP NUMBER             806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94305E-02 0.87877E+00
   Friction velocity        uk    :  0.94305E-02 0.87877E+00
   Dimensionless distance   yplus :  0.75922E-01 0.70747E+01
   Friction thermal sca.    tstar : -0.58594E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56647E-01 0.52785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70086E-02      32   0.35566E-03   0.16705E+01 0.84116E+02 
c  Velocity[X]                                      0.10001E+01 
c  Velocity[Y]                                      0.67044E+00 
c  Velocity[Z]                                      0.10172E-29 
c  Pressure     0.12492E-06     408   0.97230E-08   0.12615E+00 0.24022E+03 
c  nu_tilda     0.47948E-05      31   0.14271E-04   0.18103E-06 0.12982E+03 
c  TempC        0.29017E+02      27   0.41992E-03   0.50042E+01 0.22087E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6361          10.252          4.5729          4.5729
v  Velocity[Y]            -3.5338          7.0283        0.013907        0.013907
v  Velocity[Z]       -7.7967e-015     8.1775e-015    -1.2941e-017    -1.2941e-017
v  ǁVelocityǁ         0.0010929          10.252          5.1812          5.1812
v  Pressure               -54.251          21.057         -5.9032         -5.9032
v  nu_tilda           4.2466e-007       0.0042692      0.00098242      0.00098242
v  TempC                       21          73.085          21.626          21.626
v  TurbVisc           2.8558e-014       0.0050317       0.0011478       0.0011478
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              806:        0.27590E+01

===============================================================


 INSTANT    0.807000000E+03   TIME STEP NUMBER             807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55055E-02 0.87865E+00
   Friction velocity        uk    :  0.55055E-02 0.87865E+00
   Dimensionless distance   yplus :  0.44323E-01 0.70738E+01
   Friction thermal sca.    tstar : -0.62662E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33070E-01 0.52778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70124E-02      32   0.34921E-03   0.16901E+01 0.84346E+02 
c  Velocity[X]                                      0.10176E+01 
c  Velocity[Y]                                      0.67257E+00 
c  Velocity[Z]                                      0.10631E-29 
c  Pressure     0.11343E-06     472   0.95825E-08   0.11946E+00 0.39449E+03 
c  nu_tilda     0.47965E-05      31   0.76876E-05   0.18099E-06 0.12977E+03 
c  TempC        0.29029E+02      27   0.47820E-03   0.43995E+01 0.20206E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6383          10.254          4.5729          4.5729
v  Velocity[Y]            -3.5324          7.0042         0.01384         0.01384
v  Velocity[Z]       -7.4256e-015     8.1797e-015     -1.293e-017     -1.293e-017
v  ǁVelocityǁ        0.00061209          10.255          5.1816          5.1816
v  Pressure               -54.274          20.971          -5.935          -5.935
v  nu_tilda           4.2494e-007       0.0042692      0.00098306      0.00098306
v  TempC                       21          73.487          21.627          21.627
v  TurbVisc           2.8612e-014       0.0050317       0.0011486       0.0011486
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              807:        0.23050E+01

===============================================================


 INSTANT    0.808000000E+03   TIME STEP NUMBER             808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52265E-02 0.87731E+00
   Friction velocity        uk    :  0.52265E-02 0.87731E+00
   Dimensionless distance   yplus :  0.42077E-01 0.70629E+01
   Friction thermal sca.    tstar : -0.65586E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31394E-01 0.52697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70161E-02      32   0.37719E-03   0.16754E+01 0.84324E+02 
c  Velocity[X]                                      0.99508E+00 
c  Velocity[Y]                                      0.68032E+00 
c  Velocity[Z]                                      0.11117E-29 
c  Pressure     0.81924E-07     424   0.96994E-08   0.84770E-01 0.32003E+03 
c  nu_tilda     0.47981E-05      31   0.14267E-04   0.18096E-06 0.12972E+03 
c  TempC        0.29041E+02      27   0.37266E-03   0.60193E+01 0.22529E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6402          10.257          4.5729          4.5729
v  Velocity[Y]             -3.531          7.0231        0.013771        0.013771
v  Velocity[Z]       -7.2371e-015     8.1814e-015    -1.2923e-017    -1.2923e-017
v  ǁVelocityǁ        0.00091969          10.257           5.182           5.182
v  Pressure               -54.292          21.055         -5.9287         -5.9287
v  nu_tilda           4.2516e-007       0.0042692      0.00098368      0.00098368
v  TempC                       21          73.115          21.627          21.627
v  TurbVisc           2.8685e-014       0.0050317       0.0011493       0.0011493
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              808:        0.23830E+01

===============================================================


 INSTANT    0.809000000E+03   TIME STEP NUMBER             809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90342E-02 0.87840E+00
   Friction velocity        uk    :  0.90342E-02 0.87840E+00
   Dimensionless distance   yplus :  0.72732E-01 0.70718E+01
   Friction thermal sca.    tstar : -0.70539E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54266E-01 0.52763E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70198E-02      32   0.33309E-03   0.16992E+01 0.84541E+02 
c  Velocity[X]                                      0.10207E+01 
c  Velocity[Y]                                      0.67845E+00 
c  Velocity[Z]                                      0.90083E-30 
c  Pressure     0.11033E-06     473   0.90283E-08   0.11413E+00 0.52674E+03 
c  nu_tilda     0.47997E-05      31   0.76921E-05   0.18092E-06 0.12968E+03 
c  TempC        0.29053E+02      28   0.43044E-03   0.40163E+01 0.17922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6422          10.259          4.5729          4.5729
v  Velocity[Y]            -3.5296          7.0004        0.013703        0.013703
v  Velocity[Z]       -7.6181e-015     8.1832e-015     -1.291e-017     -1.291e-017
v  ǁVelocityǁ        0.00061096          10.259          5.1824          5.1824
v  Pressure               -54.315           20.93         -5.9658         -5.9658
v  nu_tilda           4.2536e-007       0.0042692      0.00098432      0.00098432
v  TempC                       21          73.152          21.628          21.628
v  TurbVisc           2.8745e-014       0.0050317       0.0011501       0.0011501
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              809:        0.22240E+01

===============================================================


 INSTANT    0.810000000E+03   TIME STEP NUMBER             810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23326E-02 0.87781E+00
   Friction velocity        uk    :  0.23326E-02 0.87781E+00
   Dimensionless distance   yplus :  0.18779E-01 0.70670E+01
   Friction thermal sca.    tstar : -0.71761E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14011E-01 0.52728E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70235E-02      32   0.36251E-03   0.16738E+01 0.84302E+02 
c  Velocity[X]                                      0.10033E+01 
c  Velocity[Y]                                      0.67054E+00 
c  Velocity[Z]                                      0.11408E-29 
c  Pressure     0.88508E-07     425   0.92274E-08   0.90285E-01 0.35226E+03 
c  nu_tilda     0.48014E-05      31   0.14274E-04   0.18089E-06 0.12963E+03 
c  TempC        0.29065E+02      27   0.47613E-03   0.43184E+01 0.20851E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6442          10.261          4.5729          4.5729
v  Velocity[Y]            -3.5281          7.0219        0.013633        0.013633
v  Velocity[Z]       -8.8714e-015     8.1886e-015    -1.2904e-017    -1.2904e-017
v  ǁVelocityǁ        0.00060991          10.261          5.1828          5.1828
v  Pressure               -54.328          21.023         -5.9567         -5.9567
v  nu_tilda           4.2547e-007       0.0042692      0.00098494      0.00098494
v  TempC                       21          73.453          21.628          21.628
v  TurbVisc             2.88e-014       0.0050317       0.0011508       0.0011508
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              810:        0.20600E+01

===============================================================


 INSTANT    0.811000000E+03   TIME STEP NUMBER             811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37517E-02 0.87920E+00
   Friction velocity        uk    :  0.37517E-02 0.87920E+00
   Dimensionless distance   yplus :  0.30204E-01 0.70781E+01
   Friction thermal sca.    tstar : -0.84251E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22536E-01 0.52811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70272E-02      32   0.34651E-03   0.16680E+01 0.84359E+02 
c  Velocity[X]                                      0.98395E+00 
c  Velocity[Y]                                      0.68403E+00 
c  Velocity[Z]                                      0.12548E-29 
c  Pressure     0.98955E-07     341   0.90394E-08   0.10249E+00 0.26365E+03 
c  nu_tilda     0.48030E-05      31   0.76680E-05   0.18086E-06 0.12959E+03 
c  TempC        0.29076E+02      27   0.39273E-03   0.51897E+01 0.21782E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.646          10.264          4.5729          4.5729
v  Velocity[Y]            -3.5268          7.0321        0.013564        0.013564
v  Velocity[Z]       -8.4832e-015     8.1952e-015    -1.2887e-017    -1.2887e-017
v  ǁVelocityǁ         0.0010134          10.264          5.1832          5.1832
v  Pressure               -54.354          21.053         -5.9637         -5.9637
v  nu_tilda           4.2547e-007       0.0042692      0.00098558      0.00098558
v  TempC                       21          73.083          21.628          21.628
v  TurbVisc            2.883e-014       0.0050317       0.0011516       0.0011516
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              811:        0.18770E+01

===============================================================


 INSTANT    0.812000000E+03   TIME STEP NUMBER             812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72266E-02 0.87865E+00
   Friction velocity        uk    :  0.72266E-02 0.87865E+00
   Dimensionless distance   yplus :  0.58179E-01 0.70737E+01
   Friction thermal sca.    tstar : -0.85404E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43408E-01 0.52778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70309E-02      32   0.36637E-03   0.16986E+01 0.84616E+02 
c  Velocity[X]                                      0.10210E+01 
c  Velocity[Y]                                      0.67764E+00 
c  Velocity[Z]                                      0.99592E-30 
c  Pressure     0.12096E-06     473   0.93365E-08   0.12478E+00 0.82201E+03 
c  nu_tilda     0.48046E-05      31   0.14297E-04   0.18083E-06 0.12954E+03 
c  TempC        0.29088E+02      27   0.34183E-03   0.37466E+01 0.18845E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6478          10.266          4.5729          4.5729
v  Velocity[Y]            -3.5253          7.0015        0.013495        0.013495
v  Velocity[Z]       -9.5109e-015     8.2014e-015    -1.2882e-017    -1.2882e-017
v  ǁVelocityǁ        0.00073931          10.266          5.1835          5.1835
v  Pressure               -54.362          20.889         -6.0063         -6.0063
v  nu_tilda           4.2557e-007       0.0042692      0.00098619      0.00098619
v  TempC                       21          73.083          21.629          21.629
v  TurbVisc            2.883e-014       0.0050317       0.0011523       0.0011523
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              812:        0.22560E+01

===============================================================


 INSTANT    0.813000000E+03   TIME STEP NUMBER             813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76731E-02 0.87765E+00
   Friction velocity        uk    :  0.76731E-02 0.87765E+00
   Dimensionless distance   yplus :  0.61773E-01 0.70657E+01
   Friction thermal sca.    tstar : -0.10515E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46090E-01 0.52718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70345E-02      32   0.40307E-03   0.17060E+01 0.84707E+02 
c  Velocity[X]                                      0.10341E+01 
c  Velocity[Y]                                      0.67184E+00 
c  Velocity[Z]                                      0.13798E-29 
c  Pressure     0.12978E-06     442   0.94264E-08   0.13362E+00 0.77580E+03 
c  nu_tilda     0.48063E-05      31   0.76739E-05   0.18079E-06 0.12950E+03 
c  TempC        0.29100E+02      26   0.39043E-03   0.40073E+01 0.19242E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6497          10.269          4.5729          4.5729
v  Velocity[Y]            -3.5238          7.0235        0.013425        0.013425
v  Velocity[Z]       -1.0515e-014     8.2077e-015    -1.2901e-017    -1.2901e-017
v  ǁVelocityǁ         0.0016402          10.269          5.1839          5.1839
v  Pressure               -54.382          21.033          -5.983          -5.983
v  nu_tilda           4.2568e-007       0.0042692      0.00098684      0.00098684
v  TempC                       21          73.878          21.629          21.629
v  TurbVisc           2.8858e-014       0.0050317       0.0011531       0.0011531
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              813:        0.21220E+01

===============================================================


 INSTANT    0.814000000E+03   TIME STEP NUMBER             814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12468E-01 0.87879E+00
   Friction velocity        uk    :  0.12468E-01 0.87879E+00
   Dimensionless distance   yplus :  0.10038E+00 0.70748E+01
   Friction thermal sca.    tstar : -0.10772E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74892E-01 0.52786E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70382E-02      32   0.36920E-03   0.17133E+01 0.84901E+02 
c  Velocity[X]                                      0.10270E+01 
c  Velocity[Y]                                      0.68629E+00 
c  Velocity[Z]                                      0.12334E-29 
c  Pressure     0.12784E-06     473   0.90631E-08   0.13277E+00 0.72570E+03 
c  nu_tilda     0.48079E-05      31   0.14291E-04   0.18077E-06 0.12945E+03 
c  TempC        0.29112E+02      28   0.50582E-03   0.56477E+01 0.21580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6513          10.271          4.5729          4.5729
v  Velocity[Y]            -3.5222          7.0013        0.013354        0.013354
v  Velocity[Z]       -8.8045e-015     8.2082e-015    -1.2881e-017    -1.2881e-017
v  ǁVelocityǁ         0.0010708          10.271          5.1843          5.1843
v  Pressure               -54.399          20.907         -6.0257         -6.0257
v  nu_tilda           4.2577e-007       0.0042692      0.00098745      0.00098745
v  TempC                       21          73.082           21.63           21.63
v  TurbVisc           2.8886e-014       0.0050317       0.0011538       0.0011538
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              814:        0.22950E+01

===============================================================


 INSTANT    0.815000000E+03   TIME STEP NUMBER             815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42238E-02 0.87808E+00
   Friction velocity        uk    :  0.42238E-02 0.87808E+00
   Dimensionless distance   yplus :  0.34005E-01 0.70691E+01
   Friction thermal sca.    tstar : -0.15164E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25371E-01 0.52743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70419E-02      32   0.35368E-03   0.16807E+01 0.84563E+02 
c  Velocity[X]                                      0.10015E+01 
c  Velocity[Y]                                      0.67921E+00 
c  Velocity[Z]                                      0.12456E-29 
c  Pressure     0.83673E-07     440   0.95089E-08   0.85617E-01 0.58795E+03 
c  nu_tilda     0.48095E-05      31   0.76705E-05   0.18073E-06 0.12941E+03 
c  TempC        0.29124E+02      27   0.39320E-03   0.66769E+01 0.26583E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6529          10.274          4.5729          4.5729
v  Velocity[Y]            -3.5207          7.0279        0.013284        0.013284
v  Velocity[Z]       -1.0237e-014     8.2079e-015    -1.2879e-017    -1.2879e-017
v  ǁVelocityǁ         0.0012605          10.274          5.1847          5.1847
v  Pressure               -54.424          21.015         -6.0134         -6.0134
v  nu_tilda           4.2582e-007       0.0042692       0.0009881       0.0009881
v  TempC                       21           73.35           21.63           21.63
v  TurbVisc           2.8913e-014       0.0050317       0.0011546       0.0011546
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              815:        0.21140E+01

===============================================================


 INSTANT    0.816000000E+03   TIME STEP NUMBER             816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91937E-02 0.87930E+00
   Friction velocity        uk    :  0.91937E-02 0.87930E+00
   Dimensionless distance   yplus :  0.74016E-01 0.70790E+01
   Friction thermal sca.    tstar : -0.17788E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55224E-01 0.52817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70456E-02      32   0.39583E-03   0.16752E+01 0.84469E+02 
c  Velocity[X]                                      0.99773E+00 
c  Velocity[Y]                                      0.67749E+00 
c  Velocity[Z]                                      0.12913E-29 
c  Pressure     0.11036E-06     392   0.98382E-08   0.11309E+00 0.19072E+03 
c  nu_tilda     0.48111E-05      31   0.14296E-04   0.18070E-06 0.12936E+03 
c  TempC        0.29136E+02      26   0.45636E-03   0.38939E+01 0.20996E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6544          10.276          4.5729          4.5729
v  Velocity[Y]            -3.5191          7.0269        0.013214        0.013214
v  Velocity[Z]       -1.1112e-014     8.2129e-015    -1.2892e-017    -1.2892e-017
v  ǁVelocityǁ         0.0013406          10.276          5.1851          5.1851
v  Pressure               -54.433          21.006         -6.0236         -6.0236
v  nu_tilda           4.2581e-007       0.0042692      0.00098871      0.00098871
v  TempC                       21          73.082          21.631          21.631
v  TurbVisc           2.8926e-014       0.0050317       0.0011553       0.0011553
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              816:        0.19640E+01

===============================================================


 INSTANT    0.817000000E+03   TIME STEP NUMBER             817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10106E-01 0.87869E+00
   Friction velocity        uk    :  0.10106E-01 0.87869E+00
   Dimensionless distance   yplus :  0.81364E-01 0.70740E+01
   Friction thermal sca.    tstar : -0.27258E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60706E-01 0.52780E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70493E-02      32   0.38115E-03   0.17054E+01 0.84882E+02 
c  Velocity[X]                                      0.10061E+01 
c  Velocity[Y]                                      0.69929E+00 
c  Velocity[Z]                                      0.98704E-30 
c  Pressure     0.99347E-07     457   0.97457E-08   0.10396E+00 0.46223E+03 
c  nu_tilda     0.48128E-05      31   0.76426E-05   0.18067E-06 0.12932E+03 
c  TempC        0.29147E+02      26   0.45524E-03   0.60397E+01 0.24425E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6559          10.278          4.5729          4.5729
v  Velocity[Y]            -3.5175          7.0018        0.013143        0.013143
v  Velocity[Z]       -1.1154e-014     8.2157e-015    -1.2885e-017    -1.2885e-017
v  ǁVelocityǁ           0.00106          10.279          5.1854          5.1854
v  Pressure               -54.454          20.901         -6.0581         -6.0581
v  nu_tilda            4.258e-007       0.0042692      0.00098936      0.00098936
v  TempC                       21          73.099          21.631          21.631
v  TurbVisc           2.8922e-014       0.0050317       0.0011561       0.0011561
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              817:        0.21070E+01

===============================================================


 INSTANT    0.818000000E+03   TIME STEP NUMBER             818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25002E-02 0.87763E+00
   Friction velocity        uk    :  0.25002E-02 0.87763E+00
   Dimensionless distance   yplus :  0.20129E-01 0.70655E+01
   Friction thermal sca.    tstar : -0.19063E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15018E-01 0.52716E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70530E-02      32   0.33317E-03   0.17202E+01 0.85139E+02 
c  Velocity[X]                                      0.10220E+01 
c  Velocity[Y]                                      0.69826E+00 
c  Velocity[Z]                                      0.87656E-30 
c  Pressure     0.10845E-06     393   0.97382E-08   0.11146E+00 0.27022E+03 
c  nu_tilda     0.48144E-05      31   0.14326E-04   0.18064E-06 0.12928E+03 
c  TempC        0.29159E+02      26   0.41043E-03   0.57416E+01 0.24333E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6573          10.281          4.5729          4.5729
v  Velocity[Y]             -3.516          7.0244        0.013072        0.013072
v  Velocity[Z]       -1.0721e-014     8.2243e-015    -1.2884e-017    -1.2884e-017
v  ǁVelocityǁ         0.0015169          10.281          5.1858          5.1858
v  Pressure               -54.472          20.975          -6.055          -6.055
v  nu_tilda           4.2579e-007       0.0042692      0.00098997      0.00098997
v  TempC                       21          74.001          21.632          21.632
v  TurbVisc           2.8919e-014       0.0050317       0.0011568       0.0011568
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              818:        0.21150E+01

===============================================================


 INSTANT    0.819000000E+03   TIME STEP NUMBER             819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11616E-01 0.87875E+00
   Friction velocity        uk    :  0.11616E-01 0.87875E+00
   Dimensionless distance   yplus :  0.93517E-01 0.70745E+01
   Friction thermal sca.    tstar : -0.16010E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69774E-01 0.52784E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70567E-02      32   0.38641E-03   0.17029E+01 0.84874E+02 
c  Velocity[X]                                      0.10222E+01 
c  Velocity[Y]                                      0.68071E+00 
c  Velocity[Z]                                      0.11458E-29 
c  Pressure     0.11422E-06     457   0.99386E-08   0.11737E+00 0.55068E+03 
c  nu_tilda     0.48160E-05      31   0.76516E-05   0.18061E-06 0.12924E+03 
c  TempC        0.29171E+02      27   0.41984E-03   0.41886E+01 0.21413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6586          10.283          4.5729          4.5729
v  Velocity[Y]            -3.5143          7.0031        0.013001        0.013001
v  Velocity[Z]        -1.175e-014     8.2273e-015    -1.2873e-017    -1.2873e-017
v  ǁVelocityǁ         0.0012031          10.283          5.1862          5.1862
v  Pressure               -54.492          20.844         -6.0928         -6.0928
v  nu_tilda           4.2585e-007       0.0042692      0.00099062      0.00099062
v  TempC                       21          73.081          21.632          21.632
v  TurbVisc           2.8917e-014       0.0050317       0.0011576       0.0011576
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              819:        0.23440E+01

===============================================================


 INSTANT    0.820000000E+03   TIME STEP NUMBER             820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84517E-02 0.87836E+00
   Friction velocity        uk    :  0.84517E-02 0.87836E+00
   Dimensionless distance   yplus :  0.68042E-01 0.70714E+01
   Friction thermal sca.    tstar : -0.11179E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50767E-01 0.52760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70603E-02      32   0.36414E-03   0.17122E+01 0.85095E+02 
c  Velocity[X]                                      0.10105E+01 
c  Velocity[Y]                                      0.70171E+00 
c  Velocity[Z]                                      0.13576E-29 
c  Pressure     0.95107E-07     457   0.93846E-08   0.98166E-01 0.58134E+03 
c  nu_tilda     0.48176E-05      31   0.14320E-04   0.18058E-06 0.12919E+03 
c  TempC        0.29183E+02      27   0.34370E-03   0.51209E+01 0.23187E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.66          10.285          4.5729          4.5729
v  Velocity[Y]            -3.5126          7.0238        0.012929        0.012929
v  Velocity[Z]       -1.2342e-014     8.2349e-015     -1.288e-017     -1.288e-017
v  ǁVelocityǁ         0.0011415          10.285          5.1866          5.1866
v  Pressure               -54.507           20.99         -6.0721         -6.0721
v  nu_tilda           4.2587e-007       0.0042692      0.00099124      0.00099124
v  TempC                       21           73.31          21.633          21.633
v  TurbVisc           2.8932e-014       0.0050317       0.0011583       0.0011583
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              820:        0.23310E+01

===============================================================


 INSTANT    0.821000000E+03   TIME STEP NUMBER             821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32498E-02 0.87948E+00
   Friction velocity        uk    :  0.32498E-02 0.87948E+00
   Dimensionless distance   yplus :  0.26163E-01 0.70804E+01
   Friction thermal sca.    tstar : -0.10920E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19521E-01 0.52828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70640E-02      32   0.36969E-03   0.16830E+01 0.84864E+02 
c  Velocity[X]                                      0.99662E+00 
c  Velocity[Y]                                      0.68640E+00 
c  Velocity[Z]                                      0.10962E-29 
c  Pressure     0.91797E-07     409   0.93945E-08   0.94436E-01 0.19884E+03 
c  nu_tilda     0.48192E-05      31   0.76532E-05   0.18055E-06 0.12915E+03 
c  TempC        0.29194E+02      27   0.55301E-03   0.41062E+01 0.20437E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6612          10.287          4.5729          4.5729
v  Velocity[Y]            -3.5109           7.035        0.012857        0.012857
v  Velocity[Z]        -1.238e-014     8.2358e-015    -1.2863e-017    -1.2863e-017
v  ǁVelocityǁ         0.0016308          10.288          5.1869          5.1869
v  Pressure               -54.529          20.967          -6.089          -6.089
v  nu_tilda           4.2587e-007       0.0042693      0.00099188      0.00099188
v  TempC                       21          73.553          21.633          21.633
v  TurbVisc            2.894e-014       0.0050317       0.0011591       0.0011591
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              821:        0.22300E+01

===============================================================


 INSTANT    0.822000000E+03   TIME STEP NUMBER             822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12433E-01 0.87903E+00
   Friction velocity        uk    :  0.12433E-01 0.87903E+00
   Dimensionless distance   yplus :  0.10010E+00 0.70768E+01
   Friction thermal sca.    tstar : -0.89420E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74684E-01 0.52801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70677E-02      32   0.37400E-03   0.17140E+01 0.85100E+02 
c  Velocity[X]                                      0.10315E+01 
c  Velocity[Y]                                      0.68249E+00 
c  Velocity[Z]                                      0.10796E-29 
c  Pressure     0.12259E-06     457   0.93301E-08   0.12762E+00 0.59452E+03 
c  nu_tilda     0.48209E-05      31   0.14323E-04   0.18052E-06 0.12911E+03 
c  TempC        0.29206E+02      28   0.42092E-03   0.58680E+01 0.23967E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6624          10.289          4.5729          4.5729
v  Velocity[Y]            -3.5093           7.011        0.012785        0.012785
v  Velocity[Z]       -1.2832e-014     8.2408e-015    -1.2869e-017    -1.2869e-017
v  ǁVelocityǁ          0.001075           10.29          5.1873          5.1873
v  Pressure               -54.539          20.854          -6.121          -6.121
v  nu_tilda           4.2595e-007       0.0042693       0.0009925       0.0009925
v  TempC                       21          73.679          21.633          21.633
v  TurbVisc           2.8938e-014       0.0050317       0.0011598       0.0011598
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              822:        0.22950E+01

===============================================================


 INSTANT    0.823000000E+03   TIME STEP NUMBER             823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51357E-02 0.87793E+00
   Friction velocity        uk    :  0.51357E-02 0.87793E+00
   Dimensionless distance   yplus :  0.41346E-01 0.70679E+01
   Friction thermal sca.    tstar : -0.88241E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30849E-01 0.52735E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70713E-02      32   0.33994E-03   0.17158E+01 0.85088E+02 
c  Velocity[X]                                      0.10135E+01 
c  Velocity[Y]                                      0.70224E+00 
c  Velocity[Z]                                      0.15231E-29 
c  Pressure     0.12371E-06     458   0.92540E-08   0.12597E+00 0.68827E+03 
c  nu_tilda     0.48225E-05      31   0.76271E-05   0.18050E-06 0.12907E+03 
c  TempC        0.29218E+02      27   0.39259E-03   0.46309E+01 0.19289E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6636          10.291          4.5729          4.5729
v  Velocity[Y]            -3.5076          7.0254        0.012713        0.012713
v  Velocity[Z]       -1.4046e-014     8.2433e-015     -1.289e-017     -1.289e-017
v  ǁVelocityǁ        0.00095986          10.292          5.1877          5.1877
v  Pressure               -54.555          20.981         -6.1013         -6.1013
v  nu_tilda             4.26e-007       0.0042693      0.00099314      0.00099314
v  TempC                       21          73.081          21.634          21.634
v  TurbVisc           2.8961e-014       0.0050317       0.0011606       0.0011606
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              823:        0.22700E+01

===============================================================


 INSTANT    0.824000000E+03   TIME STEP NUMBER             824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85009E-02 0.87880E+00
   Friction velocity        uk    :  0.85009E-02 0.87880E+00
   Dimensionless distance   yplus :  0.68438E-01 0.70750E+01
   Friction thermal sca.    tstar : -0.80420E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51062E-01 0.52787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70750E-02      32   0.33020E-03   0.16926E+01 0.84927E+02 
c  Velocity[X]                                      0.10045E+01 
c  Velocity[Y]                                      0.68805E+00 
c  Velocity[Z]                                      0.16906E-29 
c  Pressure     0.96801E-07     474   0.94952E-08   0.10107E+00 0.80846E+03 
c  nu_tilda     0.48241E-05      31   0.14352E-04   0.18048E-06 0.12903E+03 
c  TempC        0.29230E+02      27   0.43049E-03   0.32192E+01 0.18112E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6647          10.293          4.5729          4.5729
v  Velocity[Y]            -3.5059          7.0035         0.01264         0.01264
v  Velocity[Z]       -1.2249e-014     8.2414e-015    -1.2862e-017    -1.2862e-017
v  ǁVelocityǁ         0.0013581          10.294           5.188           5.188
v  Pressure               -54.571          20.833         -6.1477         -6.1477
v  nu_tilda           4.2608e-007       0.0042693      0.00099376      0.00099376
v  TempC                       21          73.731          21.634          21.634
v  TurbVisc           2.8974e-014       0.0050317       0.0011613       0.0011613
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              824:        0.21720E+01

===============================================================


 INSTANT    0.825000000E+03   TIME STEP NUMBER             825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10338E-01 0.87817E+00
   Friction velocity        uk    :  0.10338E-01 0.87817E+00
   Dimensionless distance   yplus :  0.83228E-01 0.70699E+01
   Friction thermal sca.    tstar : -0.74442E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62097E-01 0.52749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70786E-02      32   0.35985E-03   0.16895E+01 0.84933E+02 
c  Velocity[X]                                      0.10048E+01 
c  Velocity[Y]                                      0.68475E+00 
c  Velocity[Z]                                      0.12475E-29 
c  Pressure     0.88515E-07     472   0.95746E-08   0.91954E-01 0.75692E+03 
c  nu_tilda     0.48257E-05      31   0.76255E-05   0.18044E-06 0.12899E+03 
c  TempC        0.29242E+02      27   0.39017E-03   0.47818E+01 0.21972E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6657          10.295          4.5729          4.5729
v  Velocity[Y]            -3.5042          7.0301        0.012568        0.012568
v  Velocity[Z]       -1.3158e-014     8.2449e-015    -1.2869e-017    -1.2869e-017
v  ǁVelocityǁ        0.00045181          10.296          5.1884          5.1884
v  Pressure               -54.594          20.982         -6.1268         -6.1268
v  nu_tilda           4.2612e-007       0.0042693      0.00099441      0.00099441
v  TempC                       21          74.013          21.635          21.635
v  TurbVisc           2.8996e-014       0.0050317       0.0011621       0.0011621
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              825:        0.21610E+01

===============================================================


 INSTANT    0.826000000E+03   TIME STEP NUMBER             826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20548E-02 0.87904E+00
   Friction velocity        uk    :  0.20548E-02 0.87904E+00
   Dimensionless distance   yplus :  0.16542E-01 0.70769E+01
   Friction thermal sca.    tstar : -0.69504E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12342E-01 0.52801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70823E-02      32   0.38288E-03   0.17033E+01 0.85177E+02 
c  Velocity[X]                                      0.99632E+00 
c  Velocity[Y]                                      0.70696E+00 
c  Velocity[Z]                                      0.98756E-30 
c  Pressure     0.11567E-06     453   0.93222E-08   0.11791E+00 0.54580E+03 
c  nu_tilda     0.48273E-05      31   0.14340E-04   0.18042E-06 0.12895E+03 
c  TempC        0.29253E+02      27   0.46550E-03   0.44056E+01 0.21272E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6665          10.297          4.5729          4.5729
v  Velocity[Y]            -3.5024          7.0305        0.012495        0.012495
v  Velocity[Z]       -1.3378e-014      8.248e-015    -1.2869e-017    -1.2869e-017
v  ǁVelocityǁ        0.00078562          10.298          5.1888          5.1888
v  Pressure               -54.605          20.888         -6.1583         -6.1583
v  nu_tilda           4.2615e-007       0.0042693      0.00099502      0.00099502
v  TempC                       21           73.27          21.635          21.635
v  TurbVisc           2.9008e-014       0.0050317       0.0011628       0.0011628
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              826:        0.21090E+01

===============================================================


 INSTANT    0.827000000E+03   TIME STEP NUMBER             827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89682E-02 0.87895E+00
   Friction velocity        uk    :  0.89682E-02 0.87895E+00
   Dimensionless distance   yplus :  0.72200E-01 0.70762E+01
   Friction thermal sca.    tstar : -0.66632E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53869E-01 0.52796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70860E-02      32   0.32831E-03   0.17378E+01 0.85467E+02 
c  Velocity[X]                                      0.10430E+01 
c  Velocity[Y]                                      0.69477E+00 
c  Velocity[Z]                                      0.13300E-29 
c  Pressure     0.11749E-06     408   0.94689E-08   0.12361E+00 0.20534E+03 
c  nu_tilda     0.48290E-05      31   0.76383E-05   0.18040E-06 0.12891E+03 
c  TempC        0.29265E+02      26   0.45599E-03   0.54577E+01 0.24803E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6674          10.299          4.5729          4.5729
v  Velocity[Y]            -3.5007           7.006        0.012422        0.012422
v  Velocity[Z]       -1.5493e-014      8.254e-015    -1.2887e-017    -1.2887e-017
v  ǁVelocityǁ        0.00065291            10.3          5.1891          5.1891
v  Pressure               -54.621          20.861         -6.1691         -6.1691
v  nu_tilda           4.2622e-007       0.0042693      0.00099567      0.00099567
v  TempC                       21          73.959          21.636          21.636
v  TurbVisc           2.9013e-014       0.0050318       0.0011636       0.0011636
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              827:        0.20250E+01

===============================================================


 INSTANT    0.828000000E+03   TIME STEP NUMBER             828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84502E-02 0.87767E+00
   Friction velocity        uk    :  0.84502E-02 0.87767E+00
   Dimensionless distance   yplus :  0.68030E-01 0.70658E+01
   Friction thermal sca.    tstar : -0.62811E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50758E-01 0.52719E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70896E-02      32   0.35312E-03   0.16917E+01 0.85058E+02 
c  Velocity[X]                                      0.10063E+01 
c  Velocity[Y]                                      0.68533E+00 
c  Velocity[Z]                                      0.11089E-29 
c  Pressure     0.92946E-07     345   0.99663E-08   0.95588E-01 0.21918E+03 
c  nu_tilda     0.48306E-05      31   0.14350E-04   0.18038E-06 0.12887E+03 
c  TempC        0.29277E+02      26   0.44639E-03   0.65260E+01 0.24583E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6682          10.301          4.5729          4.5729
v  Velocity[Y]            -3.4989          7.0264        0.012349        0.012349
v  Velocity[Z]       -1.3599e-014      8.258e-015    -1.2876e-017    -1.2876e-017
v  ǁVelocityǁ        0.00047288          10.301          5.1895          5.1895
v  Pressure               -54.639          20.925         -6.1702         -6.1702
v  nu_tilda           4.2622e-007       0.0042693      0.00099628      0.00099628
v  TempC                       21           73.08          21.636          21.636
v  TurbVisc           2.9033e-014       0.0050318       0.0011643       0.0011643
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              828:        0.18330E+01

===============================================================


 INSTANT    0.829000000E+03   TIME STEP NUMBER             829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57180E-02 0.87879E+00
   Friction velocity        uk    :  0.57180E-02 0.87879E+00
   Dimensionless distance   yplus :  0.46034E-01 0.70748E+01
   Friction thermal sca.    tstar : -0.63055E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34347E-01 0.52786E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70933E-02      32   0.35799E-03   0.17144E+01 0.85358E+02 
c  Velocity[X]                                      0.10059E+01 
c  Velocity[Y]                                      0.70843E+00 
c  Velocity[Z]                                      0.10622E-29 
c  Pressure     0.10884E-06     426   0.99187E-08   0.11347E+00 0.35372E+03 
c  nu_tilda     0.48322E-05      31   0.76140E-05   0.18036E-06 0.12884E+03 
c  TempC        0.29289E+02      26   0.36742E-03   0.61570E+01 0.23986E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6689          10.303          4.5729          4.5729
v  Velocity[Y]            -3.4972          7.0084        0.012276        0.012276
v  Velocity[Z]       -1.6061e-014     8.2623e-015    -1.2889e-017    -1.2889e-017
v  ǁVelocityǁ         0.0014692          10.303          5.1899          5.1899
v  Pressure               -54.653          20.839         -6.1951         -6.1951
v  nu_tilda           4.2627e-007       0.0042693      0.00099693      0.00099693
v  TempC                       21           73.08          21.637          21.637
v  TurbVisc           2.9034e-014       0.0050318       0.0011651       0.0011651
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              829:        0.23730E+01

===============================================================


 INSTANT    0.830000000E+03   TIME STEP NUMBER             830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72816E-02 0.87818E+00
   Friction velocity        uk    :  0.72816E-02 0.87818E+00
   Dimensionless distance   yplus :  0.58622E-01 0.70699E+01
   Friction thermal sca.    tstar : -0.56975E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43739E-01 0.52750E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70969E-02      32   0.31552E-03   0.17087E+01 0.85244E+02 
c  Velocity[X]                                      0.10143E+01 
c  Velocity[Y]                                      0.69442E+00 
c  Velocity[Z]                                      0.11008E-29 
c  Pressure     0.96709E-07     360   0.97635E-08   0.99021E-01 0.23852E+03 
c  nu_tilda     0.48338E-05      31   0.14375E-04   0.18035E-06 0.12880E+03 
c  TempC        0.29300E+02      27   0.36341E-03   0.48171E+01 0.22653E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6695          10.305          4.5729          4.5729
v  Velocity[Y]            -3.4953          7.0265        0.012202        0.012202
v  Velocity[Z]       -1.4361e-014     8.2641e-015     -1.288e-017     -1.288e-017
v  ǁVelocityǁ         0.0010907          10.305          5.1902          5.1902
v  Pressure               -54.672          20.911         -6.1954         -6.1954
v  nu_tilda           4.2631e-007       0.0042693      0.00099754      0.00099754
v  TempC                       21          74.323          21.637          21.637
v  TurbVisc           2.9048e-014       0.0050318       0.0011659       0.0011659
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              830:        0.20400E+01

===============================================================


 INSTANT    0.831000000E+03   TIME STEP NUMBER             831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62904E-02 0.87928E+00
   Friction velocity        uk    :  0.62904E-02 0.87928E+00
   Dimensionless distance   yplus :  0.50642E-01 0.70788E+01
   Friction thermal sca.    tstar : -0.58116E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37785E-01 0.52816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71006E-02      32   0.40549E-03   0.16726E+01 0.84971E+02 
c  Velocity[X]                                      0.98624E+00 
c  Velocity[Y]                                      0.68634E+00 
c  Velocity[Z]                                      0.13622E-29 
c  Pressure     0.86218E-07     362   0.96989E-08   0.88921E-01 0.20319E+03 
c  nu_tilda     0.48354E-05      31   0.76285E-05   0.18032E-06 0.12876E+03 
c  TempC        0.29312E+02      26   0.49834E-03   0.58767E+01 0.23310E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6702          10.306          4.5729          4.5729
v  Velocity[Y]            -3.4935          7.0356        0.012128        0.012128
v  Velocity[Z]       -1.6886e-014     8.2669e-015    -1.2888e-017    -1.2888e-017
v  ǁVelocityǁ          0.001164          10.307          5.1906          5.1906
v  Pressure               -54.686          20.905         -6.2046         -6.2046
v  nu_tilda           4.2627e-007       0.0042693      0.00099819      0.00099819
v  TempC                       21           73.08          21.638          21.638
v  TurbVisc           2.9057e-014       0.0050318       0.0011666       0.0011666
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              831:        0.18930E+01

===============================================================


 INSTANT    0.832000000E+03   TIME STEP NUMBER             832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80214E-02 0.87897E+00
   Friction velocity        uk    :  0.80214E-02 0.87897E+00
   Dimensionless distance   yplus :  0.64578E-01 0.70763E+01
   Friction thermal sca.    tstar : -0.54288E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48182E-01 0.52797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71042E-02      32   0.34483E-03   0.17421E+01 0.85734E+02 
c  Velocity[X]                                      0.10346E+01 
c  Velocity[Y]                                      0.70756E+00 
c  Velocity[Z]                                      0.11174E-29 
c  Pressure     0.13093E-06     442   0.96362E-08   0.13687E+00 0.55924E+03 
c  nu_tilda     0.48370E-05      31   0.14369E-04   0.18030E-06 0.12872E+03 
c  TempC        0.29324E+02      27   0.41838E-03   0.69547E+01 0.27619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6708          10.308          4.5729          4.5729
v  Velocity[Y]            -3.4916          7.0091        0.012054        0.012054
v  Velocity[Z]        -1.513e-014     8.2682e-015    -1.2876e-017    -1.2876e-017
v  ǁVelocityǁ         0.0014204          10.309          5.1909          5.1909
v  Pressure               -54.701          20.806         -6.2374         -6.2374
v  nu_tilda           4.2632e-007       0.0042693      0.00099881      0.00099881
v  TempC                       21          73.196          21.638          21.638
v  TurbVisc           2.9049e-014       0.0050318       0.0011674       0.0011674
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              832:        0.20830E+01

===============================================================


 INSTANT    0.833000000E+03   TIME STEP NUMBER             833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10970E-01 0.87769E+00
   Friction velocity        uk    :  0.10970E-01 0.87769E+00
   Dimensionless distance   yplus :  0.88312E-01 0.70660E+01
   Friction thermal sca.    tstar : -0.54871E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65891E-01 0.52720E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71079E-02      32   0.33074E-03   0.17004E+01 0.85330E+02 
c  Velocity[X]                                      0.10028E+01 
c  Velocity[Y]                                      0.69762E+00 
c  Velocity[Z]                                      0.10425E-29 
c  Pressure     0.77289E-07     426   0.95583E-08   0.79517E-01 0.54404E+03 
c  nu_tilda     0.48386E-05      31   0.76301E-05   0.18027E-06 0.12869E+03 
c  TempC        0.29336E+02      27   0.53456E-03   0.45065E+01 0.21460E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6714           10.31          4.5729          4.5729
v  Velocity[Y]            -3.4899          7.0306        0.011981        0.011981
v  Velocity[Z]       -1.7908e-014     8.2668e-015    -1.2886e-017    -1.2886e-017
v  ǁVelocityǁ         0.0010486          10.311          5.1913          5.1913
v  Pressure               -54.718          20.902         -6.2255         -6.2255
v  nu_tilda           4.2639e-007       0.0042693      0.00099946      0.00099946
v  TempC                       21          73.433          21.638          21.638
v  TurbVisc            2.906e-014       0.0050318       0.0011681       0.0011681
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              833:        0.20500E+01

===============================================================


 INSTANT    0.834000000E+03   TIME STEP NUMBER             834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42714E-02 0.87873E+00
   Friction velocity        uk    :  0.42714E-02 0.87873E+00
   Dimensionless distance   yplus :  0.34388E-01 0.70744E+01
   Friction thermal sca.    tstar : -0.54395E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25657E-01 0.52783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71115E-02      32   0.39251E-03   0.17121E+01 0.85329E+02 
c  Velocity[X]                                      0.10246E+01 
c  Velocity[Y]                                      0.68752E+00 
c  Velocity[Z]                                      0.98497E-30 
c  Pressure     0.14275E-06     456   0.95896E-08   0.14695E+00 0.56563E+03 
c  nu_tilda     0.48403E-05      31   0.14373E-04   0.18025E-06 0.12865E+03 
c  TempC        0.29347E+02      27   0.45698E-03   0.74358E+01 0.26561E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6719          10.312          4.5729          4.5729
v  Velocity[Y]            -3.4881          7.0044        0.011907        0.011907
v  Velocity[Z]       -1.9037e-014     8.2699e-015    -1.2885e-017    -1.2885e-017
v  ǁVelocityǁ          0.001343          10.313          5.1916          5.1916
v  Pressure                -54.72          20.796         -6.2544         -6.2544
v  nu_tilda           4.2651e-007       0.0042693       0.0010001       0.0010001
v  TempC                       21          73.495          21.639          21.639
v  TurbVisc            2.908e-014       0.0050318       0.0011689       0.0011689
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              834:        0.21240E+01

===============================================================


 INSTANT    0.835000000E+03   TIME STEP NUMBER             835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53739E-02 0.87815E+00
   Friction velocity        uk    :  0.53739E-02 0.87815E+00
   Dimensionless distance   yplus :  0.43263E-01 0.70697E+01
   Friction thermal sca.    tstar : -0.55851E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32279E-01 0.52748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71151E-02      32   0.37190E-03   0.17162E+01 0.85503E+02 
c  Velocity[X]                                      0.10141E+01 
c  Velocity[Y]                                      0.70217E+00 
c  Velocity[Z]                                      0.16784E-29 
c  Pressure     0.10336E-06     425   0.94308E-08   0.10712E+00 0.56026E+03 
c  nu_tilda     0.48419E-05      31   0.75908E-05   0.18024E-06 0.12861E+03 
c  TempC        0.29359E+02      27   0.43216E-03   0.66186E+01 0.25696E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6724          10.314          4.5729          4.5729
v  Velocity[Y]            -3.4862          7.0286        0.011832        0.011832
v  Velocity[Z]       -1.5094e-014     8.2706e-015    -1.2852e-017    -1.2852e-017
v  ǁVelocityǁ         0.0013147          10.315           5.192           5.192
v  Pressure               -54.747          20.906         -6.2453         -6.2453
v  nu_tilda           4.2657e-007       0.0042693       0.0010007       0.0010007
v  TempC                       21          73.079          21.639          21.639
v  TurbVisc           2.9112e-014       0.0050318       0.0011696       0.0011696
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              835:        0.20560E+01

===============================================================


 INSTANT    0.836000000E+03   TIME STEP NUMBER             836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10040E-01 0.87935E+00
   Friction velocity        uk    :  0.10040E-01 0.87935E+00
   Dimensionless distance   yplus :  0.80833E-01 0.70794E+01
   Friction thermal sca.    tstar : -0.54933E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60310E-01 0.52820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71188E-02      32   0.36458E-03   0.17023E+01 0.85532E+02 
c  Velocity[X]                                      0.10042E+01 
c  Velocity[Y]                                      0.69809E+00 
c  Velocity[Z]                                      0.10730E-29 
c  Pressure     0.91807E-07     410   0.94084E-08   0.94367E-01 0.28992E+03 
c  nu_tilda     0.48435E-05      31   0.14396E-04   0.18022E-06 0.12858E+03 
c  TempC        0.29371E+02      26   0.38596E-03   0.51048E+01 0.23913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6727          10.316          4.5729          4.5729
v  Velocity[Y]            -3.4843          7.0365        0.011758        0.011758
v  Velocity[Z]       -1.6826e-014     8.2773e-015    -1.2852e-017    -1.2852e-017
v  ǁVelocityǁ         0.0010558          10.317          5.1924          5.1924
v  Pressure               -54.758          20.876         -6.2637         -6.2637
v  nu_tilda           4.2658e-007       0.0042693       0.0010013       0.0010013
v  TempC                       21          73.552           21.64           21.64
v  TurbVisc           2.9128e-014       0.0050318       0.0011704       0.0011704
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              836:        0.20130E+01

===============================================================


 INSTANT    0.837000000E+03   TIME STEP NUMBER             837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51594E-02 0.87892E+00
   Friction velocity        uk    :  0.51594E-02 0.87892E+00
   Dimensionless distance   yplus :  0.41537E-01 0.70759E+01
   Friction thermal sca.    tstar : -0.54494E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30991E-01 0.52794E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71224E-02      32   0.36094E-03   0.17414E+01 0.85808E+02 
c  Velocity[X]                                      0.10504E+01 
c  Velocity[Y]                                      0.69098E+00 
c  Velocity[Z]                                      0.98070E-30 
c  Pressure     0.12814E-06     457   0.98931E-08   0.13261E+00 0.43608E+03 
c  nu_tilda     0.48451E-05      31   0.76192E-05   0.18020E-06 0.12854E+03 
c  TempC        0.29382E+02      27   0.39265E-03   0.53133E+01 0.23901E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.673          10.318          4.5729          4.5729
v  Velocity[Y]            -3.4823          7.0086        0.011683        0.011683
v  Velocity[Z]       -1.8411e-014     8.2794e-015    -1.2854e-017    -1.2854e-017
v  ǁVelocityǁ         0.0014477          10.319          5.1927          5.1927
v  Pressure               -54.773          20.765         -6.2936         -6.2936
v  nu_tilda           4.2673e-007       0.0042693        0.001002        0.001002
v  TempC                       21          73.078           21.64           21.64
v  TurbVisc           2.9132e-014       0.0050318       0.0011711       0.0011711
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              837:        0.21410E+01

===============================================================


 INSTANT    0.838000000E+03   TIME STEP NUMBER             838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11509E-01 0.87786E+00
   Friction velocity        uk    :  0.11509E-01 0.87786E+00
   Dimensionless distance   yplus :  0.92659E-01 0.70674E+01
   Friction thermal sca.    tstar : -0.55553E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69134E-01 0.52730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71260E-02      32   0.33174E-03   0.17103E+01 0.85567E+02 
c  Velocity[X]                                      0.10076E+01 
c  Velocity[Y]                                      0.70272E+00 
c  Velocity[Z]                                      0.93559E-30 
c  Pressure     0.99222E-07     421   0.91568E-08   0.10252E+00 0.45699E+03 
c  nu_tilda     0.48467E-05      31   0.14397E-04   0.18018E-06 0.12851E+03 
c  TempC        0.29394E+02      27   0.52376E-03   0.57531E+01 0.23574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6732           10.32          4.5729          4.5729
v  Velocity[Y]            -3.4806           7.025        0.011609        0.011609
v  Velocity[Z]        -1.951e-014     8.2854e-015    -1.2852e-017    -1.2852e-017
v  ǁVelocityǁ         0.0011312          10.321          5.1931          5.1931
v  Pressure               -54.784          20.881         -6.2785         -6.2785
v  nu_tilda            4.268e-007       0.0042693       0.0010026       0.0010026
v  TempC                       21          73.078          21.641          21.641
v  TurbVisc           2.9172e-014       0.0050318       0.0011719       0.0011719
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              838:        0.20370E+01

===============================================================


 INSTANT    0.839000000E+03   TIME STEP NUMBER             839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76329E-02 0.87901E+00
   Friction velocity        uk    :  0.76329E-02 0.87901E+00
   Dimensionless distance   yplus :  0.61450E-01 0.70766E+01
   Friction thermal sca.    tstar : -0.55023E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45849E-01 0.52800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71297E-02      32   0.34306E-03   0.17070E+01 0.85544E+02 
c  Velocity[X]                                      0.10089E+01 
c  Velocity[Y]                                      0.69805E+00 
c  Velocity[Z]                                      0.10332E-29 
c  Pressure     0.10522E-06     437   0.96168E-08   0.11067E+00 0.35507E+03 
c  nu_tilda     0.48483E-05      31   0.76067E-05   0.18016E-06 0.12848E+03 
c  TempC        0.29406E+02      26   0.46873E-03   0.68828E+01 0.28748E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6734          10.322          4.5729          4.5729
v  Velocity[Y]            -3.4787          7.0091        0.011534        0.011534
v  Velocity[Z]       -1.8543e-014     8.2854e-015    -1.2837e-017    -1.2837e-017
v  ǁVelocityǁ        0.00046185          10.322          5.1934          5.1934
v  Pressure                 -54.8          20.801          -6.306          -6.306
v  nu_tilda           4.2686e-007       0.0042693       0.0010032       0.0010032
v  TempC                       21           74.43          21.641          21.641
v  TurbVisc           2.9193e-014       0.0050318       0.0011726       0.0011726
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              839:        0.20770E+01

===============================================================


 INSTANT    0.840000000E+03   TIME STEP NUMBER             840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70061E-02 0.87813E+00
   Friction velocity        uk    :  0.70061E-02 0.87813E+00
   Dimensionless distance   yplus :  0.56404E-01 0.70696E+01
   Friction thermal sca.    tstar : -0.55451E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42084E-01 0.52747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71333E-02      32   0.40585E-03   0.17034E+01 0.85549E+02 
c  Velocity[X]                                      0.10106E+01 
c  Velocity[Y]                                      0.69283E+00 
c  Velocity[Z]                                      0.11956E-29 
c  Pressure     0.89416E-07     362   0.92418E-08   0.92093E-01 0.21870E+03 
c  nu_tilda     0.48499E-05      31   0.14397E-04   0.18015E-06 0.12844E+03 
c  TempC        0.29418E+02      27   0.45685E-03   0.55191E+01 0.23732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6735          10.324          4.5729          4.5729
v  Velocity[Y]            -3.4768          7.0322         0.01146         0.01146
v  Velocity[Z]       -1.9118e-014     8.2893e-015    -1.2831e-017    -1.2831e-017
v  ǁVelocityǁ        0.00057976          10.324          5.1938          5.1938
v  Pressure               -54.811          20.858         -6.3046         -6.3046
v  nu_tilda           4.2694e-007       0.0042693       0.0010039       0.0010039
v  TempC                       21          73.078          21.641          21.641
v  TurbVisc           2.9207e-014       0.0050318       0.0011734       0.0011734
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              840:        0.19000E+01

===============================================================


 INSTANT    0.841000000E+03   TIME STEP NUMBER             841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77315E-02 0.87939E+00
   Friction velocity        uk    :  0.77315E-02 0.87939E+00
   Dimensionless distance   yplus :  0.62244E-01 0.70797E+01
   Friction thermal sca.    tstar : -0.54870E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46441E-01 0.52822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71369E-02      32   0.36552E-03   0.17381E+01 0.85876E+02 
c  Velocity[X]                                      0.10262E+01 
c  Velocity[Y]                                      0.71185E+00 
c  Velocity[Z]                                      0.11280E-29 
c  Pressure     0.13019E-06     408   0.94292E-08   0.13108E+00 0.19597E+03 
c  nu_tilda     0.48515E-05      31   0.75898E-05   0.18014E-06 0.12841E+03 
c  TempC        0.29429E+02      26   0.34453E-03   0.60929E+01 0.24266E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6735          10.325          4.5729          4.5729
v  Velocity[Y]            -3.4749          7.0358        0.011385        0.011385
v  Velocity[Z]       -1.8772e-014     8.2887e-015    -1.2816e-017    -1.2816e-017
v  ǁVelocityǁ        0.00078242          10.326          5.1941          5.1941
v  Pressure               -54.829          20.832         -6.3211         -6.3211
v  nu_tilda             4.27e-007       0.0042693       0.0010045       0.0010045
v  TempC                       21          73.299          21.642          21.642
v  TurbVisc           2.9229e-014       0.0050318       0.0011741       0.0011741
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              841:        0.21820E+01

===============================================================


 INSTANT    0.842000000E+03   TIME STEP NUMBER             842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57027E-02 0.87931E+00
   Friction velocity        uk    :  0.57027E-02 0.87931E+00
   Dimensionless distance   yplus :  0.45911E-01 0.70791E+01
   Friction thermal sca.    tstar : -0.54990E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34255E-01 0.52818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71405E-02      32   0.31197E-03   0.17439E+01 0.86008E+02 
c  Velocity[X]                                      0.10408E+01 
c  Velocity[Y]                                      0.70304E+00 
c  Velocity[Z]                                      0.89868E-30 
c  Pressure     0.10569E-06     409   0.97244E-08   0.11132E+00 0.39862E+03 
c  nu_tilda     0.48531E-05      31   0.14428E-04   0.18014E-06 0.12838E+03 
c  TempC        0.29441E+02      27   0.36050E-03   0.43495E+01 0.21193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6735          10.327          4.5729          4.5729
v  Velocity[Y]            -3.4729          7.0099         0.01131         0.01131
v  Velocity[Z]        -1.966e-014     8.2923e-015    -1.2814e-017    -1.2814e-017
v  ǁVelocityǁ        0.00061036          10.328          5.1944          5.1944
v  Pressure               -54.836          20.766         -6.3436         -6.3436
v  nu_tilda           4.2708e-007       0.0042693       0.0010051       0.0010051
v  TempC                       21          73.218          21.642          21.642
v  TurbVisc           2.9246e-014       0.0050318       0.0011749       0.0011749
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              842:        0.20190E+01

===============================================================


 INSTANT    0.843000000E+03   TIME STEP NUMBER             843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81704E-02 0.87799E+00
   Friction velocity        uk    :  0.81704E-02 0.87799E+00
   Dimensionless distance   yplus :  0.65777E-01 0.70684E+01
   Friction thermal sca.    tstar : -0.56194E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49077E-01 0.52738E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71441E-02      32   0.36007E-03   0.16966E+01 0.85588E+02 
c  Velocity[X]                                      0.10024E+01 
c  Velocity[Y]                                      0.69418E+00 
c  Velocity[Z]                                      0.81435E-30 
c  Pressure     0.81124E-07     409   0.93972E-08   0.83718E-01 0.53773E+03 
c  nu_tilda     0.48547E-05      31   0.76051E-05   0.18012E-06 0.12834E+03 
c  TempC        0.29453E+02      27   0.55041E-03   0.52978E+01 0.22903E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6735          10.329          4.5729          4.5729
v  Velocity[Y]            -3.4709          7.0325        0.011235        0.011235
v  Velocity[Z]       -1.9656e-014     8.2913e-015    -1.2803e-017    -1.2803e-017
v  ǁVelocityǁ         0.0013693          10.329          5.1948          5.1948
v  Pressure               -54.857          20.868         -6.3337         -6.3337
v  nu_tilda           4.2709e-007       0.0042693       0.0010058       0.0010058
v  TempC                       21          73.815          21.643          21.643
v  TurbVisc           2.9269e-014       0.0050318       0.0011756       0.0011756
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              843:        0.19960E+01

===============================================================


 INSTANT    0.844000000E+03   TIME STEP NUMBER             844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10652E-01 0.87894E+00
   Friction velocity        uk    :  0.10652E-01 0.87894E+00
   Dimensionless distance   yplus :  0.85759E-01 0.70761E+01
   Friction thermal sca.    tstar : -0.55318E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63986E-01 0.52795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71477E-02      32   0.38114E-03   0.17210E+01 0.85843E+02 
c  Velocity[X]                                      0.10137E+01 
c  Velocity[Y]                                      0.70733E+00 
c  Velocity[Z]                                      0.12516E-29 
c  Pressure     0.11480E-06     473   0.92774E-08   0.11938E+00 0.74626E+03 
c  nu_tilda     0.48563E-05      31   0.14417E-04   0.18011E-06 0.12831E+03 
c  TempC        0.29464E+02      27   0.35744E-03   0.84523E+01 0.29999E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6734           10.33          4.5729          4.5729
v  Velocity[Y]            -3.4692          7.0048         0.01116         0.01116
v  Velocity[Z]       -2.0835e-014     8.2897e-015    -1.2799e-017    -1.2799e-017
v  ǁVelocityǁ         0.0010248          10.331          5.1951          5.1951
v  Pressure               -54.862          20.723         -6.3733         -6.3733
v  nu_tilda           4.2712e-007       0.0042693       0.0010064       0.0010064
v  TempC                       21          73.078          21.643          21.643
v  TurbVisc            2.927e-014       0.0050318       0.0011764       0.0011764
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              844:        0.21420E+01

===============================================================


 INSTANT    0.845000000E+03   TIME STEP NUMBER             845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35742E-02 0.87824E+00
   Friction velocity        uk    :  0.35742E-02 0.87824E+00
   Dimensionless distance   yplus :  0.28775E-01 0.70704E+01
   Friction thermal sca.    tstar : -0.56096E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21469E-01 0.52753E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71513E-02      32   0.36797E-03   0.17139E+01 0.85767E+02 
c  Velocity[X]                                      0.10123E+01 
c  Velocity[Y]                                      0.70163E+00 
c  Velocity[Z]                                      0.12464E-29 
c  Pressure     0.11038E-06     472   0.98269E-08   0.11308E+00 0.77789E+03 
c  nu_tilda     0.48580E-05      31   0.76091E-05   0.18009E-06 0.12828E+03 
c  TempC        0.29476E+02      27   0.33137E-03   0.43958E+01 0.20299E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6735          10.332          4.5729          4.5729
v  Velocity[Y]            -3.4672          7.0294        0.011085        0.011085
v  Velocity[Z]       -2.1456e-014     8.2929e-015    -1.2785e-017    -1.2785e-017
v  ǁVelocityǁ         0.0013567          10.332          5.1955          5.1955
v  Pressure               -54.873          20.864         -6.3468         -6.3468
v  nu_tilda           4.2719e-007       0.0042693        0.001007        0.001007
v  TempC                       21          73.193          21.644          21.644
v  TurbVisc            2.928e-014       0.0050318       0.0011771       0.0011771
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              845:        0.21570E+01

===============================================================


 INSTANT    0.846000000E+03   TIME STEP NUMBER             846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10551E-01 0.87961E+00
   Friction velocity        uk    :  0.10551E-01 0.87961E+00
   Dimensionless distance   yplus :  0.84947E-01 0.70814E+01
   Friction thermal sca.    tstar : -0.55404E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63380E-01 0.52836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71550E-02      32   0.37057E-03   0.17170E+01 0.85881E+02 
c  Velocity[X]                                      0.10217E+01 
c  Velocity[Y]                                      0.69529E+00 
c  Velocity[Z]                                      0.12099E-29 
c  Pressure     0.11288E-06     425   0.95749E-08   0.11676E+00 0.32390E+03 
c  nu_tilda     0.48596E-05      31   0.14419E-04   0.18008E-06 0.12825E+03 
c  TempC        0.29488E+02      27   0.45697E-03   0.37085E+01 0.17759E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6733          10.333          4.5729          4.5729
v  Velocity[Y]            -3.4653          7.0386         0.01101         0.01101
v  Velocity[Z]       -1.8399e-014     8.2944e-015    -1.2748e-017    -1.2748e-017
v  ǁVelocityǁ         0.0011638          10.334          5.1958          5.1958
v  Pressure                -54.89          20.838         -6.3704         -6.3704
v  nu_tilda            4.272e-007       0.0042693       0.0010077       0.0010077
v  TempC                       21           73.67          21.644          21.644
v  TurbVisc           2.9299e-014       0.0050318       0.0011779       0.0011779
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              846:        0.20450E+01

===============================================================


 INSTANT    0.847000000E+03   TIME STEP NUMBER             847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84076E-02 0.87917E+00
   Friction velocity        uk    :  0.84076E-02 0.87917E+00
   Dimensionless distance   yplus :  0.67687E-01 0.70779E+01
   Friction thermal sca.    tstar : -0.57239E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50502E-01 0.52809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71586E-02      32   0.33899E-03   0.17478E+01 0.86180E+02 
c  Velocity[X]                                      0.10362E+01 
c  Velocity[Y]                                      0.71163E+00 
c  Velocity[Z]                                      0.99046E-30 
c  Pressure     0.11649E-06     457   0.99961E-08   0.12043E+00 0.45149E+03 
c  nu_tilda     0.48612E-05      31   0.75861E-05   0.18007E-06 0.12822E+03 
c  TempC        0.29499E+02      27   0.45663E-03   0.53750E+01 0.22243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6731          10.335          4.5729          4.5729
v  Velocity[Y]            -3.4634          7.0079        0.010935        0.010935
v  Velocity[Z]        -2.022e-014     8.2985e-015    -1.2744e-017    -1.2744e-017
v  ǁVelocityǁ         0.0010544          10.335          5.1962          5.1962
v  Pressure               -54.901           20.72         -6.3999         -6.3999
v  nu_tilda           4.2729e-007       0.0042693       0.0010083       0.0010083
v  TempC                       21          73.342          21.645          21.645
v  TurbVisc           2.9303e-014       0.0050318       0.0011787       0.0011787
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              847:        0.21250E+01

===============================================================


 INSTANT    0.848000000E+03   TIME STEP NUMBER             848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59767E-02 0.87810E+00
   Friction velocity        uk    :  0.59767E-02 0.87810E+00
   Dimensionless distance   yplus :  0.48116E-01 0.70693E+01
   Friction thermal sca.    tstar : -0.56304E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35900E-01 0.52745E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71622E-02      32   0.31903E-03   0.17136E+01 0.85892E+02 
c  Velocity[X]                                      0.10113E+01 
c  Velocity[Y]                                      0.70231E+00 
c  Velocity[Z]                                      0.98568E-30 
c  Pressure     0.87294E-07     409   0.99167E-08   0.90430E-01 0.33379E+03 
c  nu_tilda     0.48628E-05      31   0.14454E-04   0.18007E-06 0.12819E+03 
c  TempC        0.29511E+02      27   0.36751E-03   0.56057E+01 0.23703E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6728          10.336          4.5729          4.5729
v  Velocity[Y]            -3.4614          7.0277        0.010859        0.010859
v  Velocity[Z]       -2.0473e-014     8.3008e-015    -1.2732e-017    -1.2732e-017
v  ǁVelocityǁ          0.001586          10.337          5.1965          5.1965
v  Pressure               -54.914          20.813         -6.3932         -6.3932
v  nu_tilda           4.2732e-007       0.0042693       0.0010089       0.0010089
v  TempC                       21          73.163          21.645          21.645
v  TurbVisc           2.9325e-014       0.0050318       0.0011794       0.0011794
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              848:        0.20060E+01

===============================================================


 INSTANT    0.849000000E+03   TIME STEP NUMBER             849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24055E-02 0.87927E+00
   Friction velocity        uk    :  0.24055E-02 0.87927E+00
   Dimensionless distance   yplus :  0.19366E-01 0.70787E+01
   Friction thermal sca.    tstar : -0.58406E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14449E-01 0.52815E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71658E-02      32   0.40209E-03   0.17180E+01 0.85955E+02 
c  Velocity[X]                                      0.10167E+01 
c  Velocity[Y]                                      0.70137E+00 
c  Velocity[Z]                                      0.11802E-29 
c  Pressure     0.12851E-06     421   0.91996E-08   0.13341E+00 0.28407E+03 
c  nu_tilda     0.48644E-05      31   0.75992E-05   0.18005E-06 0.12816E+03 
c  TempC        0.29523E+02      27   0.49348E-03   0.50551E+01 0.23060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6725          10.338          4.5729          4.5729
v  Velocity[Y]            -3.4595          7.0101        0.010785        0.010785
v  Velocity[Z]       -2.1593e-014     8.3047e-015    -1.2723e-017    -1.2723e-017
v  ǁVelocityǁ          0.001078          10.338          5.1968          5.1968
v  Pressure               -54.918          20.748         -6.4124         -6.4124
v  nu_tilda           4.2735e-007       0.0042693       0.0010096       0.0010096
v  TempC                       21          73.566          21.645          21.645
v  TurbVisc           2.9335e-014       0.0050318       0.0011802       0.0011802
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              849:        0.20410E+01

===============================================================


 INSTANT    0.850000000E+03   TIME STEP NUMBER             850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68355E-02 0.87847E+00
   Friction velocity        uk    :  0.68355E-02 0.87847E+00
   Dimensionless distance   yplus :  0.55031E-01 0.70723E+01
   Friction thermal sca.    tstar : -0.61179E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41059E-01 0.52767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71694E-02      32   0.38476E-03   0.17607E+01 0.86469E+02 
c  Velocity[X]                                      0.10453E+01 
c  Velocity[Y]                                      0.71539E+00 
c  Velocity[Z]                                      0.10604E-29 
c  Pressure     0.12124E-06     329   0.97827E-08   0.12460E+00 0.18790E+03 
c  nu_tilda     0.48660E-05      31   0.14443E-04   0.18004E-06 0.12813E+03 
c  TempC        0.29534E+02      26   0.44155E-03   0.67776E+01 0.26908E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.672          10.339          4.5729          4.5729
v  Velocity[Y]            -3.4575          7.0336        0.010709        0.010709
v  Velocity[Z]       -1.9735e-014     8.3058e-015    -1.2694e-017    -1.2694e-017
v  ǁVelocityǁ         0.0011994           10.34          5.1972          5.1972
v  Pressure               -54.938          20.801         -6.4175         -6.4175
v  nu_tilda           4.2735e-007       0.0042693       0.0010102       0.0010102
v  TempC                       21          73.077          21.646          21.646
v  TurbVisc           2.9342e-014       0.0050318       0.0011809       0.0011809
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              850:        0.18050E+01

===============================================================


 INSTANT    0.851000000E+03   TIME STEP NUMBER             851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89706E-02 0.87977E+00
   Friction velocity        uk    :  0.89706E-02 0.87977E+00
   Dimensionless distance   yplus :  0.72220E-01 0.70827E+01
   Friction thermal sca.    tstar : -0.64356E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53884E-01 0.52845E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71729E-02      32   0.32735E-03   0.17523E+01 0.86353E+02 
c  Velocity[X]                                      0.10449E+01 
c  Velocity[Y]                                      0.70744E+00 
c  Velocity[Z]                                      0.98296E-30 
c  Pressure     0.12200E-06     346   0.93667E-08   0.12366E+00 0.20723E+03 
c  nu_tilda     0.48676E-05      31   0.76060E-05   0.18003E-06 0.12810E+03 
c  TempC        0.29546E+02      27   0.38713E-03   0.55311E+01 0.23017E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6715           10.34          4.5729          4.5729
v  Velocity[Y]            -3.4556          7.0329        0.010634        0.010634
v  Velocity[Z]       -2.2395e-014     8.3077e-015    -1.2692e-017    -1.2692e-017
v  ǁVelocityǁ         0.0012362          10.341          5.1975          5.1975
v  Pressure               -54.948          20.803         -6.4245         -6.4245
v  nu_tilda           4.2738e-007       0.0042693       0.0010108       0.0010108
v  TempC                       21          73.762          21.646          21.646
v  TurbVisc           2.9344e-014       0.0050318       0.0011817       0.0011817
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              851:        0.18490E+01

===============================================================


 INSTANT    0.852000000E+03   TIME STEP NUMBER             852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11199E-01 0.87934E+00
   Friction velocity        uk    :  0.11199E-01 0.87934E+00
   Dimensionless distance   yplus :  0.90162E-01 0.70793E+01
   Friction thermal sca.    tstar : -0.66725E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67271E-01 0.52819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71765E-02      32   0.34513E-03   0.17327E+01 0.86162E+02 
c  Velocity[X]                                      0.10291E+01 
c  Velocity[Y]                                      0.70361E+00 
c  Velocity[Z]                                      0.96859E-30 
c  Pressure     0.10598E-06     441   0.96452E-08   0.11124E+00 0.47773E+03 
c  nu_tilda     0.48692E-05      31   0.14449E-04   0.18002E-06 0.12807E+03 
c  TempC        0.29558E+02      27   0.46525E-03   0.57145E+01 0.22017E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.671          10.342          4.5729          4.5729
v  Velocity[Y]            -3.4537          7.0089        0.010559        0.010559
v  Velocity[Z]       -2.3412e-014     8.3083e-015    -1.2682e-017    -1.2682e-017
v  ǁVelocityǁ         0.0010059          10.342          5.1979          5.1979
v  Pressure               -54.952          20.713           -6.45           -6.45
v  nu_tilda           4.2747e-007       0.0042693       0.0010115       0.0010115
v  TempC                       21          73.077          21.647          21.647
v  TurbVisc           2.9351e-014       0.0050318       0.0011824       0.0011824
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              852:        0.20750E+01

===============================================================


 INSTANT    0.853000000E+03   TIME STEP NUMBER             853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16882E-02 0.87831E+00
   Friction velocity        uk    :  0.16882E-02 0.87831E+00
   Dimensionless distance   yplus :  0.13592E-01 0.70710E+01
   Friction thermal sca.    tstar : -0.68897E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10141E-01 0.52757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71801E-02      32   0.37495E-03   0.17293E+01 0.86281E+02 
c  Velocity[X]                                      0.10099E+01 
c  Velocity[Y]                                      0.71943E+00 
c  Velocity[Z]                                      0.11820E-29 
c  Pressure     0.85216E-07     441   0.97378E-08   0.87025E-01 0.56635E+03 
c  nu_tilda     0.48708E-05      31   0.75737E-05   0.18002E-06 0.12804E+03 
c  TempC        0.29569E+02      27   0.36735E-03   0.67623E+01 0.25725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6704          10.343          4.5729          4.5729
v  Velocity[Y]            -3.4517          7.0315        0.010484        0.010484
v  Velocity[Z]       -2.3083e-014      8.309e-015     -1.266e-017     -1.266e-017
v  ǁVelocityǁ        0.00010978          10.344          5.1982          5.1982
v  Pressure               -54.969          20.818          -6.437          -6.437
v  nu_tilda            4.275e-007       0.0042693       0.0010121       0.0010121
v  TempC                       21          73.411          21.647          21.647
v  TurbVisc           2.9375e-014       0.0050318       0.0011832       0.0011832
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              853:        0.20740E+01

===============================================================


 INSTANT    0.854000000E+03   TIME STEP NUMBER             854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28373E-02 0.87948E+00
   Friction velocity        uk    :  0.28373E-02 0.87948E+00
   Dimensionless distance   yplus :  0.22842E-01 0.70805E+01
   Friction thermal sca.    tstar : -0.66856E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17043E-01 0.52828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71837E-02      32   0.36904E-03   0.17605E+01 0.86627E+02 
c  Velocity[X]                                      0.10356E+01 
c  Velocity[Y]                                      0.72490E+00 
c  Velocity[Z]                                      0.11922E-29 
c  Pressure     0.12985E-06     469   0.99308E-08   0.13424E+00 0.66178E+03 
c  nu_tilda     0.48724E-05      31   0.14473E-04   0.18002E-06 0.12801E+03 
c  TempC        0.29581E+02      26   0.33894E-03   0.47546E+01 0.21902E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6698          10.344          4.5729          4.5729
v  Velocity[Y]            -3.4498          7.0121        0.010409        0.010409
v  Velocity[Z]       -2.2805e-014     8.3099e-015    -1.2638e-017    -1.2638e-017
v  ǁVelocityǁ        0.00017712          10.345          5.1985          5.1985
v  Pressure               -54.972          20.698         -6.4735         -6.4735
v  nu_tilda           4.2755e-007       0.0042693       0.0010127       0.0010127
v  TempC                       21          73.225          21.648          21.648
v  TurbVisc           2.9384e-014       0.0050318       0.0011839       0.0011839
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              854:        0.21340E+01

===============================================================


 INSTANT    0.855000000E+03   TIME STEP NUMBER             855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25036E-02 0.87885E+00
   Friction velocity        uk    :  0.25036E-02 0.87885E+00
   Dimensionless distance   yplus :  0.20156E-01 0.70754E+01
   Friction thermal sca.    tstar : -0.79628E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15039E-01 0.52790E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71873E-02      32   0.35782E-03   0.17347E+01 0.86267E+02 
c  Velocity[X]                                      0.10290E+01 
c  Velocity[Y]                                      0.70573E+00 
c  Velocity[Z]                                      0.10418E-29 
c  Pressure     0.89794E-07     425   0.93021E-08   0.91708E-01 0.54491E+03 
c  nu_tilda     0.48740E-05      31   0.75703E-05   0.18001E-06 0.12798E+03 
c  TempC        0.29593E+02      27   0.54377E-03   0.48772E+01 0.22725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6692          10.346          4.5729          4.5729
v  Velocity[Y]            -3.4479           7.034        0.010334        0.010334
v  Velocity[Z]        -2.271e-014     8.3104e-015     -1.262e-017     -1.262e-017
v  ǁVelocityǁ         0.0010195          10.346          5.1989          5.1989
v  Pressure               -54.989          20.797         -6.4615         -6.4615
v  nu_tilda           4.2757e-007       0.0042693       0.0010134       0.0010134
v  TempC                       21          73.433          21.648          21.648
v  TurbVisc           2.9397e-014       0.0050318       0.0011847       0.0011847
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              855:        0.20490E+01

===============================================================


 INSTANT    0.856000000E+03   TIME STEP NUMBER             856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49051E-02 0.87997E+00
   Friction velocity        uk    :  0.49051E-02 0.87997E+00
   Dimensionless distance   yplus :  0.39490E-01 0.70844E+01
   Friction thermal sca.    tstar : -0.78574E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29464E-01 0.52857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71909E-02      32   0.34446E-03   0.17283E+01 0.86395E+02 
c  Velocity[X]                                      0.10016E+01 
c  Velocity[Y]                                      0.72673E+00 
c  Velocity[Z]                                      0.11030E-29 
c  Pressure     0.75979E-07     394   0.95245E-08   0.78160E-01 0.21143E+03 
c  nu_tilda     0.48756E-05      31   0.14466E-04   0.18001E-06 0.12796E+03 
c  TempC        0.29604E+02      26   0.38824E-03   0.98814E+01 0.32456E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6687          10.347          4.5729          4.5729
v  Velocity[Y]             -3.446          7.0384        0.010259        0.010259
v  Velocity[Z]       -2.3306e-014     8.3104e-015    -1.2606e-017    -1.2606e-017
v  ǁVelocityǁ         0.0013536          10.348          5.1992          5.1992
v  Pressure               -54.996          20.788         -6.4749         -6.4749
v  nu_tilda           4.2756e-007       0.0042693        0.001014        0.001014
v  TempC                       21          73.365          21.648          21.648
v  TurbVisc           2.9404e-014       0.0050318       0.0011854       0.0011854
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              856:        0.19790E+01

===============================================================


 INSTANT    0.857000000E+03   TIME STEP NUMBER             857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12159E-01 0.87962E+00
   Friction velocity        uk    :  0.12159E-01 0.87962E+00
   Dimensionless distance   yplus :  0.97886E-01 0.70816E+01
   Friction thermal sca.    tstar : -0.91925E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73034E-01 0.52836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71945E-02      32   0.30948E-03   0.17441E+01 0.86473E+02 
c  Velocity[X]                                      0.10312E+01 
c  Velocity[Y]                                      0.71285E+00 
c  Velocity[Z]                                      0.94461E-30 
c  Pressure     0.13134E-06     393   0.90830E-08   0.13750E+00 0.22208E+03 
c  nu_tilda     0.48772E-05      31   0.75799E-05   0.18000E-06 0.12793E+03 
c  TempC        0.29616E+02      27   0.44256E-03   0.55170E+01 0.23217E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6682          10.349          4.5729          4.5729
v  Velocity[Y]             -3.444           7.016        0.010185        0.010185
v  Velocity[Z]       -2.3703e-014     8.3124e-015    -1.2589e-017    -1.2589e-017
v  ǁVelocityǁ         0.0011111          10.349          5.1995          5.1995
v  Pressure               -54.999          20.746         -6.4842         -6.4842
v  nu_tilda           4.2763e-007       0.0042693       0.0010146       0.0010146
v  TempC                       21          73.346          21.649          21.649
v  TurbVisc             2.94e-014       0.0050318       0.0011862       0.0011862
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              857:        0.19670E+01

===============================================================


 INSTANT    0.858000000E+03   TIME STEP NUMBER             858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78116E-02 0.87813E+00
   Friction velocity        uk    :  0.78116E-02 0.87813E+00
   Dimensionless distance   yplus :  0.62889E-01 0.70695E+01
   Friction thermal sca.    tstar : -0.86916E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46922E-01 0.52747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71980E-02      32   0.42174E-03   0.17127E+01 0.86210E+02 
c  Velocity[X]                                      0.10083E+01 
c  Velocity[Y]                                      0.70437E+00 
c  Velocity[Z]                                      0.11239E-29 
c  Pressure     0.95998E-07     378   0.92331E-08   0.99144E-01 0.16143E+03 
c  nu_tilda     0.48788E-05      31   0.14472E-04   0.18000E-06 0.12790E+03 
c  TempC        0.29627E+02      27   0.44043E-03   0.56498E+01 0.24328E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6675           10.35          4.5729          4.5729
v  Velocity[Y]            -3.4421          7.0352         0.01011         0.01011
v  Velocity[Z]       -2.1835e-014     8.3119e-015     -1.256e-017     -1.256e-017
v  ǁVelocityǁ         0.0011379          10.351          5.1999          5.1999
v  Pressure               -55.016          20.777         -6.4957         -6.4957
v  nu_tilda           4.2768e-007       0.0042693       0.0010153       0.0010153
v  TempC                       21          73.317          21.649          21.649
v  TurbVisc            2.942e-014       0.0050318       0.0011869       0.0011869
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              858:        0.19290E+01

===============================================================


 INSTANT    0.859000000E+03   TIME STEP NUMBER             859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82624E-02 0.87920E+00
   Friction velocity        uk    :  0.82624E-02 0.87920E+00
   Dimensionless distance   yplus :  0.66518E-01 0.70781E+01
   Friction thermal sca.    tstar : -0.92784E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49630E-01 0.52811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72016E-02      32   0.35483E-03   0.17718E+01 0.86770E+02 
c  Velocity[X]                                      0.10439E+01 
c  Velocity[Y]                                      0.72794E+00 
c  Velocity[Z]                                      0.11353E-29 
c  Pressure     0.13120E-06     441   0.91733E-08   0.13487E+00 0.39511E+03 
c  nu_tilda     0.48804E-05      31   0.75529E-05   0.18000E-06 0.12788E+03 
c  TempC        0.29639E+02      27   0.29913E-03   0.79114E+01 0.27685E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6668          10.352          4.5729          4.5729
v  Velocity[Y]            -3.4403          7.0101        0.010035        0.010035
v  Velocity[Z]       -2.2924e-014      8.314e-015    -1.2547e-017    -1.2547e-017
v  ǁVelocityǁ         0.0014737          10.352          5.2002          5.2002
v  Pressure               -55.022          20.679          -6.522          -6.522
v  nu_tilda           4.2776e-007       0.0042693       0.0010159       0.0010159
v  TempC                       21          73.401           21.65           21.65
v  TurbVisc           2.9433e-014       0.0050318       0.0011877       0.0011877
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              859:        0.20660E+01

===============================================================


 INSTANT    0.860000000E+03   TIME STEP NUMBER             860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11629E-01 0.87865E+00
   Friction velocity        uk    :  0.11629E-01 0.87865E+00
   Dimensionless distance   yplus :  0.93620E-01 0.70738E+01
   Friction thermal sca.    tstar : -0.11529E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69851E-01 0.52778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72052E-02      32   0.30329E-03   0.17435E+01 0.86564E+02 
c  Velocity[X]                                      0.10294E+01 
c  Velocity[Y]                                      0.71414E+00 
c  Velocity[Z]                                      0.93186E-30 
c  Pressure     0.90721E-07     408   0.99405E-08   0.93620E-01 0.37930E+03 
c  nu_tilda     0.48820E-05      31   0.14499E-04   0.18000E-06 0.12785E+03 
c  TempC        0.29651E+02      26   0.47603E-03   0.48611E+01 0.21968E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6659          10.353          4.5729          4.5729
v  Velocity[Y]            -3.4384          7.0324       0.0099606       0.0099606
v  Velocity[Z]       -2.3026e-014     8.3149e-015    -1.2532e-017    -1.2532e-017
v  ǁVelocityǁ        0.00099712          10.354          5.2005          5.2005
v  Pressure               -55.034          20.782         -6.5128         -6.5128
v  nu_tilda           4.2783e-007       0.0042693       0.0010165       0.0010165
v  TempC                       21          73.248           21.65           21.65
v  TurbVisc           2.9455e-014       0.0050318       0.0011885       0.0011885
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              860:        0.22520E+01

===============================================================


 INSTANT    0.861000000E+03   TIME STEP NUMBER             861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34387E-02 0.87981E+00
   Friction velocity        uk    :  0.34387E-02 0.87981E+00
   Dimensionless distance   yplus :  0.27684E-01 0.70831E+01
   Friction thermal sca.    tstar : -0.12546E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20655E-01 0.52848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72087E-02      32   0.35038E-03   0.17088E+01 0.86283E+02 
c  Velocity[X]                                      0.10018E+01 
c  Velocity[Y]                                      0.70699E+00 
c  Velocity[Z]                                      0.12578E-29 
c  Pressure     0.98861E-07     346   0.98093E-08   0.10140E+00 0.27118E+03 
c  nu_tilda     0.48836E-05      31   0.75641E-05   0.17999E-06 0.12782E+03 
c  TempC        0.29662E+02      27   0.44518E-03   0.63707E+01 0.26662E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6652          10.354          4.5729          4.5729
v  Velocity[Y]            -3.4365          7.0431       0.0098865       0.0098865
v  Velocity[Z]       -2.3886e-014     8.3162e-015    -1.2517e-017    -1.2517e-017
v  ǁVelocityǁ         0.0012398          10.355          5.2008          5.2008
v  Pressure               -55.039          20.803         -6.5134         -6.5134
v  nu_tilda           4.2781e-007       0.0042693       0.0010172       0.0010172
v  TempC                       21          73.323           21.65           21.65
v  TurbVisc           2.9475e-014       0.0050318       0.0011892       0.0011892
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              861:        0.20260E+01

===============================================================


 INSTANT    0.862000000E+03   TIME STEP NUMBER             862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96155E-02 0.87933E+00
   Friction velocity        uk    :  0.96155E-02 0.87933E+00
   Dimensionless distance   yplus :  0.77411E-01 0.70792E+01
   Friction thermal sca.    tstar : -0.16803E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57758E-01 0.52819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72123E-02      32   0.35759E-03   0.17604E+01 0.86840E+02 
c  Velocity[X]                                      0.10289E+01 
c  Velocity[Y]                                      0.73145E+00 
c  Velocity[Z]                                      0.10266E-29 
c  Pressure     0.11251E-06     474   0.95705E-08   0.11748E+00 0.81605E+03 
c  nu_tilda     0.48852E-05      31   0.14492E-04   0.18000E-06 0.12780E+03 
c  TempC        0.29674E+02      26   0.35082E-03   0.58618E+01 0.24319E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6641          10.356          4.5729          4.5729
v  Velocity[Y]            -3.4346          7.0117        0.009812        0.009812
v  Velocity[Z]       -2.3122e-014     8.3158e-015    -1.2491e-017    -1.2491e-017
v  ǁVelocityǁ         0.0012194          10.356          5.2012          5.2012
v  Pressure               -55.052          20.647         -6.5604         -6.5604
v  nu_tilda           4.2785e-007       0.0042693       0.0010178       0.0010178
v  TempC                       21          73.204          21.651          21.651
v  TurbVisc            2.947e-014       0.0050318         0.00119         0.00119
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              862:        0.21610E+01

===============================================================


 INSTANT    0.863000000E+03   TIME STEP NUMBER             863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94121E-02 0.87826E+00
   Friction velocity        uk    :  0.94121E-02 0.87826E+00
   Dimensionless distance   yplus :  0.75774E-01 0.70706E+01
   Friction thermal sca.    tstar : -0.16936E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56536E-01 0.52754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72159E-02      32   0.36489E-03   0.17447E+01 0.86753E+02 
c  Velocity[X]                                      0.10278E+01 
c  Velocity[Y]                                      0.71694E+00 
c  Velocity[Z]                                      0.85532E-30 
c  Pressure     0.87110E-07     441   0.99799E-08   0.89747E-01 0.65876E+03 
c  nu_tilda     0.48868E-05      31   0.75678E-05   0.17999E-06 0.12777E+03 
c  TempC        0.29685E+02      27   0.51851E-03   0.49527E+01 0.21669E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6631          10.357          4.5729          4.5729
v  Velocity[Y]            -3.4327          7.0325       0.0097379       0.0097379
v  Velocity[Z]       -2.5182e-014     8.3178e-015    -1.2484e-017    -1.2484e-017
v  ǁVelocityǁ        0.00079123          10.358          5.2015          5.2015
v  Pressure               -55.064          20.771         -6.5413         -6.5413
v  nu_tilda           4.2791e-007       0.0042693       0.0010184       0.0010184
v  TempC                       21          73.263          21.651          21.651
v  TurbVisc           2.9481e-014       0.0050318       0.0011907       0.0011907
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              863:        0.20910E+01

===============================================================


 INSTANT    0.864000000E+03   TIME STEP NUMBER             864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41149E-02 0.87942E+00
   Friction velocity        uk    :  0.41149E-02 0.87942E+00
   Dimensionless distance   yplus :  0.33127E-01 0.70800E+01
   Friction thermal sca.    tstar : -0.18176E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24717E-01 0.52824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72194E-02      32   0.38739E-03   0.17785E+01 0.87057E+02 
c  Velocity[X]                                      0.10684E+01 
c  Velocity[Y]                                      0.71013E+00 
c  Velocity[Z]                                      0.11054E-29 
c  Pressure     0.13657E-06     442   0.92017E-08   0.14269E+00 0.51614E+03 
c  nu_tilda     0.48884E-05      31   0.14493E-04   0.18000E-06 0.12775E+03 
c  TempC        0.29697E+02      28   0.47014E-03   0.73623E+01 0.27519E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6621          10.358          4.5729          4.5729
v  Velocity[Y]            -3.4308          7.0133       0.0096639       0.0096639
v  Velocity[Z]       -2.5459e-014     8.3187e-015     -1.247e-017     -1.247e-017
v  ǁVelocityǁ        0.00080841          10.359          5.2018          5.2018
v  Pressure               -55.064          20.676         -6.5687         -6.5687
v  nu_tilda             4.28e-007       0.0042693       0.0010191       0.0010191
v  TempC                       21          73.076          21.652          21.652
v  TurbVisc           2.9496e-014       0.0050318       0.0011915       0.0011915
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              864:        0.20640E+01

===============================================================


 INSTANT    0.865000000E+03   TIME STEP NUMBER             865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98774E-02 0.87870E+00
   Friction velocity        uk    :  0.98774E-02 0.87870E+00
   Dimensionless distance   yplus :  0.79520E-01 0.70741E+01
   Friction thermal sca.    tstar : -0.27294E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59331E-01 0.52781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72230E-02      32   0.34121E-03   0.17606E+01 0.86948E+02 
c  Velocity[X]                                      0.10298E+01 
c  Velocity[Y]                                      0.73084E+00 
c  Velocity[Z]                                      0.11836E-29 
c  Pressure     0.10166E-06     441   0.91207E-08   0.10372E+00 0.52065E+03 
c  nu_tilda     0.48900E-05      31   0.75493E-05   0.18000E-06 0.12772E+03 
c  TempC        0.29709E+02      27   0.42163E-03   0.59319E+01 0.25390E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.661          10.359          4.5729          4.5729
v  Velocity[Y]            -3.4289          7.0364         0.00959         0.00959
v  Velocity[Z]       -2.5199e-014      8.319e-015    -1.2449e-017    -1.2449e-017
v  ǁVelocityǁ        0.00046334           10.36          5.2021          5.2021
v  Pressure               -55.076          20.775         -6.5579         -6.5579
v  nu_tilda           4.2803e-007       0.0042693       0.0010197       0.0010197
v  TempC                       21          73.419          21.652          21.652
v  TurbVisc           2.9521e-014       0.0050318       0.0011922       0.0011922
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              865:        0.20790E+01

===============================================================


 INSTANT    0.866000000E+03   TIME STEP NUMBER             866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75697E-02 0.87990E+00
   Friction velocity        uk    :  0.75697E-02 0.87990E+00
   Dimensionless distance   yplus :  0.60941E-01 0.70838E+01
   Friction thermal sca.    tstar : -0.21087E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45469E-01 0.52853E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72266E-02      32   0.34714E-03   0.17337E+01 0.86629E+02 
c  Velocity[X]                                      0.10180E+01 
c  Velocity[Y]                                      0.71570E+00 
c  Velocity[Z]                                      0.91003E-30 
c  Pressure     0.11724E-06     409   0.94309E-08   0.11886E+00 0.26959E+03 
c  nu_tilda     0.48916E-05      31   0.14520E-04   0.18001E-06 0.12770E+03 
c  TempC        0.29720E+02      27   0.43843E-03   0.39896E+01 0.20339E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6599           10.36          4.5729          4.5729
v  Velocity[Y]            -3.4271          7.0398       0.0095162       0.0095162
v  Velocity[Z]       -2.4612e-014     8.3201e-015     -1.242e-017     -1.242e-017
v  ǁVelocityǁ        0.00045991          10.361          5.2025          5.2025
v  Pressure                -55.08          20.745         -6.5737         -6.5737
v  nu_tilda           4.2802e-007       0.0042693       0.0010203       0.0010203
v  TempC                       21          73.176          21.652          21.652
v  TurbVisc           2.9529e-014       0.0050318        0.001193        0.001193
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              866:        0.20060E+01

===============================================================


 INSTANT    0.867000000E+03   TIME STEP NUMBER             867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74079E-02 0.87974E+00
   Friction velocity        uk    :  0.74079E-02 0.87974E+00
   Dimensionless distance   yplus :  0.59638E-01 0.70825E+01
   Friction thermal sca.    tstar : -0.13839E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44497E-01 0.52843E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72301E-02      32   0.33667E-03   0.17519E+01 0.86797E+02 
c  Velocity[X]                                      0.10400E+01 
c  Velocity[Y]                                      0.71189E+00 
c  Velocity[Z]                                      0.99743E-30 
c  Pressure     0.10387E-06     425   0.98594E-08   0.10945E+00 0.24839E+03 
c  nu_tilda     0.48932E-05      31   0.75542E-05   0.18001E-06 0.12768E+03 
c  TempC        0.29732E+02      27   0.49297E-03   0.45033E+01 0.21714E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6589          10.361          4.5729          4.5729
v  Velocity[Y]            -3.4252          7.0157       0.0094426       0.0094426
v  Velocity[Z]       -2.4645e-014     8.3202e-015    -1.2396e-017    -1.2396e-017
v  ǁVelocityǁ         0.0015033          10.362          5.2028          5.2028
v  Pressure                -55.09          20.687         -6.5927         -6.5927
v  nu_tilda            4.281e-007       0.0042693        0.001021        0.001021
v  TempC                       21          73.465          21.653          21.653
v  TurbVisc           2.9528e-014       0.0050318       0.0011937       0.0011937
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              867:        0.20290E+01

===============================================================


 INSTANT    0.868000000E+03   TIME STEP NUMBER             868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61070E-02 0.87829E+00
   Friction velocity        uk    :  0.61070E-02 0.87829E+00
   Dimensionless distance   yplus :  0.49165E-01 0.70709E+01
   Friction thermal sca.    tstar : -0.13456E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36683E-01 0.52757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72337E-02      32   0.38750E-03   0.17460E+01 0.86922E+02 
c  Velocity[X]                                      0.10135E+01 
c  Velocity[Y]                                      0.73252E+00 
c  Velocity[Z]                                      0.94927E-30 
c  Pressure     0.83046E-07     409   0.92759E-08   0.85718E-01 0.22929E+03 
c  nu_tilda     0.48948E-05      31   0.14517E-04   0.18002E-06 0.12765E+03 
c  TempC        0.29743E+02      27   0.35459E-03   0.62760E+01 0.26624E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6576          10.363          4.5729          4.5729
v  Velocity[Y]            -3.4234          7.0344        0.009369        0.009369
v  Velocity[Z]       -2.4881e-014     8.3203e-015    -1.2381e-017    -1.2381e-017
v  ǁVelocityǁ         0.0009908          10.363          5.2031          5.2031
v  Pressure               -55.096          20.749         -6.5908         -6.5908
v  nu_tilda           4.2815e-007       0.0042693       0.0010216       0.0010216
v  TempC                       21          73.119          21.653          21.653
v  TurbVisc            2.955e-014       0.0050318       0.0011945       0.0011945
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              868:        0.20010E+01

===============================================================


 INSTANT    0.869000000E+03   TIME STEP NUMBER             869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41824E-02 0.87941E+00
   Friction velocity        uk    :  0.41824E-02 0.87941E+00
   Dimensionless distance   yplus :  0.33671E-01 0.70798E+01
   Friction thermal sca.    tstar : -0.13704E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25123E-01 0.52823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72372E-02      32   0.33708E-03   0.17681E+01 0.87040E+02 
c  Velocity[X]                                      0.10474E+01 
c  Velocity[Y]                                      0.72080E+00 
c  Velocity[Z]                                      0.11632E-29 
c  Pressure     0.13933E-06     426   0.99741E-08   0.14226E+00 0.36878E+03 
c  nu_tilda     0.48964E-05      31   0.75633E-05   0.18002E-06 0.12763E+03 
c  TempC        0.29755E+02      27   0.37214E-03   0.44820E+01 0.22045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6567          10.364          4.5729          4.5729
v  Velocity[Y]            -3.4215          7.0112       0.0092961       0.0092961
v  Velocity[Z]       -2.4971e-014     8.3204e-015    -1.2361e-017    -1.2361e-017
v  ǁVelocityǁ         0.0012084          10.364          5.2034          5.2034
v  Pressure               -55.094          20.654         -6.6118         -6.6118
v  nu_tilda           4.2826e-007       0.0042693       0.0010222       0.0010222
v  TempC                       21          73.429          21.654          21.654
v  TurbVisc           2.9564e-014       0.0050318       0.0011953       0.0011953
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              869:        0.20340E+01

===============================================================


 INSTANT    0.870000000E+03   TIME STEP NUMBER             870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93739E-02 0.87893E+00
   Friction velocity        uk    :  0.93739E-02 0.87893E+00
   Dimensionless distance   yplus :  0.75467E-01 0.70760E+01
   Friction thermal sca.    tstar : -0.98608E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56306E-01 0.52795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72408E-02      32   0.34294E-03   0.17439E+01 0.86852E+02 
c  Velocity[X]                                      0.10321E+01 
c  Velocity[Y]                                      0.71180E+00 
c  Velocity[Z]                                      0.12652E-29 
c  Pressure     0.10197E-06     392   0.96535E-08   0.10536E+00 0.33383E+03 
c  nu_tilda     0.48980E-05      31   0.14519E-04   0.18003E-06 0.12761E+03 
c  TempC        0.29766E+02      28   0.44314E-03   0.50263E+01 0.20802E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6555          10.365          4.5729          4.5729
v  Velocity[Y]            -3.4197          7.0352       0.0092228       0.0092228
v  Velocity[Z]       -2.3939e-014     8.3188e-015     -1.233e-017     -1.233e-017
v  ǁVelocityǁ         0.0012463          10.366          5.2038          5.2038
v  Pressure               -55.111          20.753         -6.6083         -6.6083
v  nu_tilda           4.2829e-007       0.0042693       0.0010229       0.0010229
v  TempC                       21          73.076          21.654          21.654
v  TurbVisc           2.9594e-014       0.0050318        0.001196        0.001196
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              870:        0.19610E+01

===============================================================


 INSTANT    0.871000000E+03   TIME STEP NUMBER             871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97985E-02 0.88012E+00
   Friction velocity        uk    :  0.97985E-02 0.88012E+00
   Dimensionless distance   yplus :  0.78884E-01 0.70856E+01
   Friction thermal sca.    tstar : -0.10302E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58857E-01 0.52866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72443E-02      32   0.34123E-03   0.17377E+01 0.86952E+02 
c  Velocity[X]                                      0.10050E+01 
c  Velocity[Y]                                      0.73265E+00 
c  Velocity[Z]                                      0.96010E-30 
c  Pressure     0.98783E-07     314   0.96459E-08   0.10197E+00 0.23967E+03 
c  nu_tilda     0.48995E-05      31   0.75374E-05   0.18003E-06 0.12759E+03 
c  TempC        0.29778E+02      27   0.37481E-03   0.47879E+01 0.21459E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6543          10.366          4.5729          4.5729
v  Velocity[Y]            -3.4178          7.0439       0.0091499       0.0091499
v  Velocity[Z]       -2.4489e-014     8.3196e-015    -1.2312e-017    -1.2312e-017
v  ǁVelocityǁ        0.00098264          10.366          5.2041          5.2041
v  Pressure               -55.117          20.773          -6.612          -6.612
v  nu_tilda           4.2827e-007       0.0042693       0.0010235       0.0010235
v  TempC                       21           73.19          21.655          21.655
v  TurbVisc           2.9603e-014       0.0050318       0.0011968       0.0011968
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              871:        0.17620E+01

===============================================================


 INSTANT    0.872000000E+03   TIME STEP NUMBER             872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36288E-02 0.87953E+00
   Friction velocity        uk    :  0.36288E-02 0.87953E+00
   Dimensionless distance   yplus :  0.29214E-01 0.70809E+01
   Friction thermal sca.    tstar : -0.84924E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21797E-01 0.52831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72479E-02      32   0.35071E-03   0.17527E+01 0.87041E+02 
c  Velocity[X]                                      0.10321E+01 
c  Velocity[Y]                                      0.72053E+00 
c  Velocity[Z]                                      0.11127E-29 
c  Pressure     0.10749E-06     474   0.95070E-08   0.11120E+00 0.79727E+03 
c  nu_tilda     0.49011E-05      31   0.14543E-04   0.18004E-06 0.12756E+03 
c  TempC        0.29790E+02      27   0.47041E-03   0.36048E+01 0.19496E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.653          10.367          4.5729          4.5729
v  Velocity[Y]            -3.4161          7.0134       0.0090772       0.0090772
v  Velocity[Z]       -2.4465e-014     8.3192e-015    -1.2295e-017    -1.2295e-017
v  ǁVelocityǁ         0.0014862          10.367          5.2044          5.2044
v  Pressure               -55.121          20.614         -6.6553         -6.6553
v  nu_tilda           4.2836e-007       0.0042693       0.0010241       0.0010241
v  TempC                       21          74.119          21.655          21.655
v  TurbVisc           2.9596e-014       0.0050318       0.0011975       0.0011975
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              872:        0.21500E+01

===============================================================


 INSTANT    0.873000000E+03   TIME STEP NUMBER             873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11799E-01 0.87851E+00
   Friction velocity        uk    :  0.11799E-01 0.87851E+00
   Dimensionless distance   yplus :  0.94990E-01 0.70726E+01
   Friction thermal sca.    tstar : -0.84803E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70874E-01 0.52769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72514E-02      32   0.36281E-03   0.17699E+01 0.87214E+02 
c  Velocity[X]                                      0.10542E+01 
c  Velocity[Y]                                      0.71571E+00 
c  Velocity[Z]                                      0.10332E-29 
c  Pressure     0.11129E-06     473   0.93516E-08   0.11539E+00 0.78545E+03 
c  nu_tilda     0.49027E-05      31   0.75502E-05   0.18004E-06 0.12754E+03 
c  TempC        0.29801E+02      27   0.45760E-03   0.46799E+01 0.21811E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6518          10.368          4.5729          4.5729
v  Velocity[Y]            -3.4143          7.0362       0.0090049       0.0090049
v  Velocity[Z]         -2.48e-014     8.3209e-015    -1.2274e-017    -1.2274e-017
v  ǁVelocityǁ         0.0011139          10.368          5.2047          5.2047
v  Pressure               -55.125           20.76         -6.6277         -6.6277
v  nu_tilda           4.2841e-007       0.0042693       0.0010248       0.0010248
v  TempC                       21          73.076          21.655          21.655
v  TurbVisc           2.9622e-014       0.0050318       0.0011983       0.0011983
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              873:        0.21520E+01

===============================================================


 INSTANT    0.874000000E+03   TIME STEP NUMBER             874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81961E-02 0.87957E+00
   Friction velocity        uk    :  0.81961E-02 0.87957E+00
   Dimensionless distance   yplus :  0.65984E-01 0.70812E+01
   Friction thermal sca.    tstar : -0.81802E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49232E-01 0.52833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72549E-02      32   0.35466E-03   0.17685E+01 0.87298E+02 
c  Velocity[X]                                      0.10339E+01 
c  Velocity[Y]                                      0.73460E+00 
c  Velocity[Z]                                      0.89897E-30 
c  Pressure     0.11072E-06     458   0.90845E-08   0.11505E+00 0.62630E+03 
c  nu_tilda     0.49043E-05      31   0.14538E-04   0.18006E-06 0.12752E+03 
c  TempC        0.29813E+02      27   0.44663E-03   0.54001E+01 0.23829E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6504          10.368          4.5729          4.5729
v  Velocity[Y]            -3.4126          7.0138       0.0089327       0.0089327
v  Velocity[Z]        -2.421e-014      8.319e-015    -1.2254e-017    -1.2254e-017
v  ǁVelocityǁ         0.0010899          10.369           5.205           5.205
v  Pressure               -55.131           20.65         -6.6644         -6.6644
v  nu_tilda           4.2841e-007       0.0042693       0.0010254       0.0010254
v  TempC                       21          73.306          21.656          21.656
v  TurbVisc           2.9634e-014       0.0050318        0.001199        0.001199
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              874:        0.21260E+01

===============================================================


 INSTANT    0.875000000E+03   TIME STEP NUMBER             875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78092E-02 0.87880E+00
   Friction velocity        uk    :  0.78092E-02 0.87880E+00
   Dimensionless distance   yplus :  0.62869E-01 0.70749E+01
   Friction thermal sca.    tstar : -0.75208E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46908E-01 0.52787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72584E-02      32   0.32717E-03   0.17541E+01 0.87135E+02 
c  Velocity[X]                                      0.10313E+01 
c  Velocity[Y]                                      0.72276E+00 
c  Velocity[Z]                                      0.88660E-30 
c  Pressure     0.10156E-06     453   0.98410E-08   0.10470E+00 0.63672E+03 
c  nu_tilda     0.49059E-05      31   0.75481E-05   0.18007E-06 0.12750E+03 
c  TempC        0.29824E+02      26   0.36876E-03   0.55328E+01 0.25458E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6491          10.369          4.5729          4.5729
v  Velocity[Y]            -3.4107          7.0409       0.0088609       0.0088609
v  Velocity[Z]       -2.4183e-014     8.3208e-015     -1.223e-017     -1.223e-017
v  ǁVelocityǁ        0.00016758           10.37          5.2054          5.2054
v  Pressure               -55.136          20.765         -6.6448         -6.6448
v  nu_tilda           4.2845e-007       0.0042693        0.001026        0.001026
v  TempC                       21          73.075          21.656          21.656
v  TurbVisc           2.9634e-014       0.0050319       0.0011998       0.0011998
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              875:        0.21090E+01

===============================================================


 INSTANT    0.876000000E+03   TIME STEP NUMBER             876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45624E-02 0.87989E+00
   Friction velocity        uk    :  0.45624E-02 0.87989E+00
   Dimensionless distance   yplus :  0.36730E-01 0.70837E+01
   Friction thermal sca.    tstar : -0.73042E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27405E-01 0.52852E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72620E-02      32   0.39562E-03   0.17562E+01 0.87140E+02 
c  Velocity[X]                                      0.10411E+01 
c  Velocity[Y]                                      0.71514E+00 
c  Velocity[Z]                                      0.99414E-30 
c  Pressure     0.11510E-06     441   0.97184E-08   0.11731E+00 0.42000E+03 
c  nu_tilda     0.49075E-05      31   0.14538E-04   0.18008E-06 0.12748E+03 
c  TempC        0.29836E+02      26   0.36624E-03   0.55534E+01 0.22349E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6476           10.37          4.5729          4.5729
v  Velocity[Y]             -3.409          7.0386       0.0087892       0.0087892
v  Velocity[Z]       -2.3794e-014     8.3197e-015    -1.2209e-017    -1.2209e-017
v  ǁVelocityǁ        0.00017888          10.371          5.2057          5.2057
v  Pressure               -55.144          20.708         -6.6723         -6.6723
v  nu_tilda           4.2851e-007       0.0042693       0.0010267       0.0010267
v  TempC                       21          73.599          21.657          21.657
v  TurbVisc           2.9647e-014       0.0050319       0.0012005       0.0012005
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              876:        0.20760E+01

===============================================================


 INSTANT    0.877000000E+03   TIME STEP NUMBER             877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40318E-02 0.87951E+00
   Friction velocity        uk    :  0.40318E-02 0.87951E+00
   Dimensionless distance   yplus :  0.32459E-01 0.70807E+01
   Friction thermal sca.    tstar : -0.69638E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24218E-01 0.52830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72655E-02      32   0.37822E-03   0.18117E+01 0.87782E+02 
c  Velocity[X]                                      0.10793E+01 
c  Velocity[Y]                                      0.73245E+00 
c  Velocity[Z]                                      0.11941E-29 
c  Pressure     0.11724E-06     410   0.95055E-08   0.12295E+00 0.24911E+03 
c  nu_tilda     0.49091E-05      31   0.75355E-05   0.18010E-06 0.12746E+03 
c  TempC        0.29847E+02      27   0.49219E-03   0.50861E+01 0.21035E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6461          10.371          4.5729          4.5729
v  Velocity[Y]            -3.4072          7.0143       0.0087176       0.0087176
v  Velocity[Z]       -2.4265e-014     8.3199e-015    -1.2193e-017    -1.2193e-017
v  ǁVelocityǁ           0.00117          10.372           5.206           5.206
v  Pressure               -55.145          20.645         -6.6871         -6.6871
v  nu_tilda            4.286e-007       0.0042694       0.0010273       0.0010273
v  TempC                       21          73.494          21.657          21.657
v  TurbVisc           2.9662e-014       0.0050319       0.0012013       0.0012013
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              877:        0.19990E+01

===============================================================


 INSTANT    0.878000000E+03   TIME STEP NUMBER             878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96461E-02 0.87851E+00
   Friction velocity        uk    :  0.96461E-02 0.87851E+00
   Dimensionless distance   yplus :  0.77658E-01 0.70726E+01
   Friction thermal sca.    tstar : -0.66687E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57941E-01 0.52769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72690E-02      32   0.30782E-03   0.17752E+01 0.87554E+02 
c  Velocity[X]                                      0.10512E+01 
c  Velocity[Y]                                      0.72399E+00 
c  Velocity[Z]                                      0.91642E-30 
c  Pressure     0.91895E-07     377   0.91564E-08   0.93916E-01 0.25084E+03 
c  nu_tilda     0.49107E-05      31   0.14565E-04   0.18011E-06 0.12744E+03 
c  TempC        0.29859E+02      27   0.37763E-03   0.73048E+01 0.26455E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6447          10.372          4.5729          4.5729
v  Velocity[Y]            -3.4055          7.0353       0.0086463       0.0086463
v  Velocity[Z]       -2.4112e-014     8.3188e-015    -1.2179e-017    -1.2179e-017
v  ǁVelocityǁ         0.0012227          10.373          5.2063          5.2063
v  Pressure               -55.157          20.722         -6.6868         -6.6868
v  nu_tilda           4.2861e-007       0.0042694       0.0010279       0.0010279
v  TempC                       21          73.075          21.657          21.657
v  TurbVisc           2.9688e-014       0.0050319       0.0012021       0.0012021
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              878:        0.19090E+01

===============================================================


 INSTANT    0.879000000E+03   TIME STEP NUMBER             879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96345E-02 0.87969E+00
   Friction velocity        uk    :  0.96345E-02 0.87969E+00
   Dimensionless distance   yplus :  0.77564E-01 0.70821E+01
   Friction thermal sca.    tstar : -0.68883E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57872E-01 0.52840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72726E-02      32   0.36468E-03   0.17456E+01 0.87186E+02 
c  Velocity[X]                                      0.10289E+01 
c  Velocity[Y]                                      0.71671E+00 
c  Velocity[Z]                                      0.10343E-29 
c  Pressure     0.10099E-06     410   0.99920E-08   0.10480E+00 0.29354E+03 
c  nu_tilda     0.49123E-05      31   0.75341E-05   0.18012E-06 0.12742E+03 
c  TempC        0.29870E+02      27   0.40157E-03   0.46291E+01 0.20720E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6433          10.373          4.5729          4.5729
v  Velocity[Y]            -3.4038          7.0191       0.0085756       0.0085756
v  Velocity[Z]       -2.4251e-014     8.3186e-015    -1.2162e-017    -1.2162e-017
v  ǁVelocityǁ        0.00097713          10.374          5.2066          5.2066
v  Pressure               -55.156          20.649          -6.705          -6.705
v  nu_tilda           4.2865e-007       0.0042694       0.0010286       0.0010286
v  TempC                       21           74.19          21.658          21.658
v  TurbVisc           2.9692e-014       0.0050319       0.0012028       0.0012028
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              879:        0.20130E+01

===============================================================


 INSTANT    0.880000000E+03   TIME STEP NUMBER             880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41589E-02 0.87901E+00
   Friction velocity        uk    :  0.41589E-02 0.87901E+00
   Dimensionless distance   yplus :  0.33482E-01 0.70767E+01
   Friction thermal sca.    tstar : -0.60707E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24981E-01 0.52800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72761E-02      32   0.35206E-03   0.17599E+01 0.87339E+02 
c  Velocity[X]                                      0.10322E+01 
c  Velocity[Y]                                      0.72773E+00 
c  Velocity[Z]                                      0.11223E-29 
c  Pressure     0.11549E-06     314   0.96805E-08   0.11774E+00 0.17817E+03 
c  nu_tilda     0.49139E-05      31   0.14563E-04   0.18014E-06 0.12740E+03 
c  TempC        0.29882E+02      27   0.43287E-03   0.40713E+01 0.20288E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6418          10.374          4.5729          4.5729
v  Velocity[Y]            -3.4021          7.0348       0.0085049       0.0085049
v  Velocity[Z]       -2.3807e-014     8.3173e-015    -1.2151e-017    -1.2151e-017
v  ǁVelocityǁ         0.0015002          10.375          5.2069          5.2069
v  Pressure               -55.167            20.7         -6.7091         -6.7091
v  nu_tilda           4.2869e-007       0.0042694       0.0010292       0.0010292
v  TempC                       21          73.132          21.658          21.658
v  TurbVisc           2.9701e-014       0.0050319       0.0012036       0.0012036
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              880:        0.17700E+01

===============================================================


 INSTANT    0.881000000E+03   TIME STEP NUMBER             881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11941E-01 0.88015E+00
   Friction velocity        uk    :  0.11941E-01 0.88015E+00
   Dimensionless distance   yplus :  0.96133E-01 0.70858E+01
   Friction thermal sca.    tstar : -0.63164E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71726E-01 0.52868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72796E-02      32   0.35688E-03   0.17309E+01 0.87133E+02 
c  Velocity[X]                                      0.10074E+01 
c  Velocity[Y]                                      0.72353E+00 
c  Velocity[Z]                                      0.95650E-30 
c  Pressure     0.85023E-07     394   0.92053E-08   0.87457E-01 0.34323E+03 
c  nu_tilda     0.49155E-05      31   0.75488E-05   0.18015E-06 0.12739E+03 
c  TempC        0.29893E+02      27   0.31932E-03   0.69147E+01 0.25366E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6403          10.375          4.5729          4.5729
v  Velocity[Y]            -3.4004          7.0449       0.0084346       0.0084346
v  Velocity[Z]       -2.3675e-014     8.3172e-015    -1.2132e-017    -1.2132e-017
v  ǁVelocityǁ         0.0010768          10.376          5.2072          5.2072
v  Pressure               -55.167          20.741         -6.7041         -6.7041
v  nu_tilda           4.2871e-007       0.0042694       0.0010299       0.0010299
v  TempC                       21          73.122          21.659          21.659
v  TurbVisc           2.9711e-014       0.0050319       0.0012043       0.0012043
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              881:        0.19660E+01

===============================================================


 INSTANT    0.882000000E+03   TIME STEP NUMBER             882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77083E-02 0.87975E+00
   Friction velocity        uk    :  0.77083E-02 0.87975E+00
   Dimensionless distance   yplus :  0.62057E-01 0.70826E+01
   Friction thermal sca.    tstar : -0.57264E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46302E-01 0.52844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72831E-02      32   0.36194E-03   0.17886E+01 0.87628E+02 
c  Velocity[X]                                      0.10695E+01 
c  Velocity[Y]                                      0.71912E+00 
c  Velocity[Z]                                      0.95833E-30 
c  Pressure     0.13875E-06     456   0.96242E-08   0.14578E+00 0.54992E+03 
c  nu_tilda     0.49171E-05      31   0.14561E-04   0.18016E-06 0.12737E+03 
c  TempC        0.29905E+02      26   0.46858E-03   0.60662E+01 0.22851E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6389          10.376          4.5729          4.5729
v  Velocity[Y]            -3.3987          7.0199       0.0083645       0.0083645
v  Velocity[Z]       -2.2759e-014     8.3175e-015    -1.2119e-017    -1.2119e-017
v  ǁVelocityǁ         0.0010882          10.377          5.2076          5.2076
v  Pressure               -55.163          20.631         -6.7319         -6.7319
v  nu_tilda           4.2879e-007       0.0042694       0.0010305       0.0010305
v  TempC                       21          73.386          21.659          21.659
v  TurbVisc           2.9718e-014       0.0050319       0.0012051       0.0012051
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              882:        0.21150E+01

===============================================================


 INSTANT    0.883000000E+03   TIME STEP NUMBER             883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79272E-02 0.87852E+00
   Friction velocity        uk    :  0.79272E-02 0.87852E+00
   Dimensionless distance   yplus :  0.63820E-01 0.70727E+01
   Friction thermal sca.    tstar : -0.59775E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47617E-01 0.52770E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72866E-02      32   0.33996E-03   0.17894E+01 0.87642E+02 
c  Velocity[X]                                      0.10575E+01 
c  Velocity[Y]                                      0.73189E+00 
c  Velocity[Z]                                      0.95014E-30 
c  Pressure     0.12270E-06     410   0.91335E-08   0.12406E+00 0.43390E+03 
c  nu_tilda     0.49187E-05      31   0.75175E-05   0.18018E-06 0.12735E+03 
c  TempC        0.29917E+02      26   0.45921E-03   0.64335E+01 0.26060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6373          10.377          4.5729          4.5729
v  Velocity[Y]             -3.397          7.0338       0.0082946       0.0082946
v  Velocity[Z]       -2.2128e-014     8.3161e-015    -1.2094e-017    -1.2094e-017
v  ǁVelocityǁ         0.0014586          10.378          5.2079          5.2079
v  Pressure               -55.174          20.712         -6.7264         -6.7264
v  nu_tilda           4.2886e-007       0.0042694       0.0010311       0.0010311
v  TempC                       21          73.698          21.659          21.659
v  TurbVisc           2.9741e-014       0.0050319       0.0012058       0.0012058
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              883:        0.20100E+01

===============================================================


 INSTANT    0.884000000E+03   TIME STEP NUMBER             884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11670E-01 0.87967E+00
   Friction velocity        uk    :  0.11670E-01 0.87967E+00
   Dimensionless distance   yplus :  0.93950E-01 0.70820E+01
   Friction thermal sca.    tstar : -0.57116E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70097E-01 0.52840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72902E-02      32   0.32026E-03   0.17671E+01 0.87534E+02 
c  Velocity[X]                                      0.10413E+01 
c  Velocity[Y]                                      0.72574E+00 
c  Velocity[Z]                                      0.90210E-30 
c  Pressure     0.98505E-07     458   0.94232E-08   0.10298E+00 0.64056E+03 
c  nu_tilda     0.49202E-05      31   0.14582E-04   0.18020E-06 0.12733E+03 
c  TempC        0.29928E+02      27   0.35376E-03   0.57636E+01 0.23791E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6356          10.378          4.5729          4.5729
v  Velocity[Y]            -3.3953          7.0135       0.0082251       0.0082251
v  Velocity[Z]       -2.1982e-014     8.3158e-015    -1.2074e-017    -1.2074e-017
v  ǁVelocityǁ        0.00096373          10.379          5.2082          5.2082
v  Pressure               -55.175          20.594         -6.7626         -6.7626
v  nu_tilda           4.2893e-007       0.0042694       0.0010317       0.0010317
v  TempC                       21          73.075           21.66           21.66
v  TurbVisc           2.9761e-014       0.0050319       0.0012066       0.0012066
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              884:        0.21040E+01

===============================================================


 INSTANT    0.885000000E+03   TIME STEP NUMBER             885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28755E-02 0.87909E+00
   Friction velocity        uk    :  0.28755E-02 0.87909E+00
   Dimensionless distance   yplus :  0.23150E-01 0.70773E+01
   Friction thermal sca.    tstar : -0.57735E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17272E-01 0.52804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72937E-02      32   0.38411E-03   0.17536E+01 0.87418E+02 
c  Velocity[X]                                      0.10326E+01 
c  Velocity[Y]                                      0.72096E+00 
c  Velocity[Z]                                      0.11920E-29 
c  Pressure     0.10039E-06     457   0.94828E-08   0.10316E+00 0.82563E+03 
c  nu_tilda     0.49218E-05      31   0.75216E-05   0.18021E-06 0.12731E+03 
c  TempC        0.29940E+02      26   0.50918E-03   0.57015E+01 0.23467E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.634          10.379          4.5729          4.5729
v  Velocity[Y]            -3.3937          7.0407        0.008156        0.008156
v  Velocity[Z]       -2.1807e-014     8.3173e-015    -1.2054e-017    -1.2054e-017
v  ǁVelocityǁ        0.00038407           10.38          5.2085          5.2085
v  Pressure               -55.176          20.748         -6.7319         -6.7319
v  nu_tilda           4.2895e-007       0.0042694       0.0010324       0.0010324
v  TempC                       21          73.293           21.66           21.66
v  TurbVisc            2.978e-014       0.0050319       0.0012073       0.0012073
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              885:        0.21070E+01

===============================================================


 INSTANT    0.886000000E+03   TIME STEP NUMBER             886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68801E-02 0.88036E+00
   Friction velocity        uk    :  0.68801E-02 0.88036E+00
   Dimensionless distance   yplus :  0.55389E-01 0.70875E+01
   Friction thermal sca.    tstar : -0.56640E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41326E-01 0.52881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.72972E-02      32   0.39170E-03   0.17842E+01 0.87834E+02 
c  Velocity[X]                                      0.10491E+01 
c  Velocity[Y]                                      0.73512E+00 
c  Velocity[Z]                                      0.11443E-29 
c  Pressure     0.11150E-06     426   0.97005E-08   0.11484E+00 0.35761E+03 
c  nu_tilda     0.49234E-05      31   0.14583E-04   0.18023E-06 0.12730E+03 
c  TempC        0.29951E+02      26   0.38483E-03   0.78013E+01 0.29515E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6323           10.38          4.5729          4.5729
v  Velocity[Y]            -3.3921          7.0482       0.0080873       0.0080873
v  Velocity[Z]       -2.1408e-014     8.3155e-015    -1.2036e-017    -1.2036e-017
v  ǁVelocityǁ        0.00030659          10.381          5.2088          5.2088
v  Pressure               -55.182          20.705         -6.7559         -6.7559
v  nu_tilda           4.2893e-007       0.0042694        0.001033        0.001033
v  TempC                       21          73.568           21.66           21.66
v  TurbVisc           2.9785e-014       0.0050319       0.0012081       0.0012081
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              886:        0.20700E+01

===============================================================


 INSTANT    0.887000000E+03   TIME STEP NUMBER             887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61383E-02 0.88000E+00
   Friction velocity        uk    :  0.61383E-02 0.88000E+00
   Dimensionless distance   yplus :  0.49417E-01 0.70846E+01
   Friction thermal sca.    tstar : -0.56658E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36871E-01 0.52859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73007E-02      32   0.31803E-03   0.18212E+01 0.88126E+02 
c  Velocity[X]                                      0.10922E+01 
c  Velocity[Y]                                      0.72897E+00 
c  Velocity[Z]                                      0.94665E-30 
c  Pressure     0.13676E-06     441   0.94944E-08   0.13954E+00 0.43739E+03 
c  nu_tilda     0.49250E-05      31   0.75279E-05   0.18025E-06 0.12728E+03 
c  TempC        0.29963E+02      27   0.40205E-03   0.51488E+01 0.22304E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6305          10.381          4.5729          4.5729
v  Velocity[Y]            -3.3905           7.019       0.0080188       0.0080188
v  Velocity[Z]       -2.1466e-014     8.3142e-015    -1.2013e-017    -1.2013e-017
v  ǁVelocityǁ        0.00098316          10.382          5.2091          5.2091
v  Pressure               -55.182          20.594          -6.784          -6.784
v  nu_tilda           4.2901e-007       0.0042694       0.0010337       0.0010337
v  TempC                       21          73.074          21.661          21.661
v  TurbVisc           2.9778e-014       0.0050319       0.0012089       0.0012089
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              887:        0.21380E+01

===============================================================


 INSTANT    0.888000000E+03   TIME STEP NUMBER             888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52212E-02 0.87897E+00
   Friction velocity        uk    :  0.52212E-02 0.87897E+00
   Dimensionless distance   yplus :  0.42034E-01 0.70763E+01
   Friction thermal sca.    tstar : -0.57791E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31362E-01 0.52797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73042E-02      32   0.34176E-03   0.17608E+01 0.87579E+02 
c  Velocity[X]                                      0.10363E+01 
c  Velocity[Y]                                      0.72444E+00 
c  Velocity[Z]                                      0.96299E-30 
c  Pressure     0.99123E-07     410   0.92657E-08   0.10190E+00 0.38232E+03 
c  nu_tilda     0.49266E-05      31   0.14588E-04   0.18028E-06 0.12726E+03 
c  TempC        0.29974E+02      27   0.43332E-03   0.55145E+01 0.21656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6287          10.381          4.5729          4.5729
v  Velocity[Y]             -3.389          7.0379       0.0079506       0.0079506
v  Velocity[Z]       -2.1572e-014     8.3144e-015    -1.1997e-017    -1.1997e-017
v  ǁVelocityǁ          0.001197          10.382          5.2094          5.2094
v  Pressure               -55.192            20.7          -6.775          -6.775
v  nu_tilda           4.2909e-007       0.0042694       0.0010343       0.0010343
v  TempC                       21          73.074          21.661          21.661
v  TurbVisc           2.9803e-014       0.0050319       0.0012096       0.0012096
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              888:        0.20000E+01

===============================================================


 INSTANT    0.889000000E+03   TIME STEP NUMBER             889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12194E-01 0.87997E+00
   Friction velocity        uk    :  0.12194E-01 0.87997E+00
   Dimensionless distance   yplus :  0.98168E-01 0.70843E+01
   Friction thermal sca.    tstar : -0.56594E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73244E-01 0.52857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73077E-02      32   0.37425E-03   0.17742E+01 0.87807E+02 
c  Velocity[X]                                      0.10336E+01 
c  Velocity[Y]                                      0.74058E+00 
c  Velocity[Z]                                      0.96092E-30 
c  Pressure     0.10615E-06     421   0.93824E-08   0.11056E+00 0.28292E+03 
c  nu_tilda     0.49282E-05      31   0.75408E-05   0.18029E-06 0.12725E+03 
c  TempC        0.29986E+02      27   0.40071E-03   0.53651E+01 0.23744E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6269          10.382          4.5729          4.5729
v  Velocity[Y]            -3.3874          7.0189       0.0078829       0.0078829
v  Velocity[Z]        -2.159e-014     8.3152e-015    -1.1987e-017    -1.1987e-017
v  ǁVelocityǁ          0.001033          10.383          5.2097          5.2097
v  Pressure               -55.186          20.632         -6.7922         -6.7922
v  nu_tilda           4.2915e-007       0.0042694       0.0010349       0.0010349
v  TempC                       21          73.103          21.662          21.662
v  TurbVisc           2.9825e-014       0.0050319       0.0012104       0.0012104
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              889:        0.20380E+01

===============================================================


 INSTANT    0.890000000E+03   TIME STEP NUMBER             890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69668E-02 0.87914E+00
   Friction velocity        uk    :  0.69668E-02 0.87914E+00
   Dimensionless distance   yplus :  0.56088E-01 0.70777E+01
   Friction thermal sca.    tstar : -0.57113E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41848E-01 0.52807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73112E-02      32   0.35924E-03   0.17965E+01 0.88102E+02 
c  Velocity[X]                                      0.10521E+01 
c  Velocity[Y]                                      0.74447E+00 
c  Velocity[Z]                                      0.12197E-29 
c  Pressure     0.10942E-06     282   0.91446E-08   0.11149E+00 0.17870E+03 
c  nu_tilda     0.49298E-05      31   0.14587E-04   0.18032E-06 0.12723E+03 
c  TempC        0.29997E+02      26   0.40338E-03   0.56074E+01 0.22719E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6252          10.383          4.5729          4.5729
v  Velocity[Y]            -3.3859          7.0426       0.0078152       0.0078152
v  Velocity[Z]       -2.1279e-014     8.3143e-015     -1.197e-017     -1.197e-017
v  ǁVelocityǁ         0.0011428          10.384            5.21            5.21
v  Pressure               -55.194           20.68         -6.7954         -6.7954
v  nu_tilda           4.2919e-007       0.0042694       0.0010356       0.0010356
v  TempC                       21          74.193          21.662          21.662
v  TurbVisc           2.9841e-014       0.0050319       0.0012111       0.0012111
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              890:        0.16970E+01

===============================================================


 INSTANT    0.891000000E+03   TIME STEP NUMBER             891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51025E-02 0.88052E+00
   Friction velocity        uk    :  0.51025E-02 0.88052E+00
   Dimensionless distance   yplus :  0.41079E-01 0.70888E+01
   Friction thermal sca.    tstar : -0.56939E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30649E-01 0.52890E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73147E-02      32   0.35614E-03   0.17608E+01 0.87641E+02 
c  Velocity[X]                                      0.10342E+01 
c  Velocity[Y]                                      0.72667E+00 
c  Velocity[Z]                                      0.10826E-29 
c  Pressure     0.11098E-06     378   0.97247E-08   0.11257E+00 0.34271E+03 
c  nu_tilda     0.49314E-05      31   0.75185E-05   0.18034E-06 0.12722E+03 
c  TempC        0.30009E+02      27   0.46639E-03   0.47178E+01 0.20126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6235          10.384          4.5729          4.5729
v  Velocity[Y]            -3.3844          7.0476       0.0077483       0.0077483
v  Velocity[Z]       -2.1021e-014     8.3136e-015    -1.1955e-017    -1.1955e-017
v  ǁVelocityǁ          0.001386          10.385          5.2103          5.2103
v  Pressure               -55.193          20.719         -6.7899         -6.7899
v  nu_tilda           4.2916e-007       0.0042694       0.0010362       0.0010362
v  TempC                       21          73.074          21.662          21.662
v  TurbVisc           2.9851e-014       0.0050319       0.0012119       0.0012119
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              891:        0.21720E+01

===============================================================


 INSTANT    0.892000000E+03   TIME STEP NUMBER             892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76785E-02 0.87999E+00
   Friction velocity        uk    :  0.76785E-02 0.87999E+00
   Dimensionless distance   yplus :  0.61817E-01 0.70845E+01
   Friction thermal sca.    tstar : -0.56493E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46122E-01 0.52858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73182E-02      32   0.31743E-03   0.17926E+01 0.88089E+02 
c  Velocity[X]                                      0.10429E+01 
c  Velocity[Y]                                      0.74970E+00 
c  Velocity[Z]                                      0.86986E-30 
c  Pressure     0.85322E-07     469   0.95992E-08   0.88843E-01 0.78502E+03 
c  nu_tilda     0.49330E-05      31   0.14615E-04   0.18037E-06 0.12720E+03 
c  TempC        0.30020E+02      26   0.38461E-03   0.48873E+01 0.21886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6216          10.385          4.5729          4.5729
v  Velocity[Y]            -3.3829          7.0196       0.0076813       0.0076813
v  Velocity[Z]       -2.0712e-014     8.3117e-015    -1.1944e-017    -1.1944e-017
v  ǁVelocityǁ        0.00095427          10.386          5.2106          5.2106
v  Pressure               -55.195          20.572         -6.8354         -6.8354
v  nu_tilda            4.292e-007       0.0042694       0.0010368       0.0010368
v  TempC                       21          73.425          21.663          21.663
v  TurbVisc           2.9844e-014       0.0050319       0.0012127       0.0012127
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              892:        0.23840E+01

===============================================================


 INSTANT    0.893000000E+03   TIME STEP NUMBER             893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22930E-02 0.87890E+00
   Friction velocity        uk    :  0.22930E-02 0.87890E+00
   Dimensionless distance   yplus :  0.18460E-01 0.70758E+01
   Friction thermal sca.    tstar : -0.57539E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13773E-01 0.52793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73217E-02      32   0.30682E-03   0.17711E+01 0.87815E+02 
c  Velocity[X]                                      0.10363E+01 
c  Velocity[Y]                                      0.73477E+00 
c  Velocity[Z]                                      0.10601E-29 
c  Pressure     0.13480E-06     474   0.95599E-08   0.13987E+00 0.93029E+03 
c  nu_tilda     0.49346E-05      31   0.75206E-05   0.18038E-06 0.12719E+03 
c  TempC        0.30032E+02      27   0.51008E-03   0.56804E+01 0.23974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.62          10.385          4.5729          4.5729
v  Velocity[Y]            -3.3814          7.0424        0.007615        0.007615
v  Velocity[Z]       -2.0367e-014      8.314e-015    -1.1924e-017    -1.1924e-017
v  ǁVelocityǁ         0.0013083          10.386          5.2109          5.2109
v  Pressure                -55.19           20.75          -6.798          -6.798
v  nu_tilda           4.2926e-007       0.0042694       0.0010375       0.0010375
v  TempC                       21          73.097          21.663          21.663
v  TurbVisc           2.9855e-014       0.0050319       0.0012134       0.0012134
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              893:        0.21550E+01

===============================================================


 INSTANT    0.894000000E+03   TIME STEP NUMBER             894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10560E-01 0.87962E+00
   Friction velocity        uk    :  0.10560E-01 0.87962E+00
   Dimensionless distance   yplus :  0.85014E-01 0.70815E+01
   Friction thermal sca.    tstar : -0.56623E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63430E-01 0.52836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73252E-02      32   0.42383E-03   0.17703E+01 0.87833E+02 
c  Velocity[X]                                      0.10465E+01 
c  Velocity[Y]                                      0.72376E+00 
c  Velocity[Z]                                      0.98605E-30 
c  Pressure     0.12477E-06     489   0.93048E-08   0.12878E+00 0.97807E+03 
c  nu_tilda     0.49361E-05      31   0.14603E-04   0.18041E-06 0.12717E+03 
c  TempC        0.30043E+02      26   0.39966E-03   0.78694E+01 0.28803E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6181          10.386          4.5729          4.5729
v  Velocity[Y]              -3.38          7.0161       0.0075489       0.0075489
v  Velocity[Z]       -1.9922e-014     8.3111e-015    -1.1909e-017    -1.1909e-017
v  ǁVelocityǁ         0.0011057          10.387          5.2112          5.2112
v  Pressure               -55.195          20.554         -6.8527         -6.8527
v  nu_tilda           4.2932e-007       0.0042694       0.0010381       0.0010381
v  TempC                       21          73.577          21.663          21.663
v  TurbVisc            2.987e-014       0.0050319       0.0012142       0.0012142
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              894:        0.21790E+01

===============================================================


 INSTANT    0.895000000E+03   TIME STEP NUMBER             895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83661E-02 0.87916E+00
   Friction velocity        uk    :  0.83661E-02 0.87916E+00
   Dimensionless distance   yplus :  0.67353E-01 0.70778E+01
   Friction thermal sca.    tstar : -0.58221E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50253E-01 0.52809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73287E-02      32   0.33946E-03   0.18108E+01 0.88304E+02 
c  Velocity[X]                                      0.10667E+01 
c  Velocity[Y]                                      0.74407E+00 
c  Velocity[Z]                                      0.10163E-29 
c  Pressure     0.12782E-06     474   0.91564E-08   0.13125E+00 0.77450E+03 
c  nu_tilda     0.49377E-05      31   0.75219E-05   0.18043E-06 0.12716E+03 
c  TempC        0.30054E+02      26   0.44753E-03   0.51842E+01 0.22377E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6162          10.387          4.5729          4.5729
v  Velocity[Y]            -3.3785          7.0396       0.0074832       0.0074832
v  Velocity[Z]       -1.9718e-014     8.3107e-015    -1.1891e-017    -1.1891e-017
v  ǁVelocityǁ        0.00063923          10.388          5.2115          5.2115
v  Pressure               -55.197          20.705         -6.8259         -6.8259
v  nu_tilda           4.2934e-007       0.0042694       0.0010388       0.0010388
v  TempC                       21           73.64          21.664          21.664
v  TurbVisc           2.9887e-014       0.0050319       0.0012149       0.0012149
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              895:        0.21700E+01

===============================================================


 INSTANT    0.896000000E+03   TIME STEP NUMBER             896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64263E-02 0.88046E+00
   Friction velocity        uk    :  0.64263E-02 0.88046E+00
   Dimensionless distance   yplus :  0.51736E-01 0.70883E+01
   Friction thermal sca.    tstar : -0.57087E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38601E-01 0.52887E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73322E-02      32   0.31063E-03   0.17601E+01 0.87867E+02 
c  Velocity[X]                                      0.10258E+01 
c  Velocity[Y]                                      0.73432E+00 
c  Velocity[Z]                                      0.97650E-30 
c  Pressure     0.10030E-06     409   0.99088E-08   0.10260E+00 0.22235E+03 
c  nu_tilda     0.49393E-05      31   0.14604E-04   0.18046E-06 0.12715E+03 
c  TempC        0.30066E+02      27   0.36737E-03   0.51131E+01 0.22691E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6143          10.387          4.5729          4.5729
v  Velocity[Y]            -3.3771          7.0481       0.0074182       0.0074182
v  Velocity[Z]         -1.94e-014     8.3096e-015    -1.1876e-017    -1.1876e-017
v  ǁVelocityǁ        0.00053288          10.388          5.2119          5.2119
v  Pressure                 -55.2          20.697         -6.8413         -6.8413
v  nu_tilda           4.2934e-007       0.0042694       0.0010394       0.0010394
v  TempC                       21          73.074          21.664          21.664
v  TurbVisc           2.9893e-014       0.0050319       0.0012157       0.0012157
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              896:        0.19870E+01

===============================================================


 INSTANT    0.897000000E+03   TIME STEP NUMBER             897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81357E-02 0.88011E+00
   Friction velocity        uk    :  0.81357E-02 0.88011E+00
   Dimensionless distance   yplus :  0.65498E-01 0.70855E+01
   Friction thermal sca.    tstar : -0.58328E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48869E-01 0.52866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73357E-02      32   0.38409E-03   0.17673E+01 0.87886E+02 
c  Velocity[X]                                      0.10412E+01 
c  Velocity[Y]                                      0.72617E+00 
c  Velocity[Z]                                      0.93053E-30 
c  Pressure     0.11330E-06     424   0.97376E-08   0.11796E+00 0.30282E+03 
c  nu_tilda     0.49409E-05      31   0.75115E-05   0.18049E-06 0.12713E+03 
c  TempC        0.30077E+02      27   0.34636E-03   0.51998E+01 0.22157E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6124          10.388          4.5729          4.5729
v  Velocity[Y]            -3.3757          7.0262       0.0073533       0.0073533
v  Velocity[Z]       -1.9115e-014     8.3102e-015    -1.1858e-017    -1.1858e-017
v  ǁVelocityǁ        0.00094898          10.389          5.2122          5.2122
v  Pressure               -55.193          20.616         -6.8573         -6.8573
v  nu_tilda           4.2944e-007       0.0042694         0.00104         0.00104
v  TempC                       21          74.161          21.665          21.665
v  TurbVisc           2.9894e-014       0.0050319       0.0012164       0.0012164
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              897:        0.20430E+01

===============================================================


 INSTANT    0.898000000E+03   TIME STEP NUMBER             898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58248E-02 0.87894E+00
   Friction velocity        uk    :  0.58248E-02 0.87894E+00
   Dimensionless distance   yplus :  0.46894E-01 0.70760E+01
   Friction thermal sca.    tstar : -0.57767E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34988E-01 0.52795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73391E-02      32   0.33327E-03   0.17905E+01 0.88177E+02 
c  Velocity[X]                                      0.10425E+01 
c  Velocity[Y]                                      0.74798E+00 
c  Velocity[Z]                                      0.11034E-29 
c  Pressure     0.12674E-06     346   0.98245E-08   0.12964E+00 0.16951E+03 
c  nu_tilda     0.49425E-05      31   0.14638E-04   0.18052E-06 0.12712E+03 
c  TempC        0.30089E+02      26   0.53194E-03   0.52758E+01 0.22972E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6103          10.388          4.5729          4.5729
v  Velocity[Y]            -3.3744          7.0393       0.0072888       0.0072888
v  Velocity[Z]       -1.8865e-014     8.3077e-015    -1.1832e-017    -1.1832e-017
v  ǁVelocityǁ        0.00094608           10.39          5.2125          5.2125
v  Pressure               -55.202          20.664          -6.866          -6.866
v  nu_tilda           4.2951e-007       0.0042694       0.0010406       0.0010406
v  TempC                       21          73.331          21.665          21.665
v  TurbVisc           2.9921e-014       0.0050319       0.0012172       0.0012172
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              898:        0.18590E+01

===============================================================


 INSTANT    0.899000000E+03   TIME STEP NUMBER             899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98242E-02 0.87995E+00
   Friction velocity        uk    :  0.98242E-02 0.87995E+00
   Dimensionless distance   yplus :  0.79092E-01 0.70842E+01
   Friction thermal sca.    tstar : -0.62187E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59011E-01 0.52856E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73426E-02      32   0.39219E-03   0.17745E+01 0.88080E+02 
c  Velocity[X]                                      0.10397E+01 
c  Velocity[Y]                                      0.73482E+00 
c  Velocity[Z]                                      0.97281E-30 
c  Pressure     0.82539E-07     440   0.95698E-08   0.85993E-01 0.27898E+03 
c  nu_tilda     0.49441E-05      31   0.75130E-05   0.18054E-06 0.12711E+03 
c  TempC        0.30100E+02      26   0.42850E-03   0.79839E+01 0.30289E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6084          10.389          4.5729          4.5729
v  Velocity[Y]             -3.373          7.0206       0.0072248       0.0072248
v  Velocity[Z]       -1.8938e-014     8.3061e-015    -1.1818e-017    -1.1818e-017
v  ǁVelocityǁ         0.0012578           10.39          5.2127          5.2127
v  Pressure               -55.199          20.591         -6.8834         -6.8834
v  nu_tilda           4.2956e-007       0.0042694       0.0010413       0.0010413
v  TempC                       21          73.579          21.665          21.665
v  TurbVisc           2.9941e-014       0.0050319        0.001218        0.001218
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              899:        0.20840E+01

===============================================================


 INSTANT    0.900000000E+03   TIME STEP NUMBER             900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10143E-01 0.87932E+00
   Friction velocity        uk    :  0.10143E-01 0.87932E+00
   Dimensionless distance   yplus :  0.81656E-01 0.70791E+01
   Friction thermal sca.    tstar : -0.59923E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60924E-01 0.52818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73461E-02      32   0.35409E-03   0.17931E+01 0.88265E+02 
c  Velocity[X]                                      0.10635E+01 
c  Velocity[Y]                                      0.72961E+00 
c  Velocity[Z]                                      0.93881E-30 
c  Pressure     0.10264E-06     442   0.94861E-08   0.10483E+00 0.38539E+03 
c  nu_tilda     0.49457E-05      31   0.14627E-04   0.18057E-06 0.12710E+03 
c  TempC        0.30112E+02      27   0.46281E-03   0.61635E+01 0.24394E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6065           10.39          4.5729          4.5729
v  Velocity[Y]            -3.3716           7.045       0.0071611       0.0071611
v  Velocity[Z]        -1.885e-014     8.3063e-015    -1.1805e-017    -1.1805e-017
v  ǁVelocityǁ        0.00095894          10.391          5.2131          5.2131
v  Pressure               -55.199          20.693         -6.8721         -6.8721
v  nu_tilda           4.2959e-007       0.0042694       0.0010419       0.0010419
v  TempC                       21          73.073          21.666          21.666
v  TurbVisc           2.9954e-014       0.0050319       0.0012187       0.0012187
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              900:        0.20990E+01

===============================================================


 INSTANT    0.901000000E+03   TIME STEP NUMBER             901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44850E-02 0.88051E+00
   Friction velocity        uk    :  0.44850E-02 0.88051E+00
   Dimensionless distance   yplus :  0.36107E-01 0.70887E+01
   Friction thermal sca.    tstar : -0.60677E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26940E-01 0.52890E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73496E-02      32   0.32925E-03   0.17986E+01 0.88355E+02 
c  Velocity[X]                                      0.10465E+01 
c  Velocity[Y]                                      0.75202E+00 
c  Velocity[Z]                                      0.12180E-29 
c  Pressure     0.10881E-06     393   0.96681E-08   0.11000E+00 0.18664E+03 
c  nu_tilda     0.49473E-05      31   0.75194E-05   0.18060E-06 0.12708E+03 
c  TempC        0.30123E+02      27   0.36524E-03   0.77320E+01 0.27030E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6046           10.39          4.5729          4.5729
v  Velocity[Y]            -3.3703          7.0479       0.0070978       0.0070978
v  Velocity[Z]       -1.8672e-014     8.3055e-015    -1.1791e-017    -1.1791e-017
v  ǁVelocityǁ         0.0014444          10.391          5.2134          5.2134
v  Pressure               -55.198          20.678         -6.8823         -6.8823
v  nu_tilda           4.2961e-007       0.0042694       0.0010426       0.0010426
v  TempC                       21          73.076          21.666          21.666
v  TurbVisc           2.9963e-014       0.0050319       0.0012195       0.0012195
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              901:        0.19810E+01

===============================================================


 INSTANT    0.902000000E+03   TIME STEP NUMBER             902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11653E-01 0.88024E+00
   Friction velocity        uk    :  0.11653E-01 0.88024E+00
   Dimensionless distance   yplus :  0.93817E-01 0.70865E+01
   Friction thermal sca.    tstar : -0.64076E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69998E-01 0.52874E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73531E-02      32   0.30132E-03   0.17963E+01 0.88293E+02 
c  Velocity[X]                                      0.10574E+01 
c  Velocity[Y]                                      0.73890E+00 
c  Velocity[Z]                                      0.10517E-29 
c  Pressure     0.11867E-06     457   0.95715E-08   0.12479E+00 0.51994E+03 
c  nu_tilda     0.49488E-05      31   0.14632E-04   0.18064E-06 0.12707E+03 
c  TempC        0.30135E+02      26   0.40912E-03   0.49136E+01 0.22470E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6027          10.391          4.5729          4.5729
v  Velocity[Y]             -3.369           7.021       0.0070349       0.0070349
v  Velocity[Z]       -1.8316e-014     8.3127e-015    -1.1774e-017    -1.1774e-017
v  ǁVelocityǁ         0.0010288          10.392          5.2136          5.2136
v  Pressure               -55.194          20.584         -6.9116         -6.9116
v  nu_tilda           4.2963e-007       0.0042694       0.0010432       0.0010432
v  TempC                       21          73.618          21.666          21.666
v  TurbVisc           2.9967e-014       0.0050319       0.0012202       0.0012202
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              902:        0.21290E+01

===============================================================


 INSTANT    0.903000000E+03   TIME STEP NUMBER             903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71309E-02 0.87892E+00
   Friction velocity        uk    :  0.71309E-02 0.87892E+00
   Dimensionless distance   yplus :  0.57408E-01 0.70759E+01
   Friction thermal sca.    tstar : -0.62605E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42833E-01 0.52794E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73565E-02      32   0.40032E-03   0.17602E+01 0.88062E+02 
c  Velocity[X]                                      0.10309E+01 
c  Velocity[Y]                                      0.72934E+00 
c  Velocity[Z]                                      0.95158E-30 
c  Pressure     0.85098E-07     426   0.91447E-08   0.87664E-01 0.50937E+03 
c  nu_tilda     0.49504E-05      31   0.74999E-05   0.18068E-06 0.12706E+03 
c  TempC        0.30146E+02      26   0.45059E-03   0.50666E+01 0.22897E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.6007          10.391          4.5729          4.5729
v  Velocity[Y]            -3.3676          7.0437       0.0069725       0.0069725
v  Velocity[Z]       -1.8093e-014     8.3262e-015    -1.1758e-017    -1.1758e-017
v  ǁVelocityǁ         0.0010762          10.392          5.2139          5.2139
v  Pressure               -55.197          20.673         -6.8991         -6.8991
v  nu_tilda           4.2968e-007       0.0042694       0.0010438       0.0010438
v  TempC                       21          73.216          21.667          21.667
v  TurbVisc           2.9974e-014       0.0050319        0.001221        0.001221
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              903:        0.20340E+01

===============================================================


 INSTANT    0.904000000E+03   TIME STEP NUMBER             904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78651E-02 0.88008E+00
   Friction velocity        uk    :  0.78651E-02 0.88008E+00
   Dimensionless distance   yplus :  0.63320E-01 0.70853E+01
   Friction thermal sca.    tstar : -0.61045E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47244E-01 0.52864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73600E-02      32   0.35127E-03   0.18035E+01 0.88492E+02 
c  Velocity[X]                                      0.10527E+01 
c  Velocity[Y]                                      0.75080E+00 
c  Velocity[Z]                                      0.94873E-30 
c  Pressure     0.12110E-06     457   0.99811E-08   0.12449E+00 0.54973E+03 
c  nu_tilda     0.49520E-05      31   0.14657E-04   0.18071E-06 0.12705E+03 
c  TempC        0.30158E+02      27   0.45334E-03   0.56521E+01 0.24243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5986          10.392          4.5729          4.5729
v  Velocity[Y]            -3.3664           7.022       0.0069105       0.0069105
v  Velocity[Z]       -1.7953e-014     8.3436e-015    -1.1742e-017    -1.1742e-017
v  ǁVelocityǁ         0.0013694          10.393          5.2142          5.2142
v  Pressure               -55.195          20.574         -6.9302         -6.9302
v  nu_tilda           4.2974e-007       0.0042694       0.0010445       0.0010445
v  TempC                       21          73.242          21.667          21.667
v  TurbVisc           2.9987e-014       0.0050319       0.0012217       0.0012217
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              904:        0.21220E+01

===============================================================


 INSTANT    0.905000000E+03   TIME STEP NUMBER             905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11110E-01 0.87944E+00
   Friction velocity        uk    :  0.11110E-01 0.87944E+00
   Dimensionless distance   yplus :  0.89447E-01 0.70801E+01
   Friction thermal sca.    tstar : -0.70555E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66737E-01 0.52825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73635E-02      32   0.33414E-03   0.17868E+01 0.88274E+02 
c  Velocity[X]                                      0.10485E+01 
c  Velocity[Y]                                      0.73835E+00 
c  Velocity[Z]                                      0.99371E-30 
c  Pressure     0.12304E-06     458   0.95150E-08   0.12495E+00 0.68711E+03 
c  nu_tilda     0.49536E-05      31   0.75116E-05   0.18074E-06 0.12704E+03 
c  TempC        0.30169E+02      27   0.46879E-03   0.53379E+01 0.23558E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5967          10.393          4.5729          4.5729
v  Velocity[Y]            -3.3651          7.0426       0.0068492       0.0068492
v  Velocity[Z]       -1.7638e-014     8.3602e-015    -1.1719e-017    -1.1719e-017
v  ǁVelocityǁ        0.00050924          10.394          5.2145          5.2145
v  Pressure               -55.188          20.696         -6.9048         -6.9048
v  nu_tilda            4.298e-007       0.0042694       0.0010451       0.0010451
v  TempC                       21          74.143          21.667          21.667
v  TurbVisc           3.0006e-014       0.0050319       0.0012225       0.0012225
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              905:        0.21370E+01

===============================================================


 INSTANT    0.906000000E+03   TIME STEP NUMBER             906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35303E-02 0.88065E+00
   Friction velocity        uk    :  0.35303E-02 0.88065E+00
   Dimensionless distance   yplus :  0.28422E-01 0.70898E+01
   Friction thermal sca.    tstar : -0.64430E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21206E-01 0.52898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73669E-02      32   0.35445E-03   0.17571E+01 0.88119E+02 
c  Velocity[X]                                      0.10256E+01 
c  Velocity[Y]                                      0.73148E+00 
c  Velocity[Z]                                      0.11000E-29 
c  Pressure     0.87379E-07     442   0.91436E-08   0.90106E-01 0.26614E+03 
c  nu_tilda     0.49552E-05      31   0.14651E-04   0.18077E-06 0.12703E+03 
c  TempC        0.30181E+02      27   0.30448E-03   0.62794E+01 0.24389E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5946          10.393          4.5729          4.5729
v  Velocity[Y]            -3.3661          7.0499       0.0067878       0.0067878
v  Velocity[Z]       -1.7401e-014     8.3733e-015    -1.1705e-017    -1.1705e-017
v  ǁVelocityǁ        0.00034054          10.394          5.2148          5.2148
v  Pressure               -55.197           20.68         -6.9255         -6.9255
v  nu_tilda           4.2981e-007       0.0042694       0.0010457       0.0010457
v  TempC                       21          73.073          21.668          21.668
v  TurbVisc            3.002e-014       0.0050319       0.0012233       0.0012233
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              906:        0.20680E+01

===============================================================


 INSTANT    0.907000000E+03   TIME STEP NUMBER             907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64524E-02 0.88020E+00
   Friction velocity        uk    :  0.64524E-02 0.88020E+00
   Dimensionless distance   yplus :  0.51946E-01 0.70862E+01
   Friction thermal sca.    tstar : -0.67404E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38758E-01 0.52871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73704E-02      32   0.34068E-03   0.18082E+01 0.88660E+02 
c  Velocity[X]                                      0.10545E+01 
c  Velocity[Y]                                      0.75377E+00 
c  Velocity[Z]                                      0.98484E-30 
c  Pressure     0.10717E-06     442   0.91411E-08   0.11248E+00 0.35324E+03 
c  nu_tilda     0.49568E-05      31   0.75131E-05   0.18080E-06 0.12702E+03 
c  TempC        0.30192E+02      26   0.50399E-03   0.46977E+01 0.22142E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5925          10.394          4.5729          4.5729
v  Velocity[Y]            -3.3678           7.025        0.006727        0.006727
v  Velocity[Z]       -1.7254e-014     8.3848e-015    -1.1688e-017    -1.1688e-017
v  ǁVelocityǁ         0.0010439          10.395          5.2151          5.2151
v  Pressure                -55.19          20.589         -6.9474         -6.9474
v  nu_tilda           4.2985e-007       0.0042694       0.0010464       0.0010464
v  TempC                       21          73.366          21.668          21.668
v  TurbVisc           3.0023e-014       0.0050319        0.001224        0.001224
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              907:        0.20510E+01

===============================================================


 INSTANT    0.908000000E+03   TIME STEP NUMBER             908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89362E-02 0.87885E+00
   Friction velocity        uk    :  0.89362E-02 0.87885E+00
   Dimensionless distance   yplus :  0.71943E-01 0.70754E+01
   Friction thermal sca.    tstar : -0.74013E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53677E-01 0.52790E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73739E-02      32   0.35484E-03   0.17987E+01 0.88501E+02 
c  Velocity[X]                                      0.10589E+01 
c  Velocity[Y]                                      0.73983E+00 
c  Velocity[Z]                                      0.84490E-30 
c  Pressure     0.11644E-06     329   0.91256E-08   0.11744E+00 0.16293E+03 
c  nu_tilda     0.49584E-05      31   0.14657E-04   0.18084E-06 0.12701E+03 
c  TempC        0.30203E+02      27   0.42879E-03   0.87144E+01 0.30774E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5903          10.395          4.5729          4.5729
v  Velocity[Y]            -3.3703          7.0391       0.0066668       0.0066668
v  Velocity[Z]       -1.7149e-014     8.3958e-015    -1.1665e-017    -1.1665e-017
v  ǁVelocityǁ         0.0010122          10.396          5.2154          5.2154
v  Pressure               -55.193          20.628         -6.9522         -6.9522
v  nu_tilda           4.2991e-007       0.0042694        0.001047        0.001047
v  TempC                       21           73.41          21.669          21.669
v  TurbVisc           3.0035e-014       0.0050319       0.0012248       0.0012248
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              908:        0.18110E+01

===============================================================


 INSTANT    0.909000000E+03   TIME STEP NUMBER             909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68766E-02 0.88019E+00
   Friction velocity        uk    :  0.68766E-02 0.88019E+00
   Dimensionless distance   yplus :  0.55361E-01 0.70861E+01
   Friction thermal sca.    tstar : -0.72037E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41306E-01 0.52870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73773E-02      32   0.39762E-03   0.18220E+01 0.88769E+02 
c  Velocity[X]                                      0.10878E+01 
c  Velocity[Y]                                      0.73424E+00 
c  Velocity[Z]                                      0.11194E-29 
c  Pressure     0.12253E-06     392   0.99192E-08   0.12748E+00 0.22512E+03 
c  nu_tilda     0.49599E-05      31   0.75068E-05   0.18087E-06 0.12700E+03 
c  TempC        0.30215E+02      27   0.44992E-03   0.59749E+01 0.24633E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5882          10.395          4.5729          4.5729
v  Velocity[Y]            -3.3706          7.0216       0.0066069       0.0066069
v  Velocity[Z]       -1.6959e-014      8.411e-015     -1.165e-017     -1.165e-017
v  ǁVelocityǁ         0.0015591          10.396          5.2157          5.2157
v  Pressure               -55.183          20.585         -6.9606         -6.9606
v  nu_tilda           4.2998e-007       0.0042694       0.0010477       0.0010477
v  TempC                       21          73.073          21.669          21.669
v  TurbVisc           3.0053e-014       0.0050319       0.0012255       0.0012255
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              909:        0.19570E+01

===============================================================


 INSTANT    0.910000000E+03   TIME STEP NUMBER             910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12438E-01 0.87961E+00
   Friction velocity        uk    :  0.12438E-01 0.87961E+00
   Dimensionless distance   yplus :  0.10014E+00 0.70814E+01
   Friction thermal sca.    tstar : -0.70826E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74714E-01 0.52835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73808E-02      32   0.32723E-03   0.18030E+01 0.88724E+02 
c  Velocity[X]                                      0.10498E+01 
c  Velocity[Y]                                      0.75321E+00 
c  Velocity[Z]                                      0.10119E-29 
c  Pressure     0.10422E-06     312   0.92523E-08   0.10666E+00 0.21067E+03 
c  nu_tilda     0.49615E-05      31   0.14679E-04   0.18092E-06 0.12699E+03 
c  TempC        0.30226E+02      27   0.43621E-03   0.59338E+01 0.26187E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5862          10.396          4.5729          4.5729
v  Velocity[Y]            -3.3735          7.0438       0.0065475       0.0065475
v  Velocity[Z]       -1.6886e-014     8.4274e-015    -1.1628e-017    -1.1628e-017
v  ǁVelocityǁ         0.0009566          10.397           5.216           5.216
v  Pressure               -55.192          20.653         -6.9658         -6.9658
v  nu_tilda           4.2998e-007       0.0042694       0.0010483       0.0010483
v  TempC                       21          73.681          21.669          21.669
v  TurbVisc           3.0072e-014       0.0050319       0.0012263       0.0012263
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              910:        0.17670E+01

===============================================================


 INSTANT    0.911000000E+03   TIME STEP NUMBER             911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49185E-02 0.88085E+00
   Friction velocity        uk    :  0.49185E-02 0.88085E+00
   Dimensionless distance   yplus :  0.39597E-01 0.70914E+01
   Friction thermal sca.    tstar : -0.84368E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29544E-01 0.52910E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73842E-02      32   0.36386E-03   0.17614E+01 0.88338E+02 
c  Velocity[X]                                      0.10209E+01 
c  Velocity[Y]                                      0.74048E+00 
c  Velocity[Z]                                      0.13165E-29 
c  Pressure     0.77555E-07     377   0.95917E-08   0.79493E-01 0.25888E+03 
c  nu_tilda     0.49631E-05      31   0.75126E-05   0.18095E-06 0.12698E+03 
c  TempC        0.30238E+02      26   0.31545E-03   0.82376E+01 0.29272E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5841          10.397          4.5729          4.5729
v  Velocity[Y]            -3.3766          7.0551       0.0064886       0.0064886
v  Velocity[Z]       -1.6798e-014     8.4422e-015    -1.1613e-017    -1.1613e-017
v  ǁVelocityǁ         0.0011926          10.398          5.2163          5.2163
v  Pressure               -55.186          20.666         -6.9654         -6.9654
v  nu_tilda           4.2999e-007       0.0042694       0.0010489       0.0010489
v  TempC                       21          73.072           21.67           21.67
v  TurbVisc           3.0072e-014       0.0050319       0.0012271       0.0012271
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              911:        0.19240E+01

===============================================================


 INSTANT    0.912000000E+03   TIME STEP NUMBER             912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95911E-02 0.88048E+00
   Friction velocity        uk    :  0.95911E-02 0.88048E+00
   Dimensionless distance   yplus :  0.77215E-01 0.70885E+01
   Friction thermal sca.    tstar : -0.76459E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57611E-01 0.52888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73877E-02      32   0.37340E-03   0.17987E+01 0.88598E+02 
c  Velocity[X]                                      0.10641E+01 
c  Velocity[Y]                                      0.73458E+00 
c  Velocity[Z]                                      0.11789E-29 
c  Pressure     0.11966E-06     458   0.91880E-08   0.12340E+00 0.59977E+03 
c  nu_tilda     0.49647E-05      31   0.14676E-04   0.18100E-06 0.12698E+03 
c  TempC        0.30249E+02      27   0.48323E-03   0.54082E+01 0.23924E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.582          10.397          4.5729          4.5729
v  Velocity[Y]            -3.3794          7.0255         0.00643         0.00643
v  Velocity[Z]       -1.6677e-014     8.4597e-015    -1.1594e-017    -1.1594e-017
v  ǁVelocityǁ         0.0012248          10.398          5.2166          5.2166
v  Pressure                -55.18           20.55         -6.9975         -6.9975
v  nu_tilda           4.3009e-007       0.0042694       0.0010496       0.0010496
v  TempC                       21          73.498           21.67           21.67
v  TurbVisc           3.0076e-014       0.0050319       0.0012278       0.0012278
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              912:        0.21270E+01

===============================================================


 INSTANT    0.913000000E+03   TIME STEP NUMBER             913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99138E-02 0.87924E+00
   Friction velocity        uk    :  0.99138E-02 0.87924E+00
   Dimensionless distance   yplus :  0.79813E-01 0.70785E+01
   Friction thermal sca.    tstar : -0.79519E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59550E-01 0.52813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73911E-02      32   0.35871E-03   0.18155E+01 0.88901E+02 
c  Velocity[X]                                      0.10575E+01 
c  Velocity[Y]                                      0.75794E+00 
c  Velocity[Z]                                      0.10677E-29 
c  Pressure     0.10932E-06     426   0.98386E-08   0.11120E+00 0.54809E+03 
c  nu_tilda     0.49663E-05      31   0.75150E-05   0.18104E-06 0.12697E+03 
c  TempC        0.30261E+02      26   0.42915E-03   0.73455E+01 0.28110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5799          10.398          4.5729          4.5729
v  Velocity[Y]            -3.3807          7.0447       0.0063717       0.0063717
v  Velocity[Z]       -1.6509e-014     8.4696e-015    -1.1581e-017    -1.1581e-017
v  ǁVelocityǁ        0.00094679          10.399          5.2169          5.2169
v  Pressure               -55.178          20.651         -6.9824         -6.9824
v  nu_tilda           4.3015e-007       0.0042694       0.0010502       0.0010502
v  TempC                       21          73.072           21.67           21.67
v  TurbVisc           3.0102e-014       0.0050319       0.0012286       0.0012286
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              913:        0.20380E+01

===============================================================


 INSTANT    0.914000000E+03   TIME STEP NUMBER             914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44347E-02 0.88047E+00
   Friction velocity        uk    :  0.44347E-02 0.88047E+00
   Dimensionless distance   yplus :  0.35702E-01 0.70884E+01
   Friction thermal sca.    tstar : -0.93034E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26638E-01 0.52887E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73946E-02      32   0.33790E-03   0.18078E+01 0.88856E+02 
c  Velocity[X]                                      0.10648E+01 
c  Velocity[Y]                                      0.74298E+00 
c  Velocity[Z]                                      0.10272E-29 
c  Pressure     0.12122E-06     441   0.92845E-08   0.12665E+00 0.43003E+03 
c  nu_tilda     0.49679E-05      31   0.14677E-04   0.18108E-06 0.12696E+03 
c  TempC        0.30272E+02      27   0.35413E-03   0.50112E+01 0.22910E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5777          10.398          4.5729          4.5729
v  Velocity[Y]            -3.3831           7.025       0.0063142       0.0063142
v  Velocity[Z]       -1.6295e-014     8.4805e-015    -1.1559e-017    -1.1559e-017
v  ǁVelocityǁ          0.001501            10.4          5.2172          5.2172
v  Pressure               -55.176          20.578         -7.0072         -7.0072
v  nu_tilda           4.3019e-007       0.0042694       0.0010508       0.0010508
v  TempC                       21          73.072          21.671          21.671
v  TurbVisc           3.0118e-014       0.0050319       0.0012293       0.0012293
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              914:        0.20670E+01

===============================================================


 INSTANT    0.915000000E+03   TIME STEP NUMBER             915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12092E-01 0.87954E+00
   Friction velocity        uk    :  0.12092E-01 0.87954E+00
   Dimensionless distance   yplus :  0.97346E-01 0.70809E+01
   Friction thermal sca.    tstar : -0.88122E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72631E-01 0.52831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73980E-02      32   0.35460E-03   0.17793E+01 0.88571E+02 
c  Velocity[X]                                      0.10442E+01 
c  Velocity[Y]                                      0.73512E+00 
c  Velocity[Z]                                      0.10924E-29 
c  Pressure     0.91859E-07     425   0.96692E-08   0.93903E-01 0.51017E+03 
c  nu_tilda     0.49695E-05      31   0.74934E-05   0.18112E-06 0.12695E+03 
c  TempC        0.30283E+02      27   0.45145E-03   0.38648E+01 0.19877E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5755          10.399          4.5729          4.5729
v  Velocity[Y]             -3.385          7.0506       0.0062569       0.0062569
v  Velocity[Z]       -1.6038e-014     8.4934e-015    -1.1544e-017    -1.1544e-017
v  ǁVelocityǁ         0.0002215            10.4          5.2174          5.2174
v  Pressure               -55.176          20.671         -6.9945         -6.9945
v  nu_tilda           4.3021e-007       0.0042694       0.0010515       0.0010515
v  TempC                       21           74.06          21.671          21.671
v  TurbVisc            3.013e-014       0.0050319       0.0012301       0.0012301
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              915:        0.20250E+01

===============================================================


 INSTANT    0.916000000E+03   TIME STEP NUMBER             916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38032E-02 0.88071E+00
   Friction velocity        uk    :  0.38032E-02 0.88071E+00
   Dimensionless distance   yplus :  0.30618E-01 0.70903E+01
   Friction thermal sca.    tstar : -0.85878E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22844E-01 0.52902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74015E-02      32   0.37400E-03   0.17962E+01 0.88762E+02 
c  Velocity[X]                                      0.10402E+01 
c  Velocity[Y]                                      0.75602E+00 
c  Velocity[Z]                                      0.97678E-30 
c  Pressure     0.12882E-06     425   0.98732E-08   0.12967E+00 0.33350E+03 
c  nu_tilda     0.49710E-05      31   0.14702E-04   0.18116E-06 0.12694E+03 
c  TempC        0.30295E+02      27   0.41410E-03   0.62898E+01 0.25575E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5733            10.4          4.5729          4.5729
v  Velocity[Y]            -3.3877          7.0512       0.0062001       0.0062001
v  Velocity[Z]       -1.5853e-014     8.5124e-015    -1.1519e-017    -1.1519e-017
v  ǁVelocityǁ         0.0001494          10.401          5.2177          5.2177
v  Pressure               -55.172          20.629         -7.0148         -7.0148
v  nu_tilda            4.302e-007       0.0042694       0.0010521       0.0010521
v  TempC                       21          73.072          21.671          21.671
v  TurbVisc           3.0137e-014       0.0050319       0.0012309       0.0012309
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              916:        0.20550E+01

===============================================================


 INSTANT    0.917000000E+03   TIME STEP NUMBER             917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37467E-02 0.88046E+00
   Friction velocity        uk    :  0.37467E-02 0.88046E+00
   Dimensionless distance   yplus :  0.30163E-01 0.70883E+01
   Friction thermal sca.    tstar : -0.11244E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22505E-01 0.52887E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74049E-02      32   0.33648E-03   0.18387E+01 0.89150E+02 
c  Velocity[X]                                      0.10942E+01 
c  Velocity[Y]                                      0.74453E+00 
c  Velocity[Z]                                      0.10604E-29 
c  Pressure     0.13165E-06     329   0.95737E-08   0.13745E+00 0.23039E+03 
c  nu_tilda     0.49726E-05      31   0.74978E-05   0.18120E-06 0.12694E+03 
c  TempC        0.30306E+02      27   0.45002E-03   0.68654E+01 0.24480E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5712            10.4          4.5729          4.5729
v  Velocity[Y]            -3.3892          7.0275       0.0061438       0.0061438
v  Velocity[Z]       -1.5565e-014     8.5281e-015    -1.1503e-017    -1.1503e-017
v  ǁVelocityǁ         0.0013826          10.401           5.218           5.218
v  Pressure               -55.159          20.596         -7.0188         -7.0188
v  nu_tilda           4.3025e-007       0.0042694       0.0010528       0.0010528
v  TempC                       21          73.097          21.672          21.672
v  TurbVisc           3.0133e-014       0.0050319       0.0012316       0.0012316
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              917:        0.18110E+01

===============================================================


 INSTANT    0.918000000E+03   TIME STEP NUMBER             918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11270E-01 0.87921E+00
   Friction velocity        uk    :  0.11270E-01 0.87921E+00
   Dimensionless distance   yplus :  0.90728E-01 0.70783E+01
   Friction thermal sca.    tstar : -0.97729E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67693E-01 0.52812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74084E-02      32   0.34932E-03   0.17828E+01 0.88693E+02 
c  Velocity[X]                                      0.10462E+01 
c  Velocity[Y]                                      0.73657E+00 
c  Velocity[Z]                                      0.99400E-30 
c  Pressure     0.86762E-07     328   0.95770E-08   0.89434E-01 0.18019E+03 
c  nu_tilda     0.49742E-05      31   0.14697E-04   0.18124E-06 0.12693E+03 
c  TempC        0.30318E+02      27   0.38131E-03   0.54385E+01 0.22862E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.569          10.401          4.5729          4.5729
v  Velocity[Y]             -3.392          7.0468       0.0060877       0.0060877
v  Velocity[Z]       -1.5356e-014     8.5414e-015    -1.1479e-017    -1.1479e-017
v  ǁVelocityǁ        0.00092972          10.402          5.2183          5.2183
v  Pressure               -55.167          20.651         -7.0263         -7.0263
v  nu_tilda           4.3029e-007       0.0042694       0.0010534       0.0010534
v  TempC                       21          74.121          21.672          21.672
v  TurbVisc           3.0146e-014       0.0050319       0.0012324       0.0012324
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              918:        0.18190E+01

===============================================================


 INSTANT    0.919000000E+03   TIME STEP NUMBER             919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19695E-02 0.88016E+00
   Friction velocity        uk    :  0.19695E-02 0.88016E+00
   Dimensionless distance   yplus :  0.15856E-01 0.70859E+01
   Friction thermal sca.    tstar : -0.10157E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11830E-01 0.52868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74118E-02      32   0.33728E-03   0.18089E+01 0.88982E+02 
c  Velocity[X]                                      0.10482E+01 
c  Velocity[Y]                                      0.76069E+00 
c  Velocity[Z]                                      0.10905E-29 
c  Pressure     0.10578E-06     425   0.92032E-08   0.10938E+00 0.39314E+03 
c  nu_tilda     0.49758E-05      31   0.74973E-05   0.18128E-06 0.12692E+03 
c  TempC        0.30329E+02      27   0.35002E-03   0.51592E+01 0.21237E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5668          10.401          4.5729          4.5729
v  Velocity[Y]            -3.3936          7.0231       0.0060324       0.0060324
v  Velocity[Z]       -1.5102e-014     8.5506e-015     -1.146e-017     -1.146e-017
v  ǁVelocityǁ         0.0013551          10.402          5.2186          5.2186
v  Pressure               -55.157          20.548         -7.0498         -7.0498
v  nu_tilda           4.3039e-007       0.0042694        0.001054        0.001054
v  TempC                       21          73.072          21.673          21.673
v  TurbVisc           3.0158e-014       0.0050319       0.0012331       0.0012331
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              919:        0.20400E+01

===============================================================


 INSTANT    0.920000000E+03   TIME STEP NUMBER             920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11079E-01 0.87958E+00
   Friction velocity        uk    :  0.11079E-01 0.87958E+00
   Dimensionless distance   yplus :  0.89197E-01 0.70812E+01
   Friction thermal sca.    tstar : -0.13773E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66551E-01 0.52834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74153E-02      32   0.34508E-03   0.17931E+01 0.88849E+02 
c  Velocity[X]                                      0.10472E+01 
c  Velocity[Y]                                      0.74599E+00 
c  Velocity[Z]                                      0.90442E-30 
c  Pressure     0.86656E-07     410   0.98979E-08   0.88312E-01 0.29733E+03 
c  nu_tilda     0.49774E-05      31   0.14701E-04   0.18133E-06 0.12692E+03 
c  TempC        0.30340E+02      26   0.47827E-03   0.49879E+01 0.22242E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5647          10.402          4.5729          4.5729
v  Velocity[Y]            -3.3958          7.0451       0.0059774       0.0059774
v  Velocity[Z]       -1.4948e-014     8.5612e-015    -1.1435e-017    -1.1435e-017
v  ǁVelocityǁ         0.0010742          10.403          5.2189          5.2189
v  Pressure               -55.159          20.633         -7.0455         -7.0455
v  nu_tilda           4.3043e-007       0.0042694       0.0010547       0.0010547
v  TempC                       21          74.003          21.673          21.673
v  TurbVisc           3.0187e-014       0.0050319       0.0012339       0.0012339
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              920:        0.20170E+01

===============================================================


 INSTANT    0.921000000E+03   TIME STEP NUMBER             921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81977E-02 0.88096E+00
   Friction velocity        uk    :  0.81977E-02 0.88096E+00
   Dimensionless distance   yplus :  0.65997E-01 0.70924E+01
   Friction thermal sca.    tstar : -0.12325E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49241E-01 0.52917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74187E-02      32   0.38882E-03   0.17958E+01 0.88875E+02 
c  Velocity[X]                                      0.10562E+01 
c  Velocity[Y]                                      0.73962E+00 
c  Velocity[Z]                                      0.14053E-29 
c  Pressure     0.11638E-06     442   0.91888E-08   0.11979E+00 0.39383E+03 
c  nu_tilda     0.49790E-05      31   0.74862E-05   0.18138E-06 0.12691E+03 
c  TempC        0.30352E+02      27   0.44258E-03   0.74722E+01 0.26902E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5627          10.402          4.5729          4.5729
v  Velocity[Y]            -3.3969          7.0577        0.005923        0.005923
v  Velocity[Z]       -1.4754e-014     8.5704e-015    -1.1417e-017    -1.1417e-017
v  ǁVelocityǁ         0.0010047          10.403          5.2192          5.2192
v  Pressure               -55.149           20.68         -7.0355         -7.0355
v  nu_tilda           4.3037e-007       0.0042694       0.0010553       0.0010553
v  TempC                       21          73.072          21.673          21.673
v  TurbVisc           3.0197e-014       0.0050319       0.0012347       0.0012347
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              921:        0.20910E+01

===============================================================


 INSTANT    0.922000000E+03   TIME STEP NUMBER             922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69605E-02 0.88056E+00
   Friction velocity        uk    :  0.69605E-02 0.88056E+00
   Dimensionless distance   yplus :  0.56037E-01 0.70891E+01
   Friction thermal sca.    tstar : -0.10957E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41810E-01 0.52893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74222E-02      32   0.31589E-03   0.18327E+01 0.89282E+02 
c  Velocity[X]                                      0.10722E+01 
c  Velocity[Y]                                      0.76053E+00 
c  Velocity[Z]                                      0.13081E-29 
c  Pressure     0.12270E-06     485   0.96032E-08   0.12637E+00 0.94766E+03 
c  nu_tilda     0.49806E-05      31   0.14724E-04   0.18143E-06 0.12691E+03 
c  TempC        0.30363E+02      26   0.32606E-03   0.57356E+01 0.24126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5604          10.403          4.5729          4.5729
v  Velocity[Y]            -3.4003          7.0244       0.0058689       0.0058689
v  Velocity[Z]       -1.4696e-014     8.5818e-015    -1.1394e-017    -1.1394e-017
v  ǁVelocityǁ         0.0014352          10.404          5.2195          5.2195
v  Pressure               -55.151          20.501         -7.0904         -7.0904
v  nu_tilda           4.3041e-007       0.0042694       0.0010559       0.0010559
v  TempC                       21          73.175          21.674          21.674
v  TurbVisc           3.0182e-014       0.0050319       0.0012354       0.0012354
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              922:        0.23840E+01

===============================================================


 INSTANT    0.923000000E+03   TIME STEP NUMBER             923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11667E-01 0.87952E+00
   Friction velocity        uk    :  0.11667E-01 0.87952E+00
   Dimensionless distance   yplus :  0.93925E-01 0.70807E+01
   Friction thermal sca.    tstar : -0.20005E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70079E-01 0.52830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74256E-02      32   0.30601E-03   0.17852E+01 0.88846E+02 
c  Velocity[X]                                      0.10390E+01 
c  Velocity[Y]                                      0.74615E+00 
c  Velocity[Z]                                      0.10343E-29 
c  Pressure     0.92113E-07     457   0.92467E-08   0.94896E-01 0.81459E+03 
c  nu_tilda     0.49821E-05      31   0.74870E-05   0.18147E-06 0.12690E+03 
c  TempC        0.30375E+02      27   0.43311E-03   0.36056E+01 0.19356E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5582          10.403          4.5729          4.5729
v  Velocity[Y]            -3.4016          7.0474       0.0058152       0.0058152
v  Velocity[Z]       -1.4587e-014     8.5981e-015    -1.1377e-017    -1.1377e-017
v  ǁVelocityǁ        0.00093701          10.404          5.2197          5.2197
v  Pressure               -55.147          20.656         -7.0602         -7.0602
v  nu_tilda           4.3048e-007       0.0042694       0.0010566       0.0010566
v  TempC                       21          73.364          21.674          21.674
v  TurbVisc           3.0194e-014       0.0050319       0.0012362       0.0012362
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              923:        0.23340E+01

===============================================================


 INSTANT    0.924000000E+03   TIME STEP NUMBER             924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43061E-02 0.88053E+00
   Friction velocity        uk    :  0.43061E-02 0.88053E+00
   Dimensionless distance   yplus :  0.34667E-01 0.70889E+01
   Friction thermal sca.    tstar : -0.15834E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25866E-01 0.52891E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74290E-02      32   0.38863E-03   0.17886E+01 0.88875E+02 
c  Velocity[X]                                      0.10493E+01 
c  Velocity[Y]                                      0.73935E+00 
c  Velocity[Z]                                      0.91495E-30 
c  Pressure     0.10885E-06     457   0.96201E-08   0.11354E+00 0.62806E+03 
c  nu_tilda     0.49837E-05      31   0.14717E-04   0.18153E-06 0.12690E+03 
c  TempC        0.30386E+02      27   0.43312E-03   0.59299E+01 0.24651E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.556          10.403          4.5729          4.5729
v  Velocity[Y]            -3.4036          7.0263        0.005762        0.005762
v  Velocity[Z]        -1.452e-014     8.6134e-015    -1.1357e-017    -1.1357e-017
v  ǁVelocityǁ         0.0012713          10.404            5.22            5.22
v  Pressure                -55.14          20.535         -7.0938         -7.0938
v  nu_tilda           4.3055e-007       0.0042694       0.0010572       0.0010572
v  TempC                       21          73.096          21.674          21.674
v  TurbVisc           3.0213e-014       0.0050319       0.0012369       0.0012369
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              924:        0.21210E+01

===============================================================


 INSTANT    0.925000000E+03   TIME STEP NUMBER             925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10422E-01 0.87977E+00
   Friction velocity        uk    :  0.10422E-01 0.87977E+00
   Dimensionless distance   yplus :  0.83906E-01 0.70828E+01
   Friction thermal sca.    tstar : -0.14782E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62603E-01 0.52846E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74324E-02      32   0.37235E-03   0.18365E+01 0.89415E+02 
c  Velocity[X]                                      0.10736E+01 
c  Velocity[Y]                                      0.76286E+00 
c  Velocity[Z]                                      0.10964E-29 
c  Pressure     0.11633E-06     457   0.90237E-08   0.11802E+00 0.60302E+03 
c  nu_tilda     0.49853E-05      31   0.74944E-05   0.18157E-06 0.12689E+03 
c  TempC        0.30397E+02      26   0.30320E-03   0.72076E+01 0.27155E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5538          10.404          4.5729          4.5729
v  Velocity[Y]            -3.4049          7.0523       0.0057092       0.0057092
v  Velocity[Z]       -1.4455e-014     8.6231e-015    -1.1343e-017    -1.1343e-017
v  ǁVelocityǁ        0.00024999          10.405          5.2203          5.2203
v  Pressure               -55.136          20.651         -7.0761         -7.0761
v  nu_tilda           4.3059e-007       0.0042694       0.0010579       0.0010579
v  TempC                       21          73.071          21.675          21.675
v  TurbVisc           3.0232e-014       0.0050319       0.0012377       0.0012377
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              925:        0.21450E+01

===============================================================


 INSTANT    0.926000000E+03   TIME STEP NUMBER             926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38352E-02 0.88104E+00
   Friction velocity        uk    :  0.38352E-02 0.88104E+00
   Dimensionless distance   yplus :  0.30876E-01 0.70929E+01
   Friction thermal sca.    tstar : -0.55076E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23037E-01 0.52921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74359E-02      32   0.31168E-03   0.18176E+01 0.89184E+02 
c  Velocity[X]                                      0.10700E+01 
c  Velocity[Y]                                      0.74766E+00 
c  Velocity[Z]                                      0.95892E-30 
c  Pressure     0.13405E-06     409   0.96581E-08   0.13516E+00 0.26154E+03 
c  nu_tilda     0.49869E-05      31   0.14720E-04   0.18162E-06 0.12689E+03 
c  TempC        0.30409E+02      26   0.47479E-03   0.46536E+01 0.22468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5515          10.404          4.5729          4.5729
v  Velocity[Y]            -3.4068          7.0546        0.005657        0.005657
v  Velocity[Z]       -1.4343e-014     8.6363e-015    -1.1323e-017    -1.1323e-017
v  ǁVelocityǁ         0.0005429          10.405          5.2206          5.2206
v  Pressure               -55.133          20.624         -7.0919         -7.0919
v  nu_tilda           4.3059e-007       0.0042694       0.0010585       0.0010585
v  TempC                       21          73.895          21.675          21.675
v  TurbVisc           3.0244e-014       0.0050319       0.0012385       0.0012385
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              926:        0.19860E+01

===============================================================


 INSTANT    0.927000000E+03   TIME STEP NUMBER             927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43761E-02 0.88080E+00
   Friction velocity        uk    :  0.43761E-02 0.88080E+00
   Dimensionless distance   yplus :  0.35230E-01 0.70910E+01
   Friction thermal sca.    tstar : -0.35613E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26286E-01 0.52907E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74393E-02      32   0.33745E-03   0.18023E+01 0.89019E+02 
c  Velocity[X]                                      0.10608E+01 
c  Velocity[Y]                                      0.74150E+00 
c  Velocity[Z]                                      0.95447E-30 
c  Pressure     0.10335E-06     409   0.99898E-08   0.10826E+00 0.25292E+03 
c  nu_tilda     0.49885E-05      31   0.74723E-05   0.18167E-06 0.12688E+03 
c  TempC        0.30420E+02      26   0.43079E-03   0.67951E+01 0.27360E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5492          10.405          4.5729          4.5729
v  Velocity[Y]            -3.4079          7.0298        0.005605        0.005605
v  Velocity[Z]       -1.4187e-014     8.6426e-015    -1.1305e-017    -1.1305e-017
v  ǁVelocityǁ         0.0015699          10.406          5.2209          5.2209
v  Pressure               -55.125          20.563         -7.1083         -7.1083
v  nu_tilda           4.3063e-007       0.0042694       0.0010592       0.0010592
v  TempC                       21          73.071          21.675          21.675
v  TurbVisc           3.0242e-014       0.0050319       0.0012392       0.0012392
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              927:        0.20090E+01

===============================================================


 INSTANT    0.928000000E+03   TIME STEP NUMBER             928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12571E-01 0.87941E+00
   Friction velocity        uk    :  0.12571E-01 0.87941E+00
   Dimensionless distance   yplus :  0.10121E+00 0.70799E+01
   Friction thermal sca.    tstar : -0.24838E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75512E-01 0.52824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74427E-02      32   0.36207E-03   0.17982E+01 0.89160E+02 
c  Velocity[X]                                      0.10382E+01 
c  Velocity[Y]                                      0.76006E+00 
c  Velocity[Z]                                      0.94579E-30 
c  Pressure     0.93236E-07     345   0.91081E-08   0.95484E-01 0.19783E+03 
c  nu_tilda     0.49901E-05      31   0.14749E-04   0.18172E-06 0.12688E+03 
c  TempC        0.30432E+02      26   0.34969E-03   0.75317E+01 0.27064E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5469          10.405          4.5729          4.5729
v  Velocity[Y]            -3.4098          7.0478       0.0055535       0.0055535
v  Velocity[Z]        -1.404e-014     8.6553e-015    -1.1291e-017    -1.1291e-017
v  ǁVelocityǁ         0.0009585          10.406          5.2211          5.2211
v  Pressure               -55.123          20.619         -7.1106         -7.1106
v  nu_tilda           4.3064e-007       0.0042694       0.0010598       0.0010598
v  TempC                       21          73.228          21.676          21.676
v  TurbVisc           3.0254e-014       0.0050319         0.00124         0.00124
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              928:        0.18520E+01

===============================================================


 INSTANT    0.929000000E+03   TIME STEP NUMBER             929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57483E-02 0.88049E+00
   Friction velocity        uk    :  0.57483E-02 0.88049E+00
   Dimensionless distance   yplus :  0.46278E-01 0.70886E+01
   Friction thermal sca.    tstar : -0.19032E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34528E-01 0.52889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74461E-02      32   0.36980E-03   0.18189E+01 0.89272E+02 
c  Velocity[X]                                      0.10695E+01 
c  Velocity[Y]                                      0.74947E+00 
c  Velocity[Z]                                      0.14726E-29 
c  Pressure     0.14114E-06     377   0.95645E-08   0.14471E+00 0.25355E+03 
c  nu_tilda     0.49917E-05      31   0.74748E-05   0.18176E-06 0.12688E+03 
c  TempC        0.30443E+02      27   0.43268E-03   0.53559E+01 0.22263E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5448          10.405          4.5729          4.5729
v  Velocity[Y]            -3.4103           7.031       0.0055025       0.0055025
v  Velocity[Z]       -1.3778e-014     8.6665e-015    -1.1276e-017    -1.1276e-017
v  ǁVelocityǁ         0.0011388          10.407          5.2214          5.2214
v  Pressure               -55.107          20.562         -7.1173         -7.1173
v  nu_tilda           4.3072e-007       0.0042694       0.0010604       0.0010604
v  TempC                       21          73.071          21.676          21.676
v  TurbVisc           3.0258e-014       0.0050319       0.0012408       0.0012408
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              929:        0.19360E+01

===============================================================


 INSTANT    0.930000000E+03   TIME STEP NUMBER             930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91447E-02 0.87997E+00
   Friction velocity        uk    :  0.91447E-02 0.87997E+00
   Dimensionless distance   yplus :  0.73621E-01 0.70844E+01
   Friction thermal sca.    tstar : -0.21034E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54929E-01 0.52858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74495E-02      32   0.34157E-03   0.18083E+01 0.89162E+02 
c  Velocity[X]                                      0.10657E+01 
c  Velocity[Y]                                      0.74259E+00 
c  Velocity[Z]                                      0.11158E-29 
c  Pressure     0.10139E-06     297   0.93034E-08   0.10300E+00 0.20295E+03 
c  nu_tilda     0.49932E-05      31   0.14741E-04   0.18182E-06 0.12687E+03 
c  TempC        0.30454E+02      26   0.46834E-03   0.62983E+01 0.25526E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5427          10.406          4.5729          4.5729
v  Velocity[Y]             -3.412          7.0491       0.0054518       0.0054518
v  Velocity[Z]       -1.3652e-014     8.6762e-015    -1.1259e-017    -1.1259e-017
v  ǁVelocityǁ         0.0012445          10.407          5.2217          5.2217
v  Pressure               -55.114          20.628         -7.1237         -7.1237
v  nu_tilda           4.3079e-007       0.0042694       0.0010611       0.0010611
v  TempC                       21          73.407          21.676          21.676
v  TurbVisc           3.0281e-014       0.0050319       0.0012415       0.0012415
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              930:        0.17380E+01

===============================================================


 INSTANT    0.931000000E+03   TIME STEP NUMBER             931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10205E-01 0.88109E+00
   Friction velocity        uk    :  0.10205E-01 0.88109E+00
   Dimensionless distance   yplus :  0.82157E-01 0.70934E+01
   Friction thermal sca.    tstar : -0.26933E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61298E-01 0.52924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74530E-02      32   0.32273E-03   0.17961E+01 0.89194E+02 
c  Velocity[X]                                      0.10300E+01 
c  Velocity[Y]                                      0.76611E+00 
c  Velocity[Z]                                      0.10566E-29 
c  Pressure     0.11409E-06     298   0.97718E-08   0.11692E+00 0.21357E+03 
c  nu_tilda     0.49948E-05      31   0.74735E-05   0.18187E-06 0.12687E+03 
c  TempC        0.30466E+02      27   0.33605E-03   0.75456E+01 0.28415E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5405          10.406          4.5729          4.5729
v  Velocity[Y]            -3.4133          7.0561       0.0054015       0.0054015
v  Velocity[Z]       -1.3458e-014     8.6865e-015    -1.1244e-017    -1.1244e-017
v  ǁVelocityǁ        0.00092774          10.407           5.222           5.222
v  Pressure               -55.104          20.628         -7.1279         -7.1279
v  nu_tilda           4.3078e-007       0.0042694       0.0010617       0.0010617
v  TempC                       21          73.546          21.677          21.677
v  TurbVisc           3.0298e-014       0.0050319       0.0012423       0.0012423
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              931:        0.17390E+01

===============================================================


 INSTANT    0.932000000E+03   TIME STEP NUMBER             932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41042E-02 0.88076E+00
   Friction velocity        uk    :  0.41042E-02 0.88076E+00
   Dimensionless distance   yplus :  0.33041E-01 0.70907E+01
   Friction thermal sca.    tstar : -0.12741E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24653E-01 0.52905E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74564E-02      32   0.31306E-03   0.18102E+01 0.89267E+02 
c  Velocity[X]                                      0.10584E+01 
c  Velocity[Y]                                      0.75185E+00 
c  Velocity[Z]                                      0.10205E-29 
c  Pressure     0.11747E-06     441   0.92198E-08   0.12319E+00 0.46436E+03 
c  nu_tilda     0.49964E-05      31   0.14744E-04   0.18193E-06 0.12687E+03 
c  TempC        0.30477E+02      26   0.49992E-03   0.48301E+01 0.23562E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5384          10.406          4.5729          4.5729
v  Velocity[Y]            -3.4151           7.031       0.0053519       0.0053519
v  Velocity[Z]       -1.3238e-014     8.7017e-015    -1.1228e-017    -1.1228e-017
v  ǁVelocityǁ         0.0014749          10.407          5.2222          5.2222
v  Pressure               -55.097          20.543         -7.1529         -7.1529
v  nu_tilda           4.3079e-007       0.0042694       0.0010623       0.0010623
v  TempC                       21          73.071          21.677          21.677
v  TurbVisc           3.0297e-014       0.0050319        0.001243        0.001243
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              932:        0.20580E+01

===============================================================


 INSTANT    0.933000000E+03   TIME STEP NUMBER             933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11985E-01 0.87940E+00
   Friction velocity        uk    :  0.11985E-01 0.87940E+00
   Dimensionless distance   yplus :  0.96491E-01 0.70797E+01
   Friction thermal sca.    tstar : -0.13797E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71993E-01 0.52823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74598E-02      32   0.37898E-03   0.18062E+01 0.89182E+02 
c  Velocity[X]                                      0.10627E+01 
c  Velocity[Y]                                      0.74349E+00 
c  Velocity[Z]                                      0.97210E-30 
c  Pressure     0.13746E-06     393   0.96863E-08   0.13828E+00 0.42082E+03 
c  nu_tilda     0.49980E-05      31   0.74582E-05   0.18199E-06 0.12687E+03 
c  TempC        0.30488E+02      26   0.43995E-03   0.66981E+01 0.28059E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5361          10.407          4.5729          4.5729
v  Velocity[Y]            -3.4172          7.0488       0.0053029       0.0053029
v  Velocity[Z]       -1.3099e-014       8.71e-015    -1.1208e-017    -1.1208e-017
v  ǁVelocityǁ         0.0010146          10.408          5.2225          5.2225
v  Pressure               -55.095          20.612         -7.1451         -7.1451
v  nu_tilda           4.3084e-007       0.0042694        0.001063        0.001063
v  TempC                       21          74.139          21.678          21.678
v  TurbVisc           3.0299e-014       0.0050319       0.0012438       0.0012438
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              933:        0.19780E+01

===============================================================


 INSTANT    0.934000000E+03   TIME STEP NUMBER             934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73447E-02 0.88072E+00
   Friction velocity        uk    :  0.73447E-02 0.88072E+00
   Dimensionless distance   yplus :  0.59130E-01 0.70904E+01
   Friction thermal sca.    tstar : -0.14399E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44118E-01 0.52902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74632E-02      32   0.33700E-03   0.18426E+01 0.89674E+02 
c  Velocity[X]                                      0.10795E+01 
c  Velocity[Y]                                      0.76305E+00 
c  Velocity[Z]                                      0.10057E-29 
c  Pressure     0.12250E-06     472   0.98765E-08   0.12703E+00 0.66757E+03 
c  nu_tilda     0.49996E-05      31   0.14771E-04   0.18205E-06 0.12687E+03 
c  TempC        0.30500E+02      27   0.35650E-03   0.51950E+01 0.22790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5338          10.408          4.5729          4.5729
v  Velocity[Y]            -3.4177          7.0258       0.0052538       0.0052538
v  Velocity[Z]        -1.298e-014     8.7226e-015    -1.1193e-017    -1.1193e-017
v  ǁVelocityǁ        0.00086449          10.409          5.2228          5.2228
v  Pressure                -55.09          20.493         -7.1842         -7.1842
v  nu_tilda           4.3093e-007       0.0042694       0.0010636       0.0010636
v  TempC                       21           73.07          21.678          21.678
v  TurbVisc           3.0313e-014       0.0050319       0.0012446       0.0012446
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              934:        0.21580E+01

===============================================================


 INSTANT    0.935000000E+03   TIME STEP NUMBER             935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87954E-02 0.88013E+00
   Friction velocity        uk    :  0.87954E-02 0.88013E+00
   Dimensionless distance   yplus :  0.70809E-01 0.70857E+01
   Friction thermal sca.    tstar : -0.10307E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52832E-01 0.52867E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74666E-02      32   0.29254E-03   0.18069E+01 0.89319E+02 
c  Velocity[X]                                      0.10527E+01 
c  Velocity[Y]                                      0.75420E+00 
c  Velocity[Z]                                      0.97188E-30 
c  Pressure     0.11552E-06     488   0.95594E-08   0.11802E+00 0.85218E+03 
c  nu_tilda     0.50012E-05      31   0.74557E-05   0.18210E-06 0.12687E+03 
c  TempC        0.30511E+02      27   0.46619E-03   0.43127E+01 0.20734E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5315          10.408          4.5729          4.5729
v  Velocity[Y]            -3.4189          7.0518       0.0052054       0.0052054
v  Velocity[Z]       -1.2905e-014      8.735e-015    -1.1172e-017    -1.1172e-017
v  ǁVelocityǁ        0.00080145          10.409          5.2231          5.2231
v  Pressure               -55.079          20.655         -7.1501         -7.1501
v  nu_tilda             4.31e-007       0.0042694       0.0010643       0.0010643
v  TempC                       21          73.678          21.678          21.678
v  TurbVisc           3.0339e-014       0.0050319       0.0012453       0.0012453
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              935:        0.21850E+01

===============================================================


 INSTANT    0.936000000E+03   TIME STEP NUMBER             936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96554E-02 0.88124E+00
   Friction velocity        uk    :  0.96554E-02 0.88124E+00
   Dimensionless distance   yplus :  0.77733E-01 0.70946E+01
   Friction thermal sca.    tstar : -0.10472E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57997E-01 0.52934E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74700E-02      32   0.36241E-03   0.17687E+01 0.89002E+02 
c  Velocity[X]                                      0.10257E+01 
c  Velocity[Y]                                      0.74300E+00 
c  Velocity[Z]                                      0.10021E-29 
c  Pressure     0.92326E-07     457   0.93112E-08   0.94477E-01 0.38887E+03 
c  nu_tilda     0.50028E-05      31   0.14761E-04   0.18216E-06 0.12686E+03 
c  TempC        0.30522E+02      27   0.40231E-03   0.69151E+01 0.26837E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5292          10.409          4.5729          4.5729
v  Velocity[Y]            -3.4223          7.0615       0.0051576       0.0051576
v  Velocity[Z]       -1.2882e-014     8.7467e-015    -1.1155e-017    -1.1155e-017
v  ǁVelocityǁ         0.0009144           10.41          5.2233          5.2233
v  Pressure               -55.079          20.598         -7.1753         -7.1753
v  nu_tilda           4.3101e-007       0.0042694       0.0010649       0.0010649
v  TempC                       21          73.346          21.679          21.679
v  TurbVisc           3.0358e-014       0.0050319       0.0012461       0.0012461
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              936:        0.21330E+01

===============================================================


 INSTANT    0.937000000E+03   TIME STEP NUMBER             937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20866E-02 0.88098E+00
   Friction velocity        uk    :  0.20866E-02 0.88098E+00
   Dimensionless distance   yplus :  0.16798E-01 0.70925E+01
   Friction thermal sca.    tstar : -0.11372E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12533E-01 0.52918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74734E-02      32   0.32458E-03   0.18287E+01 0.89562E+02 
c  Velocity[X]                                      0.10634E+01 
c  Velocity[Y]                                      0.76538E+00 
c  Velocity[Z]                                      0.15233E-29 
c  Pressure     0.12100E-06     394   0.96219E-08   0.12394E+00 0.27515E+03 
c  nu_tilda     0.50043E-05      31   0.74527E-05   0.18221E-06 0.12686E+03 
c  TempC        0.30534E+02      27   0.40465E-03   0.49568E+01 0.22120E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.527          10.409          4.5729          4.5729
v  Velocity[Y]            -3.4251          7.0314       0.0051098       0.0051098
v  Velocity[Z]       -1.2742e-014     8.7575e-015    -1.1138e-017    -1.1138e-017
v  ǁVelocityǁ         0.0013572           10.41          5.2236          5.2236
v  Pressure               -55.063          20.533         -7.1896         -7.1896
v  nu_tilda           4.3105e-007       0.0042694       0.0010656       0.0010656
v  TempC                       21          73.411          21.679          21.679
v  TurbVisc           3.0361e-014       0.0050319       0.0012469       0.0012469
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              937:        0.19650E+01

===============================================================


 INSTANT    0.938000000E+03   TIME STEP NUMBER             938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11177E-01 0.87966E+00
   Friction velocity        uk    :  0.11177E-01 0.87966E+00
   Dimensionless distance   yplus :  0.89984E-01 0.70819E+01
   Friction thermal sca.    tstar : -0.87951E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67138E-01 0.52839E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74768E-02      32   0.36629E-03   0.18037E+01 0.89464E+02 
c  Velocity[X]                                      0.10390E+01 
c  Velocity[Y]                                      0.76470E+00 
c  Velocity[Z]                                      0.11323E-29 
c  Pressure     0.84913E-07     313   0.95090E-08   0.86911E-01 0.20442E+03 
c  nu_tilda     0.50059E-05      31   0.14771E-04   0.18227E-06 0.12686E+03 
c  TempC        0.30545E+02      27   0.35558E-03   0.41584E+01 0.19831E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5248           10.41          4.5729          4.5729
v  Velocity[Y]            -3.4233          7.0499       0.0050628       0.0050628
v  Velocity[Z]       -1.2589e-014     8.7689e-015    -1.1122e-017    -1.1122e-017
v  ǁVelocityǁ         0.0010522          10.411          5.2239          5.2239
v  Pressure               -55.066          20.595         -7.1941         -7.1941
v  nu_tilda           4.3107e-007       0.0042694       0.0010662       0.0010662
v  TempC                       21           73.07          21.679          21.679
v  TurbVisc           3.0372e-014       0.0050319       0.0012476       0.0012476
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              938:        0.17730E+01

===============================================================


 INSTANT    0.939000000E+03   TIME STEP NUMBER             939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80607E-02 0.88082E+00
   Friction velocity        uk    :  0.80607E-02 0.88082E+00
   Dimensionless distance   yplus :  0.64894E-01 0.70912E+01
   Friction thermal sca.    tstar : -0.93690E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48418E-01 0.52908E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74802E-02      32   0.37581E-03   0.18331E+01 0.89685E+02 
c  Velocity[X]                                      0.10835E+01 
c  Velocity[Y]                                      0.74957E+00 
c  Velocity[Z]                                      0.11303E-29 
c  Pressure     0.12538E-06     408   0.99129E-08   0.13004E+00 0.26327E+03 
c  nu_tilda     0.50075E-05      31   0.74347E-05   0.18233E-06 0.12686E+03 
c  TempC        0.30557E+02      27   0.36199E-03   0.40352E+01 0.19351E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5227           10.41          4.5729          4.5729
v  Velocity[Y]            -3.4251          7.0332       0.0050158       0.0050158
v  Velocity[Z]       -1.2385e-014     8.7788e-015    -1.1103e-017    -1.1103e-017
v  ǁVelocityǁ         0.0010156          10.411          5.2242          5.2242
v  Pressure               -55.053          20.529         -7.2061         -7.2061
v  nu_tilda           4.3113e-007       0.0042694       0.0010668       0.0010668
v  TempC                       21          73.074           21.68           21.68
v  TurbVisc           3.0377e-014       0.0050319       0.0012484       0.0012484
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              939:        0.19970E+01

===============================================================


 INSTANT    0.940000000E+03   TIME STEP NUMBER             940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74739E-02 0.88012E+00
   Friction velocity        uk    :  0.74739E-02 0.88012E+00
   Dimensionless distance   yplus :  0.60170E-01 0.70856E+01
   Friction thermal sca.    tstar : -0.92968E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44894E-01 0.52866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74836E-02      32   0.31565E-03   0.18516E+01 0.89802E+02 
c  Velocity[X]                                      0.10836E+01 
c  Velocity[Y]                                      0.76801E+00 
c  Velocity[Z]                                      0.99240E-30 
c  Pressure     0.13304E-06     376   0.98552E-08   0.13400E+00 0.24635E+03 
c  nu_tilda     0.50091E-05      31   0.14792E-04   0.18239E-06 0.12686E+03 
c  TempC        0.30568E+02      26   0.55854E-03   0.48727E+01 0.23043E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5205          10.411          4.5729          4.5729
v  Velocity[Y]            -3.4281          7.0488       0.0049697       0.0049697
v  Velocity[Z]       -1.2211e-014     8.7923e-015    -1.1088e-017    -1.1088e-017
v  ǁVelocityǁ         0.0014393          10.412          5.2244          5.2244
v  Pressure                -55.05          20.601         -7.2041         -7.2041
v  nu_tilda           4.3115e-007       0.0042694       0.0010675       0.0010675
v  TempC                       21           73.34           21.68           21.68
v  TurbVisc           3.0395e-014       0.0050319       0.0012491       0.0012491
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              940:        0.19240E+01

===============================================================


 INSTANT    0.941000000E+03   TIME STEP NUMBER             941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11761E-01 0.88145E+00
   Friction velocity        uk    :  0.11761E-01 0.88145E+00
   Dimensionless distance   yplus :  0.94686E-01 0.70963E+01
   Friction thermal sca.    tstar : -0.80729E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70646E-01 0.52946E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74870E-02      32   0.31214E-03   0.17932E+01 0.89329E+02 
c  Velocity[X]                                      0.10391E+01 
c  Velocity[Y]                                      0.75405E+00 
c  Velocity[Z]                                      0.10567E-29 
c  Pressure     0.88879E-07     392   0.98672E-08   0.91464E-01 0.30240E+03 
c  nu_tilda     0.50107E-05      31   0.74283E-05   0.18245E-06 0.12686E+03 
c  TempC        0.30579E+02      27   0.38212E-03   0.76833E+01 0.29020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5184          10.411          4.5729          4.5729
v  Velocity[Y]            -3.4304          7.0587       0.0049237       0.0049237
v  Velocity[Z]       -1.2062e-014     8.8008e-015    -1.1067e-017    -1.1067e-017
v  ǁVelocityǁ        0.00091901          10.412          5.2247          5.2247
v  Pressure                -55.04          20.631         -7.2007         -7.2007
v  nu_tilda           4.3114e-007       0.0042694       0.0010681       0.0010681
v  TempC                       21          73.246           21.68           21.68
v  TurbVisc           3.0399e-014       0.0050319       0.0012499       0.0012499
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              941:        0.19480E+01

===============================================================


 INSTANT    0.942000000E+03   TIME STEP NUMBER             942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40075E-02 0.88098E+00
   Friction velocity        uk    :  0.40075E-02 0.88098E+00
   Dimensionless distance   yplus :  0.32263E-01 0.70925E+01
   Friction thermal sca.    tstar : -0.80751E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24072E-01 0.52918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74904E-02      32   0.36126E-03   0.18009E+01 0.89433E+02 
c  Velocity[X]                                      0.10529E+01 
c  Velocity[Y]                                      0.74806E+00 
c  Velocity[Z]                                      0.11993E-29 
c  Pressure     0.99735E-07     457   0.96507E-08   0.10324E+00 0.71076E+03 
c  nu_tilda     0.50123E-05      31   0.14786E-04   0.18252E-06 0.12686E+03 
c  TempC        0.30591E+02      27   0.44872E-03   0.48970E+01 0.22699E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5162          10.412          4.5729          4.5729
v  Velocity[Y]            -3.4322          7.0331       0.0048782       0.0048782
v  Velocity[Z]       -1.1928e-014     8.8128e-015     -1.105e-017     -1.105e-017
v  ǁVelocityǁ         0.0012933          10.413           5.225           5.225
v  Pressure               -55.036          20.495         -7.2417         -7.2417
v  nu_tilda           4.3119e-007       0.0042694       0.0010687       0.0010687
v  TempC                       21           73.07          21.681          21.681
v  TurbVisc           3.0399e-014       0.0050319       0.0012507       0.0012507
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              942:        0.21230E+01

===============================================================


 INSTANT    0.943000000E+03   TIME STEP NUMBER             943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10699E-01 0.87978E+00
   Friction velocity        uk    :  0.10699E-01 0.87978E+00
   Dimensionless distance   yplus :  0.86136E-01 0.70829E+01
   Friction thermal sca.    tstar : -0.84539E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64267E-01 0.52846E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74938E-02      32   0.36195E-03   0.18324E+01 0.89824E+02 
c  Velocity[X]                                      0.10605E+01 
c  Velocity[Y]                                      0.77182E+00 
c  Velocity[Z]                                      0.17958E-29 
c  Pressure     0.12129E-06     426   0.97643E-08   0.12297E+00 0.54943E+03 
c  nu_tilda     0.50139E-05      31   0.74373E-05   0.18258E-06 0.12686E+03 
c  TempC        0.30602E+02      26   0.41290E-03   0.81327E+01 0.28554E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5139          10.412          4.5729          4.5729
v  Velocity[Y]            -3.4333          7.0556       0.0048329       0.0048329
v  Velocity[Z]       -1.1783e-014     8.8208e-015    -1.1032e-017    -1.1032e-017
v  ǁVelocityǁ         0.0006273          10.413          5.2252          5.2252
v  Pressure               -55.029            20.6         -7.2269         -7.2269
v  nu_tilda           4.3124e-007       0.0042694       0.0010694       0.0010694
v  TempC                       21          73.669          21.681          21.681
v  TurbVisc           3.0413e-014       0.0050319       0.0012514       0.0012514
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              943:        0.20310E+01

===============================================================


 INSTANT    0.944000000E+03   TIME STEP NUMBER             944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83713E-02 0.88100E+00
   Friction velocity        uk    :  0.83713E-02 0.88100E+00
   Dimensionless distance   yplus :  0.67395E-01 0.70926E+01
   Friction thermal sca.    tstar : -0.72319E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50284E-01 0.52919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74972E-02      32   0.32116E-03   0.18278E+01 0.89735E+02 
c  Velocity[X]                                      0.10713E+01 
c  Velocity[Y]                                      0.75654E+00 
c  Velocity[Z]                                      0.11849E-29 
c  Pressure     0.12353E-06     442   0.92232E-08   0.12719E+00 0.59052E+03 
c  nu_tilda     0.50155E-05      31   0.14789E-04   0.18264E-06 0.12686E+03 
c  TempC        0.30613E+02      27   0.43279E-03   0.61951E+01 0.25510E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5116          10.412          4.5729          4.5729
v  Velocity[Y]            -3.4355          7.0291       0.0047883       0.0047883
v  Velocity[Z]       -1.1602e-014     8.8353e-015    -1.1019e-017    -1.1019e-017
v  ǁVelocityǁ        0.00021351          10.414          5.2255          5.2255
v  Pressure                -55.02          20.488         -7.2584         -7.2584
v  nu_tilda           4.3129e-007       0.0042694         0.00107         0.00107
v  TempC                       21          73.511          21.681          21.681
v  TurbVisc           3.0425e-014       0.0050319       0.0012522       0.0012522
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              944:        0.21230E+01

===============================================================


 INSTANT    0.945000000E+03   TIME STEP NUMBER             945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31053E-02 0.88022E+00
   Friction velocity        uk    :  0.31053E-02 0.88022E+00
   Dimensionless distance   yplus :  0.25000E-01 0.70864E+01
   Friction thermal sca.    tstar : -0.75734E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18653E-01 0.52872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75006E-02      32   0.34769E-03   0.17941E+01 0.89454E+02 
c  Velocity[X]                                      0.10463E+01 
c  Velocity[Y]                                      0.74773E+00 
c  Velocity[Z]                                      0.10753E-29 
c  Pressure     0.88658E-07     457   0.92773E-08   0.90449E-01 0.68459E+03 
c  nu_tilda     0.50170E-05      31   0.74146E-05   0.18271E-06 0.12686E+03 
c  TempC        0.30625E+02      27   0.37760E-03   0.57498E+01 0.24901E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5094          10.413          4.5729          4.5729
v  Velocity[Y]            -3.4364          7.0556        0.004744        0.004744
v  Velocity[Z]       -1.1456e-014     8.8435e-015    -1.0995e-017    -1.0995e-017
v  ǁVelocityǁ         0.0014604          10.414          5.2258          5.2258
v  Pressure               -55.012          20.616         -7.2349         -7.2349
v  nu_tilda            4.313e-007       0.0042694       0.0010707       0.0010707
v  TempC                       21          73.136          21.682          21.682
v  TurbVisc           3.0441e-014       0.0050319        0.001253        0.001253
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              945:        0.21250E+01

===============================================================


 INSTANT    0.946000000E+03   TIME STEP NUMBER             946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12507E-01 0.88153E+00
   Friction velocity        uk    :  0.12507E-01 0.88153E+00
   Dimensionless distance   yplus :  0.10069E+00 0.70969E+01
   Friction thermal sca.    tstar : -0.74606E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75128E-01 0.52951E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75040E-02      32   0.33367E-03   0.18007E+01 0.89613E+02 
c  Velocity[X]                                      0.10332E+01 
c  Velocity[Y]                                      0.76753E+00 
c  Velocity[Z]                                      0.11595E-29 
c  Pressure     0.11280E-06     408   0.96097E-08   0.11599E+00 0.28750E+03 
c  nu_tilda     0.50186E-05      31   0.14813E-04   0.18278E-06 0.12687E+03 
c  TempC        0.30636E+02      27   0.32482E-03   0.71442E+01 0.26631E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5071          10.413          4.5729          4.5729
v  Velocity[Y]            -3.4392           7.062       0.0047004       0.0047004
v  Velocity[Z]       -1.1376e-014     8.8562e-015     -1.098e-017     -1.098e-017
v  ǁVelocityǁ        0.00093117          10.414           5.226           5.226
v  Pressure               -55.005          20.593         -7.2537         -7.2537
v  nu_tilda           4.3125e-007       0.0042694       0.0010713       0.0010713
v  TempC                       21          73.156          21.682          21.682
v  TurbVisc           3.0443e-014       0.0050319       0.0012537       0.0012537
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              946:        0.19980E+01

===============================================================


 INSTANT    0.947000000E+03   TIME STEP NUMBER             947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51604E-02 0.88098E+00
   Friction velocity        uk    :  0.51604E-02 0.88098E+00
   Dimensionless distance   yplus :  0.41545E-01 0.70925E+01
   Friction thermal sca.    tstar : -0.69003E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30997E-01 0.52918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75074E-02      32   0.33206E-03   0.18268E+01 0.89728E+02 
c  Velocity[X]                                      0.10699E+01 
c  Velocity[Y]                                      0.75694E+00 
c  Velocity[Z]                                      0.11009E-29 
c  Pressure     0.13368E-06     457   0.97311E-08   0.13611E+00 0.39998E+03 
c  nu_tilda     0.50202E-05      31   0.74117E-05   0.18284E-06 0.12687E+03 
c  TempC        0.30647E+02      26   0.49127E-03   0.53776E+01 0.23784E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.505          10.414          4.5729          4.5729
v  Velocity[Y]            -3.4402          7.0334       0.0046568       0.0046568
v  Velocity[Z]       -1.1161e-014     8.8638e-015    -1.0953e-017    -1.0953e-017
v  ǁVelocityǁ         0.0011964          10.415          5.2263          5.2263
v  Pressure               -54.995          20.484         -7.2776         -7.2776
v  nu_tilda           4.3133e-007       0.0042694        0.001072        0.001072
v  TempC                       21          73.069          21.682          21.682
v  TurbVisc           3.0429e-014       0.0050319       0.0012545       0.0012545
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              947:        0.21220E+01

===============================================================


 INSTANT    0.948000000E+03   TIME STEP NUMBER             948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98686E-02 0.87992E+00
   Friction velocity        uk    :  0.98686E-02 0.87992E+00
   Dimensionless distance   yplus :  0.79449E-01 0.70840E+01
   Friction thermal sca.    tstar : -0.67889E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59278E-01 0.52854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75108E-02      32   0.34593E-03   0.18270E+01 0.89819E+02 
c  Velocity[X]                                      0.10755E+01 
c  Velocity[Y]                                      0.75146E+00 
c  Velocity[Z]                                      0.90227E-30 
c  Pressure     0.99652E-07     410   0.98808E-08   0.10222E+00 0.31280E+03 
c  nu_tilda     0.50218E-05      31   0.14814E-04   0.18290E-06 0.12687E+03 
c  TempC        0.30659E+02      27   0.38349E-03   0.72599E+01 0.28767E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5028          10.414          4.5729          4.5729
v  Velocity[Y]            -3.4425          7.0528       0.0046137       0.0046137
v  Velocity[Z]       -1.1072e-014     8.8771e-015    -1.0936e-017    -1.0936e-017
v  ǁVelocityǁ         0.0011935          10.415          5.2266          5.2266
v  Pressure               -54.993          20.573         -7.2726         -7.2726
v  nu_tilda           4.3141e-007       0.0042694       0.0010726       0.0010726
v  TempC                       21          73.799          21.683          21.683
v  TurbVisc           3.0452e-014       0.0050319       0.0012553       0.0012553
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              948:        0.20560E+01

===============================================================


 INSTANT    0.949000000E+03   TIME STEP NUMBER             949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98277E-02 0.88106E+00
   Friction velocity        uk    :  0.98277E-02 0.88106E+00
   Dimensionless distance   yplus :  0.79120E-01 0.70931E+01
   Friction thermal sca.    tstar : -0.71132E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59032E-01 0.52923E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75141E-02      32   0.34504E-03   0.18240E+01 0.89912E+02 
c  Velocity[X]                                      0.10526E+01 
c  Velocity[Y]                                      0.77141E+00 
c  Velocity[Z]                                      0.15318E-29 
c  Pressure     0.97687E-07     438   0.89761E-08   0.10115E+00 0.29351E+03 
c  nu_tilda     0.50234E-05      31   0.74245E-05   0.18296E-06 0.12687E+03 
c  TempC        0.30670E+02      27   0.33332E-03   0.73177E+01 0.26858E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5006          10.414          4.5729          4.5729
v  Velocity[Y]            -3.4436          7.0333        0.004571        0.004571
v  Velocity[Z]       -1.0976e-014     8.8841e-015    -1.0909e-017    -1.0909e-017
v  ǁVelocityǁ         0.0009323          10.416          5.2268          5.2268
v  Pressure               -54.982          20.504         -7.2913         -7.2913
v  nu_tilda           4.3145e-007       0.0042694       0.0010733       0.0010733
v  TempC                       21          73.689          21.683          21.683
v  TurbVisc           3.0474e-014       0.0050319        0.001256        0.001256
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              949:        0.20900E+01

===============================================================


 INSTANT    0.950000000E+03   TIME STEP NUMBER             950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26385E-02 0.88026E+00
   Friction velocity        uk    :  0.26385E-02 0.88026E+00
   Dimensionless distance   yplus :  0.21241E-01 0.70867E+01
   Friction thermal sca.    tstar : -0.62855E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15848E-01 0.52875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75175E-02      32   0.33505E-03   0.18004E+01 0.89652E+02 
c  Velocity[X]                                      0.10443E+01 
c  Velocity[Y]                                      0.75616E+00 
c  Velocity[Z]                                      0.10494E-29 
c  Pressure     0.91113E-07     393   0.92725E-08   0.92731E-01 0.23082E+03 
c  nu_tilda     0.50250E-05      31   0.14813E-04   0.18303E-06 0.12687E+03 
c  TempC        0.30681E+02      27   0.41128E-03   0.46027E+01 0.21498E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4984          10.415          4.5729          4.5729
v  Velocity[Y]            -3.4459          7.0577       0.0045287       0.0045287
v  Velocity[Z]       -1.0843e-014     8.8979e-015    -1.0889e-017    -1.0889e-017
v  ǁVelocityǁ         0.0015495          10.416          5.2271          5.2271
v  Pressure               -54.979          20.566         -7.2904         -7.2904
v  nu_tilda           4.3144e-007       0.0042694       0.0010739       0.0010739
v  TempC                       21          73.249          21.683          21.683
v  TurbVisc           3.0484e-014       0.0050319       0.0012568       0.0012568
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              950:        0.19560E+01

===============================================================


 INSTANT    0.951000000E+03   TIME STEP NUMBER             951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12516E-01 0.88156E+00
   Friction velocity        uk    :  0.12516E-01 0.88156E+00
   Dimensionless distance   yplus :  0.10076E+00 0.70971E+01
   Friction thermal sca.    tstar : -0.65498E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75180E-01 0.52953E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75209E-02      32   0.37395E-03   0.17931E+01 0.89502E+02 
c  Velocity[X]                                      0.10423E+01 
c  Velocity[Y]                                      0.75073E+00 
c  Velocity[Z]                                      0.10686E-29 
c  Pressure     0.11831E-06     438   0.92190E-08   0.11989E+00 0.36982E+03 
c  nu_tilda     0.50266E-05      31   0.73993E-05   0.18311E-06 0.12688E+03 
c  TempC        0.30693E+02      26   0.43952E-03   0.52683E+01 0.23159E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4964          10.415          4.5729          4.5729
v  Velocity[Y]            -3.4467          7.0638       0.0044868       0.0044868
v  Velocity[Z]       -1.0681e-014     8.9077e-015    -1.0877e-017    -1.0877e-017
v  ǁVelocityǁ        0.00097644          10.416          5.2273          5.2273
v  Pressure               -54.961          20.598         -7.2801         -7.2801
v  nu_tilda           4.3145e-007       0.0042694       0.0010745       0.0010745
v  TempC                       21          73.598          21.684          21.684
v  TurbVisc           3.0483e-014       0.0050319       0.0012575       0.0012575
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              951:        0.20800E+01

===============================================================


 INSTANT    0.952000000E+03   TIME STEP NUMBER             952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68065E-02 0.88114E+00
   Friction velocity        uk    :  0.68065E-02 0.88114E+00
   Dimensionless distance   yplus :  0.54797E-01 0.70938E+01
   Friction thermal sca.    tstar : -0.64838E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40885E-01 0.52927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75243E-02      32   0.35346E-03   0.18295E+01 0.90007E+02 
c  Velocity[X]                                      0.10546E+01 
c  Velocity[Y]                                      0.77497E+00 
c  Velocity[Z]                                      0.12217E-29 
c  Pressure     0.93895E-07     506   0.92258E-08   0.97546E-01 0.81667E+03 
c  nu_tilda     0.50282E-05      31   0.14839E-04   0.18318E-06 0.12688E+03 
c  TempC        0.30704E+02      27   0.34181E-03   0.64151E+01 0.25053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4941          10.416          4.5729          4.5729
v  Velocity[Y]            -3.4485          7.0354        0.004445        0.004445
v  Velocity[Z]       -1.0656e-014     8.9164e-015    -1.0845e-017    -1.0845e-017
v  ǁVelocityǁ         0.0011434          10.417          5.2276          5.2276
v  Pressure               -54.961          20.453         -7.3302         -7.3302
v  nu_tilda           4.3154e-007       0.0042694       0.0010752       0.0010752
v  TempC                       21          73.069          21.684          21.684
v  TurbVisc           3.0486e-014       0.0050319       0.0012583       0.0012583
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              952:        0.22380E+01

===============================================================


 INSTANT    0.953000000E+03   TIME STEP NUMBER             953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93595E-02 0.88003E+00
   Friction velocity        uk    :  0.93595E-02 0.88003E+00
   Dimensionless distance   yplus :  0.75350E-01 0.70849E+01
   Friction thermal sca.    tstar : -0.61478E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56220E-01 0.52861E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75276E-02      32   0.32434E-03   0.18314E+01 0.90022E+02 
c  Velocity[X]                                      0.10703E+01 
c  Velocity[Y]                                      0.76102E+00 
c  Velocity[Z]                                      0.14980E-29 
c  Pressure     0.10459E-06     472   0.99972E-08   0.10749E+00 0.80878E+03 
c  nu_tilda     0.50297E-05      31   0.73940E-05   0.18324E-06 0.12688E+03 
c  TempC        0.30715E+02      27   0.50510E-03   0.50714E+01 0.23293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4919          10.416          4.5729          4.5729
v  Velocity[Y]            -3.4491          7.0591       0.0044039       0.0044039
v  Velocity[Z]       -1.0528e-014     8.9268e-015    -1.0823e-017    -1.0823e-017
v  ǁVelocityǁ        0.00038932          10.417          5.2279          5.2279
v  Pressure                -54.95          20.603         -7.2984         -7.2984
v  nu_tilda           4.3154e-007       0.0042694       0.0010758       0.0010758
v  TempC                       21           73.56          21.685          21.685
v  TurbVisc           3.0511e-014       0.0050319       0.0012591       0.0012591
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              953:        0.23340E+01

===============================================================


 INSTANT    0.954000000E+03   TIME STEP NUMBER             954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49984E-02 0.88094E+00
   Friction velocity        uk    :  0.49984E-02 0.88094E+00
   Dimensionless distance   yplus :  0.40240E-01 0.70922E+01
   Friction thermal sca.    tstar : -0.60546E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30024E-01 0.52915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75310E-02      32   0.35409E-03   0.18253E+01 0.89962E+02 
c  Velocity[X]                                      0.10730E+01 
c  Velocity[Y]                                      0.75225E+00 
c  Velocity[Z]                                      0.11191E-29 
c  Pressure     0.11501E-06     472   0.98477E-08   0.11784E+00 0.87516E+03 
c  nu_tilda     0.50313E-05      31   0.14830E-04   0.18332E-06 0.12689E+03 
c  TempC        0.30726E+02      26   0.45256E-03   0.69108E+01 0.28651E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4895          10.416          4.5729          4.5729
v  Velocity[Y]            -3.4508          7.0314       0.0043633       0.0043633
v  Velocity[Z]       -1.0448e-014     8.9373e-015    -1.0803e-017    -1.0803e-017
v  ǁVelocityǁ        0.00057991          10.417          5.2281          5.2281
v  Pressure               -54.944          20.436         -7.3484         -7.3484
v  nu_tilda           4.3158e-007       0.0042694       0.0010764       0.0010764
v  TempC                       21          73.069          21.685          21.685
v  TurbVisc           3.0511e-014       0.0050319       0.0012598       0.0012598
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              954:        0.24740E+01

===============================================================


 INSTANT    0.955000000E+03   TIME STEP NUMBER             955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42091E-02 0.88033E+00
   Friction velocity        uk    :  0.42091E-02 0.88033E+00
   Dimensionless distance   yplus :  0.33886E-01 0.70873E+01
   Friction thermal sca.    tstar : -0.63016E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25283E-01 0.52879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75344E-02      32   0.30873E-03   0.18194E+01 0.89907E+02 
c  Velocity[X]                                      0.10553E+01 
c  Velocity[Y]                                      0.76405E+00 
c  Velocity[Z]                                      0.15079E-29 
c  Pressure     0.10409E-06     457   0.95769E-08   0.10668E+00 0.83636E+03 
c  nu_tilda     0.50329E-05      31   0.74048E-05   0.18339E-06 0.12689E+03 
c  TempC        0.30738E+02      27   0.34685E-03   0.63799E+01 0.25645E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4875          10.417          4.5729          4.5729
v  Velocity[Y]            -3.4511          7.0564       0.0043227       0.0043227
v  Velocity[Z]        -1.029e-014     8.9483e-015    -1.0785e-017    -1.0785e-017
v  ǁVelocityǁ         0.0014241          10.418          5.2284          5.2284
v  Pressure                -54.93          20.592         -7.3143         -7.3143
v  nu_tilda           4.3162e-007       0.0042694       0.0010771       0.0010771
v  TempC                       21          73.069          21.685          21.685
v  TurbVisc           3.0521e-014       0.0050319       0.0012606       0.0012606
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              955:        0.21360E+01

===============================================================


 INSTANT    0.956000000E+03   TIME STEP NUMBER             956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11723E-01 0.88165E+00
   Friction velocity        uk    :  0.11723E-01 0.88165E+00
   Dimensionless distance   yplus :  0.94377E-01 0.70979E+01
   Friction thermal sca.    tstar : -0.57424E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70416E-01 0.52958E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75378E-02      32   0.34155E-03   0.17897E+01 0.89703E+02 
c  Velocity[X]                                      0.10300E+01 
c  Velocity[Y]                                      0.75963E+00 
c  Velocity[Z]                                      0.11371E-29 
c  Pressure     0.10462E-06     426   0.92525E-08   0.10698E+00 0.33914E+03 
c  nu_tilda     0.50345E-05      31   0.14833E-04   0.18347E-06 0.12689E+03 
c  TempC        0.30749E+02      27   0.41799E-03   0.45532E+01 0.21485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4854          10.417          4.5729          4.5729
v  Velocity[Y]            -3.4522          7.0649       0.0042829       0.0042829
v  Velocity[Z]       -1.0247e-014     8.9573e-015     -1.075e-017     -1.075e-017
v  ǁVelocityǁ        0.00099621          10.418          5.2286          5.2286
v  Pressure               -54.932          20.561         -7.3398         -7.3398
v  nu_tilda           4.3161e-007       0.0042694       0.0010777       0.0010777
v  TempC                       21           74.13          21.686          21.686
v  TurbVisc           3.0534e-014        0.005032       0.0012614       0.0012614
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              956:        0.20270E+01

===============================================================


 INSTANT    0.957000000E+03   TIME STEP NUMBER             957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72999E-02 0.88121E+00
   Friction velocity        uk    :  0.72999E-02 0.88121E+00
   Dimensionless distance   yplus :  0.58770E-01 0.70943E+01
   Friction thermal sca.    tstar : -0.59490E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43849E-01 0.52932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75411E-02      32   0.38095E-03   0.18254E+01 0.89996E+02 
c  Velocity[X]                                      0.10722E+01 
c  Velocity[Y]                                      0.75319E+00 
c  Velocity[Z]                                      0.11707E-29 
c  Pressure     0.12973E-06     424   0.93158E-08   0.13388E+00 0.34354E+03 
c  nu_tilda     0.50361E-05      31   0.73877E-05   0.18354E-06 0.12690E+03 
c  TempC        0.30760E+02      26   0.38698E-03   0.56871E+01 0.24237E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4833          10.417          4.5729          4.5729
v  Velocity[Y]            -3.4523          7.0427       0.0042431       0.0042431
v  Velocity[Z]       -1.0127e-014     8.9658e-015    -1.0728e-017    -1.0728e-017
v  ǁVelocityǁ         0.0010625          10.418          5.2289          5.2289
v  Pressure               -54.917          20.466         -7.3577         -7.3577
v  nu_tilda           4.3165e-007       0.0042694       0.0010784       0.0010784
v  TempC                       21          73.069          21.686          21.686
v  TurbVisc           3.0532e-014        0.005032       0.0012621       0.0012621
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              957:        0.20550E+01

===============================================================


 INSTANT    0.958000000E+03   TIME STEP NUMBER             958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84165E-02 0.88015E+00
   Friction velocity        uk    :  0.84165E-02 0.88015E+00
   Dimensionless distance   yplus :  0.67758E-01 0.70858E+01
   Friction thermal sca.    tstar : -0.58575E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50555E-01 0.52868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75445E-02      32   0.32378E-03   0.18354E+01 0.90141E+02 
c  Velocity[X]                                      0.10712E+01 
c  Velocity[Y]                                      0.76428E+00 
c  Velocity[Z]                                      0.10494E-29 
c  Pressure     0.11916E-06     392   0.97090E-08   0.12098E+00 0.28856E+03 
c  nu_tilda     0.50377E-05      31   0.14864E-04   0.18362E-06 0.12690E+03 
c  TempC        0.30772E+02      26   0.47160E-03   0.46553E+01 0.22090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4811          10.417          4.5729          4.5729
v  Velocity[Y]            -3.4534          7.0556       0.0042041       0.0042041
v  Velocity[Z]       -9.9986e-015     8.9795e-015    -1.0714e-017    -1.0714e-017
v  ǁVelocityǁ         0.0013568          10.419          5.2291          5.2291
v  Pressure               -54.912          20.552         -7.3539         -7.3539
v  nu_tilda           4.3166e-007       0.0042694        0.001079        0.001079
v  TempC                       21          73.123          21.686          21.686
v  TurbVisc            3.054e-014        0.005032       0.0012629       0.0012629
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              958:        0.19720E+01

===============================================================


 INSTANT    0.959000000E+03   TIME STEP NUMBER             959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11238E-01 0.88113E+00
   Friction velocity        uk    :  0.11238E-01 0.88113E+00
   Dimensionless distance   yplus :  0.90477E-01 0.70937E+01
   Friction thermal sca.    tstar : -0.56642E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67506E-01 0.52927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75478E-02      32   0.31065E-03   0.18085E+01 0.89893E+02 
c  Velocity[X]                                      0.10510E+01 
c  Velocity[Y]                                      0.75749E+00 
c  Velocity[Z]                                      0.10431E-29 
c  Pressure     0.95515E-07     410   0.93518E-08   0.98977E-01 0.27056E+03 
c  nu_tilda     0.50393E-05      31   0.73807E-05   0.18368E-06 0.12691E+03 
c  TempC        0.30783E+02      28   0.39451E-03   0.49665E+01 0.21983E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.479          10.418          4.5729          4.5729
v  Velocity[Y]            -3.4534          7.0364        0.004165        0.004165
v  Velocity[Z]       -9.8763e-015     8.9861e-015    -1.0685e-017    -1.0685e-017
v  ǁVelocityǁ        0.00089613          10.419          5.2294          5.2294
v  Pressure               -54.898          20.483         -7.3687         -7.3687
v  nu_tilda           4.3167e-007       0.0042694       0.0010797       0.0010797
v  TempC                       21          73.489          21.687          21.687
v  TurbVisc           3.0543e-014        0.005032       0.0012637       0.0012637
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              959:        0.19940E+01

===============================================================


 INSTANT    0.960000000E+03   TIME STEP NUMBER             960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87245E-03 0.88043E+00
   Friction velocity        uk    :  0.87245E-03 0.88043E+00
   Dimensionless distance   yplus :  0.70238E-02 0.70881E+01
   Friction thermal sca.    tstar : -0.57770E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52406E-02 0.52885E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75512E-02      32   0.34051E-03   0.18031E+01 0.89862E+02 
c  Velocity[X]                                      0.10482E+01 
c  Velocity[Y]                                      0.75496E+00 
c  Velocity[Z]                                      0.96821E-30 
c  Pressure     0.99612E-07     410   0.91171E-08   0.10250E+00 0.32809E+03 
c  nu_tilda     0.50409E-05      31   0.14855E-04   0.18376E-06 0.12691E+03 
c  TempC        0.30794E+02      27   0.44808E-03   0.42867E+01 0.21316E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4768          10.418          4.5729          4.5729
v  Velocity[Y]            -3.4541          7.0606       0.0041268       0.0041268
v  Velocity[Z]       -9.7603e-015     8.9996e-015    -1.0669e-017    -1.0669e-017
v  ǁVelocityǁ         0.0013585          10.419          5.2297          5.2297
v  Pressure               -54.896          20.575         -7.3627         -7.3627
v  nu_tilda           4.3168e-007       0.0042694       0.0010803       0.0010803
v  TempC                       21          73.634          21.687          21.687
v  TurbVisc           3.0548e-014        0.005032       0.0012644       0.0012644
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              960:        0.20020E+01

===============================================================


 INSTANT    0.961000000E+03   TIME STEP NUMBER             961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11276E-01 0.88146E+00
   Friction velocity        uk    :  0.11276E-01 0.88146E+00
   Dimensionless distance   yplus :  0.90780E-01 0.70963E+01
   Friction thermal sca.    tstar : -0.57792E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67732E-01 0.52947E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75545E-02      32   0.35878E-03   0.18167E+01 0.90005E+02 
c  Velocity[X]                                      0.10481E+01 
c  Velocity[Y]                                      0.76863E+00 
c  Velocity[Z]                                      0.14075E-29 
c  Pressure     0.11663E-06     393   0.95130E-08   0.11730E+00 0.19577E+03 
c  nu_tilda     0.50425E-05      31   0.73811E-05   0.18383E-06 0.12692E+03 
c  TempC        0.30806E+02      26   0.40231E-03   0.67807E+01 0.26319E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4746          10.418          4.5729          4.5729
v  Velocity[Y]            -3.4542          7.0638       0.0040885       0.0040885
v  Velocity[Z]        -9.663e-015     9.0057e-015    -1.0641e-017    -1.0641e-017
v  ǁVelocityǁ        0.00098625          10.419          5.2299          5.2299
v  Pressure               -54.882          20.549         -7.3711         -7.3711
v  nu_tilda           4.3169e-007       0.0042694        0.001081        0.001081
v  TempC                       21          73.071          21.687          21.687
v  TurbVisc            3.055e-014        0.005032       0.0012652       0.0012652
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              961:        0.19430E+01

===============================================================


 INSTANT    0.962000000E+03   TIME STEP NUMBER             962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84791E-02 0.88127E+00
   Friction velocity        uk    :  0.84791E-02 0.88127E+00
   Dimensionless distance   yplus :  0.68262E-01 0.70948E+01
   Friction thermal sca.    tstar : -0.56397E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50931E-01 0.52935E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75579E-02      32   0.34662E-03   0.18548E+01 0.90407E+02 
c  Velocity[X]                                      0.10931E+01 
c  Velocity[Y]                                      0.76167E+00 
c  Velocity[Z]                                      0.14349E-29 
c  Pressure     0.11907E-06     458   0.93835E-08   0.12334E+00 0.65471E+03 
c  nu_tilda     0.50441E-05      31   0.14861E-04   0.18391E-06 0.12692E+03 
c  TempC        0.30817E+02      26   0.42379E-03   0.48301E+01 0.22258E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4723          10.419          4.5729          4.5729
v  Velocity[Y]            -3.4569          7.0374       0.0040507       0.0040507
v  Velocity[Z]       -9.7051e-015     9.0178e-015    -1.0627e-017    -1.0627e-017
v  ǁVelocityǁ        0.00057715           10.42          5.2302          5.2302
v  Pressure               -54.875           20.43         -7.4093         -7.4093
v  nu_tilda           4.3176e-007       0.0042694       0.0010816       0.0010816
v  TempC                       21          73.278          21.688          21.688
v  TurbVisc           3.0552e-014        0.005032        0.001266        0.001266
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              962:        0.21300E+01

===============================================================


 INSTANT    0.963000000E+03   TIME STEP NUMBER             963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76936E-02 0.88016E+00
   Friction velocity        uk    :  0.76936E-02 0.88016E+00
   Dimensionless distance   yplus :  0.61939E-01 0.70859E+01
   Friction thermal sca.    tstar : -0.57519E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46213E-01 0.52869E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75612E-02      32   0.33143E-03   0.18243E+01 0.90161E+02 
c  Velocity[X]                                      0.10675E+01 
c  Velocity[Y]                                      0.75689E+00 
c  Velocity[Z]                                      0.15533E-29 
c  Pressure     0.12831E-06     473   0.91909E-08   0.13134E+00 0.82931E+03 
c  nu_tilda     0.50456E-05      31   0.73600E-05   0.18399E-06 0.12693E+03 
c  TempC        0.30828E+02      27   0.39257E-03   0.53055E+01 0.23354E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4702          10.419          4.5729          4.5729
v  Velocity[Y]            -3.4562          7.0599       0.0040133       0.0040133
v  Velocity[Z]       -9.8247e-015     9.0277e-015    -1.0597e-017    -1.0597e-017
v  ǁVelocityǁ          0.001257           10.42          5.2304          5.2304
v  Pressure               -54.857          20.584         -7.3751         -7.3751
v  nu_tilda           4.3182e-007       0.0042694       0.0010823       0.0010823
v  TempC                       21          73.562          21.688          21.688
v  TurbVisc           3.0572e-014        0.005032       0.0012667       0.0012667
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              963:        0.21600E+01

===============================================================


 INSTANT    0.964000000E+03   TIME STEP NUMBER             964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12096E-01 0.88123E+00
   Friction velocity        uk    :  0.12096E-01 0.88123E+00
   Dimensionless distance   yplus :  0.97384E-01 0.70945E+01
   Friction thermal sca.    tstar : -0.56959E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72659E-01 0.52933E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75646E-02      32   0.33582E-03   0.18224E+01 0.90152E+02 
c  Velocity[X]                                      0.10540E+01 
c  Velocity[Y]                                      0.76840E+00 
c  Velocity[Z]                                      0.10938E-29 
c  Pressure     0.12076E-06     474   0.96880E-08   0.12591E+00 0.73988E+03 
c  nu_tilda     0.50472E-05      31   0.14882E-04   0.18407E-06 0.12694E+03 
c  TempC        0.30839E+02      27   0.28737E-03   0.59930E+01 0.23876E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4683          10.419          4.5729          4.5729
v  Velocity[Y]            -3.4567          7.0374       0.0039762       0.0039762
v  Velocity[Z]       -9.3864e-015     9.0364e-015    -1.0559e-017    -1.0559e-017
v  ǁVelocityǁ        0.00089805           10.42          5.2307          5.2307
v  Pressure               -54.858          20.449         -7.4202         -7.4202
v  nu_tilda           4.3181e-007       0.0042694       0.0010829       0.0010829
v  TempC                       21           73.07          21.688          21.688
v  TurbVisc           3.0589e-014        0.005032       0.0012675       0.0012675
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              964:        0.21540E+01

===============================================================


 INSTANT    0.965000000E+03   TIME STEP NUMBER             965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34770E-02 0.88035E+00
   Friction velocity        uk    :  0.34770E-02 0.88035E+00
   Dimensionless distance   yplus :  0.27992E-01 0.70874E+01
   Friction thermal sca.    tstar : -0.57294E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20885E-01 0.52880E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75679E-02      32   0.33333E-03   0.18319E+01 0.90169E+02 
c  Velocity[X]                                      0.10703E+01 
c  Velocity[Y]                                      0.76158E+00 
c  Velocity[Z]                                      0.11302E-29 
c  Pressure     0.12935E-06     441   0.90300E-08   0.12925E+00 0.51312E+03 
c  nu_tilda     0.50488E-05      31   0.73561E-05   0.18415E-06 0.12694E+03 
c  TempC        0.30851E+02      26   0.52171E-03   0.38106E+01 0.19271E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4663           10.42          4.5729          4.5729
v  Velocity[Y]            -3.4581          7.0582       0.0039395       0.0039395
v  Velocity[Z]       -9.2505e-015     9.0449e-015    -1.0536e-017    -1.0536e-017
v  ǁVelocityǁ         0.0012649          10.421          5.2309          5.2309
v  Pressure               -54.845          20.532         -7.4039         -7.4039
v  nu_tilda           4.3181e-007       0.0042694       0.0010835       0.0010835
v  TempC                       21           73.07          21.689          21.689
v  TurbVisc           3.0588e-014        0.005032       0.0012682       0.0012682
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              965:        0.20860E+01

===============================================================


 INSTANT    0.966000000E+03   TIME STEP NUMBER             966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10567E-01 0.88182E+00
   Friction velocity        uk    :  0.10567E-01 0.88182E+00
   Dimensionless distance   yplus :  0.85070E-01 0.70992E+01
   Friction thermal sca.    tstar : -0.56792E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63472E-01 0.52968E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75713E-02      32   0.35339E-03   0.18222E+01 0.90184E+02 
c  Velocity[X]                                      0.10676E+01 
c  Velocity[Y]                                      0.75464E+00 
c  Velocity[Z]                                      0.98242E-30 
c  Pressure     0.11787E-06     393   0.90203E-08   0.12015E+00 0.19374E+03 
c  nu_tilda     0.50504E-05      31   0.14877E-04   0.18423E-06 0.12695E+03 
c  TempC        0.30862E+02      27   0.37771E-03   0.66544E+01 0.26899E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4643           10.42          4.5729          4.5729
v  Velocity[Y]            -3.4584          7.0651       0.0039033       0.0039033
v  Velocity[Z]       -9.1072e-015     9.0574e-015    -1.0511e-017    -1.0511e-017
v  ǁVelocityǁ         0.0011273          10.421          5.2312          5.2312
v  Pressure               -54.837          20.539         -7.4157         -7.4157
v  nu_tilda            4.318e-007       0.0042694       0.0010842       0.0010842
v  TempC                       21           73.07          21.689          21.689
v  TurbVisc           3.0588e-014        0.005032        0.001269        0.001269
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              966:        0.19670E+01

===============================================================


 INSTANT    0.967000000E+03   TIME STEP NUMBER             967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92513E-02 0.88150E+00
   Friction velocity        uk    :  0.92513E-02 0.88150E+00
   Dimensionless distance   yplus :  0.74479E-01 0.70966E+01
   Friction thermal sca.    tstar : -0.56431E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55570E-01 0.52949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75746E-02      32   0.31188E-03   0.18305E+01 0.90302E+02 
c  Velocity[X]                                      0.10619E+01 
c  Velocity[Y]                                      0.76863E+00 
c  Velocity[Z]                                      0.14328E-29 
c  Pressure     0.11717E-06     441   0.94917E-08   0.12168E+00 0.33075E+03 
c  nu_tilda     0.50520E-05      31   0.73553E-05   0.18431E-06 0.12695E+03 
c  TempC        0.30873E+02      27   0.30887E-03   0.49376E+01 0.21662E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4622          10.421          4.5729          4.5729
v  Velocity[Y]              -3.46          7.0404       0.0038671       0.0038671
v  Velocity[Z]       -9.7342e-015     9.0632e-015    -1.0482e-017    -1.0482e-017
v  ǁVelocityǁ        0.00094875          10.422          5.2314          5.2314
v  Pressure               -54.823          20.451         -7.4355         -7.4355
v  nu_tilda           4.3182e-007       0.0042694       0.0010848       0.0010848
v  TempC                       21          73.283          21.689          21.689
v  TurbVisc           3.0584e-014        0.005032       0.0012698       0.0012698
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              967:        0.21370E+01

===============================================================


 INSTANT    0.968000000E+03   TIME STEP NUMBER             968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63958E-02 0.88023E+00
   Friction velocity        uk    :  0.63958E-02 0.88023E+00
   Dimensionless distance   yplus :  0.51490E-01 0.70864E+01
   Friction thermal sca.    tstar : -0.57788E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38418E-01 0.52873E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75780E-02      32   0.31358E-03   0.18026E+01 0.90080E+02 
c  Velocity[X]                                      0.10414E+01 
c  Velocity[Y]                                      0.76115E+00 
c  Velocity[Z]                                      0.10651E-29 
c  Pressure     0.90035E-07     361   0.89788E-08   0.91727E-01 0.22668E+03 
c  nu_tilda     0.50536E-05      31   0.14885E-04   0.18439E-06 0.12696E+03 
c  TempC        0.30885E+02      26   0.48514E-03   0.40840E+01 0.20984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4601          10.421          4.5729          4.5729
v  Velocity[Y]             -3.462          7.0609       0.0038317       0.0038317
v  Velocity[Z]       -8.8493e-015     9.0756e-015    -1.0447e-017    -1.0447e-017
v  ǁVelocityǁ          0.001541          10.422          5.2316          5.2316
v  Pressure               -54.822          20.519         -7.4366         -7.4366
v  nu_tilda           4.3183e-007       0.0042694       0.0010854       0.0010854
v  TempC                       21          73.516           21.69           21.69
v  TurbVisc           3.0591e-014        0.005032       0.0012705       0.0012705
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              968:        0.20690E+01

===============================================================


 INSTANT    0.969000000E+03   TIME STEP NUMBER             969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12494E-01 0.88142E+00
   Friction velocity        uk    :  0.12494E-01 0.88142E+00
   Dimensionless distance   yplus :  0.10059E+00 0.70960E+01
   Friction thermal sca.    tstar : -0.56692E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75049E-01 0.52944E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75813E-02      32   0.37472E-03   0.18221E+01 0.90200E+02 
c  Velocity[X]                                      0.10599E+01 
c  Velocity[Y]                                      0.76220E+00 
c  Velocity[Z]                                      0.10338E-29 
c  Pressure     0.11036E-06     456   0.97528E-08   0.11280E+00 0.37069E+03 
c  nu_tilda     0.50552E-05      31   0.73352E-05   0.18447E-06 0.12697E+03 
c  TempC        0.30896E+02      26   0.40095E-03   0.71034E+01 0.28249E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4579          10.422          4.5729          4.5729
v  Velocity[Y]            -3.4612          7.0396       0.0037961       0.0037961
v  Velocity[Z]       -8.8907e-015     9.0809e-015    -1.0429e-017    -1.0429e-017
v  ǁVelocityǁ        0.00091905          10.423          5.2319          5.2319
v  Pressure               -54.806          20.422         -7.4586         -7.4586
v  nu_tilda           4.3185e-007       0.0042694       0.0010861       0.0010861
v  TempC                       21          73.069           21.69           21.69
v  TurbVisc           3.0594e-014        0.005032       0.0012713       0.0012713
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              969:        0.23510E+01

===============================================================


 INSTANT    0.970000000E+03   TIME STEP NUMBER             970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53521E-02 0.88077E+00
   Friction velocity        uk    :  0.53521E-02 0.88077E+00
   Dimensionless distance   yplus :  0.43088E-01 0.70908E+01
   Friction thermal sca.    tstar : -0.57491E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32149E-01 0.52905E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75847E-02      32   0.34761E-03   0.18465E+01 0.90530E+02 
c  Velocity[X]                                      0.10675E+01 
c  Velocity[Y]                                      0.77894E+00 
c  Velocity[Z]                                      0.14740E-29 
c  Pressure     0.11942E-06     394   0.97663E-08   0.12026E+00 0.27328E+03 
c  nu_tilda     0.50568E-05      31   0.14911E-04   0.18455E-06 0.12698E+03 
c  TempC        0.30907E+02      26   0.30240E-03   0.49898E+01 0.22824E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4558          10.422          4.5729          4.5729
v  Velocity[Y]            -3.4635          7.0602       0.0037612       0.0037612
v  Velocity[Z]       -9.4494e-015     9.0943e-015    -1.0402e-017    -1.0402e-017
v  ǁVelocityǁ         0.0011968          10.423          5.2321          5.2321
v  Pressure               -54.801          20.501         -7.4553         -7.4553
v  nu_tilda           4.3182e-007       0.0042694       0.0010867       0.0010867
v  TempC                       21          73.178           21.69           21.69
v  TurbVisc           3.0599e-014        0.005032       0.0012721       0.0012721
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              970:        0.21470E+01

===============================================================


 INSTANT    0.971000000E+03   TIME STEP NUMBER             971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99929E-02 0.88221E+00
   Friction velocity        uk    :  0.99929E-02 0.88221E+00
   Dimensionless distance   yplus :  0.80449E-01 0.71024E+01
   Friction thermal sca.    tstar : -0.56901E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60024E-01 0.52992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75880E-02      32   0.31320E-03   0.18174E+01 0.90343E+02 
c  Velocity[X]                                      0.10467E+01 
c  Velocity[Y]                                      0.77072E+00 
c  Velocity[Z]                                      0.10584E-29 
c  Pressure     0.10993E-06     424   0.93173E-08   0.11278E+00 0.35024E+03 
c  nu_tilda     0.50584E-05      31   0.73352E-05   0.18463E-06 0.12698E+03 
c  TempC        0.30918E+02      27   0.44398E-03   0.39245E+01 0.18205E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4536          10.423          4.5729          4.5729
v  Velocity[Y]            -3.4632          7.0724       0.0037265       0.0037265
v  Velocity[Z]       -1.0332e-014     9.0998e-015    -1.0374e-017    -1.0374e-017
v  ǁVelocityǁ        0.00040696          10.423          5.2324          5.2324
v  Pressure               -54.787          20.547         -7.4487         -7.4487
v  nu_tilda            4.318e-007       0.0042694       0.0010874       0.0010874
v  TempC                       21          73.504          21.691          21.691
v  TurbVisc           3.0591e-014        0.005032       0.0012728       0.0012728
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              971:        0.22740E+01

===============================================================


 INSTANT    0.972000000E+03   TIME STEP NUMBER             972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22574E-02 0.88160E+00
   Friction velocity        uk    :  0.22574E-02 0.88160E+00
   Dimensionless distance   yplus :  0.18174E-01 0.70975E+01
   Friction thermal sca.    tstar : -0.56738E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13560E-01 0.52955E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75913E-02      32   0.35741E-03   0.18265E+01 0.90328E+02 
c  Velocity[X]                                      0.10675E+01 
c  Velocity[Y]                                      0.75899E+00 
c  Velocity[Z]                                      0.10047E-29 
c  Pressure     0.12284E-06     488   0.96508E-08   0.12577E+00 0.83328E+03 
c  nu_tilda     0.50600E-05      31   0.14901E-04   0.18472E-06 0.12699E+03 
c  TempC        0.30930E+02      27   0.38678E-03   0.47766E+01 0.22223E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4517          10.423          4.5729          4.5729
v  Velocity[Y]            -3.4644          7.0407       0.0036921       0.0036921
v  Velocity[Z]        -9.942e-015     9.1112e-015    -1.0348e-017    -1.0348e-017
v  ǁVelocityǁ        0.00055657          10.424          5.2326          5.2326
v  Pressure               -54.778          20.383         -7.4949         -7.4949
v  nu_tilda           4.3189e-007       0.0042694        0.001088        0.001088
v  TempC                       21           73.12          21.691          21.691
v  TurbVisc           3.0584e-014        0.005032       0.0012736       0.0012736
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              972:        0.23060E+01

===============================================================


 INSTANT    0.973000000E+03   TIME STEP NUMBER             973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24747E-02 0.88049E+00
   Friction velocity        uk    :  0.24747E-02 0.88049E+00
   Dimensionless distance   yplus :  0.19923E-01 0.70886E+01
   Friction thermal sca.    tstar : -0.57535E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14865E-01 0.52889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75946E-02      32   0.30936E-03   0.18267E+01 0.90393E+02 
c  Velocity[X]                                      0.10483E+01 
c  Velocity[Y]                                      0.77839E+00 
c  Velocity[Z]                                      0.19235E-29 
c  Pressure     0.11697E-06     490   0.97235E-08   0.12020E+00 0.89690E+03 
c  nu_tilda     0.50616E-05      31   0.73359E-05   0.18480E-06 0.12700E+03 
c  TempC        0.30941E+02      26   0.49788E-03   0.48802E+01 0.23101E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4499          10.423          4.5729          4.5729
v  Velocity[Y]            -3.4647          7.0607       0.0036579       0.0036579
v  Velocity[Z]        -1.093e-014     9.1205e-015    -1.0297e-017    -1.0297e-017
v  ǁVelocityǁ          0.001504          10.424          5.2329          5.2329
v  Pressure               -54.761          20.549         -7.4566         -7.4566
v  nu_tilda           4.3195e-007       0.0042694       0.0010887       0.0010887
v  TempC                       21          73.139          21.691          21.691
v  TurbVisc           3.0608e-014        0.005032       0.0012744       0.0012744
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              973:        0.23240E+01

===============================================================


 INSTANT    0.974000000E+03   TIME STEP NUMBER             974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12296E-01 0.88149E+00
   Friction velocity        uk    :  0.12296E-01 0.88149E+00
   Dimensionless distance   yplus :  0.98994E-01 0.70966E+01
   Friction thermal sca.    tstar : -0.56508E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73861E-01 0.52949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75980E-02      32   0.34262E-03   0.18232E+01 0.90411E+02 
c  Velocity[X]                                      0.10462E+01 
c  Velocity[Y]                                      0.77696E+00 
c  Velocity[Z]                                      0.13209E-29 
c  Pressure     0.12006E-06     490   0.94093E-08   0.12359E+00 0.84273E+03 
c  nu_tilda     0.50632E-05      31   0.14906E-04   0.18489E-06 0.12701E+03 
c  TempC        0.30952E+02      26   0.37396E-03   0.74465E+01 0.28521E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4478          10.424          4.5729          4.5729
v  Velocity[Y]            -3.4662          7.0401       0.0036245       0.0036245
v  Velocity[Z]       -8.5879e-015     9.1275e-015    -1.0254e-017    -1.0254e-017
v  ǁVelocityǁ        0.00094831          10.425          5.2331          5.2331
v  Pressure                -54.76          20.398         -7.5082         -7.5082
v  nu_tilda           4.3202e-007       0.0042694       0.0010893       0.0010893
v  TempC                       21          74.166          21.692          21.692
v  TurbVisc           3.0627e-014        0.005032       0.0012751       0.0012751
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              974:        0.24080E+01

===============================================================


 INSTANT    0.975000000E+03   TIME STEP NUMBER             975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64683E-02 0.88076E+00
   Friction velocity        uk    :  0.64683E-02 0.88076E+00
   Dimensionless distance   yplus :  0.52074E-01 0.70907E+01
   Friction thermal sca.    tstar : -0.57506E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38853E-01 0.52904E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76013E-02      32   0.36386E-03   0.18257E+01 0.90408E+02 
c  Velocity[X]                                      0.10621E+01 
c  Velocity[Y]                                      0.76364E+00 
c  Velocity[Z]                                      0.11114E-29 
c  Pressure     0.10906E-06     473   0.93853E-08   0.11017E+00 0.63697E+03 
c  nu_tilda     0.50648E-05      31   0.73197E-05   0.18498E-06 0.12702E+03 
c  TempC        0.30963E+02      26   0.33989E-03   0.48814E+01 0.22144E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4458          10.424          4.5729          4.5729
v  Velocity[Y]            -3.4665          7.0674        0.003591        0.003591
v  Velocity[Z]       -1.0085e-014     9.1352e-015    -1.0227e-017    -1.0227e-017
v  ǁVelocityǁ          0.001106          10.425          5.2333          5.2333
v  Pressure               -54.746          20.509          -7.485          -7.485
v  nu_tilda           4.3202e-007       0.0042694         0.00109         0.00109
v  TempC                       21           73.07          21.692          21.692
v  TurbVisc           3.0646e-014        0.005032       0.0012759       0.0012759
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              975:        0.21830E+01

===============================================================


 INSTANT    0.976000000E+03   TIME STEP NUMBER             976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90903E-02 0.88216E+00
   Friction velocity        uk    :  0.90903E-02 0.88216E+00
   Dimensionless distance   yplus :  0.73183E-01 0.71020E+01
   Friction thermal sca.    tstar : -0.56829E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54603E-01 0.52989E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76046E-02      32   0.31518E-03   0.18267E+01 0.90470E+02 
c  Velocity[X]                                      0.10444E+01 
c  Velocity[Y]                                      0.78224E+00 
c  Velocity[Z]                                      0.10939E-29 
c  Pressure     0.10316E-06     426   0.91352E-08   0.10480E+00 0.28449E+03 
c  nu_tilda     0.50664E-05      31   0.14930E-04   0.18506E-06 0.12703E+03 
c  TempC        0.30975E+02      26   0.46254E-03   0.44170E+01 0.20944E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4438          10.424          4.5729          4.5729
v  Velocity[Y]            -3.4677          7.0686       0.0035582       0.0035582
v  Velocity[Z]       -9.3486e-015     9.1459e-015    -1.0198e-017    -1.0198e-017
v  ǁVelocityǁ         0.0012818          10.425          5.2336          5.2336
v  Pressure               -54.743           20.49         -7.5055         -7.5055
v  nu_tilda           4.3199e-007       0.0042694       0.0010906       0.0010906
v  TempC                       21          73.514          21.692          21.692
v  TurbVisc           3.0647e-014        0.005032       0.0012767       0.0012767
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              976:        0.20740E+01

===============================================================


 INSTANT    0.977000000E+03   TIME STEP NUMBER             977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10726E-01 0.88168E+00
   Friction velocity        uk    :  0.10726E-01 0.88168E+00
   Dimensionless distance   yplus :  0.86352E-01 0.70982E+01
   Friction thermal sca.    tstar : -0.56190E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64428E-01 0.52960E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76080E-02      32   0.32222E-03   0.18208E+01 0.90365E+02 
c  Velocity[X]                                      0.10526E+01 
c  Velocity[Y]                                      0.76818E+00 
c  Velocity[Z]                                      0.17867E-29 
c  Pressure     0.10487E-06     424   0.96875E-08   0.10879E+00 0.27839E+03 
c  nu_tilda     0.50680E-05      31   0.73242E-05   0.18514E-06 0.12703E+03 
c  TempC        0.30986E+02      27   0.37152E-03   0.81706E+01 0.27515E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4418          10.425          4.5729          4.5729
v  Velocity[Y]            -3.4685          7.0435       0.0035252       0.0035252
v  Velocity[Z]       -1.0633e-014      9.153e-015    -1.0151e-017    -1.0151e-017
v  ǁVelocityǁ        0.00088768          10.426          5.2338          5.2338
v  Pressure                -54.72          20.421         -7.5159         -7.5159
v  nu_tilda           4.3205e-007       0.0042694       0.0010913       0.0010913
v  TempC                       21          73.356          21.693          21.693
v  TurbVisc           3.0639e-014        0.005032       0.0012774       0.0012774
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              977:        0.20420E+01

===============================================================


 INSTANT    0.978000000E+03   TIME STEP NUMBER             978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32688E-02 0.88044E+00
   Friction velocity        uk    :  0.32688E-02 0.88044E+00
   Dimensionless distance   yplus :  0.26316E-01 0.70881E+01
   Friction thermal sca.    tstar : -0.56973E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19635E-01 0.52885E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76113E-02      32   0.35714E-03   0.18225E+01 0.90482E+02 
c  Velocity[X]                                      0.10594E+01 
c  Velocity[Y]                                      0.76311E+00 
c  Velocity[Z]                                      0.11959E-29 
c  Pressure     0.11090E-06     313   0.93667E-08   0.11313E+00 0.18159E+03 
c  nu_tilda     0.50696E-05      31   0.14928E-04   0.18523E-06 0.12704E+03 
c  TempC        0.30997E+02      27   0.45010E-03   0.58666E+01 0.23641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4397          10.425          4.5729          4.5729
v  Velocity[Y]            -3.4695           7.064       0.0034931       0.0034931
v  Velocity[Z]       -9.1005e-015     9.1634e-015    -1.0113e-017    -1.0113e-017
v  ǁVelocityǁ         0.0014402          10.426          5.2341          5.2341
v  Pressure                -54.72          20.473         -7.5226         -7.5226
v  nu_tilda           4.3206e-007       0.0042694       0.0010919       0.0010919
v  TempC                       21          73.069          21.693          21.693
v  TurbVisc           3.0654e-014        0.005032       0.0012782       0.0012782
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              978:        0.17840E+01

===============================================================


 INSTANT    0.979000000E+03   TIME STEP NUMBER             979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11442E-01 0.88146E+00
   Friction velocity        uk    :  0.11442E-01 0.88146E+00
   Dimensionless distance   yplus :  0.92116E-01 0.70964E+01
   Friction thermal sca.    tstar : -0.56626E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68729E-01 0.52947E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76146E-02      32   0.37384E-03   0.18649E+01 0.90852E+02 
c  Velocity[X]                                      0.10761E+01 
c  Velocity[Y]                                      0.78881E+00 
c  Velocity[Z]                                      0.17375E-29 
c  Pressure     0.12579E-06     426   0.99419E-08   0.12822E+00 0.28492E+03 
c  nu_tilda     0.50711E-05      31   0.73266E-05   0.18532E-06 0.12705E+03 
c  TempC        0.31008E+02      27   0.37645E-03   0.57455E+01 0.25896E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4376          10.425          4.5729          4.5729
v  Velocity[Y]            -3.4696          7.0394       0.0034611       0.0034611
v  Velocity[Z]       -1.0187e-014     1.0165e-014    -1.0067e-017    -1.0067e-017
v  ǁVelocityǁ        0.00097159          10.426          5.2343          5.2343
v  Pressure                 -54.7          20.402         -7.5358         -7.5358
v  nu_tilda           4.3211e-007       0.0042694       0.0010925       0.0010925
v  TempC                       21            73.6          21.693          21.693
v  TurbVisc           3.0658e-014        0.005032        0.001279        0.001279
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              979:        0.20380E+01

===============================================================


 INSTANT    0.980000000E+03   TIME STEP NUMBER             980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78326E-02 0.88091E+00
   Friction velocity        uk    :  0.78326E-02 0.88091E+00
   Dimensionless distance   yplus :  0.63058E-01 0.70919E+01
   Friction thermal sca.    tstar : -0.57437E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47048E-01 0.52914E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76179E-02      32   0.29388E-03   0.18520E+01 0.90779E+02 
c  Velocity[X]                                      0.10798E+01 
c  Velocity[Y]                                      0.77225E+00 
c  Velocity[Z]                                      0.10927E-29 
c  Pressure     0.97252E-07     313   0.98848E-08   0.98999E-01 0.19933E+03 
c  nu_tilda     0.50727E-05      31   0.14931E-04   0.18541E-06 0.12706E+03 
c  TempC        0.31020E+02      26   0.29342E-03   0.54260E+01 0.23638E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4358          10.426          4.5729          4.5729
v  Velocity[Y]            -3.4703          7.0624       0.0034292       0.0034292
v  Velocity[Z]       -8.9154e-015     9.1794e-015    -1.0034e-017    -1.0034e-017
v  ǁVelocityǁ        0.00057439          10.427          5.2345          5.2345
v  Pressure                 -54.7          20.462         -7.5409         -7.5409
v  nu_tilda           4.3208e-007       0.0042694       0.0010932       0.0010932
v  TempC                       21           73.07          21.694          21.694
v  TurbVisc           3.0672e-014        0.005032       0.0012797       0.0012797
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              980:        0.17680E+01

===============================================================


 INSTANT    0.981000000E+03   TIME STEP NUMBER             981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76434E-02 0.88222E+00
   Friction velocity        uk    :  0.76434E-02 0.88222E+00
   Dimensionless distance   yplus :  0.61534E-01 0.71025E+01
   Friction thermal sca.    tstar : -0.56638E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45911E-01 0.52992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76212E-02      32   0.34132E-03   0.17970E+01 0.90303E+02 
c  Velocity[X]                                      0.10325E+01 
c  Velocity[Y]                                      0.76442E+00 
c  Velocity[Z]                                      0.12872E-29 
c  Pressure     0.96172E-07     425   0.90612E-08   0.98259E-01 0.35825E+03 
c  nu_tilda     0.50743E-05      31   0.73142E-05   0.18550E-06 0.12707E+03 
c  TempC        0.31031E+02      27   0.43427E-03   0.29655E+01 0.16822E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4339          10.426          4.5729          4.5729
v  Velocity[Y]              -3.47          7.0732       0.0033977       0.0033977
v  Velocity[Z]       -1.0286e-014     1.0788e-014    -9.9926e-018    -9.9926e-018
v  ǁVelocityǁ         0.0011433          10.427          5.2348          5.2348
v  Pressure               -54.681          20.504         -7.5325         -7.5325
v  nu_tilda             4.32e-007       0.0042694       0.0010938       0.0010938
v  TempC                       21          73.426          21.694          21.694
v  TurbVisc           3.0662e-014        0.005032       0.0012805       0.0012805
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              981:        0.20550E+01

===============================================================


 INSTANT    0.982000000E+03   TIME STEP NUMBER             982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11353E-01 0.88177E+00
   Friction velocity        uk    :  0.11353E-01 0.88177E+00
   Dimensionless distance   yplus :  0.91400E-01 0.70988E+01
   Friction thermal sca.    tstar : -0.56563E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68195E-01 0.52965E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76245E-02      32   0.32508E-03   0.18422E+01 0.90793E+02 
c  Velocity[X]                                      0.10528E+01 
c  Velocity[Y]                                      0.78947E+00 
c  Velocity[Z]                                      0.13444E-29 
c  Pressure     0.10857E-06     474   0.95566E-08   0.11226E+00 0.81086E+03 
c  nu_tilda     0.50759E-05      31   0.14954E-04   0.18559E-06 0.12708E+03 
c  TempC        0.31042E+02      27   0.47898E-03   0.52361E+01 0.21748E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4319          10.426          4.5729          4.5729
v  Velocity[Y]            -3.4711          7.0466       0.0033666       0.0033666
v  Velocity[Z]       -1.0383e-014      9.194e-015    -9.9653e-018    -9.9653e-018
v  ǁVelocityǁ        0.00088063          10.427           5.235           5.235
v  Pressure               -54.677          20.353         -7.5806         -7.5806
v  nu_tilda           4.3198e-007       0.0042694       0.0010944       0.0010944
v  TempC                       21           73.07          21.694          21.694
v  TurbVisc           3.0642e-014        0.005032       0.0012813       0.0012813
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              982:        0.21720E+01

===============================================================


 INSTANT    0.983000000E+03   TIME STEP NUMBER             983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33759E-03 0.88062E+00
   Friction velocity        uk    :  0.33759E-03 0.88062E+00
   Dimensionless distance   yplus :  0.27178E-02 0.70896E+01
   Friction thermal sca.    tstar : -0.57563E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20278E-02 0.52896E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76278E-02      32   0.30094E-03   0.18259E+01 0.90570E+02 
c  Velocity[X]                                      0.10526E+01 
c  Velocity[Y]                                      0.77325E+00 
c  Velocity[Z]                                      0.12006E-29 
c  Pressure     0.10819E-06     472   0.93286E-08   0.10883E+00 0.63456E+03 
c  nu_tilda     0.50775E-05      31   0.73116E-05   0.18568E-06 0.12709E+03 
c  TempC        0.31053E+02      26   0.35662E-03   0.51050E+01 0.23120E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.43          10.427          4.5729          4.5729
v  Velocity[Y]            -3.4711          7.0647       0.0033357       0.0033357
v  Velocity[Z]       -1.0231e-014     1.1384e-014    -9.9217e-018    -9.9217e-018
v  ǁVelocityǁ          0.001332          10.428          5.2352          5.2352
v  Pressure               -54.661          20.462          -7.557          -7.557
v  nu_tilda           4.3203e-007       0.0042694       0.0010951       0.0010951
v  TempC                       21           73.07          21.695          21.695
v  TurbVisc           3.0634e-014        0.005032        0.001282        0.001282
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              983:        0.23530E+01

===============================================================


 INSTANT    0.984000000E+03   TIME STEP NUMBER             984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80138E-02 0.88170E+00
   Friction velocity        uk    :  0.80138E-02 0.88170E+00
   Dimensionless distance   yplus :  0.64517E-01 0.70983E+01
   Friction thermal sca.    tstar : -0.56933E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48137E-01 0.52961E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76312E-02      32   0.37704E-03   0.18128E+01 0.90443E+02 
c  Velocity[X]                                      0.10492E+01 
c  Velocity[Y]                                      0.76363E+00 
c  Velocity[Z]                                      0.15661E-29 
c  Pressure     0.11054E-06     440   0.95341E-08   0.11421E+00 0.47753E+03 
c  nu_tilda     0.50791E-05      31   0.14949E-04   0.18577E-06 0.12710E+03 
c  TempC        0.31064E+02      26   0.47042E-03   0.45906E+01 0.22525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4281          10.427          4.5729          4.5729
v  Velocity[Y]            -3.4715          7.0429       0.0033054       0.0033054
v  Velocity[Z]       -1.0715e-014     1.4216e-014    -9.8644e-018    -9.8644e-018
v  ǁVelocityǁ         0.0010802          10.428          5.2355          5.2355
v  Pressure               -54.651          20.377         -7.5831         -7.5831
v  nu_tilda           4.3216e-007       0.0042695       0.0010957       0.0010957
v  TempC                       21          74.111          21.695          21.695
v  TurbVisc           3.0649e-014        0.005032       0.0012828       0.0012828
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              984:        0.23190E+01

===============================================================


 INSTANT    0.985000000E+03   TIME STEP NUMBER             985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88175E-02 0.88108E+00
   Friction velocity        uk    :  0.88175E-02 0.88108E+00
   Dimensionless distance   yplus :  0.70987E-01 0.70933E+01
   Friction thermal sca.    tstar : -0.57393E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52964E-01 0.52924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76344E-02      32   0.32901E-03   0.18572E+01 0.90974E+02 
c  Velocity[X]                                      0.10721E+01 
c  Velocity[Y]                                      0.78504E+00 
c  Velocity[Z]                                      0.19344E-29 
c  Pressure     0.12955E-06     441   0.98271E-08   0.13204E+00 0.50733E+03 
c  nu_tilda     0.50807E-05      31   0.73073E-05   0.18586E-06 0.12711E+03 
c  TempC        0.31076E+02      26   0.35959E-03   0.66903E+01 0.26790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4261          10.427          4.5729          4.5729
v  Velocity[Y]             -3.471          7.0674       0.0032749       0.0032749
v  Velocity[Z]       -9.5099e-015     1.0844e-014    -9.8362e-018    -9.8362e-018
v  ǁVelocityǁ        0.00097039          10.428          5.2357          5.2357
v  Pressure                -54.64          20.473           -7.57           -7.57
v  nu_tilda           4.3219e-007       0.0042695       0.0010964       0.0010964
v  TempC                       21           73.07          21.696          21.696
v  TurbVisc           3.0687e-014        0.005032       0.0012836       0.0012836
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              985:        0.20780E+01

===============================================================


 INSTANT    0.986000000E+03   TIME STEP NUMBER             986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71704E-02 0.88228E+00
   Friction velocity        uk    :  0.71704E-02 0.88228E+00
   Dimensionless distance   yplus :  0.57727E-01 0.71029E+01
   Friction thermal sca.    tstar : -0.56546E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43071E-01 0.52996E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76378E-02      32   0.31203E-03   0.18323E+01 0.90680E+02 
c  Velocity[X]                                      0.10586E+01 
c  Velocity[Y]                                      0.77375E+00 
c  Velocity[Z]                                      0.11765E-29 
c  Pressure     0.11557E-06     442   0.99431E-08   0.11630E+00 0.36650E+03 
c  nu_tilda     0.50823E-05      31   0.14950E-04   0.18595E-06 0.12712E+03 
c  TempC        0.31087E+02      26   0.39037E-03   0.51907E+01 0.22125E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.424          10.428          4.5729          4.5729
v  Velocity[Y]             -3.472          7.0705       0.0032453       0.0032453
v  Velocity[Z]       -1.0408e-014     1.2027e-014    -9.7939e-018    -9.7939e-018
v  ǁVelocityǁ         0.0014859          10.428          5.2359          5.2359
v  Pressure               -54.635          20.427         -7.5943         -7.5943
v  nu_tilda           4.3215e-007       0.0042695        0.001097        0.001097
v  TempC                       21          73.086          21.696          21.696
v  TurbVisc           3.0696e-014        0.005032       0.0012843       0.0012843
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              986:        0.20900E+01

===============================================================


 INSTANT    0.987000000E+03   TIME STEP NUMBER             987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89154E-02 0.88206E+00
   Friction velocity        uk    :  0.89154E-02 0.88206E+00
   Dimensionless distance   yplus :  0.71775E-01 0.71012E+01
   Friction thermal sca.    tstar : -0.56618E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53552E-01 0.52983E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76410E-02      32   0.33689E-03   0.18313E+01 0.90672E+02 
c  Velocity[X]                                      0.10644E+01 
c  Velocity[Y]                                      0.76692E+00 
c  Velocity[Z]                                      0.13595E-29 
c  Pressure     0.11650E-06     408   0.99426E-08   0.12108E+00 0.25431E+03 
c  nu_tilda     0.50839E-05      31   0.72977E-05   0.18605E-06 0.12713E+03 
c  TempC        0.31098E+02      26   0.45180E-03   0.50047E+01 0.22107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4222          10.428          4.5729          4.5729
v  Velocity[Y]            -3.4717          7.0469       0.0032156       0.0032156
v  Velocity[Z]       -1.0937e-014     1.5328e-014    -9.7384e-018    -9.7384e-018
v  ǁVelocityǁ        0.00089566          10.429          5.2361          5.2361
v  Pressure               -54.611          20.373         -7.6024         -7.6024
v  nu_tilda           4.3219e-007       0.0042695       0.0010977       0.0010977
v  TempC                       21          73.346          21.696          21.696
v  TurbVisc           3.0683e-014        0.005032       0.0012851       0.0012851
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              987:        0.20990E+01

===============================================================


 INSTANT    0.988000000E+03   TIME STEP NUMBER             988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47038E-02 0.88076E+00
   Friction velocity        uk    :  0.47038E-02 0.88076E+00
   Dimensionless distance   yplus :  0.37869E-01 0.70907E+01
   Friction thermal sca.    tstar : -0.57393E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28254E-01 0.52905E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76443E-02      32   0.34714E-03   0.18297E+01 0.90828E+02 
c  Velocity[X]                                      0.10409E+01 
c  Velocity[Y]                                      0.78878E+00 
c  Velocity[Z]                                      0.13338E-29 
c  Pressure     0.91051E-07     378   0.92484E-08   0.92292E-01 0.17496E+03 
c  nu_tilda     0.50855E-05      31   0.14979E-04   0.18614E-06 0.12715E+03 
c  TempC        0.31109E+02      27   0.36715E-03   0.53205E+01 0.23129E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4203          10.428          4.5729          4.5729
v  Velocity[Y]             -3.472          7.0655       0.0031864       0.0031864
v  Velocity[Z]       -1.0576e-014     1.1652e-014    -9.7143e-018    -9.7143e-018
v  ǁVelocityǁ         0.0012464          10.429          5.2364          5.2364
v  Pressure               -54.614          20.418         -7.6124         -7.6124
v  nu_tilda           4.3221e-007       0.0042695       0.0010983       0.0010983
v  TempC                       21          73.069          21.697          21.697
v  TurbVisc           3.0696e-014        0.005032       0.0012858       0.0012858
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              988:        0.20670E+01

===============================================================


 INSTANT    0.989000000E+03   TIME STEP NUMBER             989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12431E-02 0.88190E+00
   Friction velocity        uk    :  0.12431E-02 0.88190E+00
   Dimensionless distance   yplus :  0.10008E-01 0.70999E+01
   Friction thermal sca.    tstar : -0.56682E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74672E-02 0.52973E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76476E-02      32   0.35697E-03   0.18534E+01 0.91062E+02 
c  Velocity[X]                                      0.10648E+01 
c  Velocity[Y]                                      0.78864E+00 
c  Velocity[Z]                                      0.12157E-29 
c  Pressure     0.12324E-06     409   0.94886E-08   0.12620E+00 0.28530E+03 
c  nu_tilda     0.50871E-05      31   0.72969E-05   0.18622E-06 0.12716E+03 
c  TempC        0.31121E+02      27   0.43154E-03   0.44095E+01 0.20097E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4185          10.428          4.5729          4.5729
v  Velocity[Y]            -3.4722          7.0487       0.0031573       0.0031573
v  Velocity[Z]       -1.1459e-014     1.3553e-014    -9.6789e-018    -9.6789e-018
v  ǁVelocityǁ         0.0004866          10.429          5.2366          5.2366
v  Pressure               -54.594          20.349         -7.6261         -7.6261
v  nu_tilda           4.3227e-007       0.0042695        0.001099        0.001099
v  TempC                       21           74.12          21.697          21.697
v  TurbVisc           3.0701e-014        0.005032       0.0012866       0.0012866
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              989:        0.20010E+01

===============================================================


 INSTANT    0.990000000E+03   TIME STEP NUMBER             990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18291E-02 0.88129E+00
   Friction velocity        uk    :  0.18291E-02 0.88129E+00
   Dimensionless distance   yplus :  0.14726E-01 0.70950E+01
   Friction thermal sca.    tstar : -0.57341E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10987E-01 0.52936E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76509E-02      32   0.34466E-03   0.18459E+01 0.90925E+02 
c  Velocity[X]                                      0.10754E+01 
c  Velocity[Y]                                      0.77050E+00 
c  Velocity[Z]                                      0.11414E-29 
c  Pressure     0.12156E-06     393   0.89144E-08   0.12251E+00 0.25641E+03 
c  nu_tilda     0.50887E-05      31   0.14972E-04   0.18632E-06 0.12717E+03 
c  TempC        0.31132E+02      27   0.42251E-03   0.41326E+01 0.21039E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4166          10.429          4.5729          4.5729
v  Velocity[Y]            -3.4722           7.068       0.0031287       0.0031287
v  Velocity[Z]       -1.1735e-014     1.6159e-014    -9.6275e-018    -9.6275e-018
v  ǁVelocityǁ        0.00072919           10.43          5.2368          5.2368
v  Pressure               -54.588          20.422         -7.6243         -7.6243
v  nu_tilda           4.3227e-007       0.0042695       0.0010996       0.0010996
v  TempC                       21          73.533          21.697          21.697
v  TurbVisc           3.0718e-014        0.005032       0.0012874       0.0012874
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              990:        0.19800E+01

===============================================================


 INSTANT    0.991000000E+03   TIME STEP NUMBER             991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59482E-02 0.88249E+00
   Friction velocity        uk    :  0.59482E-02 0.88249E+00
   Dimensionless distance   yplus :  0.47887E-01 0.71046E+01
   Friction thermal sca.    tstar : -0.56909E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35729E-01 0.53008E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76542E-02      32   0.32052E-03   0.18276E+01 0.90872E+02 
c  Velocity[X]                                      0.10344E+01 
c  Velocity[Y]                                      0.79324E+00 
c  Velocity[Z]                                      0.14430E-29 
c  Pressure     0.92022E-07     424   0.92737E-08   0.93763E-01 0.32650E+03 
c  nu_tilda     0.50903E-05      31   0.72966E-05   0.18641E-06 0.12718E+03 
c  TempC        0.31143E+02      26   0.34493E-03   0.44933E+01 0.20098E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4147          10.429          4.5729          4.5729
v  Velocity[Y]            -3.4706          7.0747          0.0031          0.0031
v  Velocity[Z]       -1.1058e-014     1.5476e-014    -9.5928e-018    -9.5928e-018
v  ǁVelocityǁ         0.0015684           10.43           5.237           5.237
v  Pressure               -54.574          20.456          -7.618          -7.618
v  nu_tilda           4.3219e-007       0.0042695       0.0011002       0.0011002
v  TempC                       21          73.068          21.698          21.698
v  TurbVisc           3.0718e-014        0.005032       0.0012881       0.0012881
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              991:        0.20170E+01

===============================================================


 INSTANT    0.992000000E+03   TIME STEP NUMBER             992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12726E-01 0.88206E+00
   Friction velocity        uk    :  0.12726E-01 0.88206E+00
   Dimensionless distance   yplus :  0.10246E+00 0.71012E+01
   Friction thermal sca.    tstar : -0.56810E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76443E-01 0.52983E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76575E-02      32   0.29482E-03   0.18363E+01 0.90912E+02 
c  Velocity[X]                                      0.10578E+01 
c  Velocity[Y]                                      0.77850E+00 
c  Velocity[Z]                                      0.15724E-29 
c  Pressure     0.12138E-06     472   0.98941E-08   0.12578E+00 0.69077E+03 
c  nu_tilda     0.50919E-05      31   0.14978E-04   0.18651E-06 0.12719E+03 
c  TempC        0.31154E+02      26   0.47593E-03   0.44886E+01 0.21060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4127          10.429          4.5729          4.5729
v  Velocity[Y]            -3.4729          7.0505       0.0030722       0.0030722
v  Velocity[Z]       -1.0699e-014     1.6996e-014    -9.5447e-018    -9.5447e-018
v  ǁVelocityǁ        0.00092673           10.43          5.2373          5.2373
v  Pressure               -54.565          20.328         -7.6583         -7.6583
v  nu_tilda           4.3219e-007       0.0042695       0.0011009       0.0011009
v  TempC                       21          73.068          21.698          21.698
v  TurbVisc           3.0696e-014        0.005032       0.0012889       0.0012889
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              992:        0.21560E+01

===============================================================


 INSTANT    0.993000000E+03   TIME STEP NUMBER             993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61573E-02 0.88069E+00
   Friction velocity        uk    :  0.61573E-02 0.88069E+00
   Dimensionless distance   yplus :  0.49570E-01 0.70902E+01
   Friction thermal sca.    tstar : -0.57496E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36985E-01 0.52901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76608E-02      32   0.36396E-03   0.18192E+01 0.90735E+02 
c  Velocity[X]                                      0.10504E+01 
c  Velocity[Y]                                      0.76880E+00 
c  Velocity[Z]                                      0.11049E-29 
c  Pressure     0.12261E-06     440   0.98049E-08   0.12315E+00 0.45370E+03 
c  nu_tilda     0.50935E-05      31   0.72784E-05   0.18661E-06 0.12721E+03 
c  TempC        0.31165E+02      26   0.40776E-03   0.66393E+01 0.26841E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4108          10.429          4.5729          4.5729
v  Velocity[Y]            -3.4735          7.0673       0.0030441       0.0030441
v  Velocity[Z]       -1.0667e-014      1.638e-014    -9.5112e-018    -9.5112e-018
v  ǁVelocityǁ         0.0011311           10.43          5.2375          5.2375
v  Pressure               -54.551          20.399         -7.6454         -7.6454
v  nu_tilda           4.3222e-007       0.0042695       0.0011015       0.0011015
v  TempC                       21          73.127          21.698          21.698
v  TurbVisc           3.0696e-014        0.005032       0.0012897       0.0012897
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              993:        0.20620E+01

===============================================================


 INSTANT    0.994000000E+03   TIME STEP NUMBER             994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83382E-02 0.88202E+00
   Friction velocity        uk    :  0.83382E-02 0.88202E+00
   Dimensionless distance   yplus :  0.67128E-01 0.71009E+01
   Friction thermal sca.    tstar : -0.57004E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50085E-01 0.52980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76641E-02      32   0.36530E-03   0.18791E+01 0.91332E+02 
c  Velocity[X]                                      0.10857E+01 
c  Velocity[Y]                                      0.79341E+00 
c  Velocity[Z]                                      0.11871E-29 
c  Pressure     0.15394E-06     457   0.94778E-08   0.15953E+00 0.48664E+03 
c  nu_tilda     0.50951E-05      31   0.15001E-04   0.18671E-06 0.12722E+03 
c  TempC        0.31177E+02      27   0.44652E-03   0.42259E+01 0.21499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4089           10.43          4.5729          4.5729
v  Velocity[Y]            -3.4736          7.0441       0.0030167       0.0030167
v  Velocity[Z]       -1.0645e-014     1.8581e-014    -9.4627e-018    -9.4627e-018
v  ǁVelocityǁ         0.0012673           10.43          5.2377          5.2377
v  Pressure               -54.538          20.319         -7.6733         -7.6733
v  nu_tilda           4.3226e-007       0.0042695       0.0011022       0.0011022
v  TempC                       21          74.058          21.699          21.699
v  TurbVisc           3.0702e-014        0.005032       0.0012904       0.0012904
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              994:        0.21320E+01

===============================================================


 INSTANT    0.995000000E+03   TIME STEP NUMBER             995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10672E-01 0.88141E+00
   Friction velocity        uk    :  0.10672E-01 0.88141E+00
   Dimensionless distance   yplus :  0.85916E-01 0.70959E+01
   Friction thermal sca.    tstar : -0.57854E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64103E-01 0.52944E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76673E-02      32   0.29094E-03   0.18486E+01 0.91101E+02 
c  Velocity[X]                                      0.10689E+01 
c  Velocity[Y]                                      0.77961E+00 
c  Velocity[Z]                                      0.11112E-29 
c  Pressure     0.10185E-06     473   0.98770E-08   0.10375E+00 0.71454E+03 
c  nu_tilda     0.50967E-05      31   0.72680E-05   0.18680E-06 0.12723E+03 
c  TempC        0.31188E+02      27   0.37453E-03   0.54437E+01 0.24824E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4073           10.43          4.5729          4.5729
v  Velocity[Y]            -3.4728          7.0711       0.0029893       0.0029893
v  Velocity[Z]       -1.0405e-014     1.7427e-014    -9.4316e-018    -9.4316e-018
v  ǁVelocityǁ        0.00087832          10.431          5.2379          5.2379
v  Pressure               -54.524          20.452          -7.646          -7.646
v  nu_tilda           4.3228e-007       0.0042695       0.0011028       0.0011028
v  TempC                       21          73.512          21.699          21.699
v  TurbVisc           3.0714e-014        0.005032       0.0012912       0.0012912
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              995:        0.21680E+01

===============================================================


 INSTANT    0.996000000E+03   TIME STEP NUMBER             996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35966E-02 0.88264E+00
   Friction velocity        uk    :  0.35966E-02 0.88264E+00
   Dimensionless distance   yplus :  0.28955E-01 0.71058E+01
   Friction thermal sca.    tstar : -0.57173E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21604E-01 0.53017E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76706E-02      32   0.36391E-03   0.18102E+01 0.90731E+02 
c  Velocity[X]                                      0.10392E+01 
c  Velocity[Y]                                      0.77101E+00 
c  Velocity[Z]                                      0.10232E-29 
c  Pressure     0.12084E-06     473   0.92432E-08   0.12090E+00 0.58550E+03 
c  nu_tilda     0.50983E-05      31   0.14992E-04   0.18690E-06 0.12724E+03 
c  TempC        0.31199E+02      26   0.32377E-03   0.62486E+01 0.25830E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4055           10.43          4.5729          4.5729
v  Velocity[Y]            -3.4738          7.0756       0.0029625       0.0029625
v  Velocity[Z]       -1.0052e-014     1.5446e-014    -9.4083e-018    -9.4083e-018
v  ǁVelocityǁ         0.0014654          10.431          5.2382          5.2382
v  Pressure               -54.522          20.362         -7.6849         -7.6849
v  nu_tilda           4.3228e-007       0.0042695       0.0011034       0.0011034
v  TempC                       21          73.081          21.699          21.699
v  TurbVisc            3.072e-014        0.005032        0.001292        0.001292
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              996:        0.21850E+01

===============================================================


 INSTANT    0.997000000E+03   TIME STEP NUMBER             997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12106E-01 0.88250E+00
   Friction velocity        uk    :  0.12106E-01 0.88250E+00
   Dimensionless distance   yplus :  0.97463E-01 0.71047E+01
   Friction thermal sca.    tstar : -0.57023E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72718E-01 0.53009E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76739E-02      32   0.33594E-03   0.18550E+01 0.91100E+02 
c  Velocity[X]                                      0.10839E+01 
c  Velocity[Y]                                      0.77109E+00 
c  Velocity[Z]                                      0.17625E-29 
c  Pressure     0.11156E-06     346   0.93714E-08   0.11557E+00 0.22705E+03 
c  nu_tilda     0.51000E-05      31   0.72806E-05   0.18700E-06 0.12726E+03 
c  TempC        0.31210E+02      26   0.48608E-03   0.52582E+01 0.23504E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4037          10.431          4.5729          4.5729
v  Velocity[Y]            -3.4732           7.051       0.0029354       0.0029354
v  Velocity[Z]       -1.0495e-014     1.7959e-014    -9.3682e-018    -9.3682e-018
v  ǁVelocityǁ        0.00090103          10.432          5.2384          5.2384
v  Pressure               -54.502          20.323         -7.6908         -7.6908
v  nu_tilda           4.3235e-007       0.0042695       0.0011041       0.0011041
v  TempC                       21          73.069            21.7            21.7
v  TurbVisc            3.072e-014        0.005032       0.0012927       0.0012927
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              997:        0.19570E+01

===============================================================


 INSTANT    0.998000000E+03   TIME STEP NUMBER             998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76548E-02 0.88114E+00
   Friction velocity        uk    :  0.76548E-02 0.88114E+00
   Dimensionless distance   yplus :  0.61627E-01 0.70938E+01
   Friction thermal sca.    tstar : -0.57480E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45980E-01 0.52928E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76772E-02      32   0.32273E-03   0.18361E+01 0.91079E+02 
c  Velocity[X]                                      0.10457E+01 
c  Velocity[Y]                                      0.79043E+00 
c  Velocity[Z]                                      0.11532E-29 
c  Pressure     0.10060E-06     410   0.96345E-08   0.10263E+00 0.27542E+03 
c  nu_tilda     0.51016E-05      31   0.15002E-04   0.18710E-06 0.12727E+03 
c  TempC        0.31221E+02      27   0.36422E-03   0.66957E+01 0.28349E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4019          10.431          4.5729          4.5729
v  Velocity[Y]            -3.4735          7.0699       0.0029093       0.0029093
v  Velocity[Z]       -1.0601e-014     1.9298e-014    -9.3284e-018    -9.3284e-018
v  ǁVelocityǁ        0.00042116          10.432          5.2386          5.2386
v  Pressure               -54.496          20.403         -7.6881         -7.6881
v  nu_tilda           4.3239e-007       0.0042695       0.0011047       0.0011047
v  TempC                       21          73.278            21.7            21.7
v  TurbVisc           3.0741e-014        0.005032       0.0012935       0.0012935
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              998:        0.20760E+01

===============================================================


 INSTANT    0.999000000E+03   TIME STEP NUMBER             999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38402E-02 0.88215E+00
   Friction velocity        uk    :  0.38402E-02 0.88215E+00
   Dimensionless distance   yplus :  0.30917E-01 0.71019E+01
   Friction thermal sca.    tstar : -0.56852E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23067E-01 0.52988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76804E-02      32   0.30970E-03   0.18415E+01 0.91117E+02 
c  Velocity[X]                                      0.10502E+01 
c  Velocity[Y]                                      0.79127E+00 
c  Velocity[Z]                                      0.99551E-30 
c  Pressure     0.11448E-06     472   0.95889E-08   0.11769E+00 0.40874E+03 
c  nu_tilda     0.51032E-05      31   0.72640E-05   0.18720E-06 0.12728E+03 
c  TempC        0.31232E+02      26   0.32719E-03   0.58896E+01 0.24973E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.4          10.432          4.5729          4.5729
v  Velocity[Y]            -3.4735          7.0476       0.0028829       0.0028829
v  Velocity[Z]       -1.0639e-014     1.8611e-014    -9.3045e-018    -9.3045e-018
v  ǁVelocityǁ         0.0013879          10.433          5.2388          5.2388
v  Pressure               -54.478          20.296         -7.7108         -7.7108
v  nu_tilda           4.3244e-007       0.0042695       0.0011054       0.0011054
v  TempC                       21          73.806          21.701          21.701
v  TurbVisc            3.075e-014        0.005032       0.0012943       0.0012943
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP              999:        0.21740E+01

===============================================================


 INSTANT    0.100000000E+04   TIME STEP NUMBER            1000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11579E-01 0.88148E+00
   Friction velocity        uk    :  0.11579E-01 0.88148E+00
   Dimensionless distance   yplus :  0.93221E-01 0.70965E+01
   Friction thermal sca.    tstar : -0.58103E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69553E-01 0.52948E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76837E-02      32   0.37103E-03   0.18239E+01 0.90954E+02 
c  Velocity[X]                                      0.10488E+01 
c  Velocity[Y]                                      0.77516E+00 
c  Velocity[Z]                                      0.13217E-29 
c  Pressure     0.98673E-07     394   0.91210E-08   0.10041E+00 0.24817E+03 
c  nu_tilda     0.51048E-05      31   0.15024E-04   0.18730E-06 0.12730E+03 
c  TempC        0.31244E+02      27   0.43799E-03   0.40142E+01 0.20400E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3982          10.432          4.5729          4.5729
v  Velocity[Y]            -3.4742          7.0708       0.0028572       0.0028572
v  Velocity[Z]       -1.0476e-014      1.888e-014    -9.2738e-018    -9.2738e-018
v  ǁVelocityǁ        0.00087043          10.433           5.239           5.239
v  Pressure               -54.474          20.367         -7.7101         -7.7101
v  nu_tilda           4.3244e-007       0.0042695        0.001106        0.001106
v  TempC                       21          73.069          21.701          21.701
v  TurbVisc           3.0766e-014        0.005032        0.001295        0.001295
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1000:        0.19950E+01

===============================================================


 INSTANT    0.100100000E+04   TIME STEP NUMBER            1001
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22255E-02 0.88284E+00
   Friction velocity        uk    :  0.22255E-02 0.88284E+00
   Dimensionless distance   yplus :  0.17917E-01 0.71074E+01
   Friction thermal sca.    tstar : -0.57293E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13368E-01 0.53029E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76870E-02      32   0.35863E-03   0.18603E+01 0.91410E+02 
c  Velocity[X]                                      0.10642E+01 
c  Velocity[Y]                                      0.79617E+00 
c  Velocity[Z]                                      0.11803E-29 
c  Pressure     0.12668E-06     426   0.91672E-08   0.12864E+00 0.34369E+03 
c  nu_tilda     0.51064E-05      31   0.72604E-05   0.18739E-06 0.12731E+03 
c  TempC        0.31255E+02      26   0.38884E-03   0.60201E+01 0.24642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3963          10.432          4.5729          4.5729
v  Velocity[Y]            -3.4738          7.0808       0.0028314       0.0028314
v  Velocity[Z]       -1.0454e-014     1.8719e-014    -9.2463e-018    -9.2463e-018
v  ǁVelocityǁ         0.0013185          10.433          5.2392          5.2392
v  Pressure               -54.458          20.413         -7.7035         -7.7035
v  nu_tilda           4.3242e-007       0.0042695       0.0011067       0.0011067
v  TempC                       21           73.07          21.701          21.701
v  TurbVisc           3.0767e-014        0.005032       0.0012958       0.0012958
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1001:        0.21090E+01

===============================================================


 INSTANT    0.100200000E+04   TIME STEP NUMBER            1002
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11111E-01 0.88235E+00
   Friction velocity        uk    :  0.11111E-01 0.88235E+00
   Dimensionless distance   yplus :  0.89448E-01 0.71035E+01
   Friction thermal sca.    tstar : -0.56488E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66739E-01 0.53000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76902E-02      32   0.29596E-03   0.18707E+01 0.91441E+02 
c  Velocity[X]                                      0.10878E+01 
c  Velocity[Y]                                      0.78287E+00 
c  Velocity[Z]                                      0.12493E-29 
c  Pressure     0.11848E-06     489   0.98352E-08   0.12088E+00 0.92843E+03 
c  nu_tilda     0.51080E-05      31   0.15017E-04   0.18750E-06 0.12732E+03 
c  TempC        0.31266E+02      26   0.31809E-03   0.74539E+01 0.27221E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3945          10.433          4.5729          4.5729
v  Velocity[Y]            -3.4745          7.0497       0.0028059       0.0028059
v  Velocity[Z]       -1.0469e-014     1.9375e-014    -9.2146e-018    -9.2146e-018
v  ǁVelocityǁ         0.0010736          10.433          5.2394          5.2394
v  Pressure               -54.449          20.229         -7.7555         -7.7555
v  nu_tilda            4.325e-007       0.0042695       0.0011073       0.0011073
v  TempC                       21          73.433          21.702          21.702
v  TurbVisc           3.0761e-014        0.005032       0.0012965       0.0012965
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1002:        0.22160E+01

===============================================================


 INSTANT    0.100300000E+04   TIME STEP NUMBER            1003
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88421E-02 0.88137E+00
   Friction velocity        uk    :  0.88421E-02 0.88137E+00
   Dimensionless distance   yplus :  0.71185E-01 0.70957E+01
   Friction thermal sca.    tstar : -0.58071E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53112E-01 0.52942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76935E-02      32   0.33035E-03   0.18212E+01 0.90981E+02 
c  Velocity[X]                                      0.10459E+01 
c  Velocity[Y]                                      0.77535E+00 
c  Velocity[Z]                                      0.15612E-29 
c  Pressure     0.87548E-07     488   0.93619E-08   0.89591E-01 0.83712E+03 
c  nu_tilda     0.51096E-05      31   0.72658E-05   0.18760E-06 0.12734E+03 
c  TempC        0.31277E+02      26   0.48270E-03   0.51174E+01 0.23390E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3928          10.433          4.5729          4.5729
v  Velocity[Y]            -3.4738          7.0718       0.0027809       0.0027809
v  Velocity[Z]        -1.065e-014     1.9518e-014    -9.1916e-018    -9.1916e-018
v  ǁVelocityǁ        0.00095298          10.434          5.2397          5.2397
v  Pressure               -54.434          20.393         -7.7225         -7.7225
v  nu_tilda           4.3246e-007       0.0042695        0.001108        0.001108
v  TempC                       21          73.069          21.702          21.702
v  TurbVisc           3.0782e-014        0.005032       0.0012973       0.0012973
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1003:        0.21910E+01

===============================================================


 INSTANT    0.100400000E+04   TIME STEP NUMBER            1004
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70125E-02 0.88234E+00
   Friction velocity        uk    :  0.70125E-02 0.88234E+00
   Dimensionless distance   yplus :  0.56456E-01 0.71035E+01
   Friction thermal sca.    tstar : -0.57370E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42122E-01 0.53000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76968E-02      32   0.36153E-03   0.18428E+01 0.91299E+02 
c  Velocity[X]                                      0.10460E+01 
c  Velocity[Y]                                      0.79682E+00 
c  Velocity[Z]                                      0.11942E-29 
c  Pressure     0.99507E-07     490   0.97399E-08   0.10284E+00 0.74081E+03 
c  nu_tilda     0.51112E-05      31   0.15021E-04   0.18770E-06 0.12735E+03 
c  TempC        0.31288E+02      26   0.44187E-03   0.64724E+01 0.28267E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3911          10.433          4.5729          4.5729
v  Velocity[Y]            -3.4739            7.05        0.002756        0.002756
v  Velocity[Z]        -1.061e-014     2.0552e-014    -9.1616e-018    -9.1616e-018
v  ǁVelocityǁ         0.0015149          10.434          5.2399          5.2399
v  Pressure               -54.426          20.256         -7.7657         -7.7657
v  nu_tilda           4.3241e-007       0.0042695       0.0011086       0.0011086
v  TempC                       21          73.069          21.702          21.702
v  TurbVisc           3.0772e-014        0.005032       0.0012981       0.0012981
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1004:        0.22180E+01

===============================================================


 INSTANT    0.100500000E+04   TIME STEP NUMBER            1005
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69421E-02 0.88158E+00
   Friction velocity        uk    :  0.69421E-02 0.88158E+00
   Dimensionless distance   yplus :  0.55889E-01 0.70973E+01
   Friction thermal sca.    tstar : -0.57861E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41699E-01 0.52954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77000E-02      32   0.34663E-03   0.18517E+01 0.91311E+02 
c  Velocity[X]                                      0.10670E+01 
c  Velocity[Y]                                      0.78474E+00 
c  Velocity[Z]                                      0.12476E-29 
c  Pressure     0.12398E-06     457   0.91664E-08   0.12438E+00 0.71705E+03 
c  nu_tilda     0.51128E-05      31   0.72479E-05   0.18781E-06 0.12737E+03 
c  TempC        0.31299E+02      27   0.35581E-03   0.52054E+01 0.23345E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3895          10.434          4.5729          4.5729
v  Velocity[Y]            -3.4732          7.0767       0.0027312       0.0027312
v  Velocity[Z]       -1.0343e-014      2.107e-014    -9.1338e-018    -9.1338e-018
v  ǁVelocityǁ        0.00089794          10.435          5.2401          5.2401
v  Pressure               -54.403           20.38         -7.7357         -7.7357
v  nu_tilda           4.3239e-007       0.0042695       0.0011092       0.0011092
v  TempC                       21          73.722          21.703          21.703
v  TurbVisc           3.0758e-014        0.005032       0.0012988       0.0012988
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1005:        0.21450E+01

===============================================================


 INSTANT    0.100600000E+04   TIME STEP NUMBER            1006
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53841E-02 0.88294E+00
   Friction velocity        uk    :  0.53841E-02 0.88294E+00
   Dimensionless distance   yplus :  0.43345E-01 0.71083E+01
   Friction thermal sca.    tstar : -0.57042E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32341E-01 0.53036E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77033E-02      32   0.33542E-03   0.18230E+01 0.91034E+02 
c  Velocity[X]                                      0.10462E+01 
c  Velocity[Y]                                      0.77679E+00 
c  Velocity[Z]                                      0.16891E-29 
c  Pressure     0.97419E-07     456   0.95038E-08   0.98729E-01 0.40169E+03 
c  nu_tilda     0.51144E-05      31   0.15044E-04   0.18791E-06 0.12738E+03 
c  TempC        0.31311E+02      27   0.43494E-03   0.34443E+01 0.18411E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3876          10.434          4.5729          4.5729
v  Velocity[Y]            -3.4734          7.0805        0.002707        0.002707
v  Velocity[Z]       -1.0005e-014     1.8784e-014    -9.1236e-018    -9.1236e-018
v  ǁVelocityǁ        0.00099514          10.435          5.2403          5.2403
v  Pressure               -54.404          20.336         -7.7651         -7.7651
v  nu_tilda           4.3233e-007       0.0042695       0.0011099       0.0011099
v  TempC                       21          73.069          21.703          21.703
v  TurbVisc           3.0751e-014        0.005032       0.0012996       0.0012996
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1006:        0.21440E+01

===============================================================


 INSTANT    0.100700000E+04   TIME STEP NUMBER            1007
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10177E-01 0.88250E+00
   Friction velocity        uk    :  0.10177E-01 0.88250E+00
   Dimensionless distance   yplus :  0.81931E-01 0.71047E+01
   Friction thermal sca.    tstar : -0.56943E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61130E-01 0.53009E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77065E-02      32   0.30378E-03   0.18550E+01 0.91429E+02 
c  Velocity[X]                                      0.10545E+01 
c  Velocity[Y]                                      0.80058E+00 
c  Velocity[Z]                                      0.12437E-29 
c  Pressure     0.95622E-07     421   0.91763E-08   0.98791E-01 0.30553E+03 
c  nu_tilda     0.51160E-05      31   0.72462E-05   0.18800E-06 0.12740E+03 
c  TempC        0.31322E+02      27   0.38784E-03   0.51132E+01 0.21610E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3858          10.434          4.5729          4.5729
v  Velocity[Y]            -3.4732          7.0537       0.0026826       0.0026826
v  Velocity[Z]       -1.0008e-014     2.0293e-014    -9.0927e-018    -9.0927e-018
v  ǁVelocityǁ        0.00085036          10.435          5.2405          5.2405
v  Pressure               -54.382          20.257         -7.7801         -7.7801
v  nu_tilda           4.3237e-007       0.0042695       0.0011105       0.0011105
v  TempC                       21           73.07          21.703          21.703
v  TurbVisc           3.0736e-014        0.005032       0.0013004       0.0013004
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1007:        0.20470E+01

===============================================================


 INSTANT    0.100800000E+04   TIME STEP NUMBER            1008
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71572E-02 0.88131E+00
   Friction velocity        uk    :  0.71572E-02 0.88131E+00
   Dimensionless distance   yplus :  0.57620E-01 0.70951E+01
   Friction thermal sca.    tstar : -0.58328E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42991E-01 0.52938E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77098E-02      32   0.30857E-03   0.18339E+01 0.91233E+02 
c  Velocity[X]                                      0.10473E+01 
c  Velocity[Y]                                      0.78658E+00 
c  Velocity[Z]                                      0.10522E-29 
c  Pressure     0.99397E-07     410   0.96824E-08   0.10162E+00 0.30586E+03 
c  nu_tilda     0.51176E-05      31   0.15041E-04   0.18811E-06 0.12741E+03 
c  TempC        0.31333E+02      26   0.37988E-03   0.45069E+01 0.21309E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3841          10.435          4.5729          4.5729
v  Velocity[Y]            -3.4725          7.0736        0.002659        0.002659
v  Velocity[Z]       -9.8182e-015     2.0538e-014    -9.0638e-018    -9.0638e-018
v  ǁVelocityǁ         0.0008889          10.436          5.2407          5.2407
v  Pressure               -54.377          20.346         -7.7751         -7.7751
v  nu_tilda           4.3241e-007       0.0042695       0.0011111       0.0011111
v  TempC                       21           73.74          21.704          21.704
v  TurbVisc           3.0745e-014        0.005032       0.0013011       0.0013011
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1008:        0.20380E+01

===============================================================


 INSTANT    0.100900000E+04   TIME STEP NUMBER            1009
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50806E-02 0.88219E+00
   Friction velocity        uk    :  0.50806E-02 0.88219E+00
   Dimensionless distance   yplus :  0.40902E-01 0.71022E+01
   Friction thermal sca.    tstar : -0.57040E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30518E-01 0.52990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77130E-02      32   0.38474E-03   0.18498E+01 0.91307E+02 
c  Velocity[X]                                      0.10708E+01 
c  Velocity[Y]                                      0.77900E+00 
c  Velocity[Z]                                      0.14962E-29 
c  Pressure     0.14126E-06     441   0.99410E-08   0.14296E+00 0.45000E+03 
c  nu_tilda     0.51192E-05      31   0.72497E-05   0.18820E-06 0.12742E+03 
c  TempC        0.31344E+02      27   0.41492E-03   0.57045E+01 0.23207E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3822          10.435          4.5729          4.5729
v  Velocity[Y]            -3.4719          7.0513       0.0026353       0.0026353
v  Velocity[Z]       -9.6342e-015     2.0142e-014    -9.0415e-018    -9.0415e-018
v  ǁVelocityǁ         0.0015213          10.436          5.2409          5.2409
v  Pressure               -54.357          20.229         -7.8011         -7.8011
v  nu_tilda           4.3246e-007       0.0042695       0.0011118       0.0011118
v  TempC                       21          73.069          21.704          21.704
v  TurbVisc           3.0757e-014        0.005032       0.0013019       0.0013019
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1009:        0.21140E+01

===============================================================


 INSTANT    0.101000000E+04   TIME STEP NUMBER            1010
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12481E-01 0.88169E+00
   Friction velocity        uk    :  0.12481E-01 0.88169E+00
   Dimensionless distance   yplus :  0.10048E+00 0.70982E+01
   Friction thermal sca.    tstar : -0.58065E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74970E-01 0.52961E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77162E-02      32   0.31240E-03   0.18777E+01 0.91692E+02 
c  Velocity[X]                                      0.10804E+01 
c  Velocity[Y]                                      0.79721E+00 
c  Velocity[Z]                                      0.10839E-29 
c  Pressure     0.12983E-06     425   0.91361E-08   0.13166E+00 0.31501E+03 
c  nu_tilda     0.51208E-05      31   0.15046E-04   0.18831E-06 0.12744E+03 
c  TempC        0.31355E+02      26   0.39869E-03   0.57783E+01 0.24272E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3807          10.435          4.5729          4.5729
v  Velocity[Y]            -3.4729          7.0726       0.0026117       0.0026117
v  Velocity[Z]       -9.4642e-015     2.0044e-014    -9.0106e-018    -9.0106e-018
v  ǁVelocityǁ        0.00095247          10.436          5.2411          5.2411
v  Pressure               -54.353           20.32         -7.7959         -7.7959
v  nu_tilda           4.3247e-007       0.0042695       0.0011124       0.0011124
v  TempC                       21          73.111          21.704          21.704
v  TurbVisc           3.0771e-014        0.005032       0.0013026       0.0013026
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1010:        0.20390E+01

===============================================================


 INSTANT    0.101100000E+04   TIME STEP NUMBER            1011
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70430E-02 0.88309E+00
   Friction velocity        uk    :  0.70430E-02 0.88309E+00
   Dimensionless distance   yplus :  0.56701E-01 0.71094E+01
   Friction thermal sca.    tstar : -0.57463E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42305E-01 0.53044E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77195E-02      32   0.29464E-03   0.18224E+01 0.91235E+02 
c  Velocity[X]                                      0.10335E+01 
c  Velocity[Y]                                      0.78890E+00 
c  Velocity[Z]                                      0.11247E-29 
c  Pressure     0.87252E-07     409   0.96108E-08   0.88779E-01 0.28956E+03 
c  nu_tilda     0.51225E-05      31   0.72297E-05   0.18842E-06 0.12746E+03 
c  TempC        0.31366E+02      26   0.36010E-03   0.44232E+01 0.21716E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.379          10.435          4.5729          4.5729
v  Velocity[Y]            -3.4718          7.0831       0.0025886       0.0025886
v  Velocity[Z]       -9.3956e-015     2.0039e-014    -8.9868e-018    -8.9868e-018
v  ǁVelocityǁ         0.0010741          10.436          5.2413          5.2413
v  Pressure               -54.335          20.352         -7.7926         -7.7926
v  nu_tilda           4.3242e-007       0.0042695       0.0011131       0.0011131
v  TempC                       21          73.436          21.705          21.705
v  TurbVisc           3.0775e-014        0.005032       0.0013034       0.0013034
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1011:        0.19860E+01

===============================================================


 INSTANT    0.101200000E+04   TIME STEP NUMBER            1012
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89249E-02 0.88259E+00
   Friction velocity        uk    :  0.89249E-02 0.88259E+00
   Dimensionless distance   yplus :  0.71851E-01 0.71055E+01
   Friction thermal sca.    tstar : -0.57163E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53609E-01 0.53015E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77227E-02      32   0.34190E-03   0.18295E+01 0.91261E+02 
c  Velocity[X]                                      0.10498E+01 
c  Velocity[Y]                                      0.77970E+00 
c  Velocity[Z]                                      0.14283E-29 
c  Pressure     0.10266E-06     472   0.99854E-08   0.10579E+00 0.81449E+03 
c  nu_tilda     0.51241E-05      31   0.15068E-04   0.18853E-06 0.12747E+03 
c  TempC        0.31377E+02      26   0.47713E-03   0.62668E+01 0.24466E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3773          10.436          4.5729          4.5729
v  Velocity[Y]            -3.4711          7.0593       0.0025657       0.0025657
v  Velocity[Z]       -9.3883e-015      2.061e-014    -8.9585e-018    -8.9585e-018
v  ǁVelocityǁ         0.0013275          10.437          5.2415          5.2415
v  Pressure               -54.328          20.191         -7.8392         -7.8392
v  nu_tilda           4.3242e-007       0.0042695       0.0011137       0.0011137
v  TempC                       21          73.069          21.705          21.705
v  TurbVisc           3.0759e-014        0.005032       0.0013042       0.0013042
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1012:        0.21810E+01

===============================================================


 INSTANT    0.101300000E+04   TIME STEP NUMBER            1013
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11185E-01 0.88150E+00
   Friction velocity        uk    :  0.11185E-01 0.88150E+00
   Dimensionless distance   yplus :  0.90045E-01 0.70967E+01
   Friction thermal sca.    tstar : -0.58220E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67183E-01 0.52949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77260E-02      32   0.31026E-03   0.18534E+01 0.91531E+02 
c  Velocity[X]                                      0.10516E+01 
c  Velocity[Y]                                      0.80175E+00 
c  Velocity[Z]                                      0.13531E-29 
c  Pressure     0.11401E-06     469   0.96062E-08   0.11429E+00 0.64497E+03 
c  nu_tilda     0.51257E-05      31   0.72344E-05   0.18863E-06 0.12749E+03 
c  TempC        0.31389E+02      26   0.45759E-03   0.65095E+01 0.28113E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3756          10.436          4.5729          4.5729
v  Velocity[Y]            -3.4716          7.0747       0.0025429       0.0025429
v  Velocity[Z]       -9.3761e-015      2.119e-014    -8.9314e-018    -8.9314e-018
v  ǁVelocityǁ        0.00086275          10.437          5.2417          5.2417
v  Pressure               -54.311          20.313         -7.8158         -7.8158
v  nu_tilda           4.3243e-007       0.0042695       0.0011144       0.0011144
v  TempC                       21          73.461          21.705          21.705
v  TurbVisc           3.0761e-014        0.005032       0.0013049       0.0013049
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1013:        0.23620E+01

===============================================================


 INSTANT    0.101400000E+04   TIME STEP NUMBER            1014
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19905E-02 0.88249E+00
   Friction velocity        uk    :  0.19905E-02 0.88249E+00
   Dimensionless distance   yplus :  0.16025E-01 0.71047E+01
   Friction thermal sca.    tstar : -0.57157E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11957E-01 0.53009E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77292E-02      32   0.36021E-03   0.18350E+01 0.91397E+02 
c  Velocity[X]                                      0.10467E+01 
c  Velocity[Y]                                      0.78838E+00 
c  Velocity[Z]                                      0.11757E-29 
c  Pressure     0.84016E-07     473   0.93463E-08   0.86252E-01 0.69272E+03 
c  nu_tilda     0.51273E-05      31   0.15063E-04   0.18874E-06 0.12751E+03 
c  TempC        0.31400E+02      26   0.36676E-03   0.52272E+01 0.24108E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3738          10.436          4.5729          4.5729
v  Velocity[Y]            -3.4712           7.053       0.0025204       0.0025204
v  Velocity[Z]       -9.3377e-015     2.2054e-014    -8.9055e-018    -8.9055e-018
v  ǁVelocityǁ         0.0013768          10.437          5.2419          5.2419
v  Pressure               -54.303          20.184         -7.8568         -7.8568
v  nu_tilda           4.3245e-007       0.0042695        0.001115        0.001115
v  TempC                       21           73.07          21.706          21.706
v  TurbVisc           3.0764e-014        0.005032       0.0013057       0.0013057
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1014:        0.24580E+01

===============================================================


 INSTANT    0.101500000E+04   TIME STEP NUMBER            1015
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11562E-01 0.88188E+00
   Friction velocity        uk    :  0.11562E-01 0.88188E+00
   Dimensionless distance   yplus :  0.93079E-01 0.70997E+01
   Friction thermal sca.    tstar : -0.58361E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69447E-01 0.52972E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77324E-02      32   0.35082E-03   0.18671E+01 0.91689E+02 
c  Velocity[X]                                      0.10833E+01 
c  Velocity[Y]                                      0.78384E+00 
c  Velocity[Z]                                      0.14219E-29 
c  Pressure     0.13386E-06     488   0.94220E-08   0.13545E+00 0.73421E+03 
c  nu_tilda     0.51289E-05      31   0.72246E-05   0.18884E-06 0.12752E+03 
c  TempC        0.31411E+02      26   0.45389E-03   0.37659E+01 0.19554E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3722          10.436          4.5729          4.5729
v  Velocity[Y]            -3.4701          7.0803       0.0024979       0.0024979
v  Velocity[Z]        -9.113e-015     2.2433e-014    -8.8828e-018    -8.8828e-018
v  ǁVelocityǁ        0.00057956          10.437          5.2421          5.2421
v  Pressure               -54.279          20.316         -7.8257         -7.8257
v  nu_tilda           4.3246e-007       0.0042695       0.0011156       0.0011156
v  TempC                       21          73.436          21.706          21.706
v  TurbVisc           3.0769e-014        0.005032       0.0013065       0.0013065
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1015:        0.21920E+01

===============================================================


 INSTANT    0.101600000E+04   TIME STEP NUMBER            1016
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12983E-02 0.88317E+00
   Friction velocity        uk    :  0.12983E-02 0.88317E+00
   Dimensionless distance   yplus :  0.10452E-01 0.71102E+01
   Friction thermal sca.    tstar : -0.57930E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77984E-02 0.53050E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77357E-02      32   0.31566E-03   0.18664E+01 0.91709E+02 
c  Velocity[X]                                      0.10618E+01 
c  Velocity[Y]                                      0.80458E+00 
c  Velocity[Z]                                      0.11939E-29 
c  Pressure     0.12389E-06     457   0.93889E-08   0.12429E+00 0.43953E+03 
c  nu_tilda     0.51305E-05      31   0.15066E-04   0.18894E-06 0.12754E+03 
c  TempC        0.31422E+02      26   0.42270E-03   0.46433E+01 0.21352E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3703          10.437          4.5729          4.5729
v  Velocity[Y]             -3.471          7.0814        0.002476        0.002476
v  Velocity[Z]       -8.8748e-015     2.1151e-014    -8.8681e-018    -8.8681e-018
v  ǁVelocityǁ        0.00088176          10.438          5.2423          5.2423
v  Pressure                -54.28          20.261         -7.8572         -7.8572
v  nu_tilda           4.3244e-007       0.0042695       0.0011163       0.0011163
v  TempC                       21          73.092          21.706          21.706
v  TurbVisc           3.0771e-014        0.005032       0.0013072       0.0013072
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1016:        0.21390E+01

===============================================================


 INSTANT    0.101700000E+04   TIME STEP NUMBER            1017
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75022E-02 0.88295E+00
   Friction velocity        uk    :  0.75022E-02 0.88295E+00
   Dimensionless distance   yplus :  0.60398E-01 0.71083E+01
   Friction thermal sca.    tstar : -0.57469E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45064E-01 0.53036E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77389E-02      32   0.28953E-03   0.18519E+01 0.91583E+02 
c  Velocity[X]                                      0.10601E+01 
c  Velocity[Y]                                      0.79176E+00 
c  Velocity[Z]                                      0.13204E-29 
c  Pressure     0.97442E-07     409   0.94580E-08   0.10084E+00 0.25892E+03 
c  nu_tilda     0.51321E-05      31   0.72017E-05   0.18905E-06 0.12755E+03 
c  TempC        0.31433E+02      26   0.39751E-03   0.38891E+01 0.18774E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3687          10.437          4.5729          4.5729
v  Velocity[Y]            -3.4701          7.0574        0.002454        0.002454
v  Velocity[Z]       -8.7306e-015     2.3231e-014    -8.8395e-018    -8.8395e-018
v  ǁVelocityǁ         0.0014849          10.438          5.2425          5.2425
v  Pressure               -54.257          20.202         -7.8682         -7.8682
v  nu_tilda           4.3246e-007       0.0042695       0.0011169       0.0011169
v  TempC                       21           73.07          21.707          21.707
v  TurbVisc           3.0766e-014        0.005032        0.001308        0.001308
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1017:        0.20100E+01

===============================================================


 INSTANT    0.101800000E+04   TIME STEP NUMBER            1018
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12252E-01 0.88161E+00
   Friction velocity        uk    :  0.12252E-01 0.88161E+00
   Dimensionless distance   yplus :  0.98639E-01 0.70975E+01
   Friction thermal sca.    tstar : -0.57984E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73596E-01 0.52956E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77421E-02      32   0.36433E-03   0.18288E+01 0.91441E+02 
c  Velocity[X]                                      0.10451E+01 
c  Velocity[Y]                                      0.78372E+00 
c  Velocity[Z]                                      0.14790E-29 
c  Pressure     0.10009E-06     393   0.90515E-08   0.10100E+00 0.21882E+03 
c  nu_tilda     0.51337E-05      31   0.15093E-04   0.18916E-06 0.12757E+03 
c  TempC        0.31444E+02      26   0.36235E-03   0.40777E+01 0.18770E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3672          10.437          4.5729          4.5729
v  Velocity[Y]            -3.4703           7.078       0.0024324       0.0024324
v  Velocity[Z]        -8.559e-015     2.2296e-014     -8.817e-018     -8.817e-018
v  ǁVelocityǁ        0.00087786          10.438          5.2427          5.2427
v  Pressure               -54.251          20.262         -7.8688         -7.8688
v  nu_tilda           4.3243e-007       0.0042695       0.0011175       0.0011175
v  TempC                       21          74.135          21.707          21.707
v  TurbVisc           3.0771e-014        0.005032       0.0013087       0.0013087
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1018:        0.19870E+01

===============================================================


 INSTANT    0.101900000E+04   TIME STEP NUMBER            1019
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46884E-02 0.88273E+00
   Friction velocity        uk    :  0.46884E-02 0.88273E+00
   Dimensionless distance   yplus :  0.37745E-01 0.71066E+01
   Friction thermal sca.    tstar : -0.57658E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28162E-01 0.53023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77453E-02      32   0.33656E-03   0.18778E+01 0.91952E+02 
c  Velocity[X]                                      0.10692E+01 
c  Velocity[Y]                                      0.80852E+00 
c  Velocity[Z]                                      0.12431E-29 
c  Pressure     0.12538E-06     441   0.99626E-08   0.12781E+00 0.33099E+03 
c  nu_tilda     0.51354E-05      31   0.71992E-05   0.18925E-06 0.12758E+03 
c  TempC        0.31455E+02      26   0.50359E-03   0.48510E+01 0.21887E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3656          10.437          4.5729          4.5729
v  Velocity[Y]            -3.4713          7.0594       0.0024111       0.0024111
v  Velocity[Z]       -8.3926e-015     2.2055e-014    -8.7946e-018    -8.7946e-018
v  ǁVelocityǁ           0.00122          10.438          5.2429          5.2429
v  Pressure                -54.23          20.179         -7.8873         -7.8873
v  nu_tilda           4.3247e-007       0.0042695       0.0011182       0.0011182
v  TempC                       21          73.258          21.707          21.707
v  TurbVisc           3.0763e-014        0.005032       0.0013095       0.0013095
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1019:        0.21080E+01

===============================================================


 INSTANT    0.102000000E+04   TIME STEP NUMBER            1020
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10387E-01 0.88215E+00
   Friction velocity        uk    :  0.10387E-01 0.88215E+00
   Dimensionless distance   yplus :  0.83623E-01 0.71019E+01
   Friction thermal sca.    tstar : -0.58785E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62392E-01 0.52988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77485E-02      32   0.28619E-03   0.18565E+01 0.91671E+02 
c  Velocity[X]                                      0.10626E+01 
c  Velocity[Y]                                      0.79388E+00 
c  Velocity[Z]                                      0.11516E-29 
c  Pressure     0.11001E-06     393   0.90060E-08   0.11035E+00 0.23956E+03 
c  nu_tilda     0.51370E-05      31   0.15086E-04   0.18937E-06 0.12760E+03 
c  TempC        0.31466E+02      27   0.36928E-03   0.65923E+01 0.27833E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3639          10.438          4.5729          4.5729
v  Velocity[Y]            -3.4717          7.0782       0.0023899       0.0023899
v  Velocity[Z]       -8.2472e-015     2.1704e-014    -8.7728e-018    -8.7728e-018
v  ǁVelocityǁ         0.0011773          10.438          5.2431          5.2431
v  Pressure               -54.227          20.251         -7.8877         -7.8877
v  nu_tilda           4.3251e-007       0.0042695       0.0011188       0.0011188
v  TempC                       21          73.069          21.708          21.708
v  TurbVisc           3.0774e-014        0.005032       0.0013103       0.0013103
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1020:        0.19850E+01

===============================================================


 INSTANT    0.102100000E+04   TIME STEP NUMBER            1021
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99922E-02 0.88330E+00
   Friction velocity        uk    :  0.99922E-02 0.88330E+00
   Dimensionless distance   yplus :  0.80444E-01 0.71111E+01
   Friction thermal sca.    tstar : -0.57745E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60021E-01 0.53057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77517E-02      32   0.33504E-03   0.18125E+01 0.91362E+02 
c  Velocity[X]                                      0.10263E+01 
c  Velocity[Y]                                      0.78618E+00 
c  Velocity[Z]                                      0.16770E-29 
c  Pressure     0.84631E-07     362   0.91498E-08   0.85899E-01 0.24273E+03 
c  nu_tilda     0.51386E-05      31   0.72009E-05   0.18947E-06 0.12762E+03 
c  TempC        0.31477E+02      27   0.29110E-03   0.45630E+01 0.21844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3622          10.438          4.5729          4.5729
v  Velocity[Y]            -3.4722           7.087       0.0023689       0.0023689
v  Velocity[Z]       -8.1658e-015     2.1929e-014    -8.7499e-018    -8.7499e-018
v  ǁVelocityǁ        0.00089171          10.439          5.2433          5.2433
v  Pressure               -54.206          20.263         -7.8875         -7.8875
v  nu_tilda           4.3244e-007       0.0042695       0.0011195       0.0011195
v  TempC                       21          73.217          21.708          21.708
v  TurbVisc           3.0787e-014        0.005032        0.001311        0.001311
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1021:        0.19240E+01

===============================================================


 INSTANT    0.102200000E+04   TIME STEP NUMBER            1022
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55189E-02 0.88288E+00
   Friction velocity        uk    :  0.55189E-02 0.88288E+00
   Dimensionless distance   yplus :  0.44431E-01 0.71077E+01
   Friction thermal sca.    tstar : -0.57232E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33150E-01 0.53032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77550E-02      32   0.31834E-03   0.18608E+01 0.91891E+02 
c  Velocity[X]                                      0.10550E+01 
c  Velocity[Y]                                      0.80581E+00 
c  Velocity[Z]                                      0.12355E-29 
c  Pressure     0.11550E-06     457   0.97890E-08   0.11991E+00 0.64351E+03 
c  nu_tilda     0.51402E-05      31   0.15093E-04   0.18959E-06 0.12764E+03 
c  TempC        0.31488E+02      26   0.47396E-03   0.44604E+01 0.21075E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3605          10.438          4.5729          4.5729
v  Velocity[Y]            -3.4735          7.0613       0.0023481       0.0023481
v  Velocity[Z]       -8.1046e-015     2.2368e-014    -8.7254e-018    -8.7254e-018
v  ǁVelocityǁ         0.0015423          10.439          5.2435          5.2435
v  Pressure               -54.199          20.145         -7.9258         -7.9258
v  nu_tilda           4.3239e-007       0.0042695       0.0011201       0.0011201
v  TempC                       21          73.283          21.709          21.709
v  TurbVisc           3.0765e-014        0.005032       0.0013118       0.0013118
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1022:        0.21470E+01

===============================================================


 INSTANT    0.102300000E+04   TIME STEP NUMBER            1023
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98753E-02 0.88152E+00
   Friction velocity        uk    :  0.98753E-02 0.88152E+00
   Dimensionless distance   yplus :  0.79503E-01 0.70968E+01
   Friction thermal sca.    tstar : -0.58313E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59318E-01 0.52950E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77582E-02      32   0.35095E-03   0.18354E+01 0.91639E+02 
c  Velocity[X]                                      0.10413E+01 
c  Velocity[Y]                                      0.79408E+00 
c  Velocity[Z]                                      0.11817E-29 
c  Pressure     0.96958E-07     456   0.96032E-08   0.97727E-01 0.64633E+03 
c  nu_tilda     0.51418E-05      31   0.71791E-05   0.18971E-06 0.12766E+03 
c  TempC        0.31500E+02      26   0.39013E-03   0.61001E+01 0.27432E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3588          10.438          4.5729          4.5729
v  Velocity[Y]            -3.4722          7.0845       0.0023276       0.0023276
v  Velocity[Z]       -8.0254e-015     2.3834e-014    -8.7103e-018    -8.7103e-018
v  ǁVelocityǁ        0.00081192          10.439          5.2437          5.2437
v  Pressure               -54.178          20.257         -7.9001         -7.9001
v  nu_tilda           4.3238e-007       0.0042695       0.0011208       0.0011208
v  TempC                       21          73.699          21.709          21.709
v  TurbVisc           3.0751e-014        0.005032       0.0013125       0.0013125
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1023:        0.21360E+01

===============================================================


 INSTANT    0.102400000E+04   TIME STEP NUMBER            1024
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70222E-02 0.88266E+00
   Friction velocity        uk    :  0.70222E-02 0.88266E+00
   Dimensionless distance   yplus :  0.56533E-01 0.71060E+01
   Friction thermal sca.    tstar : -0.57728E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42180E-01 0.53019E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77614E-02      32   0.34177E-03   0.18623E+01 0.91839E+02 
c  Velocity[X]                                      0.10730E+01 
c  Velocity[Y]                                      0.78931E+00 
c  Velocity[Z]                                      0.14919E-29 
c  Pressure     0.12878E-06     490   0.91890E-08   0.13019E+00 0.89094E+03 
c  nu_tilda     0.51434E-05      31   0.15113E-04   0.18982E-06 0.12768E+03 
c  TempC        0.31511E+02      26   0.30699E-03   0.44794E+01 0.22151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3571          10.438          4.5729          4.5729
v  Velocity[Y]             -3.473          7.0577       0.0023071       0.0023071
v  Velocity[Z]       -7.9439e-015     2.3052e-014    -8.6971e-018    -8.6971e-018
v  ǁVelocityǁ        0.00052963          10.439          5.2439          5.2439
v  Pressure               -54.172          20.086         -7.9517         -7.9517
v  nu_tilda           4.3243e-007       0.0042695       0.0011214       0.0011214
v  TempC                       21          73.069          21.709          21.709
v  TurbVisc            3.075e-014        0.005032       0.0013133       0.0013133
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1024:        0.22360E+01

===============================================================


 INSTANT    0.102500000E+04   TIME STEP NUMBER            1025
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38331E-02 0.88224E+00
   Friction velocity        uk    :  0.38331E-02 0.88224E+00
   Dimensionless distance   yplus :  0.30859E-01 0.71026E+01
   Friction thermal sca.    tstar : -0.58797E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23025E-01 0.52993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77646E-02      32   0.30698E-03   0.18648E+01 0.91973E+02 
c  Velocity[X]                                      0.10532E+01 
c  Velocity[Y]                                      0.81162E+00 
c  Velocity[Z]                                      0.10677E-29 
c  Pressure     0.12679E-06     474   0.95220E-08   0.12924E+00 0.83924E+03 
c  nu_tilda     0.51451E-05      31   0.71666E-05   0.18992E-06 0.12769E+03 
c  TempC        0.31522E+02      26   0.43429E-03   0.33141E+01 0.17725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3557          10.438          4.5729          4.5729
v  Velocity[Y]            -3.4732          7.0818       0.0022869       0.0022869
v  Velocity[Z]       -7.8168e-015      2.281e-014    -8.6812e-018    -8.6812e-018
v  ǁVelocityǁ         0.0013362          10.439           5.244           5.244
v  Pressure               -54.153          20.256         -7.9186         -7.9186
v  nu_tilda           4.3245e-007       0.0042695        0.001122        0.001122
v  TempC                       21          73.351           21.71           21.71
v  TurbVisc           3.0764e-014        0.005032       0.0013141       0.0013141
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1025:        0.21850E+01

===============================================================


 INSTANT    0.102600000E+04   TIME STEP NUMBER            1026
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11279E-01 0.88340E+00
   Friction velocity        uk    :  0.11279E-01 0.88340E+00
   Dimensionless distance   yplus :  0.90806E-01 0.71120E+01
   Friction thermal sca.    tstar : -0.57432E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67751E-01 0.53063E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77678E-02      32   0.29633E-03   0.18396E+01 0.91825E+02 
c  Velocity[X]                                      0.10413E+01 
c  Velocity[Y]                                      0.79821E+00 
c  Velocity[Z]                                      0.10190E-29 
c  Pressure     0.10025E-06     442   0.98434E-08   0.10219E+00 0.39860E+03 
c  nu_tilda     0.51467E-05      31   0.15106E-04   0.19003E-06 0.12771E+03 
c  TempC        0.31533E+02      28   0.33316E-03   0.47277E+01 0.20971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.354          10.439          4.5729          4.5729
v  Velocity[Y]            -3.4734          7.0913       0.0022671       0.0022671
v  Velocity[Z]       -7.7211e-015     2.3429e-014    -8.6649e-018    -8.6649e-018
v  ǁVelocityǁ        0.00085583          10.439          5.2442          5.2442
v  Pressure               -54.152          20.205         -7.9461         -7.9461
v  nu_tilda           4.3245e-007       0.0042695       0.0011227       0.0011227
v  TempC                       21          73.326           21.71           21.71
v  TurbVisc            3.077e-014        0.005032       0.0013148       0.0013148
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1026:        0.21570E+01

===============================================================


 INSTANT    0.102700000E+04   TIME STEP NUMBER            1027
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19742E-02 0.88302E+00
   Friction velocity        uk    :  0.19742E-02 0.88302E+00
   Dimensionless distance   yplus :  0.15894E-01 0.71089E+01
   Friction thermal sca.    tstar : -0.57494E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11859E-01 0.53040E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77710E-02      32   0.35999E-03   0.18553E+01 0.91830E+02 
c  Velocity[X]                                      0.10649E+01 
c  Velocity[Y]                                      0.79042E+00 
c  Velocity[Z]                                      0.16238E-29 
c  Pressure     0.13488E-06     410   0.91357E-08   0.13650E+00 0.34189E+03 
c  nu_tilda     0.51483E-05      31   0.71766E-05   0.19013E-06 0.12773E+03 
c  TempC        0.31544E+02      27   0.27464E-03   0.36117E+01 0.17684E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3525          10.439          4.5729          4.5729
v  Velocity[Y]            -3.4736          7.0632       0.0022472       0.0022472
v  Velocity[Z]       -7.6116e-015     2.3525e-014    -8.6515e-018    -8.6515e-018
v  ǁVelocityǁ         0.0013556           10.44          5.2444          5.2444
v  Pressure               -54.124          20.115         -7.9591         -7.9591
v  nu_tilda            4.325e-007       0.0042695       0.0011233       0.0011233
v  TempC                       21          73.069           21.71           21.71
v  TurbVisc            3.077e-014        0.005032       0.0013156       0.0013156
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1027:        0.20140E+01

===============================================================


 INSTANT    0.102800000E+04   TIME STEP NUMBER            1028
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55281E-02 0.88190E+00
   Friction velocity        uk    :  0.55281E-02 0.88190E+00
   Dimensionless distance   yplus :  0.44505E-01 0.70999E+01
   Friction thermal sca.    tstar : -0.58789E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33206E-01 0.52973E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77742E-02      32   0.30849E-03   0.18821E+01 0.92193E+02 
c  Velocity[X]                                      0.10734E+01 
c  Velocity[Y]                                      0.80869E+00 
c  Velocity[Z]                                      0.12005E-29 
c  Pressure     0.11936E-06     345   0.99014E-08   0.12141E+00 0.22544E+03 
c  nu_tilda     0.51499E-05      31   0.15119E-04   0.19025E-06 0.12774E+03 
c  TempC        0.31555E+02      26   0.48309E-03   0.41698E+01 0.19580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3508          10.439          4.5729          4.5729
v  Velocity[Y]            -3.4726          7.0809       0.0022276       0.0022276
v  Velocity[Z]       -7.5196e-015     2.3235e-014    -8.6344e-018    -8.6344e-018
v  ǁVelocityǁ        0.00010787           10.44          5.2446          5.2446
v  Pressure               -54.123          20.187         -7.9626         -7.9626
v  nu_tilda           4.3253e-007       0.0042695       0.0011239       0.0011239
v  TempC                       21          73.749          21.711          21.711
v  TurbVisc           3.0784e-014        0.005032       0.0013163       0.0013163
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1028:        0.18500E+01

===============================================================


 INSTANT    0.102900000E+04   TIME STEP NUMBER            1029
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87269E-02 0.88301E+00
   Friction velocity        uk    :  0.87269E-02 0.88301E+00
   Dimensionless distance   yplus :  0.70258E-01 0.71088E+01
   Friction thermal sca.    tstar : -0.57845E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52420E-01 0.53040E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77774E-02      32   0.31173E-03   0.18543E+01 0.91918E+02 
c  Velocity[X]                                      0.10531E+01 
c  Velocity[Y]                                      0.80114E+00 
c  Velocity[Z]                                      0.11261E-29 
c  Pressure     0.12282E-06     330   0.98765E-08   0.12669E+00 0.24258E+03 
c  nu_tilda     0.51515E-05      31   0.71535E-05   0.19036E-06 0.12776E+03 
c  TempC        0.31566E+02      26   0.38834E-03   0.72200E+01 0.27144E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3492           10.44          4.5729          4.5729
v  Velocity[Y]            -3.4738           7.063       0.0022083       0.0022083
v  Velocity[Z]       -7.3685e-015     2.3623e-014    -8.6267e-018    -8.6267e-018
v  ǁVelocityǁ        0.00094859           10.44          5.2448          5.2448
v  Pressure               -54.098          20.145         -7.9681         -7.9681
v  nu_tilda           4.3253e-007       0.0042695       0.0011246       0.0011246
v  TempC                       21          73.388          21.711          21.711
v  TurbVisc           3.0792e-014        0.005032       0.0013171       0.0013171
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1029:        0.18250E+01

===============================================================


 INSTANT    0.103000000E+04   TIME STEP NUMBER            1030
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71860E-02 0.88208E+00
   Friction velocity        uk    :  0.71860E-02 0.88208E+00
   Dimensionless distance   yplus :  0.57852E-01 0.71014E+01
   Friction thermal sca.    tstar : -0.58652E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43164E-01 0.52984E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77806E-02      32   0.35151E-03   0.18442E+01 0.91859E+02 
c  Velocity[X]                                      0.10514E+01 
c  Velocity[Y]                                      0.79276E+00 
c  Velocity[Z]                                      0.14929E-29 
c  Pressure     0.99847E-07     410   0.93447E-08   0.10186E+00 0.18398E+03 
c  nu_tilda     0.51532E-05      31   0.15136E-04   0.19047E-06 0.12778E+03 
c  TempC        0.31577E+02      26   0.39044E-03   0.49018E+01 0.21781E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3475           10.44          4.5729          4.5729
v  Velocity[Y]            -3.4739          7.0881       0.0021892       0.0021892
v  Velocity[Z]       -7.2243e-015     2.2945e-014    -8.6156e-018    -8.6156e-018
v  ǁVelocityǁ         0.0015149          10.441           5.245           5.245
v  Pressure               -54.097          20.169         -7.9827         -7.9827
v  nu_tilda           4.3251e-007       0.0042695       0.0011252       0.0011252
v  TempC                       21          73.069          21.711          21.711
v  TurbVisc           3.0792e-014        0.005032       0.0013179       0.0013179
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1030:        0.19950E+01

===============================================================


 INSTANT    0.103100000E+04   TIME STEP NUMBER            1031
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83819E-02 0.88326E+00
   Friction velocity        uk    :  0.83819E-02 0.88326E+00
   Dimensionless distance   yplus :  0.67480E-01 0.71108E+01
   Friction thermal sca.    tstar : -0.58299E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50348E-01 0.53055E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77837E-02      32   0.36385E-03   0.18761E+01 0.92187E+02 
c  Velocity[X]                                      0.10619E+01 
c  Velocity[Y]                                      0.81425E+00 
c  Velocity[Z]                                      0.12044E-29 
c  Pressure     0.12625E-06     408   0.96983E-08   0.12606E+00 0.31774E+03 
c  nu_tilda     0.51548E-05      31   0.71529E-05   0.19058E-06 0.12780E+03 
c  TempC        0.31588E+02      26   0.40908E-03   0.41748E+01 0.21888E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3458           10.44          4.5729          4.5729
v  Velocity[Y]            -3.4729           7.086       0.0021699       0.0021699
v  Velocity[Z]       -7.1058e-015     2.3399e-014    -8.6021e-018    -8.6021e-018
v  ǁVelocityǁ        0.00088179          10.441          5.2452          5.2452
v  Pressure               -54.075          20.189         -7.9751         -7.9751
v  nu_tilda           4.3249e-007       0.0042695       0.0011259       0.0011259
v  TempC                       21          73.661          21.712          21.712
v  TurbVisc           3.0785e-014        0.005032       0.0013186       0.0013186
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1031:        0.20040E+01

===============================================================


 INSTANT    0.103200000E+04   TIME STEP NUMBER            1032
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52543E-02 0.88288E+00
   Friction velocity        uk    :  0.52543E-02 0.88288E+00
   Dimensionless distance   yplus :  0.42300E-01 0.71078E+01
   Friction thermal sca.    tstar : -0.58025E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31561E-01 0.53032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77869E-02      32   0.32169E-03   0.18971E+01 0.92439E+02 
c  Velocity[X]                                      0.10954E+01 
c  Velocity[Y]                                      0.80176E+00 
c  Velocity[Z]                                      0.12114E-29 
c  Pressure     0.11515E-06     489   0.98327E-08   0.11849E+00 0.71700E+03 
c  nu_tilda     0.51564E-05      31   0.15134E-04   0.19071E-06 0.12782E+03 
c  TempC        0.31599E+02      26   0.40728E-03   0.51205E+01 0.23841E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3443           10.44          4.5729          4.5729
v  Velocity[Y]            -3.4726          7.0612       0.0021513       0.0021513
v  Velocity[Z]       -7.0492e-015     2.3509e-014    -8.5876e-018    -8.5876e-018
v  ǁVelocityǁ        0.00063569          10.441          5.2453          5.2453
v  Pressure               -54.072          20.061         -8.0195         -8.0195
v  nu_tilda           4.3253e-007       0.0042695       0.0011265       0.0011265
v  TempC                       21          73.068          21.712          21.712
v  TurbVisc           3.0779e-014        0.005032       0.0013194       0.0013194
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1032:        0.21860E+01

===============================================================


 INSTANT    0.103300000E+04   TIME STEP NUMBER            1033
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56651E-02 0.88190E+00
   Friction velocity        uk    :  0.56651E-02 0.88190E+00
   Dimensionless distance   yplus :  0.45608E-01 0.70999E+01
   Friction thermal sca.    tstar : -0.58823E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34028E-01 0.52973E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77901E-02      32   0.31630E-03   0.18459E+01 0.91973E+02 
c  Velocity[X]                                      0.10508E+01 
c  Velocity[Y]                                      0.79506E+00 
c  Velocity[Z]                                      0.15994E-29 
c  Pressure     0.90673E-07     473   0.98018E-08   0.91853E-01 0.65239E+03 
c  nu_tilda     0.51580E-05      31   0.71524E-05   0.19082E-06 0.12784E+03 
c  TempC        0.31610E+02      26   0.37461E-03   0.46250E+01 0.23702E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3428          10.441          4.5729          4.5729
v  Velocity[Y]            -3.4738          7.0845       0.0021326       0.0021326
v  Velocity[Z]       -6.9878e-015     2.3851e-014    -8.5749e-018    -8.5749e-018
v  ǁVelocityǁ         0.0012095          10.442          5.2455          5.2455
v  Pressure               -54.049          20.178         -7.9935         -7.9935
v  nu_tilda           4.3252e-007       0.0042695       0.0011271       0.0011271
v  TempC                       21          73.159          21.713          21.713
v  TurbVisc           3.0792e-014        0.005032       0.0013201       0.0013201
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1033:        0.21520E+01

===============================================================


 INSTANT    0.103400000E+04   TIME STEP NUMBER            1034
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10316E-01 0.88308E+00
   Friction velocity        uk    :  0.10316E-01 0.88308E+00
   Dimensionless distance   yplus :  0.83051E-01 0.71094E+01
   Friction thermal sca.    tstar : -0.58008E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61966E-01 0.53044E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77933E-02      32   0.32125E-03   0.18686E+01 0.92130E+02 
c  Velocity[X]                                      0.10617E+01 
c  Velocity[Y]                                      0.80691E+00 
c  Velocity[Z]                                      0.11302E-29 
c  Pressure     0.11594E-06     473   0.93375E-08   0.11861E+00 0.66849E+03 
c  nu_tilda     0.51597E-05      31   0.15137E-04   0.19094E-06 0.12786E+03 
c  TempC        0.31621E+02      26   0.28475E-03   0.44209E+01 0.21748E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3412          10.441          4.5729          4.5729
v  Velocity[Y]            -3.4732          7.0588       0.0021142       0.0021142
v  Velocity[Z]       -7.9053e-015     2.2091e-014    -8.5745e-018    -8.5745e-018
v  ǁVelocityǁ        0.00086923          10.442          5.2457          5.2457
v  Pressure               -54.039          20.053         -8.0316         -8.0316
v  nu_tilda           4.3251e-007       0.0042695       0.0011278       0.0011278
v  TempC                       21          73.068          21.713          21.713
v  TurbVisc            3.079e-014        0.005032       0.0013209       0.0013209
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1034:        0.21480E+01

===============================================================


 INSTANT    0.103500000E+04   TIME STEP NUMBER            1035
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47089E-02 0.88247E+00
   Friction velocity        uk    :  0.47089E-02 0.88247E+00
   Dimensionless distance   yplus :  0.37910E-01 0.71045E+01
   Friction thermal sca.    tstar : -0.59146E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28285E-01 0.53007E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77964E-02      32   0.32903E-03   0.18537E+01 0.92077E+02 
c  Velocity[X]                                      0.10525E+01 
c  Velocity[Y]                                      0.80122E+00 
c  Velocity[Z]                                      0.12411E-29 
c  Pressure     0.98997E-07     472   0.95412E-08   0.10034E+00 0.58988E+03 
c  nu_tilda     0.51613E-05      31   0.71280E-05   0.19105E-06 0.12788E+03 
c  TempC        0.31632E+02      27   0.51170E-03   0.32976E+01 0.18579E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3396          10.441          4.5729          4.5729
v  Velocity[Y]            -3.4727          7.0848       0.0020956       0.0020956
v  Velocity[Z]       -6.9287e-015     2.2387e-014    -8.5543e-018    -8.5543e-018
v  ǁVelocityǁ         0.0014851          10.442          5.2459          5.2459
v  Pressure               -54.023          20.163         -8.0114         -8.0114
v  nu_tilda           4.3248e-007       0.0042695       0.0011284       0.0011284
v  TempC                       21          73.093          21.713          21.713
v  TurbVisc           3.0786e-014        0.005032       0.0013216       0.0013216
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1035:        0.21520E+01

===============================================================


 INSTANT    0.103600000E+04   TIME STEP NUMBER            1036
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12308E-01 0.88382E+00
   Friction velocity        uk    :  0.12308E-01 0.88382E+00
   Dimensionless distance   yplus :  0.99087E-01 0.71154E+01
   Friction thermal sca.    tstar : -0.58405E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73930E-01 0.53089E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77996E-02      32   0.37655E-03   0.18562E+01 0.92172E+02 
c  Velocity[X]                                      0.10612E+01 
c  Velocity[Y]                                      0.79503E+00 
c  Velocity[Z]                                      0.14653E-29 
c  Pressure     0.11550E-06     441   0.96466E-08   0.11644E+00 0.39916E+03 
c  nu_tilda     0.51629E-05      31   0.15156E-04   0.19116E-06 0.12790E+03 
c  TempC        0.31643E+02      27   0.43753E-03   0.62079E+01 0.27451E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3379          10.442          4.5729          4.5729
v  Velocity[Y]            -3.4724          7.0947       0.0020774       0.0020774
v  Velocity[Z]       -7.0652e-015     2.2458e-014    -8.5495e-018    -8.5495e-018
v  ǁVelocityǁ        0.00096514          10.442           5.246           5.246
v  Pressure               -54.018          20.114         -8.0387         -8.0387
v  nu_tilda           4.3242e-007       0.0042695        0.001129        0.001129
v  TempC                       21          73.404          21.714          21.714
v  TurbVisc           3.0776e-014        0.005032       0.0013224       0.0013224
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1036:        0.20620E+01

===============================================================


 INSTANT    0.103700000E+04   TIME STEP NUMBER            1037
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75141E-02 0.88364E+00
   Friction velocity        uk    :  0.75141E-02 0.88364E+00
   Dimensionless distance   yplus :  0.60493E-01 0.71139E+01
   Friction thermal sca.    tstar : -0.58164E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45135E-01 0.53078E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78028E-02      32   0.31623E-03   0.19085E+01 0.92580E+02 
c  Velocity[X]                                      0.10979E+01 
c  Velocity[Y]                                      0.81055E+00 
c  Velocity[Z]                                      0.12186E-29 
c  Pressure     0.13057E-06     377   0.93662E-08   0.13246E+00 0.27422E+03 
c  nu_tilda     0.51645E-05      31   0.71333E-05   0.19127E-06 0.12792E+03 
c  TempC        0.31654E+02      26   0.41002E-03   0.64278E+01 0.25166E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3363          10.442          4.5729          4.5729
v  Velocity[Y]            -3.4731          7.0644       0.0020595       0.0020595
v  Velocity[Z]       -8.6222e-015     2.0925e-014      -8.55e-018      -8.55e-018
v  ǁVelocityǁ         0.0010223          10.443          5.2462          5.2462
v  Pressure               -53.991          20.053         -8.0459         -8.0459
v  nu_tilda           4.3248e-007       0.0042695       0.0011297       0.0011297
v  TempC                       21          73.069          21.714          21.714
v  TurbVisc           3.0761e-014        0.005032       0.0013232       0.0013232
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1037:        0.19130E+01

===============================================================


 INSTANT    0.103800000E+04   TIME STEP NUMBER            1038
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84193E-02 0.88248E+00
   Friction velocity        uk    :  0.84193E-02 0.88248E+00
   Dimensionless distance   yplus :  0.67781E-01 0.71046E+01
   Friction thermal sca.    tstar : -0.59109E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50572E-01 0.53008E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78060E-02      32   0.28583E-03   0.18566E+01 0.92180E+02 
c  Velocity[X]                                      0.10531E+01 
c  Velocity[Y]                                      0.80352E+00 
c  Velocity[Z]                                      0.10810E-29 
c  Pressure     0.91362E-07     297   0.96552E-08   0.92806E-01 0.19137E+03 
c  nu_tilda     0.51662E-05      31   0.15158E-04   0.19139E-06 0.12794E+03 
c  TempC        0.31665E+02      26   0.31735E-03   0.49780E+01 0.23779E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3346          10.442          4.5729          4.5729
v  Velocity[Y]            -3.4721          7.0845       0.0020417       0.0020417
v  Velocity[Z]       -8.0496e-015     2.1352e-014    -8.5346e-018    -8.5346e-018
v  ǁVelocityǁ         0.0013987          10.443          5.2464          5.2464
v  Pressure                -53.99          20.111         -8.0529         -8.0529
v  nu_tilda           4.3255e-007       0.0042695       0.0011303       0.0011303
v  TempC                       21          73.069          21.714          21.714
v  TurbVisc           3.0778e-014        0.005032       0.0013239       0.0013239
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1038:        0.17440E+01

===============================================================


 INSTANT    0.103900000E+04   TIME STEP NUMBER            1039
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10219E-01 0.88355E+00
   Friction velocity        uk    :  0.10219E-01 0.88355E+00
   Dimensionless distance   yplus :  0.82268E-01 0.71132E+01
   Friction thermal sca.    tstar : -0.58671E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61381E-01 0.53072E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78091E-02      32   0.36623E-03   0.18513E+01 0.92170E+02 
c  Velocity[X]                                      0.10508E+01 
c  Velocity[Y]                                      0.80043E+00 
c  Velocity[Z]                                      0.16084E-29 
c  Pressure     0.11178E-06     410   0.92067E-08   0.11488E+00 0.26848E+03 
c  nu_tilda     0.51678E-05      31   0.71277E-05   0.19149E-06 0.12796E+03 
c  TempC        0.31676E+02      27   0.38630E-03   0.36224E+01 0.19618E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3332          10.442          4.5729          4.5729
v  Velocity[Y]            -3.4721          7.0673       0.0020238       0.0020238
v  Velocity[Z]       -9.0251e-015     2.0032e-014    -8.5356e-018    -8.5356e-018
v  ǁVelocityǁ         0.0008517          10.443          5.2466          5.2466
v  Pressure               -53.965          20.052         -8.0637         -8.0637
v  nu_tilda            4.326e-007       0.0042695        0.001131        0.001131
v  TempC                       21           73.34          21.715          21.715
v  TurbVisc           3.0797e-014        0.005032       0.0013247       0.0013247
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1039:        0.20130E+01

===============================================================


 INSTANT    0.104000000E+04   TIME STEP NUMBER            1040
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28927E-02 0.88275E+00
   Friction velocity        uk    :  0.28927E-02 0.88275E+00
   Dimensionless distance   yplus :  0.23288E-01 0.71068E+01
   Friction thermal sca.    tstar : -0.59694E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17376E-01 0.53024E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78123E-02      32   0.34935E-03   0.18892E+01 0.92593E+02 
c  Velocity[X]                                      0.10728E+01 
c  Velocity[Y]                                      0.81636E+00 
c  Velocity[Z]                                      0.13285E-29 
c  Pressure     0.11467E-06     394   0.93809E-08   0.11437E+00 0.17678E+03 
c  nu_tilda     0.51694E-05      31   0.15161E-04   0.19162E-06 0.12798E+03 
c  TempC        0.31687E+02      26   0.41992E-03   0.39832E+01 0.19841E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3316          10.443          4.5729          4.5729
v  Velocity[Y]            -3.4719          7.0899       0.0020062       0.0020062
v  Velocity[Z]       -8.4798e-015     2.0754e-014    -8.5204e-018    -8.5204e-018
v  ǁVelocityǁ        0.00085362          10.443          5.2467          5.2467
v  Pressure               -53.965          20.078         -8.0771         -8.0771
v  nu_tilda           4.3262e-007       0.0042695       0.0011316       0.0011316
v  TempC                       21          73.176          21.715          21.715
v  TurbVisc           3.0812e-014        0.005032       0.0013254       0.0013254
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1040:        0.19710E+01

===============================================================


 INSTANT    0.104100000E+04   TIME STEP NUMBER            1041
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89881E-02 0.88418E+00
   Friction velocity        uk    :  0.89881E-02 0.88418E+00
   Dimensionless distance   yplus :  0.72360E-01 0.71182E+01
   Friction thermal sca.    tstar : -0.58981E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53989E-01 0.53110E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78154E-02      32   0.29226E-03   0.18535E+01 0.92232E+02 
c  Velocity[X]                                      0.10464E+01 
c  Velocity[Y]                                      0.80708E+00 
c  Velocity[Z]                                      0.11177E-29 
c  Pressure     0.10818E-06     442   0.90589E-08   0.10865E+00 0.38901E+03 
c  nu_tilda     0.51710E-05      31   0.71114E-05   0.19174E-06 0.12800E+03 
c  TempC        0.31698E+02      27   0.33547E-03   0.44269E+01 0.21715E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3301          10.443          4.5729          4.5729
v  Velocity[Y]            -3.4723          7.0953       0.0019888       0.0019888
v  Velocity[Z]       -9.5013e-015     1.9673e-014    -8.5099e-018    -8.5099e-018
v  ǁVelocityǁ         0.0011079          10.444          5.2469          5.2469
v  Pressure                -53.94          20.125         -8.0649         -8.0649
v  nu_tilda            4.326e-007       0.0042695       0.0011322       0.0011322
v  TempC                       21          73.069          21.715          21.715
v  TurbVisc           3.0816e-014        0.005032       0.0013262       0.0013262
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1041:        0.20880E+01

===============================================================


 INSTANT    0.104200000E+04   TIME STEP NUMBER            1042
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93982E-02 0.88364E+00
   Friction velocity        uk    :  0.93982E-02 0.88364E+00
   Dimensionless distance   yplus :  0.75662E-01 0.71139E+01
   Friction thermal sca.    tstar : -0.58282E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56452E-01 0.53078E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78186E-02      32   0.31811E-03   0.18572E+01 0.92306E+02 
c  Velocity[X]                                      0.10555E+01 
c  Velocity[Y]                                      0.80175E+00 
c  Velocity[Z]                                      0.13858E-29 
c  Pressure     0.86530E-07     489   0.96982E-08   0.88894E-01 0.86629E+03 
c  nu_tilda     0.51727E-05      31   0.15183E-04   0.19187E-06 0.12802E+03 
c  TempC        0.31709E+02      26   0.34347E-03   0.31844E+01 0.18967E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3284          10.443          4.5729          4.5729
v  Velocity[Y]             -3.472          7.0689       0.0019716       0.0019716
v  Velocity[Z]       -8.9111e-015     2.0576e-014    -8.4976e-018    -8.4976e-018
v  ǁVelocityǁ        0.00091389          10.444          5.2471          5.2471
v  Pressure               -53.937          19.961         -8.1171         -8.1171
v  nu_tilda           4.3259e-007       0.0042695       0.0011328       0.0011328
v  TempC                       21          73.465          21.716          21.716
v  TurbVisc           3.0812e-014        0.005032       0.0013269       0.0013269
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1042:        0.22340E+01

===============================================================


 INSTANT    0.104300000E+04   TIME STEP NUMBER            1043
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65398E-02 0.88253E+00
   Friction velocity        uk    :  0.65398E-02 0.88253E+00
   Dimensionless distance   yplus :  0.52650E-01 0.71050E+01
   Friction thermal sca.    tstar : -0.59842E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39283E-01 0.53011E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78217E-02      32   0.31599E-03   0.18581E+01 0.92361E+02 
c  Velocity[X]                                      0.10466E+01 
c  Velocity[Y]                                      0.81144E+00 
c  Velocity[Z]                                      0.13737E-29 
c  Pressure     0.11931E-06     490   0.96910E-08   0.12162E+00 0.95949E+03 
c  nu_tilda     0.51743E-05      31   0.71085E-05   0.19199E-06 0.12804E+03 
c  TempC        0.31721E+02      26   0.56899E-03   0.36380E+01 0.19905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3269          10.443          4.5729          4.5729
v  Velocity[Y]            -3.4718          7.0902       0.0019544       0.0019544
v  Velocity[Z]       -1.0246e-014     1.9155e-014    -8.4957e-018    -8.4957e-018
v  ǁVelocityǁ         0.0015912          10.444          5.2473          5.2473
v  Pressure               -53.911          20.144         -8.0731         -8.0731
v  nu_tilda           4.3256e-007       0.0042695       0.0011335       0.0011335
v  TempC                       21          73.069          21.716          21.716
v  TurbVisc            3.081e-014        0.005032       0.0013277       0.0013277
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1043:        0.22010E+01

===============================================================


 INSTANT    0.104400000E+04   TIME STEP NUMBER            1044
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12947E-01 0.88326E+00
   Friction velocity        uk    :  0.12947E-01 0.88326E+00
   Dimensionless distance   yplus :  0.10423E+00 0.71108E+01
   Friction thermal sca.    tstar : -0.58803E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77766E-01 0.53055E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78249E-02      32   0.34393E-03   0.18741E+01 0.92511E+02 
c  Velocity[X]                                      0.10654E+01 
c  Velocity[Y]                                      0.80867E+00 
c  Velocity[Z]                                      0.13513E-29 
c  Pressure     0.12056E-06     490   0.94806E-08   0.12132E+00 0.10802E+04 
c  nu_tilda     0.51759E-05      31   0.15177E-04   0.19211E-06 0.12807E+03 
c  TempC        0.31732E+02      27   0.43660E-03   0.71575E+01 0.28398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3253          10.443          4.5729          4.5729
v  Velocity[Y]            -3.4718          7.0633       0.0019376       0.0019376
v  Velocity[Z]       -9.6254e-015     1.9736e-014    -8.4867e-018    -8.4867e-018
v  ǁVelocityǁ        0.00090536          10.444          5.2474          5.2474
v  Pressure               -53.904          19.928         -8.1348         -8.1348
v  nu_tilda           4.3259e-007       0.0042695       0.0011341       0.0011341
v  TempC                       21          73.068          21.716          21.716
v  TurbVisc           3.0799e-014        0.005032       0.0013285       0.0013285
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1044:        0.24830E+01

===============================================================


 INSTANT    0.104500000E+04   TIME STEP NUMBER            1045
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62956E-02 0.88286E+00
   Friction velocity        uk    :  0.62956E-02 0.88286E+00
   Dimensionless distance   yplus :  0.50684E-01 0.71076E+01
   Friction thermal sca.    tstar : -0.60257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37816E-01 0.53031E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78280E-02      32   0.32390E-03   0.18835E+01 0.92629E+02 
c  Velocity[X]                                      0.10797E+01 
c  Velocity[Y]                                      0.80379E+00 
c  Velocity[Z]                                      0.15059E-29 
c  Pressure     0.10770E-06     473   0.99637E-08   0.10884E+00 0.76882E+03 
c  nu_tilda     0.51776E-05      31   0.71065E-05   0.19222E-06 0.12808E+03 
c  TempC        0.31743E+02      26   0.43876E-03   0.55309E+01 0.24347E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3236          10.444          4.5729          4.5729
v  Velocity[Y]            -3.4714          7.0895       0.0019205       0.0019205
v  Velocity[Z]       -9.2054e-015      1.811e-014    -8.4711e-018    -8.4711e-018
v  ǁVelocityǁ         0.0011121          10.444          5.2476          5.2476
v  Pressure               -53.887          20.082         -8.1053         -8.1053
v  nu_tilda           4.3257e-007       0.0042695       0.0011348       0.0011348
v  TempC                       21          73.574          21.717          21.717
v  TurbVisc            3.081e-014        0.005032       0.0013292       0.0013292
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1045:        0.23210E+01

===============================================================


 INSTANT    0.104600000E+04   TIME STEP NUMBER            1046
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94831E-02 0.88421E+00
   Friction velocity        uk    :  0.94831E-02 0.88421E+00
   Dimensionless distance   yplus :  0.76345E-01 0.71185E+01
   Friction thermal sca.    tstar : -0.59047E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56962E-01 0.53112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78312E-02      32   0.32030E-03   0.18507E+01 0.92449E+02 
c  Velocity[X]                                      0.10351E+01 
c  Velocity[Y]                                      0.81558E+00 
c  Velocity[Z]                                      0.11377E-29 
c  Pressure     0.89216E-07     442   0.99009E-08   0.90329E-01 0.31467E+03 
c  nu_tilda     0.51792E-05      31   0.15183E-04   0.19234E-06 0.12810E+03 
c  TempC        0.31754E+02      26   0.43138E-03   0.49426E+01 0.22975E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.322          10.444          4.5729          4.5729
v  Velocity[Y]            -3.4707          7.0967       0.0019041       0.0019041
v  Velocity[Z]       -1.0036e-014     1.9049e-014    -8.4663e-018    -8.4663e-018
v  ǁVelocityǁ         0.0012855          10.445          5.2478          5.2478
v  Pressure               -53.882          20.057         -8.1279         -8.1279
v  nu_tilda           4.3246e-007       0.0042695       0.0011354       0.0011354
v  TempC                       21           73.07          21.717          21.717
v  TurbVisc           3.0802e-014        0.005032         0.00133         0.00133
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1046:        0.20750E+01

===============================================================


 INSTANT    0.104700000E+04   TIME STEP NUMBER            1047
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10956E-01 0.88377E+00
   Friction velocity        uk    :  0.10956E-01 0.88377E+00
   Dimensionless distance   yplus :  0.88206E-01 0.71150E+01
   Friction thermal sca.    tstar : -0.58705E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65811E-01 0.53086E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78343E-02      32   0.31038E-03   0.18730E+01 0.92592E+02 
c  Velocity[X]                                      0.10623E+01 
c  Velocity[Y]                                      0.81075E+00 
c  Velocity[Z]                                      0.13680E-29 
c  Pressure     0.11957E-06     441   0.91516E-08   0.12092E+00 0.43318E+03 
c  nu_tilda     0.51808E-05      31   0.70962E-05   0.19246E-06 0.12812E+03 
c  TempC        0.31764E+02      27   0.32243E-03   0.52912E+01 0.23052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3205          10.444          4.5729          4.5729
v  Velocity[Y]            -3.4707          7.0681       0.0018873       0.0018873
v  Velocity[Z]          -1.1e-014      1.758e-014    -8.4644e-018    -8.4644e-018
v  ǁVelocityǁ         0.0008477          10.445          5.2479          5.2479
v  Pressure               -53.854          19.939         -8.1464         -8.1464
v  nu_tilda           4.3243e-007       0.0042695       0.0011361       0.0011361
v  TempC                       21          73.301          21.718          21.718
v  TurbVisc           3.0771e-014        0.005032       0.0013307       0.0013307
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1047:        0.20620E+01

===============================================================


 INSTANT    0.104800000E+04   TIME STEP NUMBER            1048
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29292E-02 0.88279E+00
   Friction velocity        uk    :  0.29292E-02 0.88279E+00
   Dimensionless distance   yplus :  0.23582E-01 0.71070E+01
   Friction thermal sca.    tstar : -0.60727E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17595E-01 0.53026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78375E-02      32   0.32817E-03   0.18653E+01 0.92584E+02 
c  Velocity[X]                                      0.10553E+01 
c  Velocity[Y]                                      0.81006E+00 
c  Velocity[Z]                                      0.15902E-29 
c  Pressure     0.98495E-07     378   0.96340E-08   0.99982E-01 0.26295E+03 
c  nu_tilda     0.51825E-05      31   0.15210E-04   0.19258E-06 0.12815E+03 
c  TempC        0.31775E+02      26   0.43916E-03   0.48596E+01 0.21767E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.319          10.444          4.5729          4.5729
v  Velocity[Y]              -3.47          7.0889       0.0018712       0.0018712
v  Velocity[Z]        -1.058e-014     1.8453e-014    -8.4519e-018    -8.4519e-018
v  ǁVelocityǁ         0.0011513          10.445          5.2481          5.2481
v  Pressure               -53.853          20.025         -8.1478         -8.1478
v  nu_tilda           4.3243e-007       0.0042695       0.0011367       0.0011367
v  TempC                       21          73.069          21.718          21.718
v  TurbVisc           3.0764e-014        0.005032       0.0013315       0.0013315
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1048:        0.19380E+01

===============================================================


 INSTANT    0.104900000E+04   TIME STEP NUMBER            1049
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11183E-01 0.88385E+00
   Friction velocity        uk    :  0.11183E-01 0.88385E+00
   Dimensionless distance   yplus :  0.90030E-01 0.71156E+01
   Friction thermal sca.    tstar : -0.59363E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67172E-01 0.53090E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78406E-02      32   0.37750E-03   0.18841E+01 0.92815E+02 
c  Velocity[X]                                      0.10564E+01 
c  Velocity[Y]                                      0.82766E+00 
c  Velocity[Z]                                      0.12325E-29 
c  Pressure     0.11278E-06     377   0.97023E-08   0.11462E+00 0.26988E+03 
c  nu_tilda     0.51841E-05      31   0.70906E-05   0.19269E-06 0.12817E+03 
c  TempC        0.31786E+02      26   0.35580E-03   0.55033E+01 0.24897E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3174          10.444          4.5729          4.5729
v  Velocity[Y]            -3.4691          7.0713       0.0018547       0.0018547
v  Velocity[Z]       -1.1085e-014     1.6765e-014    -8.4487e-018    -8.4487e-018
v  ǁVelocityǁ        0.00092442          10.445          5.2482          5.2482
v  Pressure               -53.827          19.965         -8.1556         -8.1556
v  nu_tilda           4.3251e-007       0.0042695       0.0011373       0.0011373
v  TempC                       21          73.504          21.718          21.718
v  TurbVisc           3.0764e-014        0.005032       0.0013322       0.0013322
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1049:        0.19170E+01

===============================================================


 INSTANT    0.105000000E+04   TIME STEP NUMBER            1050
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85295E-02 0.88320E+00
   Friction velocity        uk    :  0.85295E-02 0.88320E+00
   Dimensionless distance   yplus :  0.68668E-01 0.71104E+01
   Friction thermal sca.    tstar : -0.60094E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51234E-01 0.53051E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78438E-02      32   0.29384E-03   0.18982E+01 0.92962E+02 
c  Velocity[X]                                      0.10803E+01 
c  Velocity[Y]                                      0.81795E+00 
c  Velocity[Z]                                      0.10548E-29 
c  Pressure     0.13711E-06     425   0.94293E-08   0.13498E+00 0.25395E+03 
c  nu_tilda     0.51857E-05      31   0.15201E-04   0.19282E-06 0.12819E+03 
c  TempC        0.31797E+02      26   0.45699E-03   0.51512E+01 0.22655E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3158          10.444          4.5729          4.5729
v  Velocity[Y]            -3.4684          7.0907       0.0018389       0.0018389
v  Velocity[Z]       -1.0803e-014     1.7721e-014    -8.4382e-018    -8.4382e-018
v  ǁVelocityǁ        0.00096172          10.445          5.2484          5.2484
v  Pressure               -53.826          19.964         -8.1764         -8.1764
v  nu_tilda           4.3254e-007       0.0042695       0.0011379       0.0011379
v  TempC                       21          73.968          21.719          21.719
v  TurbVisc           3.0785e-014        0.005032        0.001333        0.001333
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1050:        0.20350E+01

===============================================================


 INSTANT    0.105100000E+04   TIME STEP NUMBER            1051
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75912E-02 0.88482E+00
   Friction velocity        uk    :  0.75912E-02 0.88482E+00
   Dimensionless distance   yplus :  0.61115E-01 0.71234E+01
   Friction thermal sca.    tstar : -0.60021E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45598E-01 0.53149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78469E-02      32   0.32342E-03   0.18579E+01 0.92616E+02 
c  Velocity[X]                                      0.10468E+01 
c  Velocity[Y]                                      0.81112E+00 
c  Velocity[Z]                                      0.16156E-29 
c  Pressure     0.94860E-07     457   0.94360E-08   0.96275E-01 0.54315E+03 
c  nu_tilda     0.51874E-05      31   0.71005E-05   0.19294E-06 0.12821E+03 
c  TempC        0.31808E+02      27   0.41509E-03   0.63582E+01 0.25665E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3141          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4681           7.102       0.0018227       0.0018227
v  Velocity[Z]       -1.1473e-014     1.6235e-014    -8.4349e-018    -8.4349e-018
v  ǁVelocityǁ         0.0015032          10.445          5.2486          5.2486
v  Pressure               -53.802           20.05          -8.155          -8.155
v  nu_tilda           4.3248e-007       0.0042695       0.0011386       0.0011386
v  TempC                       21          73.069          21.719          21.719
v  TurbVisc           3.0795e-014        0.005032       0.0013337       0.0013337
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1051:        0.21190E+01

===============================================================


 INSTANT    0.105200000E+04   TIME STEP NUMBER            1052
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12424E-01 0.88425E+00
   Friction velocity        uk    :  0.12424E-01 0.88425E+00
   Dimensionless distance   yplus :  0.10002E+00 0.71189E+01
   Friction thermal sca.    tstar : -0.59672E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74626E-01 0.53115E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78500E-02      32   0.29801E-03   0.18896E+01 0.92952E+02 
c  Velocity[X]                                      0.10582E+01 
c  Velocity[Y]                                      0.83148E+00 
c  Velocity[Z]                                      0.13515E-29 
c  Pressure     0.11202E-06     473   0.97218E-08   0.11481E+00 0.71010E+03 
c  nu_tilda     0.51890E-05      31   0.15209E-04   0.19308E-06 0.12824E+03 
c  TempC        0.31819E+02      26   0.41336E-03   0.51386E+01 0.24120E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3125          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4676          7.0756        0.001807        0.001807
v  Velocity[Z]       -1.1436e-014     1.7147e-014    -8.4312e-018    -8.4312e-018
v  ǁVelocityǁ        0.00086899          10.446          5.2487          5.2487
v  Pressure               -53.792          19.917         -8.1956         -8.1956
v  nu_tilda           4.3247e-007       0.0042695       0.0011392       0.0011392
v  TempC                       21          73.184          21.719          21.719
v  TurbVisc           3.0778e-014        0.005032       0.0013345       0.0013345
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1052:        0.21510E+01

===============================================================


 INSTANT    0.105300000E+04   TIME STEP NUMBER            1053
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51129E-02 0.88288E+00
   Friction velocity        uk    :  0.51129E-02 0.88288E+00
   Dimensionless distance   yplus :  0.41162E-01 0.71078E+01
   Friction thermal sca.    tstar : -0.60305E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30712E-01 0.53032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78531E-02      32   0.33018E-03   0.18736E+01 0.92809E+02 
c  Velocity[X]                                      0.10536E+01 
c  Velocity[Y]                                      0.82006E+00 
c  Velocity[Z]                                      0.12013E-29 
c  Pressure     0.11698E-06     424   0.99795E-08   0.11598E+00 0.41069E+03 
c  nu_tilda     0.51906E-05      31   0.70761E-05   0.19321E-06 0.12826E+03 
c  TempC        0.31830E+02      26   0.37860E-03   0.50892E+01 0.24004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3109          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4665           7.093        0.001791        0.001791
v  Velocity[Z]       -1.0888e-014     1.5537e-014    -8.4168e-018    -8.4168e-018
v  ǁVelocityǁ         0.0011937          10.446          5.2489          5.2489
v  Pressure               -53.773          19.982         -8.1846         -8.1846
v  nu_tilda           4.3247e-007       0.0042695       0.0011399       0.0011399
v  TempC                       21          73.938           21.72           21.72
v  TurbVisc           3.0775e-014        0.005032       0.0013352       0.0013352
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1053:        0.20420E+01

===============================================================


 INSTANT    0.105400000E+04   TIME STEP NUMBER            1054
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60588E-02 0.88410E+00
   Friction velocity        uk    :  0.60588E-02 0.88410E+00
   Dimensionless distance   yplus :  0.48778E-01 0.71176E+01
   Friction thermal sca.    tstar : -0.59805E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36394E-01 0.53105E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78563E-02      32   0.36740E-03   0.19071E+01 0.93152E+02 
c  Velocity[X]                                      0.10938E+01 
c  Velocity[Y]                                      0.81328E+00 
c  Velocity[Z]                                      0.14554E-29 
c  Pressure     0.11621E-06     457   0.99488E-08   0.11917E+00 0.58094E+03 
c  nu_tilda     0.51923E-05      31   0.15231E-04   0.19334E-06 0.12829E+03 
c  TempC        0.31841E+02      26   0.26869E-03   0.50389E+01 0.21389E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3094          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4658          7.0728       0.0017753       0.0017753
v  Velocity[Z]       -1.1288e-014     1.6603e-014    -8.4095e-018    -8.4095e-018
v  ǁVelocityǁ         0.0011951          10.446           5.249           5.249
v  Pressure               -53.767          19.887         -8.2213         -8.2213
v  nu_tilda           4.3248e-007       0.0042695       0.0011405       0.0011405
v  TempC                       21          73.067           21.72           21.72
v  TurbVisc           3.0776e-014        0.005032        0.001336        0.001336
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1054:        0.21230E+01

===============================================================


 INSTANT    0.105500000E+04   TIME STEP NUMBER            1055
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10254E-01 0.88324E+00
   Friction velocity        uk    :  0.10254E-01 0.88324E+00
   Dimensionless distance   yplus :  0.82548E-01 0.71107E+01
   Friction thermal sca.    tstar : -0.60710E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61590E-01 0.53053E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78594E-02      32   0.31951E-03   0.18913E+01 0.93063E+02 
c  Velocity[X]                                      0.10589E+01 
c  Velocity[Y]                                      0.83244E+00 
c  Velocity[Z]                                      0.12956E-29 
c  Pressure     0.10598E-06     456   0.98280E-08   0.10664E+00 0.68854E+03 
c  nu_tilda     0.51939E-05      31   0.70882E-05   0.19345E-06 0.12831E+03 
c  TempC        0.31852E+02      26   0.42982E-03   0.31176E+01 0.17172E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.308          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4665          7.0975       0.0017598       0.0017598
v  Velocity[Z]       -1.1673e-014     1.4982e-014    -8.4108e-018    -8.4108e-018
v  ǁVelocityǁ        0.00085931          10.446          5.2492          5.2492
v  Pressure               -53.743          20.006         -8.1919         -8.1919
v  nu_tilda           4.3246e-007       0.0042695       0.0011411       0.0011411
v  TempC                       21          73.068           21.72           21.72
v  TurbVisc           3.0776e-014        0.005032       0.0013368       0.0013368
v  total_pressure     1.0127e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1055:        0.21070E+01

===============================================================


 INSTANT    0.105600000E+04   TIME STEP NUMBER            1056
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46953E-02 0.88445E+00
   Friction velocity        uk    :  0.46953E-02 0.88445E+00
   Dimensionless distance   yplus :  0.37801E-01 0.71205E+01
   Friction thermal sca.    tstar : -0.60257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28203E-01 0.53127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78625E-02      32   0.32857E-03   0.18678E+01 0.92831E+02 
c  Velocity[X]                                      0.10464E+01 
c  Velocity[Y]                                      0.82142E+00 
c  Velocity[Z]                                      0.13457E-29 
c  Pressure     0.12365E-06     457   0.97020E-08   0.12365E+00 0.45262E+03 
c  nu_tilda     0.51956E-05      31   0.15223E-04   0.19357E-06 0.12833E+03 
c  TempC        0.31863E+02      26   0.37290E-03   0.56663E+01 0.24717E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3064          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4651          7.1014       0.0017446       0.0017446
v  Velocity[Z]        -1.134e-014     1.5997e-014    -8.3955e-018    -8.3955e-018
v  ǁVelocityǁ         0.0012133          10.446          5.2493          5.2493
v  Pressure               -53.739           19.95         -8.2233         -8.2233
v  nu_tilda           4.3242e-007       0.0042695       0.0011417       0.0011417
v  TempC                       21          73.109          21.721          21.721
v  TurbVisc           3.0773e-014        0.005032       0.0013375       0.0013375
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1056:        0.21410E+01

===============================================================


 INSTANT    0.105700000E+04   TIME STEP NUMBER            1057
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11491E-01 0.88420E+00
   Friction velocity        uk    :  0.11491E-01 0.88420E+00
   Dimensionless distance   yplus :  0.92510E-01 0.71184E+01
   Friction thermal sca.    tstar : -0.59718E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69023E-01 0.53111E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78656E-02      32   0.31819E-03   0.19051E+01 0.93163E+02 
c  Velocity[X]                                      0.10865E+01 
c  Velocity[Y]                                      0.81864E+00 
c  Velocity[Z]                                      0.16428E-29 
c  Pressure     0.10651E-06     394   0.96965E-08   0.10997E+00 0.30169E+03 
c  nu_tilda     0.51972E-05      31   0.70869E-05   0.19369E-06 0.12835E+03 
c  TempC        0.31874E+02      26   0.48677E-03   0.46080E+01 0.22630E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3048          10.445          4.5729          4.5729
v  Velocity[Y]             -3.465           7.078        0.001729        0.001729
v  Velocity[Z]       -1.1652e-014     1.4413e-014    -8.4004e-018    -8.4004e-018
v  ǁVelocityǁ        0.00090489          10.446          5.2495          5.2495
v  Pressure               -53.712          19.875         -8.2353         -8.2353
v  nu_tilda           4.3243e-007       0.0042695       0.0011424       0.0011424
v  TempC                       21          73.422          21.721          21.721
v  TurbVisc           3.0761e-014        0.005032       0.0013383       0.0013383
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1057:        0.20380E+01

===============================================================


 INSTANT    0.105800000E+04   TIME STEP NUMBER            1058
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75813E-02 0.88290E+00
   Friction velocity        uk    :  0.75813E-02 0.88290E+00
   Dimensionless distance   yplus :  0.61035E-01 0.71080E+01
   Friction thermal sca.    tstar : -0.60736E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45539E-01 0.53033E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78687E-02      32   0.31357E-03   0.18853E+01 0.93140E+02 
c  Velocity[X]                                      0.10503E+01 
c  Velocity[Y]                                      0.83503E+00 
c  Velocity[Z]                                      0.12069E-29 
c  Pressure     0.95113E-07     346   0.92675E-08   0.95863E-01 0.21914E+03 
c  nu_tilda     0.51988E-05      31   0.15235E-04   0.19382E-06 0.12837E+03 
c  TempC        0.31885E+02      26   0.36810E-03   0.74218E+01 0.29305E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3031          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4649          7.0965       0.0017138       0.0017138
v  Velocity[Z]       -1.1496e-014     1.5412e-014    -8.3775e-018    -8.3775e-018
v  ǁVelocityǁ         0.0010197          10.446          5.2496          5.2496
v  Pressure               -53.713          19.946         -8.2396         -8.2396
v  nu_tilda           4.3243e-007       0.0042695        0.001143        0.001143
v  TempC                       21          73.535          21.722          21.722
v  TurbVisc           3.0763e-014        0.005032        0.001339        0.001339
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1058:        0.18600E+01

===============================================================


 INSTANT    0.105900000E+04   TIME STEP NUMBER            1059
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84916E-02 0.88389E+00
   Friction velocity        uk    :  0.84916E-02 0.88389E+00
   Dimensionless distance   yplus :  0.68363E-01 0.71159E+01
   Friction thermal sca.    tstar : -0.59917E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51007E-01 0.53093E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78718E-02      32   0.33024E-03   0.18848E+01 0.93051E+02 
c  Velocity[X]                                      0.10609E+01 
c  Velocity[Y]                                      0.82387E+00 
c  Velocity[Z]                                      0.12501E-29 
c  Pressure     0.11174E-06     421   0.95461E-08   0.11351E+00 0.32334E+03 
c  nu_tilda     0.52005E-05      31   0.70841E-05   0.19394E-06 0.12839E+03 
c  TempC        0.31896E+02      26   0.26190E-03   0.46985E+01 0.22720E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3014          10.445          4.5729          4.5729
v  Velocity[Y]            -3.4634          7.0754       0.0016987       0.0016987
v  Velocity[Z]       -1.1998e-014     1.3942e-014    -8.3803e-018    -8.3803e-018
v  ǁVelocityǁ         0.0014047          10.446          5.2498          5.2498
v  Pressure               -53.686          19.862          -8.252          -8.252
v  nu_tilda           4.3248e-007       0.0042695       0.0011437       0.0011437
v  TempC                       21          73.067          21.722          21.722
v  TurbVisc           3.0762e-014        0.005032       0.0013398       0.0013398
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1059:        0.20370E+01

===============================================================


 INSTANT    0.106000000E+04   TIME STEP NUMBER            1060
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11818E-01 0.88322E+00
   Friction velocity        uk    :  0.11818E-01 0.88322E+00
   Dimensionless distance   yplus :  0.95146E-01 0.71105E+01
   Friction thermal sca.    tstar : -0.61602E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70989E-01 0.53052E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78749E-02      32   0.36273E-03   0.18754E+01 0.93044E+02 
c  Velocity[X]                                      0.10570E+01 
c  Velocity[Y]                                      0.81846E+00 
c  Velocity[Z]                                      0.14751E-29 
c  Pressure     0.93025E-07     346   0.94886E-08   0.93794E-01 0.18312E+03 
c  nu_tilda     0.52021E-05      31   0.15251E-04   0.19408E-06 0.12842E+03 
c  TempC        0.31907E+02      27   0.43342E-03   0.28827E+01 0.15846E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2997          10.446          4.5729          4.5729
v  Velocity[Y]            -3.4633           7.097       0.0016837       0.0016837
v  Velocity[Z]       -1.2006e-014     1.3627e-014    -8.3654e-018    -8.3654e-018
v  ǁVelocityǁ        0.00084229          10.446          5.2499          5.2499
v  Pressure               -53.685          19.913         -8.2624         -8.2624
v  nu_tilda           4.3247e-007       0.0042695       0.0011443       0.0011443
v  TempC                       21          73.067          21.722          21.722
v  TurbVisc           3.0779e-014        0.005032       0.0013405       0.0013405
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1060:        0.18600E+01

===============================================================


 INSTANT    0.106100000E+04   TIME STEP NUMBER            1061
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29989E-02 0.88448E+00
   Friction velocity        uk    :  0.29989E-02 0.88448E+00
   Dimensionless distance   yplus :  0.24144E-01 0.71206E+01
   Friction thermal sca.    tstar : -0.60304E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18014E-01 0.53128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78780E-02      32   0.35642E-03   0.19132E+01 0.93522E+02 
c  Velocity[X]                                      0.10725E+01 
c  Velocity[Y]                                      0.84071E+00 
c  Velocity[Z]                                      0.12638E-29 
c  Pressure     0.13514E-06     426   0.94799E-08   0.13697E+00 0.35880E+03 
c  nu_tilda     0.52038E-05      31   0.70937E-05   0.19420E-06 0.12844E+03 
c  TempC        0.31918E+02      27   0.40704E-03   0.51065E+01 0.23744E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2982          10.446          4.5729          4.5729
v  Velocity[Y]            -3.4628          7.1072       0.0016688       0.0016688
v  Velocity[Z]       -1.2565e-014     1.4897e-014     -8.352e-018     -8.352e-018
v  ǁVelocityǁ         0.0012762          10.447          5.2501          5.2501
v  Pressure               -53.659          19.947         -8.2516         -8.2516
v  nu_tilda           4.3244e-007       0.0042695       0.0011449       0.0011449
v  TempC                       21          73.288          21.723          21.723
v  TurbVisc           3.0774e-014        0.005032       0.0013413       0.0013413
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1061:        0.20460E+01

===============================================================


 INSTANT    0.106200000E+04   TIME STEP NUMBER            1062
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97167E-02 0.88410E+00
   Friction velocity        uk    :  0.97167E-02 0.88410E+00
   Dimensionless distance   yplus :  0.78226E-01 0.71176E+01
   Friction thermal sca.    tstar : -0.59863E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58366E-01 0.53105E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78811E-02      32   0.29008E-03   0.19271E+01 0.93563E+02 
c  Velocity[X]                                      0.10992E+01 
c  Velocity[Y]                                      0.82788E+00 
c  Velocity[Z]                                      0.11293E-29 
c  Pressure     0.13425E-06     489   0.97576E-08   0.13511E+00 0.84230E+03 
c  nu_tilda     0.52054E-05      31   0.15248E-04   0.19434E-06 0.12847E+03 
c  TempC        0.31929E+02      26   0.44025E-03   0.52944E+01 0.22844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2967          10.446          4.5729          4.5729
v  Velocity[Y]            -3.4626          7.0755       0.0016542       0.0016542
v  Velocity[Z]       -1.2452e-014     1.3414e-014    -8.3458e-018    -8.3458e-018
v  ǁVelocityǁ         0.0011217          10.447          5.2502          5.2502
v  Pressure               -53.648          19.783         -8.2988         -8.2988
v  nu_tilda           4.3254e-007       0.0042695       0.0011455       0.0011455
v  TempC                       21          73.067          21.723          21.723
v  TurbVisc           3.0767e-014        0.005032        0.001342        0.001342
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1062:        0.22010E+01

===============================================================


 INSTANT    0.106300000E+04   TIME STEP NUMBER            1063
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96118E-02 0.88314E+00
   Friction velocity        uk    :  0.96118E-02 0.88314E+00
   Dimensionless distance   yplus :  0.77381E-01 0.71099E+01
   Friction thermal sca.    tstar : -0.61592E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57735E-01 0.53048E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78842E-02      32   0.32390E-03   0.18732E+01 0.93126E+02 
c  Velocity[X]                                      0.10516E+01 
c  Velocity[Y]                                      0.82166E+00 
c  Velocity[Z]                                      0.15203E-29 
c  Pressure     0.95195E-07     474   0.93743E-08   0.96679E-01 0.75790E+03 
c  nu_tilda     0.52070E-05      31   0.70862E-05   0.19447E-06 0.12850E+03 
c  TempC        0.31940E+02      26   0.37670E-03   0.55380E+01 0.25973E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2951          10.446          4.5729          4.5729
v  Velocity[Y]             -3.462          7.0997       0.0016392       0.0016392
v  Velocity[Z]       -1.2161e-014     1.2847e-014    -8.3235e-018    -8.3235e-018
v  ǁVelocityǁ        0.00089339          10.447          5.2504          5.2504
v  Pressure                -53.63          19.932         -8.2694         -8.2694
v  nu_tilda           4.3254e-007       0.0042695       0.0011462       0.0011462
v  TempC                       21          73.182          21.723          21.723
v  TurbVisc           3.0793e-014        0.005032       0.0013428       0.0013428
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1063:        0.21590E+01

===============================================================


 INSTANT    0.106400000E+04   TIME STEP NUMBER            1064
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62334E-02 0.88422E+00
   Friction velocity        uk    :  0.62334E-02 0.88422E+00
   Dimensionless distance   yplus :  0.50183E-01 0.71185E+01
   Friction thermal sca.    tstar : -0.60922E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37442E-01 0.53112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78873E-02      32   0.35335E-03   0.18980E+01 0.93443E+02 
c  Velocity[X]                                      0.10561E+01 
c  Velocity[Y]                                      0.84191E+00 
c  Velocity[Z]                                      0.15742E-29 
c  Pressure     0.11005E-06     488   0.95413E-08   0.11271E+00 0.83947E+03 
c  nu_tilda     0.52087E-05      31   0.15254E-04   0.19461E-06 0.12852E+03 
c  TempC        0.31951E+02      26   0.36047E-03   0.52869E+01 0.24174E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2935          10.447          4.5729          4.5729
v  Velocity[Y]            -3.4611           7.077       0.0016247       0.0016247
v  Velocity[Z]       -1.2339e-014     1.4049e-014    -8.3119e-018    -8.3119e-018
v  ǁVelocityǁ         0.0012796          10.447          5.2505          5.2505
v  Pressure               -53.624          19.773         -8.3184         -8.3184
v  nu_tilda           4.3257e-007       0.0042695       0.0011468       0.0011468
v  TempC                       21          73.067          21.724          21.724
v  TurbVisc           3.0796e-014        0.005032       0.0013435       0.0013435
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1064:        0.21930E+01

===============================================================


 INSTANT    0.106500000E+04   TIME STEP NUMBER            1065
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11882E-01 0.88357E+00
   Friction velocity        uk    :  0.11882E-01 0.88357E+00
   Dimensionless distance   yplus :  0.95658E-01 0.71134E+01
   Friction thermal sca.    tstar : -0.61872E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71371E-01 0.53074E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78904E-02      32   0.33500E-03   0.19067E+01 0.93516E+02 
c  Velocity[X]                                      0.10735E+01 
c  Velocity[Y]                                      0.83313E+00 
c  Velocity[Z]                                      0.11789E-29 
c  Pressure     0.12529E-06     458   0.93178E-08   0.12556E+00 0.79204E+03 
c  nu_tilda     0.52103E-05      31   0.70841E-05   0.19473E-06 0.12854E+03 
c  TempC        0.31962E+02      26   0.41444E-03   0.44146E+01 0.21388E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2919          10.447          4.5729          4.5729
v  Velocity[Y]            -3.4609          7.1046       0.0016102       0.0016102
v  Velocity[Z]       -1.2518e-014     1.2515e-014    -8.3113e-018    -8.3113e-018
v  ǁVelocityǁ        0.00090951          10.448          5.2507          5.2507
v  Pressure               -53.599          19.924         -8.2842         -8.2842
v  nu_tilda           4.3258e-007       0.0042695       0.0011474       0.0011474
v  TempC                       21          73.067          21.724          21.724
v  TurbVisc           3.0802e-014        0.005032       0.0013443       0.0013443
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1065:        0.21360E+01

===============================================================


 INSTANT    0.106600000E+04   TIME STEP NUMBER            1066
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66369E-02 0.88484E+00
   Friction velocity        uk    :  0.66369E-02 0.88484E+00
   Dimensionless distance   yplus :  0.53432E-01 0.71235E+01
   Friction thermal sca.    tstar : -0.60483E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39866E-01 0.53150E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78935E-02      32   0.32644E-03   0.18734E+01 0.93230E+02 
c  Velocity[X]                                      0.10490E+01 
c  Velocity[Y]                                      0.82440E+00 
c  Velocity[Z]                                      0.14115E-29 
c  Pressure     0.96406E-07     442   0.97116E-08   0.96307E-01 0.54943E+03 
c  nu_tilda     0.52120E-05      31   0.15274E-04   0.19485E-06 0.12857E+03 
c  TempC        0.31973E+02      26   0.33544E-03   0.36646E+01 0.20007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2902          10.447          4.5729          4.5729
v  Velocity[Y]            -3.4602          7.1079       0.0015958       0.0015958
v  Velocity[Z]       -1.2291e-014     1.2036e-014    -8.2904e-018    -8.2904e-018
v  ǁVelocityǁ         0.0010869          10.448          5.2508          5.2508
v  Pressure               -53.596           19.84         -8.3203         -8.3203
v  nu_tilda           4.3257e-007       0.0042695        0.001148        0.001148
v  TempC                       21          73.369          21.725          21.725
v  TurbVisc           3.0806e-014        0.005032        0.001345        0.001345
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1066:        0.20690E+01

===============================================================


 INSTANT    0.106700000E+04   TIME STEP NUMBER            1067
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47718E-02 0.88452E+00
   Friction velocity        uk    :  0.47718E-02 0.88452E+00
   Dimensionless distance   yplus :  0.38416E-01 0.71210E+01
   Friction thermal sca.    tstar : -0.60828E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28663E-01 0.53131E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78966E-02      32   0.29819E-03   0.19114E+01 0.93641E+02 
c  Velocity[X]                                      0.10631E+01 
c  Velocity[Y]                                      0.84828E+00 
c  Velocity[Z]                                      0.13494E-29 
c  Pressure     0.98730E-07     312   0.98970E-08   0.10119E+00 0.24051E+03 
c  nu_tilda     0.52136E-05      31   0.70810E-05   0.19497E-06 0.12859E+03 
c  TempC        0.31984E+02      27   0.35245E-03   0.37265E+01 0.18757E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2885          10.447          4.5729          4.5729
v  Velocity[Y]             -3.459           7.082       0.0015814       0.0015814
v  Velocity[Z]       -1.2415e-014     1.3102e-014    -8.2868e-018    -8.2868e-018
v  ǁVelocityǁ         0.0013121          10.448          5.2509          5.2509
v  Pressure               -53.569          19.805          -8.323          -8.323
v  nu_tilda           4.3262e-007       0.0042695       0.0011487       0.0011487
v  TempC                       21          73.067          21.725          21.725
v  TurbVisc           3.0803e-014        0.005032       0.0013458       0.0013458
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1067:        0.17780E+01

===============================================================


 INSTANT    0.106800000E+04   TIME STEP NUMBER            1068
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11199E-01 0.88327E+00
   Friction velocity        uk    :  0.11199E-01 0.88327E+00
   Dimensionless distance   yplus :  0.90161E-01 0.71109E+01
   Friction thermal sca.    tstar : -0.62171E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67270E-01 0.53056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.78997E-02      32   0.30014E-03   0.18950E+01 0.93507E+02 
c  Velocity[X]                                      0.10584E+01 
c  Velocity[Y]                                      0.83660E+00 
c  Velocity[Z]                                      0.12906E-29 
c  Pressure     0.99613E-07     409   0.96505E-08   0.10106E+00 0.18780E+03 
c  nu_tilda     0.52153E-05      31   0.15273E-04   0.19510E-06 0.12861E+03 
c  TempC        0.31994E+02      27   0.47777E-03   0.44546E+01 0.21570E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2869          10.447          4.5729          4.5729
v  Velocity[Y]            -3.4587           7.102       0.0015671       0.0015671
v  Velocity[Z]       -1.2338e-014     1.1695e-014    -8.2697e-018    -8.2697e-018
v  ǁVelocityǁ         0.0008364          10.448          5.2511          5.2511
v  Pressure               -53.568          19.839         -8.3374         -8.3374
v  nu_tilda           4.3263e-007       0.0042695       0.0011493       0.0011493
v  TempC                       21          73.067          21.725          21.725
v  TurbVisc           3.0817e-014        0.005032       0.0013465       0.0013465
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1068:        0.19990E+01

===============================================================


 INSTANT    0.106900000E+04   TIME STEP NUMBER            1069
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23982E-02 0.88418E+00
   Friction velocity        uk    :  0.23982E-02 0.88418E+00
   Dimensionless distance   yplus :  0.19307E-01 0.71183E+01
   Friction thermal sca.    tstar : -0.60872E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14405E-01 0.53110E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79027E-02      32   0.37774E-03   0.19055E+01 0.93552E+02 
c  Velocity[X]                                      0.10775E+01 
c  Velocity[Y]                                      0.82803E+00 
c  Velocity[Z]                                      0.14808E-29 
c  Pressure     0.12547E-06     424   0.98153E-08   0.12687E+00 0.36103E+03 
c  nu_tilda     0.52169E-05      31   0.70851E-05   0.19523E-06 0.12864E+03 
c  TempC        0.32005E+02      26   0.36878E-03   0.61361E+01 0.27155E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2853          10.448          4.5729          4.5729
v  Velocity[Y]            -3.4576          7.0801        0.001553        0.001553
v  Velocity[Z]        -1.268e-014     1.1262e-014    -8.2679e-018    -8.2679e-018
v  ǁVelocityǁ         0.0013725          10.448          5.2512          5.2512
v  Pressure                -53.54          19.742         -8.3516         -8.3516
v  nu_tilda           4.3265e-007       0.0042695         0.00115         0.00115
v  TempC                       21          73.066          21.726          21.726
v  TurbVisc           3.0819e-014        0.005032       0.0013473       0.0013473
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1069:        0.20360E+01

===============================================================


 INSTANT    0.107000000E+04   TIME STEP NUMBER            1070
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11644E-01 0.88373E+00
   Friction velocity        uk    :  0.11644E-01 0.88373E+00
   Dimensionless distance   yplus :  0.93745E-01 0.71146E+01
   Friction thermal sca.    tstar : -0.62388E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69944E-01 0.53083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79058E-02      32   0.30512E-03   0.19386E+01 0.93958E+02 
c  Velocity[X]                                      0.10919E+01 
c  Velocity[Y]                                      0.84676E+00 
c  Velocity[Z]                                      0.11249E-29 
c  Pressure     0.13097E-06     424   0.97417E-08   0.13195E+00 0.33239E+03 
c  nu_tilda     0.52186E-05      31   0.15280E-04   0.19536E-06 0.12866E+03 
c  TempC        0.32016E+02      26   0.42491E-03   0.49002E+01 0.22193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2838          10.448          4.5729          4.5729
v  Velocity[Y]            -3.4562          7.1007       0.0015389       0.0015389
v  Velocity[Z]       -1.2629e-014     1.2362e-014    -8.2461e-018    -8.2461e-018
v  ǁVelocityǁ         0.0010479          10.449          5.2514          5.2514
v  Pressure               -53.534          19.841         -8.3454         -8.3454
v  nu_tilda           4.3266e-007       0.0042695       0.0011506       0.0011506
v  TempC                       21          73.417          21.726          21.726
v  TurbVisc           3.0827e-014        0.005032        0.001348        0.001348
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1070:        0.20370E+01

===============================================================


 INSTANT    0.107100000E+04   TIME STEP NUMBER            1071
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88635E-02 0.88500E+00
   Friction velocity        uk    :  0.88635E-02 0.88500E+00
   Dimensionless distance   yplus :  0.71358E-01 0.71249E+01
   Friction thermal sca.    tstar : -0.61346E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53241E-01 0.53160E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79089E-02      32   0.28867E-03   0.18819E+01 0.93541E+02 
c  Velocity[X]                                      0.10422E+01 
c  Velocity[Y]                                      0.83968E+00 
c  Velocity[Z]                                      0.12504E-29 
c  Pressure     0.91933E-07     361   0.93306E-08   0.92420E-01 0.19949E+03 
c  nu_tilda     0.52202E-05      31   0.70640E-05   0.19550E-06 0.12869E+03 
c  TempC        0.32027E+02      26   0.42607E-03   0.79919E+01 0.27024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2821          10.448          4.5729          4.5729
v  Velocity[Y]            -3.4556          7.1123        0.001525        0.001525
v  Velocity[Z]       -1.2508e-014     1.1018e-014    -8.2298e-018    -8.2298e-018
v  ǁVelocityǁ        0.00094143          10.449          5.2515          5.2515
v  Pressure               -53.513           19.83         -8.3506         -8.3506
v  nu_tilda           4.3262e-007       0.0042695       0.0011512       0.0011512
v  TempC                       21          73.067          21.726          21.726
v  TurbVisc           3.0829e-014        0.005032       0.0013488       0.0013488
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1071:        0.18860E+01

===============================================================


 INSTANT    0.107200000E+04   TIME STEP NUMBER            1072
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70093E-02 0.88467E+00
   Friction velocity        uk    :  0.70093E-02 0.88467E+00
   Dimensionless distance   yplus :  0.56430E-01 0.71222E+01
   Friction thermal sca.    tstar : -0.61719E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42103E-01 0.53140E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79120E-02      32   0.34456E-03   0.18985E+01 0.93653E+02 
c  Velocity[X]                                      0.10682E+01 
c  Velocity[Y]                                      0.83030E+00 
c  Velocity[Z]                                      0.15872E-29 
c  Pressure     0.10947E-06     490   0.96343E-08   0.11074E+00 0.80393E+03 
c  nu_tilda     0.52219E-05      31   0.15298E-04   0.19565E-06 0.12872E+03 
c  TempC        0.32038E+02      26   0.40474E-03   0.59908E+01 0.25100E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2804          10.448          4.5729          4.5729
v  Velocity[Y]            -3.4544          7.0829        0.001511        0.001511
v  Velocity[Z]       -1.2628e-014     1.0639e-014    -8.2191e-018    -8.2191e-018
v  ǁVelocityǁ         0.0011102          10.449          5.2516          5.2516
v  Pressure               -53.508          19.677         -8.3979         -8.3979
v  nu_tilda           4.3261e-007       0.0042695       0.0011518       0.0011518
v  TempC                       21          73.066          21.727          21.727
v  TurbVisc           3.0818e-014        0.005032       0.0013495       0.0013495
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1072:        0.22020E+01

===============================================================


 INSTANT    0.107300000E+04   TIME STEP NUMBER            1073
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10685E-01 0.88374E+00
   Friction velocity        uk    :  0.10685E-01 0.88374E+00
   Dimensionless distance   yplus :  0.86020E-01 0.71147E+01
   Friction thermal sca.    tstar : -0.62855E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64181E-01 0.53083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79150E-02      32   0.33434E-03   0.19155E+01 0.93888E+02 
c  Velocity[X]                                      0.10627E+01 
c  Velocity[Y]                                      0.85289E+00 
c  Velocity[Z]                                      0.13066E-29 
c  Pressure     0.11458E-06     485   0.96232E-08   0.11603E+00 0.81903E+03 
c  nu_tilda     0.52235E-05      31   0.70663E-05   0.19578E-06 0.12875E+03 
c  TempC        0.32049E+02      26   0.32681E-03   0.48804E+01 0.23439E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2788          10.448          4.5729          4.5729
v  Velocity[Y]            -3.4533           7.104       0.0014971       0.0014971
v  Velocity[Z]       -1.2685e-014     1.1765e-014    -8.1994e-018    -8.1994e-018
v  ǁVelocityǁ        0.00086463          10.449          5.2518          5.2518
v  Pressure               -53.481           19.83         -8.3612         -8.3612
v  nu_tilda           4.3262e-007       0.0042695       0.0011525       0.0011525
v  TempC                       21          73.469          21.727          21.727
v  TurbVisc           3.0815e-014        0.005032       0.0013502       0.0013502
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1073:        0.21950E+01

===============================================================


 INSTANT    0.107400000E+04   TIME STEP NUMBER            1074
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53490E-02 0.88477E+00
   Friction velocity        uk    :  0.53490E-02 0.88477E+00
   Dimensionless distance   yplus :  0.43063E-01 0.71230E+01
   Friction thermal sca.    tstar : -0.61698E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32130E-01 0.53146E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79181E-02      32   0.33660E-03   0.19175E+01 0.93991E+02 
c  Velocity[X]                                      0.10756E+01 
c  Velocity[Y]                                      0.84192E+00 
c  Velocity[Z]                                      0.11549E-29 
c  Pressure     0.10982E-06     488   0.93181E-08   0.11237E+00 0.78565E+03 
c  nu_tilda     0.52252E-05      31   0.15294E-04   0.19592E-06 0.12877E+03 
c  TempC        0.32060E+02      26   0.29046E-03   0.46291E+01 0.21425E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.277          10.448          4.5729          4.5729
v  Velocity[Y]            -3.4525          7.0842       0.0014835       0.0014835
v  Velocity[Z]       -1.2469e-014     1.0496e-014    -8.1885e-018    -8.1885e-018
v  ǁVelocityǁ         0.0011725          10.449          5.2519          5.2519
v  Pressure               -53.478          19.693         -8.4103         -8.4103
v  nu_tilda           4.3264e-007       0.0042695       0.0011531       0.0011531
v  TempC                       21          73.067          21.727          21.727
v  TurbVisc           3.0816e-014        0.005032        0.001351        0.001351
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1074:        0.23120E+01

===============================================================


 INSTANT    0.107500000E+04   TIME STEP NUMBER            1075
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10140E-01 0.88395E+00
   Friction velocity        uk    :  0.10140E-01 0.88395E+00
   Dimensionless distance   yplus :  0.81638E-01 0.71164E+01
   Friction thermal sca.    tstar : -0.62708E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60911E-01 0.53096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79211E-02      32   0.32867E-03   0.19274E+01 0.93999E+02 
c  Velocity[X]                                      0.10915E+01 
c  Velocity[Y]                                      0.83589E+00 
c  Velocity[Z]                                      0.14914E-29 
c  Pressure     0.12664E-06     472   0.99737E-08   0.12524E+00 0.52991E+03 
c  nu_tilda     0.52268E-05      31   0.70644E-05   0.19604E-06 0.12880E+03 
c  TempC        0.32071E+02      26   0.51167E-03   0.43635E+01 0.21398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2754          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4512          7.1071       0.0014697       0.0014697
v  Velocity[Z]       -1.2469e-014      1.015e-014    -8.1705e-018    -8.1705e-018
v  ǁVelocityǁ         0.0012139          10.449           5.252           5.252
v  Pressure               -53.452          19.771         -8.3889         -8.3889
v  nu_tilda           4.3262e-007       0.0042695       0.0011537       0.0011537
v  TempC                       21          73.066          21.728          21.728
v  TurbVisc           3.0822e-014        0.005032       0.0013517       0.0013517
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1075:        0.24520E+01

===============================================================


 INSTANT    0.107600000E+04   TIME STEP NUMBER            1076
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10468E-01 0.88549E+00
   Friction velocity        uk    :  0.10468E-01 0.88549E+00
   Dimensionless distance   yplus :  0.84278E-01 0.71288E+01
   Friction thermal sca.    tstar : -0.62875E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62881E-01 0.53189E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79242E-02      32   0.30807E-03   0.19028E+01 0.93924E+02 
c  Velocity[X]                                      0.10468E+01 
c  Velocity[Y]                                      0.85599E+00 
c  Velocity[Z]                                      0.14873E-29 
c  Pressure     0.93671E-07     425   0.94040E-08   0.94534E-01 0.21517E+03 
c  nu_tilda     0.52285E-05      31   0.15304E-04   0.19617E-06 0.12882E+03 
c  TempC        0.32082E+02      27   0.38533E-03   0.73186E+01 0.29019E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2738          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4498          7.1125       0.0014561       0.0014561
v  Velocity[Z]       -1.2349e-014     1.1184e-014    -8.1527e-018    -8.1527e-018
v  ǁVelocityǁ        0.00084818          10.449          5.2522          5.2522
v  Pressure               -53.451          19.784         -8.4066         -8.4066
v  nu_tilda           4.3253e-007       0.0042695       0.0011543       0.0011543
v  TempC                       21          73.067          21.728          21.728
v  TurbVisc           3.0818e-014        0.005032       0.0013525       0.0013525
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1076:        0.20690E+01

===============================================================


 INSTANT    0.107700000E+04   TIME STEP NUMBER            1077
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45990E-02 0.88503E+00
   Friction velocity        uk    :  0.45990E-02 0.88503E+00
   Dimensionless distance   yplus :  0.37025E-01 0.71251E+01
   Friction thermal sca.    tstar : -0.61586E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27625E-01 0.53161E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79272E-02      32   0.29599E-03   0.19150E+01 0.93969E+02 
c  Velocity[X]                                      0.10702E+01 
c  Velocity[Y]                                      0.84482E+00 
c  Velocity[Z]                                      0.12665E-29 
c  Pressure     0.11086E-06     442   0.93251E-08   0.11402E+00 0.38233E+03 
c  nu_tilda     0.52302E-05      31   0.70517E-05   0.19629E-06 0.12885E+03 
c  TempC        0.32092E+02      26   0.37664E-03   0.53162E+01 0.23306E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2722          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4486          7.0905       0.0014424       0.0014424
v  Velocity[Z]       -1.2476e-014     1.0211e-014    -8.1384e-018    -8.1384e-018
v  ǁVelocityǁ         0.0014774           10.45          5.2523          5.2523
v  Pressure               -53.422          19.684         -8.4226         -8.4226
v  nu_tilda           4.3251e-007       0.0042695        0.001155        0.001155
v  TempC                       21          73.319          21.729          21.729
v  TurbVisc            3.079e-014        0.005032       0.0013532       0.0013532
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1077:        0.20780E+01

===============================================================


 INSTANT    0.107800000E+04   TIME STEP NUMBER            1078
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12329E-01 0.88371E+00
   Friction velocity        uk    :  0.12329E-01 0.88371E+00
   Dimensionless distance   yplus :  0.99255E-01 0.71145E+01
   Friction thermal sca.    tstar : -0.62828E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74055E-01 0.53082E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79303E-02      32   0.36796E-03   0.19174E+01 0.94029E+02 
c  Velocity[X]                                      0.10787E+01 
c  Velocity[Y]                                      0.83869E+00 
c  Velocity[Z]                                      0.14400E-29 
c  Pressure     0.12110E-06     425   0.90813E-08   0.12084E+00 0.18671E+03 
c  nu_tilda     0.52318E-05      31   0.15325E-04   0.19643E-06 0.12887E+03 
c  TempC        0.32103E+02      26   0.32987E-03   0.46767E+01 0.21993E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2705          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4478          7.1052       0.0014291       0.0014291
v  Velocity[Z]       -1.2538e-014     9.8056e-015    -8.1311e-018    -8.1311e-018
v  ǁVelocityǁ        0.00095674           10.45          5.2524          5.2524
v  Pressure               -53.421          19.714         -8.4371         -8.4371
v  nu_tilda            4.325e-007       0.0042695       0.0011556       0.0011556
v  TempC                       21          73.312          21.729          21.729
v  TurbVisc           3.0785e-014        0.005032        0.001354        0.001354
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1078:        0.20270E+01

===============================================================


 INSTANT    0.107900000E+04   TIME STEP NUMBER            1079
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76675E-02 0.88488E+00
   Friction velocity        uk    :  0.76675E-02 0.88488E+00
   Dimensionless distance   yplus :  0.61729E-01 0.71239E+01
   Friction thermal sca.    tstar : -0.62435E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46057E-01 0.53152E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79333E-02      32   0.35013E-03   0.19700E+01 0.94601E+02 
c  Velocity[X]                                      0.11086E+01 
c  Velocity[Y]                                      0.86146E+00 
c  Velocity[Z]                                      0.14107E-29 
c  Pressure     0.13200E-06     345   0.93054E-08   0.13513E+00 0.26831E+03 
c  nu_tilda     0.52335E-05      31   0.70465E-05   0.19655E-06 0.12890E+03 
c  TempC        0.32114E+02      26   0.34099E-03   0.44105E+01 0.20523E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2688          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4465          7.0862       0.0014153       0.0014153
v  Velocity[Z]       -1.2682e-014     1.0621e-014    -8.1149e-018    -8.1149e-018
v  ǁVelocityǁ         0.0010085           10.45          5.2525          5.2525
v  Pressure               -53.393           19.66         -8.4414         -8.4414
v  nu_tilda           4.3254e-007       0.0042695       0.0011562       0.0011562
v  TempC                       21          73.066          21.729          21.729
v  TurbVisc           3.0784e-014        0.005032       0.0013547       0.0013547
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1079:        0.18350E+01

===============================================================


 INSTANT    0.108000000E+04   TIME STEP NUMBER            1080
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84512E-02 0.88432E+00
   Friction velocity        uk    :  0.84512E-02 0.88432E+00
   Dimensionless distance   yplus :  0.68038E-01 0.71194E+01
   Friction thermal sca.    tstar : -0.64038E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50764E-01 0.53118E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79364E-02      32   0.27488E-03   0.19191E+01 0.94149E+02 
c  Velocity[X]                                      0.10717E+01 
c  Velocity[Y]                                      0.84735E+00 
c  Velocity[Z]                                      0.13408E-29 
c  Pressure     0.96711E-07     392   0.92404E-08   0.96667E-01 0.26763E+03 
c  nu_tilda     0.52351E-05      31   0.15318E-04   0.19670E-06 0.12893E+03 
c  TempC        0.32125E+02      26   0.40858E-03   0.42402E+01 0.20150E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2671          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4451          7.1102       0.0014022       0.0014022
v  Velocity[Z]       -1.1979e-014     9.8173e-015    -8.0873e-018    -8.0873e-018
v  ǁVelocityǁ         0.0009072           10.45          5.2527          5.2527
v  Pressure               -53.387          19.742         -8.4397         -8.4397
v  nu_tilda           4.3256e-007       0.0042695       0.0011568       0.0011568
v  TempC                       21          73.066           21.73           21.73
v  TurbVisc           3.0794e-014        0.005032       0.0013555       0.0013555
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1080:        0.19680E+01

===============================================================


 INSTANT    0.108100000E+04   TIME STEP NUMBER            1081
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89546E-02 0.88553E+00
   Friction velocity        uk    :  0.89546E-02 0.88553E+00
   Dimensionless distance   yplus :  0.72091E-01 0.71291E+01
   Friction thermal sca.    tstar : -0.62485E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53788E-01 0.53191E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79394E-02      32   0.34149E-03   0.18770E+01 0.93838E+02 
c  Velocity[X]                                      0.10357E+01 
c  Velocity[Y]                                      0.84135E+00 
c  Velocity[Z]                                      0.14295E-29 
c  Pressure     0.93349E-07     312   0.94005E-08   0.94038E-01 0.20901E+03 
c  nu_tilda     0.52368E-05      31   0.70422E-05   0.19684E-06 0.12896E+03 
c  TempC        0.32136E+02      27   0.37507E-03   0.40214E+01 0.20335E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2653          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4437          7.1224       0.0013889       0.0013889
v  Velocity[Z]        -1.207e-014      1.019e-014    -8.0633e-018    -8.0633e-018
v  ǁVelocityǁ        0.00083278           10.45          5.2528          5.2528
v  Pressure               -53.365          19.737         -8.4428         -8.4428
v  nu_tilda           4.3253e-007       0.0042695       0.0011575       0.0011575
v  TempC                       21          73.237           21.73           21.73
v  TurbVisc             3.08e-014        0.005032       0.0013562       0.0013562
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1081:        0.17660E+01

===============================================================


 INSTANT    0.108200000E+04   TIME STEP NUMBER            1082
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31141E-02 0.88517E+00
   Friction velocity        uk    :  0.31141E-02 0.88517E+00
   Dimensionless distance   yplus :  0.25071E-01 0.71262E+01
   Friction thermal sca.    tstar : -0.62240E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18706E-01 0.53169E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79425E-02      32   0.32879E-03   0.19421E+01 0.94424E+02 
c  Velocity[X]                                      0.10790E+01 
c  Velocity[Y]                                      0.86305E+00 
c  Velocity[Z]                                      0.12301E-29 
c  Pressure     0.11671E-06     473   0.96959E-08   0.11885E+00 0.72941E+03 
c  nu_tilda     0.52384E-05      31   0.15327E-04   0.19699E-06 0.12899E+03 
c  TempC        0.32147E+02      27   0.46202E-03   0.39052E+01 0.18949E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2634          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4424          7.0903       0.0013755       0.0013755
v  Velocity[Z]       -1.1485e-014     9.8532e-015    -8.0414e-018    -8.0414e-018
v  ǁVelocityǁ         0.0012752           10.45          5.2529          5.2529
v  Pressure                -53.36          19.603         -8.4862         -8.4862
v  nu_tilda           4.3254e-007       0.0042695       0.0011581       0.0011581
v  TempC                       21          73.067           21.73           21.73
v  TurbVisc            3.079e-014        0.005032        0.001357        0.001357
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1082:        0.21860E+01

===============================================================


 INSTANT    0.108300000E+04   TIME STEP NUMBER            1083
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10986E-01 0.88384E+00
   Friction velocity        uk    :  0.10986E-01 0.88384E+00
   Dimensionless distance   yplus :  0.88443E-01 0.71155E+01
   Friction thermal sca.    tstar : -0.63581E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65989E-01 0.53090E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79455E-02      32   0.31397E-03   0.19235E+01 0.94313E+02 
c  Velocity[X]                                      0.10722E+01 
c  Velocity[Y]                                      0.85137E+00 
c  Velocity[Z]                                      0.13958E-29 
c  Pressure     0.10715E-06     457   0.91899E-08   0.10728E+00 0.60230E+03 
c  nu_tilda     0.52401E-05      31   0.70347E-05   0.19714E-06 0.12902E+03 
c  TempC        0.32157E+02      28   0.38225E-03   0.52361E+01 0.21868E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2619          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4406          7.1123       0.0013623       0.0013623
v  Velocity[Z]       -1.1725e-014     1.0257e-014    -8.0133e-018    -8.0133e-018
v  ǁVelocityǁ         0.0011113           10.45           5.253           5.253
v  Pressure               -53.332          19.702         -8.4613         -8.4613
v  nu_tilda           4.3252e-007       0.0042695       0.0011588       0.0011588
v  TempC                       21          73.067          21.731          21.731
v  TurbVisc           3.0793e-014        0.005032       0.0013577       0.0013577
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1083:        0.21130E+01

===============================================================


 INSTANT    0.108400000E+04   TIME STEP NUMBER            1084
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95855E-02 0.88515E+00
   Friction velocity        uk    :  0.95855E-02 0.88515E+00
   Dimensionless distance   yplus :  0.77170E-01 0.71261E+01
   Friction thermal sca.    tstar : -0.63699E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57577E-01 0.53169E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79485E-02      32   0.34427E-03   0.19277E+01 0.94415E+02 
c  Velocity[X]                                      0.10808E+01 
c  Velocity[Y]                                      0.84689E+00 
c  Velocity[Z]                                      0.15603E-29 
c  Pressure     0.12343E-06     458   0.93282E-08   0.12591E+00 0.56839E+03 
c  nu_tilda     0.52418E-05      31   0.15345E-04   0.19728E-06 0.12904E+03 
c  TempC        0.32168E+02      26   0.43858E-03   0.46037E+01 0.22986E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2603          10.449          4.5729          4.5729
v  Velocity[Y]            -3.4393          7.0915       0.0013492       0.0013492
v  Velocity[Z]       -1.1323e-014     9.8323e-015    -7.9914e-018    -7.9914e-018
v  ǁVelocityǁ        0.00088598           10.45          5.2532          5.2532
v  Pressure               -53.329          19.615         -8.4984         -8.4984
v  nu_tilda            4.325e-007       0.0042695       0.0011593       0.0011593
v  TempC                       21          73.413          21.731          21.731
v  TurbVisc           3.0787e-014        0.005032       0.0013584       0.0013584
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1084:        0.21120E+01

===============================================================


 INSTANT    0.108500000E+04   TIME STEP NUMBER            1085
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62964E-02 0.88412E+00
   Friction velocity        uk    :  0.62964E-02 0.88412E+00
   Dimensionless distance   yplus :  0.50690E-01 0.71178E+01
   Friction thermal sca.    tstar : -0.63688E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37821E-01 0.53107E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79516E-02      32   0.32225E-03   0.19490E+01 0.94643E+02 
c  Velocity[X]                                      0.10787E+01 
c  Velocity[Y]                                      0.87033E+00 
c  Velocity[Z]                                      0.13407E-29 
c  Pressure     0.12065E-06     425   0.96846E-08   0.11929E+00 0.42463E+03 
c  nu_tilda     0.52434E-05      31   0.70287E-05   0.19740E-06 0.12907E+03 
c  TempC        0.32179E+02      27   0.36773E-03   0.61697E+01 0.25182E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2586           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4379          7.1105        0.001336        0.001336
v  Velocity[Z]       -1.1247e-014     1.0226e-014    -7.9632e-018    -7.9632e-018
v  ǁVelocityǁ         0.0016038           10.45          5.2533          5.2533
v  Pressure                 -53.3           19.67         -8.4836         -8.4836
v  nu_tilda           4.3252e-007       0.0042695         0.00116         0.00116
v  TempC                       21          73.067          21.732          21.732
v  TurbVisc           3.0782e-014        0.005032       0.0013592       0.0013592
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1085:        0.20440E+01

===============================================================


 INSTANT    0.108600000E+04   TIME STEP NUMBER            1086
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13075E-01 0.88567E+00
   Friction velocity        uk    :  0.13075E-01 0.88567E+00
   Dimensionless distance   yplus :  0.10526E+00 0.71302E+01
   Friction thermal sca.    tstar : -0.63280E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78536E-01 0.53199E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79546E-02      32   0.28876E-03   0.19042E+01 0.94304E+02 
c  Velocity[X]                                      0.10483E+01 
c  Velocity[Y]                                      0.85588E+00 
c  Velocity[Z]                                      0.10816E-29 
c  Pressure     0.93412E-07     425   0.90232E-08   0.94611E-01 0.23536E+03 
c  nu_tilda     0.52451E-05      31   0.15342E-04   0.19754E-06 0.12910E+03 
c  TempC        0.32190E+02      26   0.30067E-03   0.50977E+01 0.22076E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2568           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4372          7.1194       0.0013229       0.0013229
v  Velocity[Z]       -1.1419e-014     9.8401e-015    -7.9392e-018    -7.9392e-018
v  ǁVelocityǁ        0.00088788           10.45          5.2534          5.2534
v  Pressure                 -53.3          19.676         -8.5028         -8.5028
v  nu_tilda           4.3251e-007       0.0042695       0.0011606       0.0011606
v  TempC                       21          73.067          21.732          21.732
v  TurbVisc           3.0789e-014        0.005032       0.0013599       0.0013599
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1086:        0.20450E+01

===============================================================


 INSTANT    0.108700000E+04   TIME STEP NUMBER            1087
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63353E-02 0.88519E+00
   Friction velocity        uk    :  0.63353E-02 0.88519E+00
   Dimensionless distance   yplus :  0.51003E-01 0.71264E+01
   Friction thermal sca.    tstar : -0.62699E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38054E-01 0.53171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79576E-02      32   0.35060E-03   0.19172E+01 0.94401E+02 
c  Velocity[X]                                      0.10670E+01 
c  Velocity[Y]                                      0.85020E+00 
c  Velocity[Z]                                      0.18140E-29 
c  Pressure     0.11011E-06     425   0.94910E-08   0.11269E+00 0.40986E+03 
c  nu_tilda     0.52467E-05      31   0.70250E-05   0.19767E-06 0.12912E+03 
c  TempC        0.32201E+02      26   0.41904E-03   0.33851E+01 0.17244E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.255           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4353          7.0959       0.0013101       0.0013101
v  Velocity[Z]        -1.136e-014     1.0285e-014    -7.9175e-018    -7.9175e-018
v  ǁVelocityǁ          0.001107           10.45          5.2535          5.2535
v  Pressure               -53.271          19.567         -8.5202         -8.5202
v  nu_tilda            4.325e-007       0.0042695       0.0011613       0.0011613
v  TempC                       21          73.332          21.732          21.732
v  TurbVisc           3.0785e-014        0.005032       0.0013607       0.0013607
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1087:        0.20460E+01

===============================================================


 INSTANT    0.108800000E+04   TIME STEP NUMBER            1088
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95822E-02 0.88399E+00
   Friction velocity        uk    :  0.95822E-02 0.88399E+00
   Dimensionless distance   yplus :  0.77143E-01 0.71167E+01
   Friction thermal sca.    tstar : -0.64808E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57557E-01 0.53099E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79606E-02      32   0.32101E-03   0.19392E+01 0.94667E+02 
c  Velocity[X]                                      0.10694E+01 
c  Velocity[Y]                                      0.86978E+00 
c  Velocity[Z]                                      0.15691E-29 
c  Pressure     0.11664E-06     378   0.91867E-08   0.11609E+00 0.23181E+03 
c  nu_tilda     0.52484E-05      31   0.15354E-04   0.19781E-06 0.12915E+03 
c  TempC        0.32212E+02      26   0.33997E-03   0.48332E+01 0.21760E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2532           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4335          7.1149       0.0012972       0.0012972
v  Velocity[Z]        -1.182e-014     9.8542e-015    -7.8867e-018    -7.8867e-018
v  ǁVelocityǁ        0.00071614          10.451          5.2536          5.2536
v  Pressure               -53.265          19.636         -8.5208         -8.5208
v  nu_tilda           4.3249e-007       0.0042695       0.0011618       0.0011618
v  TempC                       21          73.286          21.733          21.733
v  TurbVisc           3.0783e-014        0.005032       0.0013614       0.0013614
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1088:        0.19350E+01

===============================================================


 INSTANT    0.108900000E+04   TIME STEP NUMBER            1089
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57937E-02 0.88523E+00
   Friction velocity        uk    :  0.57937E-02 0.88523E+00
   Dimensionless distance   yplus :  0.46643E-01 0.71267E+01
   Friction thermal sca.    tstar : -0.63757E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34801E-01 0.53173E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79636E-02      32   0.29614E-03   0.19337E+01 0.94607E+02 
c  Velocity[X]                                      0.10735E+01 
c  Velocity[Y]                                      0.86018E+00 
c  Velocity[Z]                                      0.11363E-29 
c  Pressure     0.10813E-06     441   0.94863E-08   0.10917E+00 0.32739E+03 
c  nu_tilda     0.52501E-05      31   0.70018E-05   0.19795E-06 0.12918E+03 
c  TempC        0.32222E+02      26   0.52086E-03   0.44755E+01 0.21808E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2514           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4328          7.0925       0.0012843       0.0012843
v  Velocity[Z]       -1.1902e-014     1.0272e-014    -7.8693e-018    -7.8693e-018
v  ǁVelocityǁ        0.00083041           10.45          5.2537          5.2537
v  Pressure               -53.241           19.56         -8.5385         -8.5385
v  nu_tilda           4.3251e-007       0.0042695       0.0011625       0.0011625
v  TempC                       21          73.285          21.733          21.733
v  TurbVisc           3.0782e-014        0.005032       0.0013622       0.0013622
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1089:        0.20830E+01

===============================================================


 INSTANT    0.109000000E+04   TIME STEP NUMBER            1090
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35054E-02 0.88442E+00
   Friction velocity        uk    :  0.35054E-02 0.88442E+00
   Dimensionless distance   yplus :  0.28221E-01 0.71202E+01
   Friction thermal sca.    tstar : -0.64303E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21056E-01 0.53125E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79667E-02      32   0.34772E-03   0.19217E+01 0.94548E+02 
c  Velocity[X]                                      0.10664E+01 
c  Velocity[Y]                                      0.85522E+00 
c  Velocity[Z]                                      0.13943E-29 
c  Pressure     0.10747E-06     378   0.92051E-08   0.10802E+00 0.17250E+03 
c  nu_tilda     0.52517E-05      31   0.15370E-04   0.19810E-06 0.12921E+03 
c  TempC        0.32233E+02      27   0.38457E-03   0.73967E+01 0.29030E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2497           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4321          7.1152       0.0012712       0.0012712
v  Velocity[Z]       -1.1505e-014     9.8564e-015    -7.8442e-018    -7.8442e-018
v  ǁVelocityǁ           0.00141          10.451          5.2539          5.2539
v  Pressure               -53.239          19.597         -8.5483         -8.5483
v  nu_tilda           4.3247e-007       0.0042695       0.0011631       0.0011631
v  TempC                       21           73.56          21.733          21.733
v  TurbVisc           3.0786e-014        0.005032       0.0013629       0.0013629
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1090:        0.19220E+01

===============================================================


 INSTANT    0.109100000E+04   TIME STEP NUMBER            1091
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11809E-01 0.88577E+00
   Friction velocity        uk    :  0.11809E-01 0.88577E+00
   Dimensionless distance   yplus :  0.95073E-01 0.71310E+01
   Friction thermal sca.    tstar : -0.63880E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70935E-01 0.53205E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79697E-02      32   0.34941E-03   0.19252E+01 0.94742E+02 
c  Velocity[X]                                      0.10495E+01 
c  Velocity[Y]                                      0.87571E+00 
c  Velocity[Z]                                      0.13982E-29 
c  Pressure     0.97793E-07     426   0.98470E-08   0.99192E-01 0.45574E+03 
c  nu_tilda     0.52534E-05      31   0.70023E-05   0.19824E-06 0.12924E+03 
c  TempC        0.32244E+02      27   0.31093E-03   0.59815E+01 0.23123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.248           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4313           7.125       0.0012586       0.0012586
v  Velocity[Z]       -1.1983e-014     1.0261e-014    -7.8152e-018    -7.8152e-018
v  ǁVelocityǁ        0.00099646          10.451           5.254           5.254
v  Pressure               -53.209          19.657          -8.531          -8.531
v  nu_tilda           4.3243e-007       0.0042695       0.0011637       0.0011637
v  TempC                       21          73.067          21.734          21.734
v  TurbVisc           3.0774e-014        0.005032       0.0013636       0.0013636
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1091:        0.20390E+01

===============================================================


 INSTANT    0.109200000E+04   TIME STEP NUMBER            1092
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83352E-02 0.88520E+00
   Friction velocity        uk    :  0.83352E-02 0.88520E+00
   Dimensionless distance   yplus :  0.67104E-01 0.71265E+01
   Friction thermal sca.    tstar : -0.63640E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50067E-01 0.53172E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79727E-02      32   0.33092E-03   0.19666E+01 0.95108E+02 
c  Velocity[X]                                      0.11021E+01 
c  Velocity[Y]                                      0.86446E+00 
c  Velocity[Z]                                      0.13129E-29 
c  Pressure     0.12636E-06     489   0.94960E-08   0.12758E+00 0.10263E+04 
c  nu_tilda     0.52551E-05      31   0.15365E-04   0.19840E-06 0.12927E+03 
c  TempC        0.32255E+02      26   0.47470E-03   0.44906E+01 0.20649E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2463           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4292          7.0937       0.0012459       0.0012459
v  Velocity[Z]       -1.1895e-014     9.9157e-015    -7.7929e-018    -7.7929e-018
v  ǁVelocityǁ        0.00096777          10.451          5.2541          5.2541
v  Pressure               -53.204          19.456         -8.5902         -8.5902
v  nu_tilda           4.3251e-007       0.0042695       0.0011643       0.0011643
v  TempC                       21          73.067          21.734          21.734
v  TurbVisc           3.0763e-014        0.005032       0.0013644       0.0013644
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1092:        0.21920E+01

===============================================================


 INSTANT    0.109300000E+04   TIME STEP NUMBER            1093
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79682E-02 0.88426E+00
   Friction velocity        uk    :  0.79682E-02 0.88426E+00
   Dimensionless distance   yplus :  0.64149E-01 0.71189E+01
   Friction thermal sca.    tstar : -0.65332E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47862E-01 0.53115E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79757E-02      32   0.33234E-03   0.19656E+01 0.95092E+02 
c  Velocity[X]                                      0.11056E+01 
c  Velocity[Y]                                      0.85993E+00 
c  Velocity[Z]                                      0.15760E-29 
c  Pressure     0.12111E-06     490   0.97549E-08   0.12104E+00 0.79316E+03 
c  nu_tilda     0.52567E-05      31   0.69934E-05   0.19854E-06 0.12930E+03 
c  TempC        0.32266E+02      27   0.36400E-03   0.50470E+01 0.23104E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2445           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4279          7.1168       0.0012332       0.0012332
v  Velocity[Z]       -1.1933e-014     1.0325e-014     -7.764e-018     -7.764e-018
v  ǁVelocityǁ         0.0014559          10.451          5.2542          5.2542
v  Pressure               -53.178            19.6         -8.5549         -8.5549
v  nu_tilda           4.3254e-007       0.0042695        0.001165        0.001165
v  TempC                       21          73.208          21.735          21.735
v  TurbVisc           3.0786e-014        0.005032       0.0013651       0.0013651
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1093:        0.22020E+01

===============================================================


 INSTANT    0.109400000E+04   TIME STEP NUMBER            1094
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12208E-01 0.88556E+00
   Friction velocity        uk    :  0.12208E-01 0.88556E+00
   Dimensionless distance   yplus :  0.98287E-01 0.71294E+01
   Friction thermal sca.    tstar : -0.64454E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73333E-01 0.53193E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79787E-02      32   0.30617E-03   0.19554E+01 0.95108E+02 
c  Velocity[X]                                      0.10756E+01 
c  Velocity[Y]                                      0.87983E+00 
c  Velocity[Z]                                      0.11949E-29 
c  Pressure     0.10154E-06     458   0.99294E-08   0.10331E+00 0.76176E+03 
c  nu_tilda     0.52584E-05      31   0.15376E-04   0.19869E-06 0.12933E+03 
c  TempC        0.32276E+02      27   0.37613E-03   0.34777E+01 0.18726E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2426           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4269          7.0948       0.0012208       0.0012208
v  Velocity[Z]       -1.1835e-014     9.8706e-015    -7.7451e-018    -7.7451e-018
v  ǁVelocityǁ        0.00083144          10.451          5.2543          5.2543
v  Pressure               -53.175          19.473         -8.6031         -8.6031
v  nu_tilda           4.3253e-007       0.0042695       0.0011656       0.0011656
v  TempC                       21          73.067          21.735          21.735
v  TurbVisc           3.0794e-014        0.005032       0.0013659       0.0013659
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1094:        0.21250E+01

===============================================================


 INSTANT    0.109500000E+04   TIME STEP NUMBER            1095
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39286E-02 0.88484E+00
   Friction velocity        uk    :  0.39286E-02 0.88484E+00
   Dimensionless distance   yplus :  0.31628E-01 0.71236E+01
   Friction thermal sca.    tstar : -0.65439E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23598E-01 0.53150E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79817E-02      32   0.30356E-03   0.19289E+01 0.94859E+02 
c  Velocity[X]                                      0.10608E+01 
c  Velocity[Y]                                      0.86813E+00 
c  Velocity[Z]                                      0.14238E-29 
c  Pressure     0.10770E-06     456   0.93661E-08   0.10764E+00 0.61522E+03 
c  nu_tilda     0.52601E-05      31   0.69788E-05   0.19883E-06 0.12936E+03 
c  TempC        0.32287E+02      26   0.38499E-03   0.44913E+01 0.20742E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2408           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4242          7.1226       0.0012079       0.0012079
v  Velocity[Z]       -1.1972e-014     1.0294e-014    -7.7198e-018    -7.7198e-018
v  ǁVelocityǁ         0.0010724          10.451          5.2544          5.2544
v  Pressure               -53.148          19.577         -8.5773         -8.5773
v  nu_tilda           4.3251e-007       0.0042695       0.0011662       0.0011662
v  TempC                       21           73.18          21.735          21.735
v  TurbVisc           3.0792e-014        0.005032       0.0013666       0.0013666
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1095:        0.21120E+01

===============================================================


 INSTANT    0.109600000E+04   TIME STEP NUMBER            1096
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73702E-02 0.88616E+00
   Friction velocity        uk    :  0.73702E-02 0.88616E+00
   Dimensionless distance   yplus :  0.59336E-01 0.71342E+01
   Friction thermal sca.    tstar : -0.65046E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44271E-01 0.53229E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79847E-02      32   0.36359E-03   0.19236E+01 0.94832E+02 
c  Velocity[X]                                      0.10618E+01 
c  Velocity[Y]                                      0.86178E+00 
c  Velocity[Z]                                      0.16408E-29 
c  Pressure     0.10078E-06     442   0.94261E-08   0.10081E+00 0.41625E+03 
c  nu_tilda     0.52618E-05      31   0.15392E-04   0.19897E-06 0.12939E+03 
c  TempC        0.32298E+02      26   0.45541E-03   0.45838E+01 0.22509E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2388           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4234           7.127       0.0011957       0.0011957
v  Velocity[Z]       -1.1985e-014     9.8787e-015    -7.7042e-018    -7.7042e-018
v  ǁVelocityǁ        0.00073901          10.451          5.2545          5.2545
v  Pressure               -53.147          19.529         -8.6069         -8.6069
v  nu_tilda           4.3245e-007       0.0042695       0.0011668       0.0011668
v  TempC                       21          73.416          21.736          21.736
v  TurbVisc           3.0786e-014        0.005032       0.0013673       0.0013673
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1096:        0.20780E+01

===============================================================


 INSTANT    0.109700000E+04   TIME STEP NUMBER            1097
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58559E-02 0.88574E+00
   Friction velocity        uk    :  0.58559E-02 0.88574E+00
   Dimensionless distance   yplus :  0.47144E-01 0.71308E+01
   Friction thermal sca.    tstar : -0.64449E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35175E-01 0.53204E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79877E-02      32   0.32452E-03   0.19843E+01 0.95414E+02 
c  Velocity[X]                                      0.10991E+01 
c  Velocity[Y]                                      0.88526E+00 
c  Velocity[Z]                                      0.12494E-29 
c  Pressure     0.13280E-06     297   0.98016E-08   0.13509E+00 0.30218E+03 
c  nu_tilda     0.52634E-05      31   0.69781E-05   0.19910E-06 0.12941E+03 
c  TempC        0.32309E+02      26   0.31388E-03   0.62263E+01 0.26602E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2371           10.45          4.5729          4.5729
v  Velocity[Y]            -3.4224          7.1003       0.0011829       0.0011829
v  Velocity[Z]        -1.209e-014     1.0353e-014    -7.6804e-018    -7.6804e-018
v  ǁVelocityǁ        0.00086784          10.451          5.2546          5.2546
v  Pressure               -53.114          19.471         -8.6081         -8.6081
v  nu_tilda           4.3247e-007       0.0042695       0.0011675       0.0011675
v  TempC                       21          73.067          21.736          21.736
v  TurbVisc           3.0768e-014        0.005032       0.0013681       0.0013681
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1097:        0.17290E+01

===============================================================


 INSTANT    0.109800000E+04   TIME STEP NUMBER            1098
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59611E-02 0.88461E+00
   Friction velocity        uk    :  0.59611E-02 0.88461E+00
   Dimensionless distance   yplus :  0.47991E-01 0.71217E+01
   Friction thermal sca.    tstar : -0.65821E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35807E-01 0.53136E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79906E-02      32   0.29088E-03   0.19431E+01 0.95124E+02 
c  Velocity[X]                                      0.10710E+01 
c  Velocity[Y]                                      0.87218E+00 
c  Velocity[Z]                                      0.11336E-29 
c  Pressure     0.10051E-06     282   0.99806E-08   0.10078E+00 0.19591E+03 
c  nu_tilda     0.52651E-05      31   0.15394E-04   0.19925E-06 0.12944E+03 
c  TempC        0.32320E+02      26   0.38835E-03   0.36646E+01 0.20010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2354          10.451          4.5729          4.5729
v  Velocity[Y]             -3.421          7.1216       0.0011706       0.0011706
v  Velocity[Z]       -1.1807e-014     9.9149e-015    -7.6621e-018    -7.6621e-018
v  ǁVelocityǁ         0.0015741          10.451          5.2547          5.2547
v  Pressure               -53.112           19.53         -8.6166         -8.6166
v  nu_tilda           4.3252e-007       0.0042695       0.0011681       0.0011681
v  TempC                       21          73.067          21.736          21.736
v  TurbVisc           3.0776e-014        0.005032       0.0013688       0.0013688
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1098:        0.16940E+01

===============================================================


 INSTANT    0.109900000E+04   TIME STEP NUMBER            1099
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12930E-01 0.88556E+00
   Friction velocity        uk    :  0.12930E-01 0.88556E+00
   Dimensionless distance   yplus :  0.10410E+00 0.71294E+01
   Friction thermal sca.    tstar : -0.65036E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77667E-01 0.53193E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79936E-02      32   0.35821E-03   0.19489E+01 0.95170E+02 
c  Velocity[X]                                      0.10822E+01 
c  Velocity[Y]                                      0.86673E+00 
c  Velocity[Z]                                      0.17380E-29 
c  Pressure     0.12284E-06     457   0.90765E-08   0.12343E+00 0.45556E+03 
c  nu_tilda     0.52668E-05      31   0.69677E-05   0.19939E-06 0.12947E+03 
c  TempC        0.32330E+02      26   0.33960E-03   0.43186E+01 0.19525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2335          10.451          4.5729          4.5729
v  Velocity[Y]            -3.4189          7.0983        0.001158        0.001158
v  Velocity[Z]        -1.166e-014     1.0338e-014    -7.6444e-018    -7.6444e-018
v  ǁVelocityǁ        0.00087943          10.451          5.2548          5.2548
v  Pressure               -53.085          19.416         -8.6398         -8.6398
v  nu_tilda           4.3255e-007       0.0042695       0.0011687       0.0011687
v  TempC                       21          73.067          21.737          21.737
v  TurbVisc           3.0789e-014        0.005032       0.0013696       0.0013696
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1099:        0.21230E+01

===============================================================


 INSTANT    0.110000000E+04   TIME STEP NUMBER            1100
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62929E-02 0.88502E+00
   Friction velocity        uk    :  0.62929E-02 0.88502E+00
   Dimensionless distance   yplus :  0.50662E-01 0.71250E+01
   Friction thermal sca.    tstar : -0.67004E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37799E-01 0.53160E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79966E-02      32   0.30202E-03   0.19621E+01 0.95395E+02 
c  Velocity[X]                                      0.10765E+01 
c  Velocity[Y]                                      0.88561E+00 
c  Velocity[Z]                                      0.13593E-29 
c  Pressure     0.10834E-06     408   0.96218E-08   0.10921E+00 0.26342E+03 
c  nu_tilda     0.52684E-05      31   0.15401E-04   0.19955E-06 0.12951E+03 
c  TempC        0.32341E+02      26   0.52600E-03   0.46194E+01 0.23118E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2317          10.451          4.5729          4.5729
v  Velocity[Y]            -3.4177            7.12       0.0011453       0.0011453
v  Velocity[Z]       -1.1689e-014     9.8945e-015    -7.6225e-018    -7.6225e-018
v  ǁVelocityǁ         0.0010956          10.452          5.2549          5.2549
v  Pressure               -53.083          19.498         -8.6398         -8.6398
v  nu_tilda           4.3254e-007       0.0042695       0.0011693       0.0011693
v  TempC                       21          73.238          21.737          21.737
v  TurbVisc           3.0797e-014        0.005032       0.0013703       0.0013703
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1100:        0.19960E+01

===============================================================


 INSTANT    0.110100000E+04   TIME STEP NUMBER            1101
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55989E-02 0.88627E+00
   Friction velocity        uk    :  0.55989E-02 0.88627E+00
   Dimensionless distance   yplus :  0.45075E-01 0.71350E+01
   Friction thermal sca.    tstar : -0.65482E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33631E-01 0.53235E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79996E-02      32   0.34450E-03   0.19248E+01 0.95119E+02 
c  Velocity[X]                                      0.10498E+01 
c  Velocity[Y]                                      0.87492E+00 
c  Velocity[Z]                                      0.10749E-29 
c  Pressure     0.87105E-07     440   0.92435E-08   0.87719E-01 0.39127E+03 
c  nu_tilda     0.52701E-05      31   0.69573E-05   0.19970E-06 0.12954E+03 
c  TempC        0.32352E+02      26   0.35622E-03   0.92624E+01 0.32207E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2298          10.451          4.5729          4.5729
v  Velocity[Y]            -3.4161          7.1316       0.0011331       0.0011331
v  Velocity[Z]       -1.1568e-014     1.0325e-014    -7.5996e-018    -7.5996e-018
v  ǁVelocityǁ         0.0012693          10.452           5.255           5.255
v  Pressure               -53.053          19.538          -8.626          -8.626
v  nu_tilda           4.3246e-007       0.0042695         0.00117         0.00117
v  TempC                       21          73.156          21.738          21.738
v  TurbVisc           3.0796e-014        0.005032        0.001371        0.001371
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1101:        0.20740E+01

===============================================================


 INSTANT    0.110200000E+04   TIME STEP NUMBER            1102
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10974E-01 0.88585E+00
   Friction velocity        uk    :  0.10974E-01 0.88585E+00
   Dimensionless distance   yplus :  0.88347E-01 0.71317E+01
   Friction thermal sca.    tstar : -0.64779E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65917E-01 0.53211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80026E-02      32   0.32991E-03   0.19805E+01 0.95617E+02 
c  Velocity[X]                                      0.11073E+01 
c  Velocity[Y]                                      0.87317E+00 
c  Velocity[Z]                                      0.15210E-29 
c  Pressure     0.13022E-06     485   0.91792E-08   0.13108E+00 0.11058E+04 
c  nu_tilda     0.52718E-05      31   0.15415E-04   0.19987E-06 0.12957E+03 
c  TempC        0.32363E+02      26   0.41824E-03   0.46606E+01 0.22301E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2279          10.451          4.5729          4.5729
v  Velocity[Y]            -3.4144          7.1021       0.0011209       0.0011209
v  Velocity[Z]        -1.139e-014     9.9737e-015     -7.586e-018     -7.586e-018
v  ǁVelocityǁ        0.00082421          10.452          5.2551          5.2551
v  Pressure               -53.049          19.321         -8.6904         -8.6904
v  nu_tilda           4.3247e-007       0.0042695       0.0011706       0.0011706
v  TempC                       21          73.067          21.738          21.738
v  TurbVisc           3.0772e-014        0.005032       0.0013718       0.0013718
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1102:        0.21880E+01

===============================================================


 INSTANT    0.110300000E+04   TIME STEP NUMBER            1103
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37179E-02 0.88503E+00
   Friction velocity        uk    :  0.37179E-02 0.88503E+00
   Dimensionless distance   yplus :  0.29931E-01 0.71251E+01
   Friction thermal sca.    tstar : -0.67590E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22332E-01 0.53161E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80055E-02      32   0.29862E-03   0.19655E+01 0.95562E+02 
c  Velocity[X]                                      0.10739E+01 
c  Velocity[Y]                                      0.89154E+00 
c  Velocity[Z]                                      0.12141E-29 
c  Pressure     0.10687E-06     488   0.96668E-08   0.10719E+00 0.10261E+04 
c  nu_tilda     0.52735E-05      31   0.69555E-05   0.20001E-06 0.12961E+03 
c  TempC        0.32373E+02      26   0.34835E-03   0.54908E+01 0.23355E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2259          10.451          4.5729          4.5729
v  Velocity[Y]            -3.4125          7.1233       0.0011084       0.0011084
v  Velocity[Z]       -1.1207e-014     1.0388e-014    -7.5633e-018    -7.5633e-018
v  ǁVelocityǁ        0.00075998          10.452          5.2552          5.2552
v  Pressure               -53.023          19.524         -8.6426         -8.6426
v  nu_tilda           4.3251e-007       0.0042695       0.0011712       0.0011712
v  TempC                       21          73.067          21.738          21.738
v  TurbVisc           3.0775e-014        0.005032       0.0013725       0.0013725
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1103:        0.22040E+01

===============================================================


 INSTANT    0.110400000E+04   TIME STEP NUMBER            1104
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23010E-02 0.88598E+00
   Friction velocity        uk    :  0.23010E-02 0.88598E+00
   Dimensionless distance   yplus :  0.18524E-01 0.71328E+01
   Friction thermal sca.    tstar : -0.66075E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13821E-01 0.53218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80085E-02      32   0.29638E-03   0.19528E+01 0.95482E+02 
c  Velocity[X]                                      0.10723E+01 
c  Velocity[Y]                                      0.88043E+00 
c  Velocity[Z]                                      0.11744E-29 
c  Pressure     0.90655E-07     473   0.93527E-08   0.92213E-01 0.92772E+03 
c  nu_tilda     0.52752E-05      31   0.15413E-04   0.20017E-06 0.12964E+03 
c  TempC        0.32384E+02      26   0.30204E-03   0.53787E+01 0.23683E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2239          10.451          4.5729          4.5729
v  Velocity[Y]             -3.411          7.1025       0.0010963       0.0010963
v  Velocity[Z]       -1.1016e-014     9.9171e-015    -7.5471e-018    -7.5471e-018
v  ǁVelocityǁ        0.00096515          10.452          5.2553          5.2553
v  Pressure                -53.02          19.353         -8.6986         -8.6986
v  nu_tilda           4.3254e-007       0.0042695       0.0011718       0.0011718
v  TempC                       21          73.347          21.739          21.739
v  TurbVisc           3.0785e-014        0.005032       0.0013732       0.0013732
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1104:        0.21490E+01

===============================================================


 INSTANT    0.110500000E+04   TIME STEP NUMBER            1105
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79944E-02 0.88519E+00
   Friction velocity        uk    :  0.79944E-02 0.88519E+00
   Dimensionless distance   yplus :  0.64361E-01 0.71264E+01
   Friction thermal sca.    tstar : -0.67154E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48020E-01 0.53171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80115E-02      32   0.35898E-03   0.19509E+01 0.95435E+02 
c  Velocity[X]                                      0.10775E+01 
c  Velocity[Y]                                      0.87335E+00 
c  Velocity[Z]                                      0.14842E-29 
c  Pressure     0.13123E-06     473   0.92625E-08   0.12982E+00 0.65649E+03 
c  nu_tilda     0.52768E-05      31   0.69555E-05   0.20030E-06 0.12967E+03 
c  TempC        0.32395E+02      26   0.52237E-03   0.50464E+01 0.23199E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2223          10.451          4.5729          4.5729
v  Velocity[Y]            -3.4094          7.1245        0.001084        0.001084
v  Velocity[Z]        -1.095e-014     1.0358e-014    -7.5242e-018    -7.5242e-018
v  ǁVelocityǁ         0.0009769          10.452          5.2554          5.2554
v  Pressure               -52.989          19.458         -8.6685         -8.6685
v  nu_tilda           4.3252e-007       0.0042695       0.0011725       0.0011725
v  TempC                       21          73.067          21.739          21.739
v  TurbVisc           3.0794e-014        0.005032        0.001374        0.001374
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1105:        0.22980E+01

===============================================================


 INSTANT    0.110600000E+04   TIME STEP NUMBER            1106
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81944E-02 0.88666E+00
   Friction velocity        uk    :  0.81944E-02 0.88666E+00
   Dimensionless distance   yplus :  0.65970E-01 0.71382E+01
   Friction thermal sca.    tstar : -0.66362E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49221E-01 0.53259E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80144E-02      32   0.30828E-03   0.19755E+01 0.95812E+02 
c  Velocity[X]                                      0.10819E+01 
c  Velocity[Y]                                      0.89362E+00 
c  Velocity[Z]                                      0.12500E-29 
c  Pressure     0.11122E-06     425   0.93369E-08   0.11233E+00 0.30342E+03 
c  nu_tilda     0.52785E-05      31   0.15422E-04   0.20045E-06 0.12970E+03 
c  TempC        0.32406E+02      27   0.37264E-03   0.81796E+01 0.30695E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2204          10.452          4.5729          4.5729
v  Velocity[Y]             -3.408          7.1321       0.0010719       0.0010719
v  Velocity[Z]       -1.0773e-014     9.9167e-015    -7.5104e-018    -7.5104e-018
v  ǁVelocityǁ         0.0014008          10.452          5.2555          5.2555
v  Pressure               -52.989          19.448         -8.6934         -8.6934
v  nu_tilda           4.3243e-007       0.0042695        0.001173        0.001173
v  TempC                       21          73.112           21.74           21.74
v  TurbVisc           3.0788e-014        0.005032       0.0013747       0.0013747
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1106:        0.22150E+01

===============================================================


 INSTANT    0.110700000E+04   TIME STEP NUMBER            1107
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11892E-01 0.88619E+00
   Friction velocity        uk    :  0.11892E-01 0.88619E+00
   Dimensionless distance   yplus :  0.95740E-01 0.71345E+01
   Friction thermal sca.    tstar : -0.65712E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71432E-01 0.53231E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80174E-02      32   0.28311E-03   0.19687E+01 0.95718E+02 
c  Velocity[X]                                      0.10830E+01 
c  Velocity[Y]                                      0.88571E+00 
c  Velocity[Z]                                      0.13950E-29 
c  Pressure     0.96879E-07     409   0.96956E-08   0.98318E-01 0.36241E+03 
c  nu_tilda     0.52802E-05      31   0.69335E-05   0.20060E-06 0.12973E+03 
c  TempC        0.32416E+02      27   0.26781E-03   0.50244E+01 0.21984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2185          10.452          4.5729          4.5729
v  Velocity[Y]            -3.4054          7.1087       0.0010595       0.0010595
v  Velocity[Z]        -1.073e-014     1.0415e-014    -7.4934e-018    -7.4934e-018
v  ǁVelocityǁ         0.0008157          10.452          5.2556          5.2556
v  Pressure               -52.959          19.354         -8.7059         -8.7059
v  nu_tilda           4.3241e-007       0.0042695       0.0011737       0.0011737
v  TempC                       21          73.067           21.74           21.74
v  TurbVisc           3.0763e-014        0.005032       0.0013755       0.0013755
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1107:        0.19350E+01

===============================================================


 INSTANT    0.110800000E+04   TIME STEP NUMBER            1108
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26582E-02 0.88494E+00
   Friction velocity        uk    :  0.26582E-02 0.88494E+00
   Dimensionless distance   yplus :  0.21400E-01 0.71244E+01
   Friction thermal sca.    tstar : -0.68002E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15967E-01 0.53156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80204E-02      32   0.34659E-03   0.19569E+01 0.95621E+02 
c  Velocity[X]                                      0.10798E+01 
c  Velocity[Y]                                      0.87715E+00 
c  Velocity[Z]                                      0.15084E-29 
c  Pressure     0.11750E-06     377   0.92044E-08   0.11654E+00 0.18699E+03 
c  nu_tilda     0.52819E-05      31   0.15443E-04   0.20076E-06 0.12976E+03 
c  TempC        0.32427E+02      26   0.45837E-03   0.26808E+01 0.16219E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2166          10.452          4.5729          4.5729
v  Velocity[Y]            -3.4039           7.125       0.0010478       0.0010478
v  Velocity[Z]       -1.0518e-014     9.9706e-015    -7.4745e-018    -7.4745e-018
v  ǁVelocityǁ         0.0012849          10.452          5.2557          5.2557
v  Pressure               -52.953          19.392         -8.7171         -8.7171
v  nu_tilda           4.3243e-007       0.0042695       0.0011743       0.0011743
v  TempC                       21          73.067           21.74           21.74
v  TurbVisc           3.0759e-014        0.005032       0.0013762       0.0013762
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1108:        0.18540E+01

===============================================================


 INSTANT    0.110900000E+04   TIME STEP NUMBER            1109
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59081E-02 0.88622E+00
   Friction velocity        uk    :  0.59081E-02 0.88622E+00
   Dimensionless distance   yplus :  0.47564E-01 0.71347E+01
   Friction thermal sca.    tstar : -0.66805E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35488E-01 0.53232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80233E-02      32   0.36524E-03   0.19691E+01 0.95772E+02 
c  Velocity[X]                                      0.10895E+01 
c  Velocity[Y]                                      0.87962E+00 
c  Velocity[Z]                                      0.12060E-29 
c  Pressure     0.10593E-06     360   0.96834E-08   0.10867E+00 0.25037E+03 
c  nu_tilda     0.52836E-05      31   0.69327E-05   0.20090E-06 0.12979E+03 
c  TempC        0.32438E+02      28   0.41149E-03   0.43969E+01 0.21938E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2147          10.452          4.5729          4.5729
v  Velocity[Y]            -3.4019          7.1072       0.0010353       0.0010353
v  Velocity[Z]       -1.0311e-014     1.0397e-014     -7.461e-018     -7.461e-018
v  ǁVelocityǁ         0.0010552          10.453          5.2558          5.2558
v  Pressure               -52.927          19.344         -8.7214         -8.7214
v  nu_tilda           4.3248e-007       0.0042695       0.0011749       0.0011749
v  TempC                       21          73.067          21.741          21.741
v  TurbVisc           3.0763e-014        0.005032       0.0013769       0.0013769
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1109:        0.18090E+01

===============================================================


 INSTANT    0.111000000E+04   TIME STEP NUMBER            1110
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81850E-02 0.88543E+00
   Friction velocity        uk    :  0.81850E-02 0.88543E+00
   Dimensionless distance   yplus :  0.65895E-01 0.71283E+01
   Friction thermal sca.    tstar : -0.67893E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49165E-01 0.53185E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80263E-02      32   0.37151E-03   0.19918E+01 0.96180E+02 
c  Velocity[X]                                      0.10919E+01 
c  Velocity[Y]                                      0.89987E+00 
c  Velocity[Z]                                      0.10299E-29 
c  Pressure     0.11854E-06     280   0.87920E-08   0.11893E+00 0.20697E+03 
c  nu_tilda     0.52852E-05      31   0.15436E-04   0.20107E-06 0.12982E+03 
c  TempC        0.32449E+02      27   0.42509E-03   0.50636E+01 0.23041E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2127          10.452          4.5729          4.5729
v  Velocity[Y]               -3.4            7.13       0.0010234       0.0010234
v  Velocity[Z]        -1.018e-014     9.9363e-015    -7.4433e-018    -7.4433e-018
v  ǁVelocityǁ         0.0008979          10.453          5.2559          5.2559
v  Pressure               -52.924          19.408         -8.7277         -8.7277
v  nu_tilda           4.3248e-007       0.0042695       0.0011755       0.0011755
v  TempC                       21          73.358          21.741          21.741
v  TurbVisc           3.0776e-014        0.005032       0.0013777       0.0013777
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1110:        0.16250E+01

===============================================================


 INSTANT    0.111100000E+04   TIME STEP NUMBER            1111
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69277E-02 0.88664E+00
   Friction velocity        uk    :  0.69277E-02 0.88664E+00
   Dimensionless distance   yplus :  0.55773E-01 0.71380E+01
   Friction thermal sca.    tstar : -0.66687E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41613E-01 0.53258E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80292E-02      32   0.29875E-03   0.19930E+01 0.96219E+02 
c  Velocity[X]                                      0.10882E+01 
c  Velocity[Y]                                      0.90479E+00 
c  Velocity[Z]                                      0.17149E-29 
c  Pressure     0.12225E-06     360   0.91381E-08   0.12092E+00 0.22955E+03 
c  nu_tilda     0.52869E-05      31   0.69317E-05   0.20123E-06 0.12986E+03 
c  TempC        0.32459E+02      26   0.37590E-03   0.60986E+01 0.25984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2106          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3983          7.1353       0.0010114       0.0010114
v  Velocity[Z]       -1.0058e-014     1.0434e-014    -7.4255e-018    -7.4255e-018
v  ǁVelocityǁ         0.0010575          10.453           5.256           5.256
v  Pressure               -52.897          19.378         -8.7319         -8.7319
v  nu_tilda           4.3242e-007       0.0042695       0.0011762       0.0011762
v  TempC                       21          73.068          21.741          21.741
v  TurbVisc           3.0776e-014        0.005032       0.0013784       0.0013784
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1111:        0.18090E+01

===============================================================


 INSTANT    0.111200000E+04   TIME STEP NUMBER            1112
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93908E-02 0.88643E+00
   Friction velocity        uk    :  0.93908E-02 0.88643E+00
   Dimensionless distance   yplus :  0.75602E-01 0.71364E+01
   Friction thermal sca.    tstar : -0.67374E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56408E-01 0.53245E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80322E-02      32   0.31938E-03   0.19765E+01 0.96035E+02 
c  Velocity[X]                                      0.10894E+01 
c  Velocity[Y]                                      0.88713E+00 
c  Velocity[Z]                                      0.14072E-29 
c  Pressure     0.10408E-06     441   0.96517E-08   0.10625E+00 0.62191E+03 
c  nu_tilda     0.52886E-05      31   0.15449E-04   0.20140E-06 0.12990E+03 
c  TempC        0.32470E+02      26   0.34935E-03   0.49713E+01 0.23971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2087          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3961          7.1096      0.00099927      0.00099927
v  Velocity[Z]       -1.0023e-014     9.9848e-015    -7.4091e-018    -7.4091e-018
v  ǁVelocityǁ        0.00083574          10.453          5.2561          5.2561
v  Pressure               -52.892          19.273         -8.7704         -8.7704
v  nu_tilda            4.324e-007       0.0042695       0.0011768       0.0011768
v  TempC                       21          73.068          21.742          21.742
v  TurbVisc           3.0761e-014        0.005032       0.0013791       0.0013791
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1112:        0.19990E+01

===============================================================


 INSTANT    0.111300000E+04   TIME STEP NUMBER            1113
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50402E-02 0.88523E+00
   Friction velocity        uk    :  0.50402E-02 0.88523E+00
   Dimensionless distance   yplus :  0.40577E-01 0.71267E+01
   Friction thermal sca.    tstar : -0.68380E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30275E-01 0.53173E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80351E-02      32   0.30785E-03   0.19869E+01 0.96193E+02 
c  Velocity[X]                                      0.10771E+01 
c  Velocity[Y]                                      0.90974E+00 
c  Velocity[Z]                                      0.11844E-29 
c  Pressure     0.10881E-06     472   0.96405E-08   0.10991E+00 0.74270E+03 
c  nu_tilda     0.52903E-05      31   0.69132E-05   0.20155E-06 0.12993E+03 
c  TempC        0.32481E+02      26   0.41806E-03   0.43038E+01 0.20466E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2069          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3936          7.1309      0.00098743      0.00098743
v  Velocity[Z]       -9.8976e-015     1.0415e-014    -7.3925e-018    -7.3925e-018
v  ǁVelocityǁ          0.001183          10.453          5.2562          5.2562
v  Pressure               -52.865          19.405         -8.7368         -8.7368
v  nu_tilda           4.3239e-007       0.0042695       0.0011774       0.0011774
v  TempC                       21          73.068          21.742          21.742
v  TurbVisc           3.0755e-014        0.005032       0.0013799       0.0013799
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1113:        0.20650E+01

===============================================================


 INSTANT    0.111400000E+04   TIME STEP NUMBER            1114
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10191E-01 0.88617E+00
   Friction velocity        uk    :  0.10191E-01 0.88617E+00
   Dimensionless distance   yplus :  0.82042E-01 0.71343E+01
   Friction thermal sca.    tstar : -0.66850E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61213E-01 0.53230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80380E-02      32   0.33233E-03   0.19945E+01 0.96205E+02 
c  Velocity[X]                                      0.11013E+01 
c  Velocity[Y]                                      0.89322E+00 
c  Velocity[Z]                                      0.16194E-29 
c  Pressure     0.12986E-06     490   0.91220E-08   0.13068E+00 0.97015E+03 
c  nu_tilda     0.52920E-05      31   0.15461E-04   0.20171E-06 0.12996E+03 
c  TempC        0.32491E+02      27   0.35842E-03   0.38092E+01 0.20596E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.205          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3915          7.1048      0.00097563      0.00097563
v  Velocity[Z]         -9.75e-015     9.9525e-015    -7.3782e-018    -7.3782e-018
v  ǁVelocityǁ         0.0011441          10.453          5.2562          5.2562
v  Pressure               -52.859           19.22         -8.7933         -8.7933
v  nu_tilda           4.3243e-007       0.0042695        0.001178        0.001178
v  TempC                       21          73.529          21.743          21.743
v  TurbVisc           3.0751e-014        0.005032       0.0013806       0.0013806
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1114:        0.21100E+01

===============================================================


 INSTANT    0.111500000E+04   TIME STEP NUMBER            1115
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75271E-02 0.88560E+00
   Friction velocity        uk    :  0.75271E-02 0.88560E+00
   Dimensionless distance   yplus :  0.60599E-01 0.71297E+01
   Friction thermal sca.    tstar : -0.69371E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45213E-01 0.53196E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80409E-02      32   0.36173E-03   0.20093E+01 0.96427E+02 
c  Velocity[X]                                      0.11187E+01 
c  Velocity[Y]                                      0.89058E+00 
c  Velocity[Z]                                      0.11967E-29 
c  Pressure     0.10801E-06     442   0.93833E-08   0.10830E+00 0.76881E+03 
c  nu_tilda     0.52937E-05      31   0.69104E-05   0.20185E-06 0.12999E+03 
c  TempC        0.32502E+02      27   0.39475E-03   0.37398E+01 0.18280E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.203          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3895          7.1317      0.00096358      0.00096358
v  Velocity[Z]       -9.6659e-015     1.0453e-014    -7.3642e-018    -7.3642e-018
v  ǁVelocityǁ        0.00085251          10.453          5.2563          5.2563
v  Pressure               -52.833          19.363         -8.7596         -8.7596
v  nu_tilda           4.3246e-007       0.0042695       0.0011786       0.0011786
v  TempC                       21          73.067          21.743          21.743
v  TurbVisc           3.0762e-014        0.005032       0.0013813       0.0013813
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1115:        0.19970E+01

===============================================================


 INSTANT    0.111600000E+04   TIME STEP NUMBER            1116
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58392E-02 0.88700E+00
   Friction velocity        uk    :  0.58392E-02 0.88700E+00
   Dimensionless distance   yplus :  0.47010E-01 0.71409E+01
   Friction thermal sca.    tstar : -0.68502E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35074E-01 0.53279E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80439E-02      32   0.31154E-03   0.19963E+01 0.96567E+02 
c  Velocity[X]                                      0.10842E+01 
c  Velocity[Y]                                      0.91219E+00 
c  Velocity[Z]                                      0.11271E-29 
c  Pressure     0.10462E-06     457   0.99494E-08   0.10447E+00 0.53259E+03 
c  nu_tilda     0.52954E-05      31   0.15457E-04   0.20200E-06 0.13002E+03 
c  TempC        0.32513E+02      26   0.38824E-03   0.43996E+01 0.21670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2009          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3873          7.1394      0.00095168      0.00095168
v  Velocity[Z]       -9.5386e-015     1.0002e-014    -7.3483e-018    -7.3483e-018
v  ǁVelocityǁ         0.0015842          10.453          5.2564          5.2564
v  Pressure                -52.83          19.298         -8.7973         -8.7973
v  nu_tilda           4.3245e-007       0.0042695       0.0011792       0.0011792
v  TempC                       21          73.068          21.743          21.743
v  TurbVisc            3.077e-014        0.005032       0.0013821       0.0013821
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1116:        0.22220E+01

===============================================================


 INSTANT    0.111700000E+04   TIME STEP NUMBER            1117
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98109E-02 0.88673E+00
   Friction velocity        uk    :  0.98109E-02 0.88673E+00
   Dimensionless distance   yplus :  0.78985E-01 0.71388E+01
   Friction thermal sca.    tstar : -0.67781E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58932E-01 0.53263E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80468E-02      32   0.30279E-03   0.19977E+01 0.96415E+02 
c  Velocity[X]                                      0.10976E+01 
c  Velocity[Y]                                      0.90008E+00 
c  Velocity[Z]                                      0.13989E-29 
c  Pressure     0.13545E-06     345   0.92349E-08   0.13574E+00 0.30919E+03 
c  nu_tilda     0.52971E-05      31   0.69144E-05   0.20215E-06 0.13006E+03 
c  TempC        0.32523E+02      26   0.42019E-03   0.48598E+01 0.23169E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1989          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3846          7.1116       0.0009396       0.0009396
v  Velocity[Z]       -9.3614e-015     1.0434e-014    -7.3287e-018    -7.3287e-018
v  ǁVelocityǁ        0.00086522          10.453          5.2565          5.2565
v  Pressure               -52.798          19.235         -8.7996         -8.7996
v  nu_tilda           4.3251e-007       0.0042695       0.0011799       0.0011799
v  TempC                       21          73.584          21.744          21.744
v  TurbVisc           3.0768e-014        0.005032       0.0013828       0.0013828
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1117:        0.20140E+01

===============================================================


 INSTANT    0.111800000E+04   TIME STEP NUMBER            1118
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51248E-02 0.88561E+00
   Friction velocity        uk    :  0.51248E-02 0.88561E+00
   Dimensionless distance   yplus :  0.41258E-01 0.71298E+01
   Friction thermal sca.    tstar : -0.69421E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30783E-01 0.53196E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80497E-02      32   0.31609E-03   0.19950E+01 0.96438E+02 
c  Velocity[X]                                      0.11006E+01 
c  Velocity[Y]                                      0.89441E+00 
c  Velocity[Z]                                      0.10373E-29 
c  Pressure     0.99665E-07     377   0.98575E-08   0.10023E+00 0.18430E+03 
c  nu_tilda     0.52987E-05      31   0.15473E-04   0.20232E-06 0.13009E+03 
c  TempC        0.32534E+02      26   0.36426E-03   0.55990E+01 0.25210E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1967          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3823          7.1324      0.00092786      0.00092786
v  Velocity[Z]       -9.3318e-015     1.0294e-014    -7.3163e-018    -7.3163e-018
v  ǁVelocityǁ        0.00069629          10.453          5.2566          5.2566
v  Pressure               -52.797          19.275         -8.8123         -8.8123
v  nu_tilda           4.3251e-007       0.0042695       0.0011805       0.0011805
v  TempC                       21          73.068          21.744          21.744
v  TurbVisc           3.0786e-014        0.005032       0.0013835       0.0013835
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1118:        0.21130E+01

===============================================================


 INSTANT    0.111900000E+04   TIME STEP NUMBER            1119
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32470E-02 0.88675E+00
   Friction velocity        uk    :  0.32470E-02 0.88675E+00
   Dimensionless distance   yplus :  0.26140E-01 0.71390E+01
   Friction thermal sca.    tstar : -0.68690E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19504E-01 0.53265E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80527E-02      32   0.32276E-03   0.19982E+01 0.96591E+02 
c  Velocity[X]                                      0.10831E+01 
c  Velocity[Y]                                      0.91505E+00 
c  Velocity[Z]                                      0.11017E-29 
c  Pressure     0.10575E-06     250   0.94964E-08   0.10763E+00 0.27240E+03 
c  nu_tilda     0.53004E-05      31   0.68933E-05   0.20248E-06 0.13013E+03 
c  TempC        0.32545E+02      26   0.35062E-03   0.60540E+01 0.24497E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1948          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3796          7.1138      0.00091595      0.00091595
v  Velocity[Z]       -9.1446e-015     1.0473e-014    -7.3039e-018    -7.3039e-018
v  ǁVelocityǁ         0.0012108          10.453          5.2567          5.2567
v  Pressure               -52.767          19.235         -8.8124         -8.8124
v  nu_tilda           4.3248e-007       0.0042695       0.0011811       0.0011811
v  TempC                       21          73.068          21.744          21.744
v  TurbVisc           3.0785e-014        0.005032       0.0013842       0.0013842
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1119:        0.17290E+01

===============================================================


 INSTANT    0.112000000E+04   TIME STEP NUMBER            1120
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48550E-02 0.88593E+00
   Friction velocity        uk    :  0.48550E-02 0.88593E+00
   Dimensionless distance   yplus :  0.39086E-01 0.71323E+01
   Friction thermal sca.    tstar : -0.70409E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29163E-01 0.53215E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80556E-02      32   0.30619E-03   0.19909E+01 0.96569E+02 
c  Velocity[X]                                      0.10868E+01 
c  Velocity[Y]                                      0.90416E+00 
c  Velocity[Z]                                      0.15311E-29 
c  Pressure     0.96451E-07     409   0.93598E-08   0.96155E-01 0.19952E+03 
c  nu_tilda     0.53021E-05      31   0.15484E-04   0.20265E-06 0.13016E+03 
c  TempC        0.32556E+02      26   0.42626E-03   0.43399E+01 0.20647E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1928          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3772          7.1392      0.00090427      0.00090427
v  Velocity[Z]       -8.9529e-015     1.0306e-014    -7.2921e-018    -7.2921e-018
v  ǁVelocityǁ        0.00082406          10.453          5.2567          5.2567
v  Pressure               -52.766          19.267          -8.828          -8.828
v  nu_tilda           4.3244e-007       0.0042695       0.0011817       0.0011817
v  TempC                       21          73.369          21.745          21.745
v  TurbVisc           3.0776e-014        0.005032        0.001385        0.001385
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1120:        0.19700E+01

===============================================================


 INSTANT    0.112100000E+04   TIME STEP NUMBER            1121
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47825E-02 0.88709E+00
   Friction velocity        uk    :  0.47825E-02 0.88709E+00
   Dimensionless distance   yplus :  0.38502E-01 0.71417E+01
   Friction thermal sca.    tstar : -0.68811E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28727E-01 0.53285E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80585E-02      32   0.36286E-03   0.19934E+01 0.96551E+02 
c  Velocity[X]                                      0.10949E+01 
c  Velocity[Y]                                      0.89853E+00 
c  Velocity[Z]                                      0.11605E-29 
c  Pressure     0.12144E-06     394   0.96732E-08   0.12022E+00 0.32252E+03 
c  nu_tilda     0.53038E-05      31   0.69031E-05   0.20282E-06 0.13020E+03 
c  TempC        0.32566E+02      27   0.35871E-03   0.45011E+01 0.20837E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1909          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3749          7.1404      0.00089244      0.00089244
v  Velocity[Z]       -8.8867e-015     1.0603e-014    -7.2772e-018    -7.2772e-018
v  ǁVelocityǁ         0.0015033          10.453          5.2568          5.2568
v  Pressure               -52.736          19.282         -8.8186         -8.8186
v  nu_tilda           4.3243e-007       0.0042695       0.0011823       0.0011823
v  TempC                       21          73.068          21.745          21.745
v  TurbVisc           3.0767e-014        0.005032       0.0013857       0.0013857
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1121:        0.20240E+01

===============================================================


 INSTANT    0.112200000E+04   TIME STEP NUMBER            1122
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79064E-02 0.88670E+00
   Friction velocity        uk    :  0.79064E-02 0.88670E+00
   Dimensionless distance   yplus :  0.63652E-01 0.71385E+01
   Friction thermal sca.    tstar : -0.68554E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47492E-01 0.53261E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80614E-02      32   0.33297E-03   0.20554E+01 0.97227E+02 
c  Velocity[X]                                      0.11336E+01 
c  Velocity[Y]                                      0.92181E+00 
c  Velocity[Z]                                      0.10663E-29 
c  Pressure     0.12935E-06     490   0.94550E-08   0.13167E+00 0.76592E+03 
c  nu_tilda     0.53055E-05      31   0.15482E-04   0.20299E-06 0.13024E+03 
c  TempC        0.32577E+02      27   0.31478E-03   0.49954E+01 0.22645E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1888          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3723          7.1136      0.00088051      0.00088051
v  Velocity[Z]       -8.7189e-015     1.0572e-014    -7.2626e-018    -7.2626e-018
v  ǁVelocityǁ        0.00089817          10.453          5.2569          5.2569
v  Pressure               -52.728          19.142         -8.8637         -8.8637
v  nu_tilda           4.3248e-007       0.0042695       0.0011829       0.0011829
v  TempC                       21          73.068          21.746          21.746
v  TurbVisc           3.0764e-014        0.005032       0.0013864       0.0013864
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1122:        0.21070E+01

===============================================================


 INSTANT    0.112300000E+04   TIME STEP NUMBER            1123
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45134E-02 0.88573E+00
   Friction velocity        uk    :  0.45134E-02 0.88573E+00
   Dimensionless distance   yplus :  0.36336E-01 0.71307E+01
   Friction thermal sca.    tstar : -0.70754E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27111E-01 0.53203E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80643E-02      32   0.28654E-03   0.20077E+01 0.96921E+02 
c  Velocity[X]                                      0.10974E+01 
c  Velocity[Y]                                      0.91035E+00 
c  Velocity[Z]                                      0.15089E-29 
c  Pressure     0.10189E-06     457   0.98643E-08   0.10209E+00 0.67540E+03 
c  nu_tilda     0.53072E-05      31   0.68970E-05   0.20315E-06 0.13027E+03 
c  TempC        0.32588E+02      26   0.47254E-03   0.49820E+01 0.22788E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1868          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3696          7.1384      0.00086871      0.00086871
v  Velocity[Z]       -8.5361e-015     1.0542e-014     -7.251e-018     -7.251e-018
v  ǁVelocityǁ         0.0010683          10.453           5.257           5.257
v  Pressure               -52.704          19.272         -8.8367         -8.8367
v  nu_tilda           4.3249e-007       0.0042695       0.0011836       0.0011836
v  TempC                       21          73.139          21.746          21.746
v  TurbVisc           3.0777e-014        0.005032       0.0013872       0.0013872
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1123:        0.20190E+01

===============================================================


 INSTANT    0.112400000E+04   TIME STEP NUMBER            1124
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63567E-02 0.88686E+00
   Friction velocity        uk    :  0.63567E-02 0.88686E+00
   Dimensionless distance   yplus :  0.51176E-01 0.71398E+01
   Friction thermal sca.    tstar : -0.69661E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38183E-01 0.53271E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80672E-02      32   0.35089E-03   0.19897E+01 0.96738E+02 
c  Velocity[X]                                      0.10860E+01 
c  Velocity[Y]                                      0.90366E+00 
c  Velocity[Z]                                      0.13932E-29 
c  Pressure     0.10398E-06     490   0.93368E-08   0.10479E+00 0.88439E+03 
c  nu_tilda     0.53089E-05      31   0.15492E-04   0.20331E-06 0.13030E+03 
c  TempC        0.32598E+02      27   0.35263E-03   0.66395E+01 0.27913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1846          10.452          4.5729          4.5729
v  Velocity[Y]             -3.367          7.1195      0.00085709      0.00085709
v  Velocity[Z]       -8.4946e-015     1.0649e-014    -7.2394e-018    -7.2394e-018
v  ǁVelocityǁ         0.0012496          10.453           5.257           5.257
v  Pressure               -52.699          19.104         -8.8888         -8.8888
v  nu_tilda           4.3253e-007       0.0042695       0.0011841       0.0011841
v  TempC                       21          73.068          21.746          21.746
v  TurbVisc           3.0779e-014        0.005032       0.0013879       0.0013879
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1124:        0.21120E+01

===============================================================


 INSTANT    0.112500000E+04   TIME STEP NUMBER            1125
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36291E-02 0.88626E+00
   Friction velocity        uk    :  0.36291E-02 0.88626E+00
   Dimensionless distance   yplus :  0.29217E-01 0.71350E+01
   Friction thermal sca.    tstar : -0.71528E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21799E-01 0.53235E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80701E-02      32   0.32976E-03   0.20209E+01 0.97037E+02 
c  Velocity[X]                                      0.10960E+01 
c  Velocity[Y]                                      0.92484E+00 
c  Velocity[Z]                                      0.12014E-29 
c  Pressure     0.11668E-06     490   0.91189E-08   0.11576E+00 0.83181E+03 
c  nu_tilda     0.53106E-05      31   0.68871E-05   0.20346E-06 0.13034E+03 
c  TempC        0.32609E+02      26   0.30040E-03   0.59670E+01 0.25269E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1825          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3641          7.1393      0.00084538      0.00084538
v  Velocity[Z]       -8.2818e-015      1.088e-014    -7.2225e-018    -7.2225e-018
v  ǁVelocityǁ        0.00075951          10.453          5.2571          5.2571
v  Pressure               -52.669           19.26         -8.8496         -8.8496
v  nu_tilda            4.325e-007       0.0042695       0.0011848       0.0011848
v  TempC                       21          73.068          21.747          21.747
v  TurbVisc           3.0791e-014        0.005032       0.0013886       0.0013886
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1125:        0.21030E+01

===============================================================


 INSTANT    0.112600000E+04   TIME STEP NUMBER            1126
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35301E-02 0.88738E+00
   Friction velocity        uk    :  0.35301E-02 0.88738E+00
   Dimensionless distance   yplus :  0.28420E-01 0.71440E+01
   Friction thermal sca.    tstar : -0.69409E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21204E-01 0.53302E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80730E-02      32   0.31410E-03   0.19979E+01 0.96941E+02 
c  Velocity[X]                                      0.10849E+01 
c  Velocity[Y]                                      0.91294E+00 
c  Velocity[Z]                                      0.14419E-29 
c  Pressure     0.98814E-07     457   0.98995E-08   0.98481E-01 0.54409E+03 
c  nu_tilda     0.53123E-05      31   0.15504E-04   0.20362E-06 0.13037E+03 
c  TempC        0.32620E+02      26   0.48295E-03   0.38310E+01 0.20324E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1803          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3614          7.1471      0.00083395      0.00083395
v  Velocity[Z]       -8.1715e-015     1.0788e-014      -7.21e-018      -7.21e-018
v  ǁVelocityǁ         0.0012874          10.453          5.2572          5.2572
v  Pressure               -52.667          19.181         -8.8862         -8.8862
v  nu_tilda           4.3238e-007       0.0042695       0.0011854       0.0011854
v  TempC                       21          73.366          21.747          21.747
v  TurbVisc           3.0782e-014        0.005032       0.0013894       0.0013894
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1126:        0.20270E+01

===============================================================


 INSTANT    0.112700000E+04   TIME STEP NUMBER            1127
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83596E-02 0.88724E+00
   Friction velocity        uk    :  0.83596E-02 0.88724E+00
   Dimensionless distance   yplus :  0.67300E-01 0.71429E+01
   Friction thermal sca.    tstar : -0.69843E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50214E-01 0.53294E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80759E-02      32   0.32041E-03   0.20102E+01 0.97045E+02 
c  Velocity[X]                                      0.10975E+01 
c  Velocity[Y]                                      0.91271E+00 
c  Velocity[Z]                                      0.13178E-29 
c  Pressure     0.13300E-06     281   0.98299E-08   0.13648E+00 0.25757E+03 
c  nu_tilda     0.53140E-05      31   0.68882E-05   0.20377E-06 0.13041E+03 
c  TempC        0.32630E+02      28   0.38163E-03   0.56776E+01 0.23110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1783          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3593          7.1238      0.00082209      0.00082209
v  Velocity[Z]       -8.0926e-015     1.0834e-014    -7.1981e-018    -7.1981e-018
v  ǁVelocityǁ        0.00090304          10.453          5.2573          5.2573
v  Pressure               -52.636          19.148         -8.8878         -8.8878
v  nu_tilda            4.324e-007       0.0042695        0.001186        0.001186
v  TempC                       21          73.068          21.747          21.747
v  TurbVisc           3.0749e-014        0.005032       0.0013901       0.0013901
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1127:        0.16170E+01

===============================================================


 INSTANT    0.112800000E+04   TIME STEP NUMBER            1128
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12821E-02 0.88565E+00
   Friction velocity        uk    :  0.12821E-02 0.88565E+00
   Dimensionless distance   yplus :  0.10322E-01 0.71301E+01
   Friction thermal sca.    tstar : -0.71442E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77012E-02 0.53198E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80788E-02      32   0.32546E-03   0.20323E+01 0.97345E+02 
c  Velocity[X]                                      0.10980E+01 
c  Velocity[Y]                                      0.93433E+00 
c  Velocity[Z]                                      0.12880E-29 
c  Pressure     0.11532E-06     456   0.92768E-08   0.11342E+00 0.31469E+03 
c  nu_tilda     0.53157E-05      31   0.15506E-04   0.20395E-06 0.13044E+03 
c  TempC        0.32641E+02      27   0.35303E-03   0.46298E+01 0.20634E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1763          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3567          7.1358      0.00081057      0.00081057
v  Velocity[Z]       -7.9501e-015     1.0787e-014     -7.186e-018     -7.186e-018
v  ǁVelocityǁ         0.0010403          10.453          5.2573          5.2573
v  Pressure               -52.635          19.129          -8.912          -8.912
v  nu_tilda           4.3246e-007       0.0042695       0.0011866       0.0011866
v  TempC                       21          73.068          21.748          21.748
v  TurbVisc           3.0753e-014        0.005032       0.0013908       0.0013908
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1128:        0.20250E+01

===============================================================


 INSTANT    0.112900000E+04   TIME STEP NUMBER            1129
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46990E-02 0.88704E+00
   Friction velocity        uk    :  0.46990E-02 0.88704E+00
   Dimensionless distance   yplus :  0.37830E-01 0.71412E+01
   Friction thermal sca.    tstar : -0.70814E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28225E-01 0.53282E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80817E-02      32   0.29822E-03   0.20167E+01 0.97257E+02 
c  Velocity[X]                                      0.10949E+01 
c  Velocity[Y]                                      0.92178E+00 
c  Velocity[Z]                                      0.14872E-29 
c  Pressure     0.11086E-06     345   0.96342E-08   0.11300E+00 0.25946E+03 
c  nu_tilda     0.53174E-05      31   0.68840E-05   0.20411E-06 0.13048E+03 
c  TempC        0.32651E+02      26   0.35248E-03   0.38828E+01 0.19334E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1742          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3537          7.1186      0.00079878      0.00079878
v  Velocity[Z]       -7.7971e-015     1.0992e-014    -7.1709e-018    -7.1709e-018
v  ǁVelocityǁ         0.0012509          10.453          5.2574          5.2574
v  Pressure               -52.604          19.107         -8.9108         -8.9108
v  nu_tilda           4.3251e-007       0.0042695       0.0011872       0.0011872
v  TempC                       21          73.068          21.748          21.748
v  TurbVisc           3.0771e-014        0.005032       0.0013915       0.0013915
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1129:        0.17650E+01

===============================================================


 INSTANT    0.113000000E+04   TIME STEP NUMBER            1130
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47363E-02 0.88628E+00
   Friction velocity        uk    :  0.47363E-02 0.88628E+00
   Dimensionless distance   yplus :  0.38131E-01 0.71351E+01
   Friction thermal sca.    tstar : -0.71904E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28450E-01 0.53236E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80846E-02      32   0.34966E-03   0.19990E+01 0.97105E+02 
c  Velocity[X]                                      0.10854E+01 
c  Velocity[Y]                                      0.91357E+00 
c  Velocity[Z]                                      0.93391E-30 
c  Pressure     0.10467E-06     376   0.93316E-08   0.10468E+00 0.17296E+03 
c  nu_tilda     0.53191E-05      32   0.15513E-04   0.20430E-06 0.13052E+03 
c  TempC        0.32662E+02      26   0.42505E-03   0.36489E+01 0.19609E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.172          10.452          4.5729          4.5729
v  Velocity[Y]              -3.35          7.1426      0.00078742      0.00078742
v  Velocity[Z]       -7.7729e-015      1.103e-014    -7.1601e-018    -7.1601e-018
v  ǁVelocityǁ        0.00080178          10.453          5.2575          5.2575
v  Pressure               -52.601          19.146         -8.9197         -8.9197
v  nu_tilda           4.3251e-007       0.0042695       0.0011878       0.0011878
v  TempC                       21          73.068          21.749          21.749
v  TurbVisc           3.0787e-014        0.005032       0.0013923       0.0013923
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1130:        0.18450E+01

===============================================================


 INSTANT    0.113100000E+04   TIME STEP NUMBER            1131
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36986E-02 0.88761E+00
   Friction velocity        uk    :  0.36986E-02 0.88761E+00
   Dimensionless distance   yplus :  0.29777E-01 0.71458E+01
   Friction thermal sca.    tstar : -0.70911E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22217E-01 0.53316E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80875E-02      32   0.30903E-03   0.20307E+01 0.97425E+02 
c  Velocity[X]                                      0.10941E+01 
c  Velocity[Y]                                      0.93656E+00 
c  Velocity[Z]                                      0.11628E-29 
c  Pressure     0.12820E-06     394   0.95107E-08   0.12640E+00 0.27244E+03 
c  nu_tilda     0.53208E-05      32   0.68682E-05   0.20448E-06 0.13056E+03 
c  TempC        0.32673E+02      26   0.31353E-03   0.59495E+01 0.25113E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1699          10.452          4.5729          4.5729
v  Velocity[Y]            -3.3473          7.1471      0.00077575      0.00077575
v  Velocity[Z]       -7.6155e-015     1.1104e-014    -7.1494e-018    -7.1494e-018
v  ǁVelocityǁ         0.0014544          10.453          5.2575          5.2575
v  Pressure               -52.571          19.147         -8.9152         -8.9152
v  nu_tilda           4.3253e-007       0.0042695       0.0011885       0.0011885
v  TempC                       21          73.068          21.749          21.749
v  TurbVisc           3.0786e-014        0.005032        0.001393        0.001393
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1131:        0.18870E+01

===============================================================


 INSTANT    0.113200000E+04   TIME STEP NUMBER            1132
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18285E-02 0.88752E+00
   Friction velocity        uk    :  0.18285E-02 0.88752E+00
   Dimensionless distance   yplus :  0.14720E-01 0.71451E+01
   Friction thermal sca.    tstar : -0.71684E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10983E-01 0.53311E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80904E-02      32   0.27717E-03   0.20336E+01 0.97517E+02 
c  Velocity[X]                                      0.11081E+01 
c  Velocity[Y]                                      0.92558E+00 
c  Velocity[Z]                                      0.16909E-29 
c  Pressure     0.10337E-06     506   0.96762E-08   0.10551E+00 0.80284E+03 
c  nu_tilda     0.53225E-05      32   0.15530E-04   0.20465E-06 0.13060E+03 
c  TempC        0.32683E+02      26   0.29063E-03   0.38597E+01 0.20553E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1676          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3448          7.1216      0.00076412      0.00076412
v  Velocity[Z]        -7.495e-015      1.115e-014    -7.1382e-018    -7.1382e-018
v  ǁVelocityǁ         0.0008923          10.453          5.2576          5.2576
v  Pressure               -52.568           19.01         -8.9657         -8.9657
v  nu_tilda           4.3258e-007       0.0042695        0.001189        0.001189
v  TempC                       21          73.198          21.749          21.749
v  TurbVisc           3.0791e-014        0.005032       0.0013937       0.0013937
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1132:        0.21520E+01

===============================================================


 INSTANT    0.113300000E+04   TIME STEP NUMBER            1133
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36622E-02 0.88626E+00
   Friction velocity        uk    :  0.36622E-02 0.88626E+00
   Dimensionless distance   yplus :  0.29483E-01 0.71350E+01
   Friction thermal sca.    tstar : -0.72766E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21998E-01 0.53235E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80932E-02      32   0.35057E-03   0.20053E+01 0.97356E+02 
c  Velocity[X]                                      0.10851E+01 
c  Velocity[Y]                                      0.92025E+00 
c  Velocity[Z]                                      0.11750E-29 
c  Pressure     0.10825E-06     490   0.96644E-08   0.10780E+00 0.73081E+03 
c  nu_tilda     0.53242E-05      32   0.68751E-05   0.20480E-06 0.13063E+03 
c  TempC        0.32694E+02      26   0.42710E-03   0.33618E+01 0.17451E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1653          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3425          7.1466      0.00075252      0.00075252
v  Velocity[Z]       -7.4187e-015     1.1163e-014    -7.1272e-018    -7.1272e-018
v  ǁVelocityǁ         0.0010444          10.453          5.2576          5.2576
v  Pressure               -52.537          19.132         -8.9313         -8.9313
v  nu_tilda           4.3261e-007       0.0042695       0.0011897       0.0011897
v  TempC                       21          73.068           21.75           21.75
v  TurbVisc           3.0807e-014        0.005032       0.0013944       0.0013944
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1133:        0.21030E+01

===============================================================


 INSTANT    0.113400000E+04   TIME STEP NUMBER            1134
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10660E-02 0.88740E+00
   Friction velocity        uk    :  0.10660E-02 0.88740E+00
   Dimensionless distance   yplus :  0.85820E-02 0.71441E+01
   Friction thermal sca.    tstar : -0.71809E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64032E-02 0.53303E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80961E-02      32   0.36494E-03   0.20488E+01 0.97791E+02 
c  Velocity[X]                                      0.11045E+01 
c  Velocity[Y]                                      0.94425E+00 
c  Velocity[Z]                                      0.11051E-29 
c  Pressure     0.12662E-06     489   0.92627E-08   0.12729E+00 0.78884E+03 
c  nu_tilda     0.53259E-05      32   0.15527E-04   0.20497E-06 0.13067E+03 
c  TempC        0.32705E+02      27   0.38095E-03   0.68426E+01 0.26524E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1632          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3398          7.1196      0.00074107      0.00074107
v  Velocity[Z]       -7.3175e-015     1.0931e-014    -7.1159e-018    -7.1159e-018
v  ǁVelocityǁ         0.0012352          10.453          5.2577          5.2577
v  Pressure               -52.533          18.994         -8.9794         -8.9794
v  nu_tilda           4.3261e-007       0.0042695       0.0011903       0.0011903
v  TempC                       21          73.068           21.75           21.75
v  TurbVisc           3.0816e-014        0.005032       0.0013952       0.0013952
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1134:        0.23670E+01

===============================================================


 INSTANT    0.113500000E+04   TIME STEP NUMBER            1135
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48077E-02 0.88667E+00
   Friction velocity        uk    :  0.48077E-02 0.88667E+00
   Dimensionless distance   yplus :  0.38705E-01 0.71383E+01
   Friction thermal sca.    tstar : -0.73511E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28879E-01 0.53260E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.80990E-02      32   0.28943E-03   0.20463E+01 0.97810E+02 
c  Velocity[X]                                      0.11154E+01 
c  Velocity[Y]                                      0.93088E+00 
c  Velocity[Z]                                      0.17733E-29 
c  Pressure     0.11329E-06     458   0.94738E-08   0.11237E+00 0.66157E+03 
c  nu_tilda     0.53276E-05      32   0.68637E-05   0.20512E-06 0.13070E+03 
c  TempC        0.32715E+02      26   0.27858E-03   0.52115E+01 0.21892E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1612          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3366          7.1458      0.00072945      0.00072945
v  Velocity[Z]       -7.1472e-015     1.0724e-014    -7.1074e-018    -7.1074e-018
v  ǁVelocityǁ        0.00080426          10.453          5.2578          5.2578
v  Pressure               -52.504          19.104         -8.9497         -8.9497
v  nu_tilda           4.3257e-007       0.0042695       0.0011909       0.0011909
v  TempC                       21          73.257          21.751          21.751
v  TurbVisc           3.0816e-014        0.005032       0.0013959       0.0013959
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1135:        0.20300E+01

===============================================================


 INSTANT    0.113600000E+04   TIME STEP NUMBER            1136
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43984E-02 0.88817E+00
   Friction velocity        uk    :  0.43984E-02 0.88817E+00
   Dimensionless distance   yplus :  0.35410E-01 0.71504E+01
   Friction thermal sca.    tstar : -0.73170E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26420E-01 0.53350E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81019E-02      32   0.33096E-03   0.20017E+01 0.97539E+02 
c  Velocity[X]                                      0.10774E+01 
c  Velocity[Y]                                      0.92425E+00 
c  Velocity[Z]                                      0.12509E-29 
c  Pressure     0.99074E-07     470   0.93837E-08   0.99509E-01 0.36535E+03 
c  nu_tilda     0.53293E-05      32   0.15537E-04   0.20529E-06 0.13074E+03 
c  TempC        0.32726E+02      26   0.44216E-03   0.35519E+01 0.18376E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.159          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3337          7.1564      0.00071788      0.00071788
v  Velocity[Z]       -7.0941e-015     1.0085e-014    -7.0953e-018    -7.0953e-018
v  ǁVelocityǁ         0.0014816          10.454          5.2578          5.2578
v  Pressure               -52.503          19.081          -8.978          -8.978
v  nu_tilda           4.3251e-007       0.0042695       0.0011915       0.0011915
v  TempC                       21          73.068          21.751          21.751
v  TurbVisc           3.0804e-014        0.005032       0.0013966       0.0013966
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1136:        0.20730E+01

===============================================================


 INSTANT    0.113700000E+04   TIME STEP NUMBER            1137
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54648E-02 0.88768E+00
   Friction velocity        uk    :  0.54648E-02 0.88768E+00
   Dimensionless distance   yplus :  0.43995E-01 0.71464E+01
   Friction thermal sca.    tstar : -0.71680E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32825E-01 0.53320E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81047E-02      32   0.32312E-03   0.20634E+01 0.98098E+02 
c  Velocity[X]                                      0.11138E+01 
c  Velocity[Y]                                      0.94958E+00 
c  Velocity[Z]                                      0.98496E-30 
c  Pressure     0.13038E-06     442   0.92499E-08   0.13087E+00 0.48228E+03 
c  nu_tilda     0.53311E-05      32   0.68518E-05   0.20546E-06 0.13077E+03 
c  TempC        0.32736E+02      26   0.40764E-03   0.76995E+01 0.28748E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1568          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3311          7.1252      0.00070629      0.00070629
v  Velocity[Z]       -6.9287e-015     1.0521e-014    -7.0842e-018    -7.0842e-018
v  ǁVelocityǁ        0.00085947          10.454          5.2579          5.2579
v  Pressure               -52.469          18.956         -8.9965         -8.9965
v  nu_tilda           4.3251e-007       0.0042695       0.0011921       0.0011921
v  TempC                       21          73.068          21.751          21.751
v  TurbVisc           3.0787e-014        0.005032       0.0013973       0.0013973
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1137:        0.22090E+01

===============================================================


 INSTANT    0.113800000E+04   TIME STEP NUMBER            1138
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65361E-02 0.88659E+00
   Friction velocity        uk    :  0.65361E-02 0.88659E+00
   Dimensionless distance   yplus :  0.52620E-01 0.71377E+01
   Friction thermal sca.    tstar : -0.74276E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39261E-01 0.53255E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81076E-02      32   0.31259E-03   0.20506E+01 0.98057E+02 
c  Velocity[X]                                      0.11143E+01 
c  Velocity[Y]                                      0.93626E+00 
c  Velocity[Z]                                      0.14956E-29 
c  Pressure     0.11030E-06     377   0.98610E-08   0.10952E+00 0.19433E+03 
c  nu_tilda     0.53328E-05      32   0.15556E-04   0.20565E-06 0.13082E+03 
c  TempC        0.32747E+02      26   0.41287E-03   0.56184E+01 0.24765E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1545          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3284           7.146      0.00069484      0.00069484
v  Velocity[Z]       -6.9287e-015     1.0307e-014    -7.0695e-018    -7.0695e-018
v  ǁVelocityǁ         0.0010842          10.454          5.2579          5.2579
v  Pressure                -52.47          19.011         -9.0067         -9.0067
v  nu_tilda           4.3248e-007       0.0042695       0.0011927       0.0011927
v  TempC                       21          73.137          21.752          21.752
v  TurbVisc           3.0786e-014        0.005032       0.0013981       0.0013981
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1138:        0.21150E+01

===============================================================


 INSTANT    0.113900000E+04   TIME STEP NUMBER            1139
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26480E-02 0.88788E+00
   Friction velocity        uk    :  0.26480E-02 0.88788E+00
   Dimensionless distance   yplus :  0.21318E-01 0.71481E+01
   Friction thermal sca.    tstar : -0.73520E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15906E-01 0.53333E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81104E-02      32   0.32135E-03   0.20347E+01 0.97919E+02 
c  Velocity[X]                                      0.11035E+01 
c  Velocity[Y]                                      0.93122E+00 
c  Velocity[Z]                                      0.12916E-29 
c  Pressure     0.11397E-06     377   0.94118E-08   0.11528E+00 0.30909E+03 
c  nu_tilda     0.53345E-05      32   0.68535E-05   0.20582E-06 0.13086E+03 
c  TempC        0.32758E+02      26   0.35336E-03   0.58306E+01 0.24367E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1522          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3255          7.1295       0.0006833       0.0006833
v  Velocity[Z]       -6.9287e-015     1.0555e-014    -7.0682e-018    -7.0682e-018
v  ǁVelocityǁ        0.00094029          10.454           5.258           5.258
v  Pressure               -52.434          18.988         -9.0004         -9.0004
v  nu_tilda           4.3245e-007       0.0042695       0.0011933       0.0011933
v  TempC                       21          73.068          21.752          21.752
v  TurbVisc           3.0776e-014        0.005032       0.0013988       0.0013988
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1139:        0.18340E+01

===============================================================


 INSTANT    0.114000000E+04   TIME STEP NUMBER            1140
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84070E-02 0.88711E+00
   Friction velocity        uk    :  0.84070E-02 0.88711E+00
   Dimensionless distance   yplus :  0.67682E-01 0.71419E+01
   Friction thermal sca.    tstar : -0.75191E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50498E-01 0.53286E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81133E-02      32   0.31961E-03   0.20463E+01 0.98143E+02 
c  Velocity[X]                                      0.10929E+01 
c  Velocity[Y]                                      0.95345E+00 
c  Velocity[Z]                                      0.10669E-29 
c  Pressure     0.10849E-06     440   0.97829E-08   0.10761E+00 0.24093E+03 
c  nu_tilda     0.53362E-05      32   0.15549E-04   0.20601E-06 0.13090E+03 
c  TempC        0.32768E+02      26   0.32317E-03   0.52936E+01 0.23374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1499          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3227          7.1525      0.00067183      0.00067183
v  Velocity[Z]       -6.9287e-015     1.0098e-014    -7.0561e-018    -7.0561e-018
v  ǁVelocityǁ        0.00081773          10.454           5.258           5.258
v  Pressure               -52.432          19.005         -9.0198         -9.0198
v  nu_tilda           4.3239e-007       0.0042695       0.0011939       0.0011939
v  TempC                       21          73.068          21.752          21.752
v  TurbVisc           3.0768e-014        0.005032       0.0013995       0.0013995
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1140:        0.19810E+01

===============================================================


 INSTANT    0.114100000E+04   TIME STEP NUMBER            1141
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39884E-02 0.88836E+00
   Friction velocity        uk    :  0.39884E-02 0.88836E+00
   Dimensionless distance   yplus :  0.32110E-01 0.71519E+01
   Friction thermal sca.    tstar : -0.73358E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23957E-01 0.53361E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81161E-02      32   0.32359E-03   0.20329E+01 0.98037E+02 
c  Velocity[X]                                      0.10894E+01 
c  Velocity[Y]                                      0.94349E+00 
c  Velocity[Z]                                      0.15263E-29 
c  Pressure     0.10816E-06     424   0.95767E-08   0.10676E+00 0.30950E+03 
c  nu_tilda     0.53379E-05      32   0.68466E-05   0.20618E-06 0.13094E+03 
c  TempC        0.32779E+02      26   0.46425E-03   0.49578E+01 0.23471E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1476          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3198          7.1583      0.00066027      0.00066027
v  Velocity[Z]       -6.9287e-015     1.0535e-014    -7.0459e-018    -7.0459e-018
v  ǁVelocityǁ         0.0015653          10.454          5.2581          5.2581
v  Pressure               -52.407          19.026          -9.012          -9.012
v  nu_tilda           4.3231e-007       0.0042695       0.0011946       0.0011946
v  TempC                       21          73.069          21.753          21.753
v  TurbVisc           3.0753e-014        0.005032       0.0014002       0.0014002
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1141:        0.19600E+01

===============================================================


 INSTANT    0.114200000E+04   TIME STEP NUMBER            1142
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48985E-02 0.88788E+00
   Friction velocity        uk    :  0.48985E-02 0.88788E+00
   Dimensionless distance   yplus :  0.39436E-01 0.71480E+01
   Friction thermal sca.    tstar : -0.72921E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29424E-01 0.53332E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81190E-02      32   0.34159E-03   0.20644E+01 0.98341E+02 
c  Velocity[X]                                      0.11271E+01 
c  Velocity[Y]                                      0.93728E+00 
c  Velocity[Z]                                      0.11007E-29 
c  Pressure     0.11537E-06     489   0.99359E-08   0.11638E+00 0.78986E+03 
c  nu_tilda     0.53396E-05      32   0.15562E-04   0.20636E-06 0.13097E+03 
c  TempC        0.32789E+02      26   0.34739E-03   0.69166E+01 0.28786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1455          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3166          7.1317      0.00064879      0.00064879
v  Velocity[Z]       -6.9287e-015     1.0066e-014    -7.0422e-018    -7.0422e-018
v  ǁVelocityǁ        0.00082277          10.454          5.2581          5.2581
v  Pressure               -52.399          18.877         -9.0569         -9.0569
v  nu_tilda           4.3232e-007       0.0042695       0.0011951       0.0011951
v  TempC                       21          73.068          21.753          21.753
v  TurbVisc            3.073e-014        0.005032        0.001401        0.001401
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1142:        0.21080E+01

===============================================================


 INSTANT    0.114300000E+04   TIME STEP NUMBER            1143
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56456E-02 0.88683E+00
   Friction velocity        uk    :  0.56456E-02 0.88683E+00
   Dimensionless distance   yplus :  0.45451E-01 0.71396E+01
   Friction thermal sca.    tstar : -0.75768E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33911E-01 0.53269E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81218E-02      32   0.30696E-03   0.20528E+01 0.98394E+02 
c  Velocity[X]                                      0.10945E+01 
c  Velocity[Y]                                      0.95828E+00 
c  Velocity[Z]                                      0.12801E-29 
c  Pressure     0.11140E-06     473   0.94233E-08   0.11189E+00 0.75396E+03 
c  nu_tilda     0.53413E-05      32   0.68333E-05   0.20652E-06 0.13101E+03 
c  TempC        0.32800E+02      26   0.39402E-03   0.55112E+01 0.22164E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1432          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3137          7.1538      0.00063759      0.00063759
v  Velocity[Z]       -6.9287e-015     1.0571e-014    -7.0316e-018    -7.0316e-018
v  ǁVelocityǁ         0.0011706          10.454          5.2582          5.2582
v  Pressure               -52.372          19.025         -9.0251         -9.0251
v  nu_tilda           4.3235e-007       0.0042695       0.0011958       0.0011958
v  TempC                       21          73.068          21.754          21.754
v  TurbVisc           3.0731e-014        0.005032       0.0014017       0.0014017
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1143:        0.20670E+01

===============================================================


 INSTANT    0.114400000E+04   TIME STEP NUMBER            1144
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40747E-02 0.88767E+00
   Friction velocity        uk    :  0.40747E-02 0.88767E+00
   Dimensionless distance   yplus :  0.32804E-01 0.71464E+01
   Friction thermal sca.    tstar : -0.74216E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24476E-01 0.53320E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81247E-02      32   0.34471E-03   0.20592E+01 0.98411E+02 
c  Velocity[X]                                      0.11134E+01 
c  Velocity[Y]                                      0.94583E+00 
c  Velocity[Z]                                      0.15853E-29 
c  Pressure     0.11850E-06     489   0.98691E-08   0.11829E+00 0.97358E+03 
c  nu_tilda     0.53431E-05      32   0.15572E-04   0.20669E-06 0.13105E+03 
c  TempC        0.32810E+02      26   0.37433E-03   0.51545E+01 0.23830E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1409          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3109          7.1261      0.00062611      0.00062611
v  Velocity[Z]       -6.9287e-015     1.0112e-014    -7.0273e-018    -7.0273e-018
v  ǁVelocityǁ         0.0010747          10.454          5.2582          5.2582
v  Pressure               -52.365          18.835         -9.0798         -9.0798
v  nu_tilda           4.3245e-007       0.0042695       0.0011964       0.0011964
v  TempC                       21          73.068          21.754          21.754
v  TurbVisc           3.0742e-014        0.005032       0.0014024       0.0014024
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1144:        0.20890E+01

===============================================================


 INSTANT    0.114500000E+04   TIME STEP NUMBER            1145
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66294E-02 0.88713E+00
   Friction velocity        uk    :  0.66294E-02 0.88713E+00
   Dimensionless distance   yplus :  0.53371E-01 0.71420E+01
   Friction thermal sca.    tstar : -0.76531E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39821E-01 0.53288E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81275E-02      32   0.31301E-03   0.20456E+01 0.98388E+02 
c  Velocity[X]                                      0.11017E+01 
c  Velocity[Y]                                      0.94388E+00 
c  Velocity[Z]                                      0.10570E-29 
c  Pressure     0.96644E-07     488   0.96120E-08   0.96212E-01 0.78477E+03 
c  nu_tilda     0.53448E-05      32   0.68330E-05   0.20685E-06 0.13108E+03 
c  TempC        0.32821E+02      27   0.27579E-03   0.48412E+01 0.22813E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1386          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3077          7.1542      0.00061463      0.00061463
v  Velocity[Z]       -6.9287e-015     1.0549e-014    -7.0171e-018    -7.0171e-018
v  ǁVelocityǁ        0.00086997          10.454          5.2583          5.2583
v  Pressure               -52.339          18.985         -9.0457         -9.0457
v  nu_tilda           4.3245e-007       0.0042695        0.001197        0.001197
v  TempC                       21          73.068          21.754          21.754
v  TurbVisc            3.077e-014        0.005032       0.0014031       0.0014031
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1145:        0.21090E+01

===============================================================


 INSTANT    0.114600000E+04   TIME STEP NUMBER            1146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69681E-02 0.88843E+00
   Friction velocity        uk    :  0.69681E-02 0.88843E+00
   Dimensionless distance   yplus :  0.56098E-01 0.71524E+01
   Friction thermal sca.    tstar : -0.74683E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41855E-01 0.53365E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81304E-02      32   0.35577E-03   0.20442E+01 0.98509E+02 
c  Velocity[X]                                      0.10794E+01 
c  Velocity[Y]                                      0.96476E+00 
c  Velocity[Z]                                      0.11108E-29 
c  Pressure     0.91561E-07     473   0.95134E-08   0.91096E-01 0.49882E+03 
c  nu_tilda     0.53465E-05      32   0.15570E-04   0.20703E-06 0.13112E+03 
c  TempC        0.32832E+02      26   0.44177E-03   0.44888E+01 0.21018E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1362          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3049          7.1609      0.00060323      0.00060323
v  Velocity[Z]       -6.9287e-015     1.0077e-014    -7.0101e-018    -7.0101e-018
v  ǁVelocityǁ          0.001162          10.454          5.2583          5.2583
v  Pressure               -52.333          18.925         -9.0786         -9.0786
v  nu_tilda           4.3238e-007       0.0042695       0.0011976       0.0011976
v  TempC                       21          73.069          21.755          21.755
v  TurbVisc            3.077e-014        0.005032       0.0014038       0.0014038
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1146:        0.20590E+01

===============================================================


 INSTANT    0.114700000E+04   TIME STEP NUMBER            1147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52028E-02 0.88813E+00
   Friction velocity        uk    :  0.52028E-02 0.88813E+00
   Dimensionless distance   yplus :  0.41886E-01 0.71501E+01
   Friction thermal sca.    tstar : -0.74287E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31252E-01 0.53348E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81332E-02      32   0.29353E-03   0.20996E+01 0.98909E+02 
c  Velocity[X]                                      0.11432E+01 
c  Velocity[Y]                                      0.95643E+00 
c  Velocity[Z]                                      0.17128E-29 
c  Pressure     0.14127E-06     409   0.91703E-08   0.14066E+00 0.34272E+03 
c  nu_tilda     0.53482E-05      32   0.68227E-05   0.20722E-06 0.13117E+03 
c  TempC        0.32842E+02      26   0.42724E-03   0.67790E+01 0.27529E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1339          10.453          4.5729          4.5729
v  Velocity[Y]            -3.3014          7.1332      0.00059198      0.00059198
v  Velocity[Z]       -7.9987e-015     1.0582e-014    -7.0059e-018    -7.0059e-018
v  ǁVelocityǁ        0.00078035          10.454          5.2584          5.2584
v  Pressure               -52.298          18.842         -9.0841         -9.0841
v  nu_tilda           4.3241e-007       0.0042695       0.0011982       0.0011982
v  TempC                       21          73.147          21.755          21.755
v  TurbVisc           3.0748e-014        0.005032       0.0014046       0.0014046
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1147:        0.19190E+01

===============================================================


 INSTANT    0.114800000E+04   TIME STEP NUMBER            1148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33101E-02 0.88719E+00
   Friction velocity        uk    :  0.33101E-02 0.88719E+00
   Dimensionless distance   yplus :  0.26648E-01 0.71425E+01
   Friction thermal sca.    tstar : -0.78145E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19883E-01 0.53291E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81360E-02      32   0.32072E-03   0.20599E+01 0.98655E+02 
c  Velocity[X]                                      0.11113E+01 
c  Velocity[Y]                                      0.94870E+00 
c  Velocity[Z]                                      0.13438E-29 
c  Pressure     0.10443E-06     362   0.92722E-08   0.10454E+00 0.20244E+03 
c  nu_tilda     0.53499E-05      32   0.15587E-04   0.20742E-06 0.13121E+03 
c  TempC        0.32853E+02      26   0.34898E-03   0.60632E+01 0.23977E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1315          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2986          7.1539      0.00058059      0.00058059
v  Velocity[Z]       -6.9287e-015     1.0123e-014    -6.9909e-018    -6.9909e-018
v  ǁVelocityǁ           0.00129          10.454          5.2584          5.2584
v  Pressure                 -52.3          18.904         -9.0955         -9.0955
v  nu_tilda           4.3243e-007       0.0042695       0.0011988       0.0011988
v  TempC                       21          73.069          21.756          21.756
v  TurbVisc           3.0758e-014        0.005032       0.0014053       0.0014053
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1148:        0.18100E+01

===============================================================


 INSTANT    0.114900000E+04   TIME STEP NUMBER            1149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75953E-02 0.88826E+00
   Friction velocity        uk    :  0.75953E-02 0.88826E+00
   Dimensionless distance   yplus :  0.61147E-01 0.71511E+01
   Friction thermal sca.    tstar : -0.75444E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45623E-01 0.53355E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81388E-02      32   0.30854E-03   0.20734E+01 0.98909E+02 
c  Velocity[X]                                      0.11021E+01 
c  Velocity[Y]                                      0.97126E+00 
c  Velocity[Z]                                      0.12533E-29 
c  Pressure     0.10720E-06     392   0.98495E-08   0.10771E+00 0.30229E+03 
c  nu_tilda     0.53517E-05      32   0.68041E-05   0.20760E-06 0.13125E+03 
c  TempC        0.32863E+02      27   0.39677E-03   0.42210E+01 0.20066E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1293          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2946          7.1353      0.00056921      0.00056921
v  Velocity[Z]       -7.2113e-015     1.0561e-014    -6.9862e-018    -6.9862e-018
v  ǁVelocityǁ        0.00093793          10.454          5.2585          5.2585
v  Pressure               -52.269          18.839         -9.1011         -9.1011
v  nu_tilda           4.3246e-007       0.0042695       0.0011994       0.0011994
v  TempC                       21          73.069          21.756          21.756
v  TurbVisc           3.0763e-014        0.005032        0.001406        0.001406
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1149:        0.18830E+01

===============================================================


 INSTANT    0.115000000E+04   TIME STEP NUMBER            1150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81205E-02 0.88751E+00
   Friction velocity        uk    :  0.81205E-02 0.88751E+00
   Dimensionless distance   yplus :  0.65376E-01 0.71451E+01
   Friction thermal sca.    tstar : -0.77335E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48778E-01 0.53310E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81417E-02      32   0.26571E-03   0.20540E+01 0.98767E+02 
c  Velocity[X]                                      0.10953E+01 
c  Velocity[Y]                                      0.95870E+00 
c  Velocity[Z]                                      0.15805E-29 
c  Pressure     0.94470E-07     296   0.92323E-08   0.94143E-01 0.19813E+03 
c  nu_tilda     0.53534E-05      32   0.15597E-04   0.20779E-06 0.13129E+03 
c  TempC        0.32874E+02      27   0.40411E-03   0.47622E+01 0.23800E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.127          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2914          7.1617      0.00055819      0.00055819
v  Velocity[Z]       -8.2084e-015     1.0089e-014    -6.9803e-018    -6.9803e-018
v  ǁVelocityǁ         0.0009568          10.454          5.2585          5.2585
v  Pressure               -52.265          18.895         -9.1092         -9.1092
v  nu_tilda           4.3246e-007       0.0042695          0.0012          0.0012
v  TempC                       21          73.096          21.756          21.756
v  TurbVisc           3.0772e-014        0.005032       0.0014067       0.0014067
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1150:        0.16480E+01

===============================================================


 INSTANT    0.115100000E+04   TIME STEP NUMBER            1151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71969E-02 0.88884E+00
   Friction velocity        uk    :  0.71969E-02 0.88884E+00
   Dimensionless distance   yplus :  0.57940E-01 0.71558E+01
   Friction thermal sca.    tstar : -0.75572E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43230E-01 0.53390E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81445E-02      32   0.32402E-03   0.20624E+01 0.98865E+02 
c  Velocity[X]                                      0.11062E+01 
c  Velocity[Y]                                      0.95614E+00 
c  Velocity[Z]                                      0.13355E-29 
c  Pressure     0.11257E-06     361   0.97457E-08   0.11109E+00 0.26296E+03 
c  nu_tilda     0.53551E-05      32   0.68078E-05   0.20796E-06 0.13133E+03 
c  TempC        0.32884E+02      26   0.29087E-03   0.56474E+01 0.23089E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1247          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2881          7.1692      0.00054663      0.00054663
v  Velocity[Z]        -7.971e-015     1.0594e-014    -6.9688e-018    -6.9688e-018
v  ǁVelocityǁ         0.0012445          10.454          5.2585          5.2585
v  Pressure               -52.234          18.852         -9.1131         -9.1131
v  nu_tilda           4.3248e-007       0.0042695       0.0012006       0.0012006
v  TempC                       21          73.069          21.757          21.757
v  TurbVisc           3.0771e-014        0.005032       0.0014074       0.0014074
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1151:        0.18140E+01

===============================================================


 INSTANT    0.115200000E+04   TIME STEP NUMBER            1152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10091E-01 0.88865E+00
   Friction velocity        uk    :  0.10091E-01 0.88865E+00
   Dimensionless distance   yplus :  0.81241E-01 0.71542E+01
   Friction thermal sca.    tstar : -0.77301E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60615E-01 0.53379E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81473E-02      32   0.29889E-03   0.20910E+01 0.99210E+02 
c  Velocity[X]                                      0.11138E+01 
c  Velocity[Y]                                      0.97720E+00 
c  Velocity[Z]                                      0.11861E-29 
c  Pressure     0.92358E-07     456   0.99810E-08   0.93633E-01 0.53428E+03 
c  nu_tilda     0.53568E-05      32   0.15598E-04   0.20814E-06 0.13137E+03 
c  TempC        0.32895E+02      26   0.46506E-03   0.45463E+01 0.21603E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1223          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2853          7.1395      0.00053531      0.00053531
v  Velocity[Z]       -8.4863e-015     1.0133e-014    -6.9636e-018    -6.9636e-018
v  ǁVelocityǁ        0.00077945          10.454          5.2586          5.2586
v  Pressure               -52.231          18.771         -9.1473         -9.1473
v  nu_tilda           4.3246e-007       0.0042695       0.0012012       0.0012012
v  TempC                       21          73.069          21.757          21.757
v  TurbVisc           3.0776e-014        0.005032       0.0014082       0.0014082
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1152:        0.20360E+01

===============================================================


 INSTANT    0.115300000E+04   TIME STEP NUMBER            1153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40216E-02 0.88734E+00
   Friction velocity        uk    :  0.40216E-02 0.88734E+00
   Dimensionless distance   yplus :  0.32377E-01 0.71437E+01
   Friction thermal sca.    tstar : -0.78028E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24157E-01 0.53300E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81501E-02      32   0.29308E-03   0.20715E+01 0.99105E+02 
c  Velocity[X]                                      0.11044E+01 
c  Velocity[Y]                                      0.96710E+00 
c  Velocity[Z]                                      0.15711E-29 
c  Pressure     0.10035E-06     474   0.92473E-08   0.99852E-01 0.69532E+03 
c  nu_tilda     0.53585E-05      32   0.67941E-05   0.20830E-06 0.13141E+03 
c  TempC        0.32905E+02      26   0.37760E-03   0.81091E+01 0.30674E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1198          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2815          7.1633        0.000524        0.000524
v  Velocity[Z]       -8.3096e-015     1.0571e-014    -6.9539e-018    -6.9539e-018
v  ǁVelocityǁ        0.00097263          10.454          5.2586          5.2586
v  Pressure               -52.203          18.893         -9.1163         -9.1163
v  nu_tilda           4.3241e-007       0.0042695       0.0012018       0.0012018
v  TempC                       21          73.167          21.757          21.757
v  TurbVisc            3.077e-014        0.005032       0.0014089       0.0014089
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1153:        0.20820E+01

===============================================================


 INSTANT    0.115400000E+04   TIME STEP NUMBER            1154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89613E-02 0.88822E+00
   Friction velocity        uk    :  0.89613E-02 0.88822E+00
   Dimensionless distance   yplus :  0.72145E-01 0.71507E+01
   Friction thermal sca.    tstar : -0.76245E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53828E-01 0.53353E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81529E-02      32   0.37346E-03   0.20897E+01 0.99241E+02 
c  Velocity[X]                                      0.11303E+01 
c  Velocity[Y]                                      0.95947E+00 
c  Velocity[Z]                                      0.13237E-29 
c  Pressure     0.12736E-06     520   0.91635E-08   0.12673E+00 0.98003E+03 
c  nu_tilda     0.53603E-05      32   0.15607E-04   0.20849E-06 0.13145E+03 
c  TempC        0.32916E+02      26   0.43612E-03   0.52980E+01 0.23756E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1173          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2785          7.1369      0.00051285      0.00051285
v  Velocity[Z]       -8.8956e-015     1.0099e-014    -6.9487e-018    -6.9487e-018
v  ǁVelocityǁ         0.0008196          10.454          5.2587          5.2587
v  Pressure               -52.196           18.71         -9.1734         -9.1734
v  nu_tilda           4.3245e-007       0.0042695       0.0012024       0.0012024
v  TempC                       21          73.069          21.758          21.758
v  TurbVisc           3.0759e-014        0.005032       0.0014096       0.0014096
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1154:        0.21740E+01

===============================================================


 INSTANT    0.115500000E+04   TIME STEP NUMBER            1155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60088E-02 0.88762E+00
   Friction velocity        uk    :  0.60088E-02 0.88762E+00
   Dimensionless distance   yplus :  0.48375E-01 0.71459E+01
   Friction thermal sca.    tstar : -0.79521E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36093E-01 0.53317E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81557E-02      32   0.29932E-03   0.21193E+01 0.99589E+02 
c  Velocity[X]                                      0.11378E+01 
c  Velocity[Y]                                      0.98154E+00 
c  Velocity[Z]                                      0.12906E-29 
c  Pressure     0.13659E-06     489   0.94222E-08   0.13563E+00 0.77654E+03 
c  nu_tilda     0.53620E-05      32   0.67775E-05   0.20867E-06 0.13149E+03 
c  TempC        0.32926E+02      26   0.36495E-03   0.63819E+01 0.25825E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1149          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2736          7.1612      0.00050129      0.00050129
v  Velocity[Z]       -9.5051e-015     1.0604e-014     -6.938e-018     -6.938e-018
v  ǁVelocityǁ         0.0011318          10.454          5.2587          5.2587
v  Pressure               -52.163           18.85         -9.1369         -9.1369
v  nu_tilda           4.3246e-007       0.0042695       0.0012031       0.0012031
v  TempC                       21          73.069          21.758          21.758
v  TurbVisc           3.0767e-014        0.005032       0.0014103       0.0014103
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1155:        0.21180E+01

===============================================================


 INSTANT    0.115600000E+04   TIME STEP NUMBER            1156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10187E-01 0.88895E+00
   Friction velocity        uk    :  0.10187E-01 0.88895E+00
   Dimensionless distance   yplus :  0.82011E-01 0.71566E+01
   Friction thermal sca.    tstar : -0.78180E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61190E-01 0.53397E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81585E-02      32   0.29804E-03   0.20797E+01 0.99415E+02 
c  Velocity[X]                                      0.11074E+01 
c  Velocity[Y]                                      0.97229E+00 
c  Velocity[Z]                                      0.16257E-29 
c  Pressure     0.10450E-06     472   0.91571E-08   0.10413E+00 0.43996E+03 
c  nu_tilda     0.53637E-05      32   0.15617E-04   0.20887E-06 0.13154E+03 
c  TempC        0.32937E+02      26   0.29114E-03   0.62198E+01 0.25900E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1126          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2706          7.1703      0.00049025      0.00049025
v  Velocity[Z]        -8.109e-015     1.0143e-014    -6.9224e-018    -6.9224e-018
v  ǁVelocityǁ         0.0010432          10.454          5.2587          5.2587
v  Pressure               -52.164          18.801         -9.1689         -9.1689
v  nu_tilda           4.3241e-007       0.0042695       0.0012036       0.0012036
v  TempC                       21          73.069          21.759          21.759
v  TurbVisc           3.0771e-014        0.005032        0.001411        0.001411
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1156:        0.20720E+01

===============================================================


 INSTANT    0.115700000E+04   TIME STEP NUMBER            1157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83445E-02 0.88859E+00
   Friction velocity        uk    :  0.83445E-02 0.88859E+00
   Dimensionless distance   yplus :  0.67179E-01 0.71538E+01
   Friction thermal sca.    tstar : -0.77180E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50123E-01 0.53375E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81613E-02      32   0.33492E-03   0.20915E+01 0.99484E+02 
c  Velocity[X]                                      0.11243E+01 
c  Velocity[Y]                                      0.96715E+00 
c  Velocity[Z]                                      0.12255E-29 
c  Pressure     0.12084E-06     425   0.95514E-08   0.12086E+00 0.43457E+03 
c  nu_tilda     0.53655E-05      32   0.67815E-05   0.20906E-06 0.13158E+03 
c  TempC        0.32948E+02      26   0.46250E-03   0.52668E+01 0.23443E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1103          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2676          7.1425      0.00047873      0.00047873
v  Velocity[Z]       -9.0107e-015     1.0581e-014    -6.9178e-018    -6.9178e-018
v  ǁVelocityǁ        0.00088121          10.454          5.2588          5.2588
v  Pressure               -52.132          18.689         -9.1844         -9.1844
v  nu_tilda           4.3246e-007       0.0042695       0.0012043       0.0012043
v  TempC                       21          73.069          21.759          21.759
v  TurbVisc           3.0758e-014        0.005032       0.0014117       0.0014117
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1157:        0.19530E+01

===============================================================


 INSTANT    0.115800000E+04   TIME STEP NUMBER            1158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74242E-02 0.88763E+00
   Friction velocity        uk    :  0.74242E-02 0.88763E+00
   Dimensionless distance   yplus :  0.59770E-01 0.71460E+01
   Friction thermal sca.    tstar : -0.80802E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44595E-01 0.53317E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81641E-02      32   0.31740E-03   0.20774E+01 0.99417E+02 
c  Velocity[X]                                      0.11103E+01 
c  Velocity[Y]                                      0.96709E+00 
c  Velocity[Z]                                      0.12034E-29 
c  Pressure     0.11022E-06     409   0.90939E-08   0.10985E+00 0.35328E+03 
c  nu_tilda     0.53672E-05      32   0.15621E-04   0.20927E-06 0.13163E+03 
c  TempC        0.32958E+02      27   0.32856E-03   0.70457E+01 0.28374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1079          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2644          7.1629      0.00046747      0.00046747
v  Velocity[Z]       -9.4315e-015     1.0108e-014    -6.9078e-018    -6.9078e-018
v  ǁVelocityǁ         0.0013569          10.454          5.2588          5.2588
v  Pressure               -52.128            18.8         -9.1796         -9.1796
v  nu_tilda           4.3251e-007       0.0042695       0.0012048       0.0012048
v  TempC                       21          73.069          21.759          21.759
v  TurbVisc           3.0772e-014        0.005032       0.0014125       0.0014125
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1158:        0.19260E+01

===============================================================


 INSTANT    0.115900000E+04   TIME STEP NUMBER            1159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92422E-02 0.88860E+00
   Friction velocity        uk    :  0.92422E-02 0.88860E+00
   Dimensionless distance   yplus :  0.74406E-01 0.71538E+01
   Friction thermal sca.    tstar : -0.78165E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55515E-01 0.53376E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81669E-02      32   0.37579E-03   0.21033E+01 0.99772E+02 
c  Velocity[X]                                      0.11125E+01 
c  Velocity[Y]                                      0.99076E+00 
c  Velocity[Z]                                      0.16317E-29 
c  Pressure     0.11612E-06     441   0.91200E-08   0.11696E+00 0.47645E+03 
c  nu_tilda     0.53689E-05      32   0.67698E-05   0.20945E-06 0.13167E+03 
c  TempC        0.32969E+02      26   0.29933E-03   0.47204E+01 0.21867E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1054          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2593          7.1439       0.0004562       0.0004562
v  Velocity[Z]       -9.3042e-015     1.0614e-014     -6.895e-018     -6.895e-018
v  ǁVelocityǁ        0.00076026          10.454          5.2588          5.2588
v  Pressure               -52.097          18.683         -9.2004         -9.2004
v  nu_tilda           4.3252e-007       0.0042695       0.0012055       0.0012055
v  TempC                       21          73.069           21.76           21.76
v  TurbVisc           3.0787e-014        0.005032       0.0014132       0.0014132
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1159:        0.20020E+01

===============================================================


 INSTANT    0.116000000E+04   TIME STEP NUMBER            1160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23213E-02 0.88791E+00
   Friction velocity        uk    :  0.23213E-02 0.88791E+00
   Dimensionless distance   yplus :  0.18688E-01 0.71483E+01
   Friction thermal sca.    tstar : -0.81590E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13944E-01 0.53334E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81697E-02      32   0.32188E-03   0.21393E+01 0.10008E+03 
c  Velocity[X]                                      0.11477E+01 
c  Velocity[Y]                                      0.99164E+00 
c  Velocity[Z]                                      0.12345E-29 
c  Pressure     0.12398E-06     297   0.99001E-08   0.12192E+00 0.20263E+03 
c  nu_tilda     0.53707E-05      32   0.15629E-04   0.20964E-06 0.13171E+03 
c  TempC        0.32979E+02      27   0.44938E-03   0.35072E+01 0.19710E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1029          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2559          7.1641      0.00044512      0.00044512
v  Velocity[Z]       -9.4408e-015     1.0153e-014    -6.8843e-018    -6.8843e-018
v  ǁVelocityǁ        0.00097732          10.454          5.2588          5.2588
v  Pressure               -52.094          18.743         -9.2053         -9.2053
v  nu_tilda            4.325e-007       0.0042695        0.001206        0.001206
v  TempC                       21          73.069           21.76           21.76
v  TurbVisc            3.079e-014        0.005032       0.0014139       0.0014139
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1160:        0.16600E+01

===============================================================


 INSTANT    0.116100000E+04   TIME STEP NUMBER            1161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97576E-02 0.88931E+00
   Friction velocity        uk    :  0.97576E-02 0.88931E+00
   Dimensionless distance   yplus :  0.78555E-01 0.71595E+01
   Friction thermal sca.    tstar : -0.79235E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58611E-01 0.53418E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81725E-02      32   0.32238E-03   0.20808E+01 0.99681E+02 
c  Velocity[X]                                      0.11025E+01 
c  Velocity[Y]                                      0.97831E+00 
c  Velocity[Z]                                      0.12207E-29 
c  Pressure     0.82540E-07     408   0.98546E-08   0.82318E-01 0.31175E+03 
c  nu_tilda     0.53724E-05      32   0.67553E-05   0.20981E-06 0.13175E+03 
c  TempC        0.32990E+02      27   0.37289E-03   0.64052E+01 0.27610E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1004          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2522          7.1747      0.00043386      0.00043386
v  Velocity[Z]       -9.4628e-015     1.0591e-014    -6.8723e-018    -6.8723e-018
v  ǁVelocityǁ        0.00083097          10.454          5.2589          5.2589
v  Pressure               -52.064          18.759         -9.1969         -9.1969
v  nu_tilda           4.3249e-007       0.0042695       0.0012067       0.0012067
v  TempC                       21          73.069           21.76           21.76
v  TurbVisc           3.0782e-014        0.005032       0.0014146       0.0014146
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1161:        0.19290E+01

===============================================================


 INSTANT    0.116200000E+04   TIME STEP NUMBER            1162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65342E-02 0.88905E+00
   Friction velocity        uk    :  0.65342E-02 0.88905E+00
   Dimensionless distance   yplus :  0.52605E-01 0.71574E+01
   Friction thermal sca.    tstar : -0.79209E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39249E-01 0.53402E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81753E-02      32   0.29737E-03   0.21229E+01 0.10013E+03 
c  Velocity[X]                                      0.11223E+01 
c  Velocity[Y]                                      0.10006E+01 
c  Velocity[Z]                                      0.15076E-29 
c  Pressure     0.11756E-06     488   0.93605E-08   0.11987E+00 0.66650E+03 
c  nu_tilda     0.53741E-05      32   0.15640E-04   0.21000E-06 0.13179E+03 
c  TempC        0.33000E+02      26   0.38115E-03   0.49281E+01 0.23726E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0978          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2476          7.1485      0.00042261      0.00042261
v  Velocity[Z]       -9.7904e-015     1.0117e-014    -6.8607e-018    -6.8607e-018
v  ǁVelocityǁ         0.0010879          10.454          5.2589          5.2589
v  Pressure               -52.059          18.652         -9.2381         -9.2381
v  nu_tilda            4.325e-007       0.0042695       0.0012072       0.0012072
v  TempC                       21          73.069          21.761          21.761
v  TurbVisc           3.0779e-014        0.005032       0.0014153       0.0014153
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1162:        0.21070E+01

===============================================================


 INSTANT    0.116300000E+04   TIME STEP NUMBER            1163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86158E-02 0.88759E+00
   Friction velocity        uk    :  0.86158E-02 0.88759E+00
   Dimensionless distance   yplus :  0.69363E-01 0.71457E+01
   Friction thermal sca.    tstar : -0.80679E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51753E-01 0.53315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81781E-02      32   0.32883E-03   0.21077E+01 0.10004E+03 
c  Velocity[X]                                      0.11207E+01 
c  Velocity[Y]                                      0.98698E+00 
c  Velocity[Z]                                      0.12813E-29 
c  Pressure     0.10702E-06     442   0.97436E-08   0.10548E+00 0.57687E+03 
c  nu_tilda     0.53759E-05      32   0.67624E-05   0.21018E-06 0.13183E+03 
c  TempC        0.33011E+02      26   0.34784E-03   0.47933E+01 0.21754E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0955          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2436          7.1717      0.00041149      0.00041149
v  Velocity[Z]        -1.003e-014     1.0622e-014    -6.8498e-018    -6.8498e-018
v  ǁVelocityǁ         0.0010488          10.454          5.2589          5.2589
v  Pressure               -52.025          18.737         -9.2118         -9.2118
v  nu_tilda           4.3249e-007       0.0042695       0.0012079       0.0012079
v  TempC                       21          73.069          21.761          21.761
v  TurbVisc           3.0782e-014        0.005032        0.001416        0.001416
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1163:        0.20200E+01

===============================================================


 INSTANT    0.116400000E+04   TIME STEP NUMBER            1164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95166E-02 0.88875E+00
   Friction velocity        uk    :  0.95166E-02 0.88875E+00
   Dimensionless distance   yplus :  0.76615E-01 0.71550E+01
   Friction thermal sca.    tstar : -0.80549E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57163E-01 0.53385E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81809E-02      32   0.33369E-03   0.21409E+01 0.10029E+03 
c  Velocity[X]                                      0.11573E+01 
c  Velocity[Y]                                      0.98358E+00 
c  Velocity[Z]                                      0.12835E-29 
c  Pressure     0.14149E-06     489   0.98052E-08   0.14013E+00 0.91860E+03 
c  nu_tilda     0.53776E-05      32   0.15639E-04   0.21038E-06 0.13188E+03 
c  TempC        0.33021E+02      26   0.38926E-03   0.44423E+01 0.21584E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0931          10.453          4.5729          4.5729
v  Velocity[Y]              -3.24          7.1454      0.00040041      0.00040041
v  Velocity[Z]       -9.2703e-015     1.0159e-014    -6.8354e-018    -6.8354e-018
v  ǁVelocityǁ        0.00086064          10.454          5.2589          5.2589
v  Pressure               -52.025          18.571         -9.2685         -9.2685
v  nu_tilda           4.3256e-007       0.0042695       0.0012084       0.0012084
v  TempC                       21          73.069          21.762          21.762
v  TurbVisc            3.078e-014        0.005032       0.0014167       0.0014167
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1164:        0.21140E+01

===============================================================


 INSTANT    0.116500000E+04   TIME STEP NUMBER            1165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72183E-02 0.88825E+00
   Friction velocity        uk    :  0.72183E-02 0.88825E+00
   Dimensionless distance   yplus :  0.58113E-01 0.71510E+01
   Friction thermal sca.    tstar : -0.83229E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43359E-01 0.53354E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81836E-02      32   0.29055E-03   0.21310E+01 0.10036E+03 
c  Velocity[X]                                      0.11260E+01 
c  Velocity[Y]                                      0.10051E+01 
c  Velocity[Z]                                      0.15453E-29 
c  Pressure     0.11677E-06     488   0.91064E-08   0.11651E+00 0.83649E+03 
c  nu_tilda     0.53793E-05      32   0.67467E-05   0.21057E-06 0.13192E+03 
c  TempC        0.33031E+02      27   0.35147E-03   0.44865E+01 0.21465E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0906          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2363          7.1702      0.00038903      0.00038903
v  Velocity[Z]       -9.9409e-015     1.0597e-014    -6.8239e-018    -6.8239e-018
v  ǁVelocityǁ          0.001307          10.454           5.259           5.259
v  Pressure               -51.995          18.731         -9.2299         -9.2299
v  nu_tilda            4.326e-007       0.0042695       0.0012091       0.0012091
v  TempC                       21          73.069          21.762          21.762
v  TurbVisc             3.08e-014        0.005032       0.0014175       0.0014175
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1165:        0.21270E+01

===============================================================


 INSTANT    0.116600000E+04   TIME STEP NUMBER            1166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11526E-01 0.88942E+00
   Friction velocity        uk    :  0.11526E-01 0.88942E+00
   Dimensionless distance   yplus :  0.92790E-01 0.71605E+01
   Friction thermal sca.    tstar : -0.80030E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69232E-01 0.53425E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81864E-02      32   0.27975E-03   0.20876E+01 0.10006E+03 
c  Velocity[X]                                      0.10944E+01 
c  Velocity[Y]                                      0.99315E+00 
c  Velocity[Z]                                      0.10793E-29 
c  Pressure     0.95591E-07     441   0.97823E-08   0.95403E-01 0.36338E+03 
c  nu_tilda     0.53811E-05      32   0.15649E-04   0.21078E-06 0.13197E+03 
c  TempC        0.33042E+02      27   0.32955E-03   0.46316E+01 0.21667E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0881          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2316          7.1797      0.00037812      0.00037812
v  Velocity[Z]       -1.0063e-014     1.0125e-014    -6.8117e-018    -6.8117e-018
v  ǁVelocityǁ        0.00075067          10.454           5.259           5.259
v  Pressure                -51.99          18.693         -9.2539         -9.2539
v  nu_tilda           4.3253e-007       0.0042695       0.0012096       0.0012096
v  TempC                       21          73.165          21.762          21.762
v  TurbVisc           3.0811e-014        0.005032       0.0014182       0.0014182
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1166:        0.20060E+01

===============================================================


 INSTANT    0.116700000E+04   TIME STEP NUMBER            1167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24448E-02 0.88899E+00
   Friction velocity        uk    :  0.24448E-02 0.88899E+00
   Dimensionless distance   yplus :  0.19682E-01 0.71570E+01
   Friction thermal sca.    tstar : -0.79786E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14685E-01 0.53399E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81892E-02      32   0.35716E-03   0.21203E+01 0.10036E+03 
c  Velocity[X]                                      0.11305E+01 
c  Velocity[Y]                                      0.98989E+00 
c  Velocity[Z]                                      0.12512E-29 
c  Pressure     0.11983E-06     456   0.95653E-08   0.11956E+00 0.53551E+03 
c  nu_tilda     0.53828E-05      32   0.67290E-05   0.21098E-06 0.13201E+03 
c  TempC        0.33052E+02      26   0.42646E-03   0.51539E+01 0.23218E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0856          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2275          7.1502       0.0003668       0.0003668
v  Velocity[Z]        -9.993e-015      1.063e-014    -6.7979e-018    -6.7979e-018
v  ǁVelocityǁ        0.00068295          10.454           5.259           5.259
v  Pressure               -51.956          18.561         -9.2769         -9.2769
v  nu_tilda           4.3253e-007       0.0042695       0.0012103       0.0012103
v  TempC                       21          73.069          21.763          21.763
v  TurbVisc            3.079e-014        0.005032       0.0014189       0.0014189
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1167:        0.20360E+01

===============================================================


 INSTANT    0.116800000E+04   TIME STEP NUMBER            1168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45841E-02 0.88782E+00
   Friction velocity        uk    :  0.45841E-02 0.88782E+00
   Dimensionless distance   yplus :  0.36905E-01 0.71476E+01
   Friction thermal sca.    tstar : -0.83981E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27535E-01 0.53329E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81919E-02      32   0.33828E-03   0.21703E+01 0.10092E+03 
c  Velocity[X]                                      0.11577E+01 
c  Velocity[Y]                                      0.10126E+01 
c  Velocity[Z]                                      0.16619E-29 
c  Pressure     0.11744E-06     346   0.98292E-08   0.11617E+00 0.22768E+03 
c  nu_tilda     0.53846E-05      32   0.15666E-04   0.21118E-06 0.13206E+03 
c  TempC        0.33063E+02      26   0.38995E-03   0.55031E+01 0.26586E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.083          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2236          7.1689       0.0003556       0.0003556
v  Velocity[Z]       -9.9994e-015     1.0167e-014    -6.7852e-018    -6.7852e-018
v  ǁVelocityǁ        0.00079737          10.454           5.259           5.259
v  Pressure               -51.954           18.63         -9.2809         -9.2809
v  nu_tilda           4.3252e-007       0.0042695       0.0012108       0.0012108
v  TempC                       21          73.069          21.763          21.763
v  TurbVisc           3.0791e-014        0.005032       0.0014196       0.0014196
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1168:        0.18230E+01

===============================================================


 INSTANT    0.116900000E+04   TIME STEP NUMBER            1169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58907E-02 0.88910E+00
   Friction velocity        uk    :  0.58907E-02 0.88910E+00
   Dimensionless distance   yplus :  0.47424E-01 0.71579E+01
   Friction thermal sca.    tstar : -0.81996E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35384E-01 0.53406E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81947E-02      32   0.30266E-03   0.21467E+01 0.10078E+03 
c  Velocity[X]                                      0.11426E+01 
c  Velocity[Y]                                      0.10041E+01 
c  Velocity[Z]                                      0.13201E-29 
c  Pressure     0.12323E-06     345   0.98785E-08   0.12433E+00 0.26732E+03 
c  nu_tilda     0.53863E-05      32   0.67279E-05   0.21136E-06 0.13210E+03 
c  TempC        0.33073E+02      26   0.32514E-03   0.44631E+01 0.22533E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0804          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2198          7.1522      0.00034452      0.00034452
v  Velocity[Z]        -1.008e-014     1.0605e-014    -6.7734e-018    -6.7734e-018
v  ǁVelocityǁ          0.001167          10.454           5.259           5.259
v  Pressure               -51.923          18.586         -9.2844         -9.2844
v  nu_tilda           4.3254e-007       0.0042695       0.0012115       0.0012115
v  TempC                       21          73.069          21.764          21.764
v  TurbVisc           3.0789e-014        0.005032       0.0014203       0.0014203
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1169:        0.20170E+01

===============================================================


 INSTANT    0.117000000E+04   TIME STEP NUMBER            1170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10567E-01 0.88832E+00
   Friction velocity        uk    :  0.10567E-01 0.88832E+00
   Dimensionless distance   yplus :  0.85075E-01 0.71515E+01
   Friction thermal sca.    tstar : -0.83328E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63476E-01 0.53359E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.81975E-02      32   0.34044E-03   0.21221E+01 0.10056E+03 
c  Velocity[X]                                      0.11281E+01 
c  Velocity[Y]                                      0.99398E+00 
c  Velocity[Z]                                      0.11333E-29 
c  Pressure     0.12361E-06     425   0.97789E-08   0.12109E+00 0.24958E+03 
c  nu_tilda     0.53881E-05      32   0.15660E-04   0.21155E-06 0.13214E+03 
c  TempC        0.33084E+02      27   0.41928E-03   0.52696E+01 0.21411E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0779          10.453          4.5729          4.5729
v  Velocity[Y]            -3.2156          7.1723      0.00033356      0.00033356
v  Velocity[Z]        -1.034e-014     1.0131e-014    -6.7629e-018    -6.7629e-018
v  ǁVelocityǁ        0.00095639          10.454          5.2591          5.2591
v  Pressure                -51.92          18.584         -9.3025         -9.3025
v  nu_tilda           4.3259e-007       0.0042695        0.001212        0.001212
v  TempC                       21          73.069          21.764          21.764
v  TurbVisc           3.0793e-014        0.005032        0.001421        0.001421
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1170:        0.20930E+01

===============================================================


 INSTANT    0.117100000E+04   TIME STEP NUMBER            1171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86354E-02 0.88987E+00
   Friction velocity        uk    :  0.86354E-02 0.88987E+00
   Dimensionless distance   yplus :  0.69521E-01 0.71641E+01
   Friction thermal sca.    tstar : -0.83373E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51870E-01 0.53452E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82002E-02      32   0.32569E-03   0.21239E+01 0.10065E+03 
c  Velocity[X]                                      0.11279E+01 
c  Velocity[Y]                                      0.99600E+00 
c  Velocity[Z]                                      0.16135E-29 
c  Pressure     0.11317E-06     456   0.93175E-08   0.11260E+00 0.53973E+03 
c  nu_tilda     0.53898E-05      32   0.67151E-05   0.21173E-06 0.13219E+03 
c  TempC        0.33094E+02      27   0.32052E-03   0.47882E+01 0.21526E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0755          10.454          4.5729          4.5729
v  Velocity[Y]            -3.2114          7.1833      0.00032221      0.00032221
v  Velocity[Z]       -1.0518e-014     1.0635e-014    -6.7528e-018    -6.7528e-018
v  ǁVelocityǁ        0.00092932          10.454          5.2591          5.2591
v  Pressure               -51.885          18.664         -9.2786         -9.2786
v  nu_tilda           4.3259e-007       0.0042695       0.0012127       0.0012127
v  TempC                       21          73.069          21.764          21.764
v  TurbVisc            3.081e-014        0.005032       0.0014217       0.0014217
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1171:        0.20320E+01

===============================================================


 INSTANT    0.117200000E+04   TIME STEP NUMBER            1172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83369E-02 0.88934E+00
   Friction velocity        uk    :  0.83369E-02 0.88934E+00
   Dimensionless distance   yplus :  0.67118E-01 0.71598E+01
   Friction thermal sca.    tstar : -0.81919E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50077E-01 0.53420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82030E-02      32   0.31486E-03   0.21553E+01 0.10102E+03 
c  Velocity[X]                                      0.11347E+01 
c  Velocity[Y]                                      0.10206E+01 
c  Velocity[Z]                                      0.13549E-29 
c  Pressure     0.11838E-06     490   0.94278E-08   0.11894E+00 0.96367E+03 
c  nu_tilda     0.53915E-05      32   0.15674E-04   0.21194E-06 0.13223E+03 
c  TempC        0.33105E+02      27   0.32836E-03   0.28146E+01 0.17475E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.073          10.454          4.5729          4.5729
v  Velocity[Y]            -3.2072          7.1556      0.00031112      0.00031112
v  Velocity[Z]       -1.0177e-014     1.0172e-014    -6.7392e-018    -6.7392e-018
v  ǁVelocityǁ         0.0011684          10.454          5.2591          5.2591
v  Pressure               -51.886          18.484         -9.3371         -9.3371
v  nu_tilda           4.3259e-007       0.0042695       0.0012132       0.0012132
v  TempC                       21          73.069          21.765          21.765
v  TurbVisc           3.0808e-014        0.005032       0.0014224       0.0014224
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1172:        0.21130E+01

===============================================================


 INSTANT    0.117300000E+04   TIME STEP NUMBER            1173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10586E-01 0.88813E+00
   Friction velocity        uk    :  0.10586E-01 0.88813E+00
   Dimensionless distance   yplus :  0.85226E-01 0.71500E+01
   Friction thermal sca.    tstar : -0.84990E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63588E-01 0.53347E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82057E-02      32   0.31069E-03   0.21458E+01 0.10099E+03 
c  Velocity[X]                                      0.11265E+01 
c  Velocity[Y]                                      0.10193E+01 
c  Velocity[Z]                                      0.12219E-29 
c  Pressure     0.11016E-06     472   0.96390E-08   0.10862E+00 0.73121E+03 
c  nu_tilda     0.53933E-05      32   0.66949E-05   0.21213E-06 0.13228E+03 
c  TempC        0.33115E+02      26   0.44696E-03   0.49564E+01 0.22619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0704          10.454          4.5729          4.5729
v  Velocity[Y]            -3.2028          7.1739       0.0002999       0.0002999
v  Velocity[Z]       -1.0638e-014     1.0611e-014    -6.7309e-018    -6.7309e-018
v  ǁVelocityǁ        0.00078672          10.454          5.2591          5.2591
v  Pressure               -51.855          18.614         -9.3034         -9.3034
v  nu_tilda           4.3257e-007       0.0042695       0.0012139       0.0012139
v  TempC                       21          73.069          21.765          21.765
v  TurbVisc           3.0807e-014        0.005032       0.0014232       0.0014232
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1173:        0.20730E+01

===============================================================


 INSTANT    0.117400000E+04   TIME STEP NUMBER            1174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57573E-02 0.88922E+00
   Friction velocity        uk    :  0.57573E-02 0.88922E+00
   Dimensionless distance   yplus :  0.46350E-01 0.71588E+01
   Friction thermal sca.    tstar : -0.82639E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34582E-01 0.53413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82085E-02      32   0.35986E-03   0.21365E+01 0.10096E+03 
c  Velocity[X]                                      0.11302E+01 
c  Velocity[Y]                                      0.10063E+01 
c  Velocity[Z]                                      0.11482E-29 
c  Pressure     0.11641E-06     489   0.95933E-08   0.11696E+00 0.10048E+04 
c  nu_tilda     0.53950E-05      32   0.15684E-04   0.21235E-06 0.13232E+03 
c  TempC        0.33126E+02      26   0.31545E-03   0.58131E+01 0.26920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0678          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1991          7.1523      0.00028885      0.00028885
v  Velocity[Z]       -1.0735e-014     1.0136e-014    -6.7198e-018    -6.7198e-018
v  ǁVelocityǁ        0.00058087          10.454          5.2591          5.2591
v  Pressure               -51.847          18.429         -9.3611         -9.3611
v  nu_tilda           4.3264e-007       0.0042695       0.0012144       0.0012144
v  TempC                       21          73.069          21.765          21.765
v  TurbVisc           3.0803e-014        0.005032       0.0014239       0.0014239
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1174:        0.21110E+01

===============================================================


 INSTANT    0.117500000E+04   TIME STEP NUMBER            1175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38990E-02 0.88866E+00
   Friction velocity        uk    :  0.38990E-02 0.88866E+00
   Dimensionless distance   yplus :  0.31390E-01 0.71543E+01
   Friction thermal sca.    tstar : -0.87049E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23420E-01 0.53379E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82112E-02      32   0.33721E-03   0.21844E+01 0.10148E+03 
c  Velocity[X]                                      0.11538E+01 
c  Velocity[Y]                                      0.10306E+01 
c  Velocity[Z]                                      0.16516E-29 
c  Pressure     0.12736E-06     489   0.91603E-08   0.12659E+00 0.10019E+04 
c  nu_tilda     0.53968E-05      32   0.66915E-05   0.21255E-06 0.13237E+03 
c  TempC        0.33136E+02      26   0.30319E-03   0.39002E+01 0.20466E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0652          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1945          7.1786      0.00027767      0.00027767
v  Velocity[Z]       -1.0772e-014      1.064e-014    -6.7076e-018    -6.7076e-018
v  ǁVelocityǁ        0.00073902          10.454          5.2591          5.2591
v  Pressure               -51.819           18.62         -9.3133         -9.3133
v  nu_tilda           4.3268e-007       0.0042695       0.0012151       0.0012151
v  TempC                       21          73.069          21.766          21.766
v  TurbVisc           3.0823e-014        0.005032       0.0014246       0.0014246
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1175:        0.20980E+01

===============================================================


 INSTANT    0.117600000E+04   TIME STEP NUMBER            1176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18613E-02 0.88983E+00
   Friction velocity        uk    :  0.18613E-02 0.88983E+00
   Dimensionless distance   yplus :  0.14985E-01 0.71638E+01
   Friction thermal sca.    tstar : -0.83761E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11180E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82140E-02      32   0.29280E-03   0.21599E+01 0.10134E+03 
c  Velocity[X]                                      0.11435E+01 
c  Velocity[Y]                                      0.10164E+01 
c  Velocity[Z]                                      0.12660E-29 
c  Pressure     0.11868E-06     472   0.93057E-08   0.11560E+00 0.73703E+03 
c  nu_tilda     0.53985E-05      32   0.15680E-04   0.21277E-06 0.13242E+03 
c  TempC        0.33146E+02      26   0.40426E-03   0.41219E+01 0.19119E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0625          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1901          7.1813      0.00026655      0.00026655
v  Velocity[Z]        -1.076e-014     1.0177e-014     -6.699e-018     -6.699e-018
v  ǁVelocityǁ         0.0013448          10.454          5.2591          5.2591
v  Pressure               -51.814          18.499         -9.3586         -9.3586
v  nu_tilda           4.3268e-007       0.0042695       0.0012156       0.0012156
v  TempC                       21          73.271          21.766          21.766
v  TurbVisc           3.0835e-014        0.005032       0.0014253       0.0014253
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1176:        0.20670E+01

===============================================================


 INSTANT    0.117700000E+04   TIME STEP NUMBER            1177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60612E-02 0.88978E+00
   Friction velocity        uk    :  0.60612E-02 0.88978E+00
   Dimensionless distance   yplus :  0.48797E-01 0.71634E+01
   Friction thermal sca.    tstar : -0.84573E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36408E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82167E-02      32   0.31953E-03   0.21553E+01 0.10129E+03 
c  Velocity[X]                                      0.11438E+01 
c  Velocity[Y]                                      0.10116E+01 
c  Velocity[Z]                                      0.15563E-29 
c  Pressure     0.11116E-06     297   0.91415E-08   0.11218E+00 0.27847E+03 
c  nu_tilda     0.54003E-05      32   0.66789E-05   0.21296E-06 0.13247E+03 
c  TempC        0.33157E+02      27   0.36022E-03   0.45304E+01 0.21472E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.06          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1857          7.1578      0.00025529      0.00025529
v  Velocity[Z]       -1.0827e-014     1.0615e-014    -6.6903e-018    -6.6903e-018
v  ǁVelocityǁ        0.00079557          10.454          5.2591          5.2591
v  Pressure                -51.78          18.466         -9.3581         -9.3581
v  nu_tilda           4.3274e-007       0.0042695       0.0012163       0.0012163
v  TempC                       21          73.069          21.767          21.767
v  TurbVisc           3.0833e-014        0.005032        0.001426        0.001426
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1177:        0.16680E+01

===============================================================


 INSTANT    0.117800000E+04   TIME STEP NUMBER            1178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60941E-02 0.88852E+00
   Friction velocity        uk    :  0.60941E-02 0.88852E+00
   Dimensionless distance   yplus :  0.49062E-01 0.71532E+01
   Friction thermal sca.    tstar : -0.86686E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36606E-01 0.53371E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82194E-02      32   0.32765E-03   0.21557E+01 0.10148E+03 
c  Velocity[X]                                      0.11208E+01 
c  Velocity[Y]                                      0.10349E+01 
c  Velocity[Z]                                      0.11913E-29 
c  Pressure     0.10059E-06     361   0.93080E-08   0.99971E-01 0.18663E+03 
c  nu_tilda     0.54020E-05      32   0.15697E-04   0.21317E-06 0.13251E+03 
c  TempC        0.33167E+02      27   0.40035E-03   0.38192E+01 0.20084E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0575          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1816          7.1775      0.00024436      0.00024436
v  Velocity[Z]       -1.0776e-014     1.0141e-014    -6.6799e-018    -6.6799e-018
v  ǁVelocityǁ         0.0011225          10.454          5.2591          5.2591
v  Pressure               -51.779          18.514         -9.3682         -9.3682
v  nu_tilda           4.3278e-007       0.0042695       0.0012168       0.0012168
v  TempC                       21          73.069          21.767          21.767
v  TurbVisc           3.0852e-014        0.005032       0.0014267       0.0014267
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1178:        0.18180E+01

===============================================================


 INSTANT    0.117900000E+04   TIME STEP NUMBER            1179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10268E-01 0.88965E+00
   Friction velocity        uk    :  0.10268E-01 0.88965E+00
   Dimensionless distance   yplus :  0.82667E-01 0.71623E+01
   Friction thermal sca.    tstar : -0.84924E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61679E-01 0.53439E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82222E-02      32   0.32042E-03   0.21767E+01 0.10163E+03 
c  Velocity[X]                                      0.11523E+01 
c  Velocity[Y]                                      0.10243E+01 
c  Velocity[Z]                                      0.11589E-29 
c  Pressure     0.13601E-06     456   0.95606E-08   0.13441E+00 0.45904E+03 
c  nu_tilda     0.54038E-05      32   0.66646E-05   0.21336E-06 0.13256E+03 
c  TempC        0.33178E+02      27   0.34223E-03   0.51310E+01 0.22468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0549          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1775          7.1551      0.00023318      0.00023318
v  Velocity[Z]       -1.0945e-014     1.0644e-014    -6.6725e-018    -6.6725e-018
v  ǁVelocityǁ        0.00092711          10.454          5.2591          5.2591
v  Pressure               -51.746          18.398         -9.3843         -9.3843
v  nu_tilda           4.3283e-007       0.0042695       0.0012175       0.0012175
v  TempC                       21          73.069          21.767          21.767
v  TurbVisc           3.0862e-014        0.005032       0.0014274       0.0014274
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1179:        0.20260E+01

===============================================================


 INSTANT    0.118000000E+04   TIME STEP NUMBER            1180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83636E-02 0.88931E+00
   Friction velocity        uk    :  0.83636E-02 0.88931E+00
   Dimensionless distance   yplus :  0.67333E-01 0.71595E+01
   Friction thermal sca.    tstar : -0.90002E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50238E-01 0.53418E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82249E-02      32   0.31934E-03   0.21598E+01 0.10158E+03 
c  Velocity[X]                                      0.11411E+01 
c  Velocity[Y]                                      0.10188E+01 
c  Velocity[Z]                                      0.11310E-29 
c  Pressure     0.10812E-06     362   0.93684E-08   0.10661E+00 0.24364E+03 
c  nu_tilda     0.54056E-05      32   0.15705E-04   0.21356E-06 0.13260E+03 
c  TempC        0.33188E+02      26   0.27669E-03   0.44416E+01 0.21427E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0523          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1735          7.1811      0.00022221      0.00022221
v  Velocity[Z]       -1.0918e-014     1.0181e-014    -6.6611e-018    -6.6611e-018
v  ǁVelocityǁ        0.00093923          10.454          5.2591          5.2591
v  Pressure               -51.743          18.478         -9.3886         -9.3886
v  nu_tilda           4.3286e-007       0.0042695        0.001218        0.001218
v  TempC                       21          73.076          21.768          21.768
v  TurbVisc           3.0877e-014        0.005032       0.0014281       0.0014281
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1180:        0.18030E+01

===============================================================


 INSTANT    0.118100000E+04   TIME STEP NUMBER            1181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85321E-02 0.89052E+00
   Friction velocity        uk    :  0.85321E-02 0.89052E+00
   Dimensionless distance   yplus :  0.68689E-01 0.71693E+01
   Friction thermal sca.    tstar : -0.86199E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51250E-01 0.53491E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82276E-02      32   0.30030E-03   0.21559E+01 0.10169E+03 
c  Velocity[X]                                      0.11117E+01 
c  Velocity[Y]                                      0.10442E+01 
c  Velocity[Z]                                      0.15846E-29 
c  Pressure     0.96568E-07     424   0.97139E-08   0.95654E-01 0.40473E+03 
c  nu_tilda     0.54073E-05      32   0.66636E-05   0.21376E-06 0.13265E+03 
c  TempC        0.33199E+02      27   0.36605E-03   0.35729E+01 0.17907E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0497          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1693           7.191      0.00021093      0.00021093
v  Velocity[Z]       -1.0914e-014     1.0618e-014    -6.6499e-018    -6.6499e-018
v  ǁVelocityǁ        0.00088139          10.454          5.2592          5.2592
v  Pressure               -51.713          18.513         -9.3726         -9.3726
v  nu_tilda           4.3282e-007       0.0042695       0.0012187       0.0012187
v  TempC                       21          73.069          21.768          21.768
v  TurbVisc           3.0886e-014        0.005032       0.0014288       0.0014288
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1181:        0.19590E+01

===============================================================


 INSTANT    0.118200000E+04   TIME STEP NUMBER            1182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87001E-02 0.89017E+00
   Friction velocity        uk    :  0.87001E-02 0.89017E+00
   Dimensionless distance   yplus :  0.70042E-01 0.71665E+01
   Friction thermal sca.    tstar : -0.85565E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52259E-01 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82304E-02      32   0.31884E-03   0.21800E+01 0.10183E+03 
c  Velocity[X]                                      0.11498E+01 
c  Velocity[Y]                                      0.10302E+01 
c  Velocity[Z]                                      0.13135E-29 
c  Pressure     0.11937E-06     473   0.90542E-08   0.11869E+00 0.88180E+03 
c  nu_tilda     0.54091E-05      32   0.15702E-04   0.21397E-06 0.13270E+03 
c  TempC        0.33209E+02      27   0.39322E-03   0.39038E+01 0.20429E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.047          10.454          4.5729          4.5729
v  Velocity[Y]             -3.166          7.1599      0.00020009      0.00020009
v  Velocity[Z]       -1.0918e-014     1.0143e-014    -6.6427e-018    -6.6427e-018
v  ǁVelocityǁ         0.0008102          10.454          5.2592          5.2592
v  Pressure               -51.708          18.356         -9.4247         -9.4247
v  nu_tilda            4.328e-007       0.0042695       0.0012192       0.0012192
v  TempC                       21          73.069          21.768          21.768
v  TurbVisc           3.0874e-014        0.005032       0.0014295       0.0014295
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1182:        0.20760E+01

===============================================================


 INSTANT    0.118300000E+04   TIME STEP NUMBER            1183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65260E-02 0.88890E+00
   Friction velocity        uk    :  0.65260E-02 0.88890E+00
   Dimensionless distance   yplus :  0.52539E-01 0.71563E+01
   Friction thermal sca.    tstar : -0.88855E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39200E-01 0.53394E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82331E-02      32   0.35236E-03   0.21992E+01 0.10210E+03 
c  Velocity[X]                                      0.11696E+01 
c  Velocity[Y]                                      0.10296E+01 
c  Velocity[Z]                                      0.15324E-29 
c  Pressure     0.12279E-06     441   0.97952E-08   0.12152E+00 0.48970E+03 
c  nu_tilda     0.54108E-05      32   0.66499E-05   0.21418E-06 0.13275E+03 
c  TempC        0.33219E+02      27   0.41707E-03   0.59165E+01 0.22743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0442          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1621          7.1842      0.00018878      0.00018878
v  Velocity[Z]       -1.0971e-014     1.0646e-014    -6.6268e-018    -6.6268e-018
v  ǁVelocityǁ         0.0012825          10.454          5.2591          5.2591
v  Pressure               -51.677          18.434          -9.406          -9.406
v  nu_tilda           4.3277e-007       0.0042695       0.0012198       0.0012198
v  TempC                       21          73.069          21.769          21.769
v  TurbVisc           3.0869e-014        0.005032       0.0014302       0.0014302
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1183:        0.20020E+01

===============================================================


 INSTANT    0.118400000E+04   TIME STEP NUMBER            1184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11416E-01 0.89013E+00
   Friction velocity        uk    :  0.11416E-01 0.89013E+00
   Dimensionless distance   yplus :  0.91907E-01 0.71662E+01
   Friction thermal sca.    tstar : -0.88787E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68573E-01 0.53468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82358E-02      32   0.32082E-03   0.22053E+01 0.10234E+03 
c  Velocity[X]                                      0.11548E+01 
c  Velocity[Y]                                      0.10505E+01 
c  Velocity[Z]                                      0.12981E-29 
c  Pressure     0.10784E-06     458   0.99165E-08   0.10755E+00 0.63830E+03 
c  nu_tilda     0.54126E-05      32   0.15716E-04   0.21441E-06 0.13280E+03 
c  TempC        0.33230E+02      27   0.33550E-03   0.62184E+01 0.25653E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0416          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1582          7.1613      0.00017788      0.00017788
v  Velocity[Z]       -1.1163e-014     1.0184e-014    -6.6177e-018    -6.6177e-018
v  ǁVelocityǁ        0.00074388          10.454          5.2591          5.2591
v  Pressure               -51.673          18.328          -9.445          -9.445
v  nu_tilda           4.3282e-007       0.0042695       0.0012204       0.0012204
v  TempC                       21          73.069          21.769          21.769
v  TurbVisc           3.0861e-014        0.005032       0.0014309       0.0014309
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1184:        0.20230E+01

===============================================================


 INSTANT    0.118500000E+04   TIME STEP NUMBER            1185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37518E-02 0.88933E+00
   Friction velocity        uk    :  0.37518E-02 0.88933E+00
   Dimensionless distance   yplus :  0.30205E-01 0.71597E+01
   Friction thermal sca.    tstar : -0.90338E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22536E-01 0.53419E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82385E-02      32   0.30500E-03   0.21831E+01 0.10205E+03 
c  Velocity[X]                                      0.11466E+01 
c  Velocity[Y]                                      0.10365E+01 
c  Velocity[Z]                                      0.13773E-29 
c  Pressure     0.12673E-06     458   0.93309E-08   0.12335E+00 0.78562E+03 
c  nu_tilda     0.54143E-05      32   0.66303E-05   0.21461E-06 0.13284E+03 
c  TempC        0.33240E+02      26   0.33145E-03   0.44710E+01 0.22795E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0391          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1544          7.1849      0.00016686      0.00016686
v  Velocity[Z]       -1.1046e-014      1.062e-014    -6.6124e-018    -6.6124e-018
v  ǁVelocityǁ         0.0014799          10.454          5.2591          5.2591
v  Pressure               -51.639          18.457         -9.4058         -9.4058
v  nu_tilda           4.3282e-007       0.0042695        0.001221        0.001221
v  TempC                       21          73.069           21.77           21.77
v  TurbVisc           3.0874e-014        0.005032       0.0014316       0.0014316
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1185:        0.20350E+01

===============================================================


 INSTANT    0.118600000E+04   TIME STEP NUMBER            1186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11235E-01 0.89079E+00
   Friction velocity        uk    :  0.11235E-01 0.89079E+00
   Dimensionless distance   yplus :  0.90445E-01 0.71714E+01
   Friction thermal sca.    tstar : -0.88367E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67482E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82412E-02      32   0.32123E-03   0.21796E+01 0.10214E+03 
c  Velocity[X]                                      0.11450E+01 
c  Velocity[Y]                                      0.10346E+01 
c  Velocity[Z]                                      0.11272E-29 
c  Pressure     0.10669E-06     474   0.99193E-08   0.10551E+00 0.67611E+03 
c  nu_tilda     0.54161E-05      32   0.15722E-04   0.21483E-06 0.13289E+03 
c  TempC        0.33251E+02      26   0.48143E-03   0.56087E+01 0.24512E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0364          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1501          7.1942      0.00015551      0.00015551
v  Velocity[Z]       -1.1107e-014     1.0146e-014     -6.591e-018     -6.591e-018
v  ǁVelocityǁ        0.00074674          10.454          5.2591          5.2591
v  Pressure               -51.639           18.37         -9.4519         -9.4519
v  nu_tilda           4.3278e-007       0.0042695       0.0012216       0.0012216
v  TempC                       21          73.069           21.77           21.77
v  TurbVisc           3.0875e-014        0.005032       0.0014324       0.0014324
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1186:        0.20790E+01

===============================================================


 INSTANT    0.118700000E+04   TIME STEP NUMBER            1187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38032E-02 0.89047E+00
   Friction velocity        uk    :  0.38032E-02 0.89047E+00
   Dimensionless distance   yplus :  0.30619E-01 0.71689E+01
   Friction thermal sca.    tstar : -0.87901E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22845E-01 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82439E-02      32   0.30215E-03   0.22001E+01 0.10244E+03 
c  Velocity[X]                                      0.11430E+01 
c  Velocity[Y]                                      0.10572E+01 
c  Velocity[Z]                                      0.10924E-29 
c  Pressure     0.11297E-06     314   0.91967E-08   0.11366E+00 0.28576E+03 
c  nu_tilda     0.54179E-05      32   0.66275E-05   0.21502E-06 0.13294E+03 
c  TempC        0.33261E+02      27   0.30446E-03   0.74001E+01 0.28795E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0337          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1464          7.1689      0.00014436      0.00014436
v  Velocity[Z]       -1.0955e-014     1.0648e-014    -6.5836e-018    -6.5836e-018
v  ǁVelocityǁ        0.00074964          10.454          5.2591          5.2591
v  Pressure               -51.606          18.332           -9.45           -9.45
v  nu_tilda           4.3281e-007       0.0042695       0.0012222       0.0012222
v  TempC                       21          73.069           21.77           21.77
v  TurbVisc           3.0863e-014        0.005032       0.0014331       0.0014331
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1187:        0.17080E+01

===============================================================


 INSTANT    0.118800000E+04   TIME STEP NUMBER            1188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77498E-02 0.88901E+00
   Friction velocity        uk    :  0.77498E-02 0.88901E+00
   Dimensionless distance   yplus :  0.62391E-01 0.71571E+01
   Friction thermal sca.    tstar : -0.91583E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46551E-01 0.53400E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82466E-02      32   0.27901E-03   0.21804E+01 0.10229E+03 
c  Velocity[X]                                      0.11363E+01 
c  Velocity[Y]                                      0.10441E+01 
c  Velocity[Z]                                      0.16256E-29 
c  Pressure     0.10703E-06     392   0.99480E-08   0.10436E+00 0.19607E+03 
c  nu_tilda     0.54196E-05      32   0.15726E-04   0.21523E-06 0.13299E+03 
c  TempC        0.33271E+02      26   0.31156E-03   0.37392E+01 0.20336E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.031          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1426          7.1842      0.00013343      0.00013343
v  Velocity[Z]       -1.0828e-014     1.0185e-014    -6.5773e-018    -6.5773e-018
v  ǁVelocityǁ        0.00082339          10.454          5.2591          5.2591
v  Pressure               -51.602          18.353         -9.4627         -9.4627
v  nu_tilda           4.3285e-007       0.0042695       0.0012228       0.0012228
v  TempC                       21          73.069          21.771          21.771
v  TurbVisc           3.0872e-014        0.005032       0.0014338       0.0014338
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1188:        0.18870E+01

===============================================================


 INSTANT    0.118900000E+04   TIME STEP NUMBER            1189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66715E-02 0.89022E+00
   Friction velocity        uk    :  0.66715E-02 0.89022E+00
   Dimensionless distance   yplus :  0.53710E-01 0.71669E+01
   Friction thermal sca.    tstar : -0.11456E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40074E-01 0.53473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82493E-02      32   0.36410E-03   0.21839E+01 0.10239E+03 
c  Velocity[X]                                      0.11418E+01 
c  Velocity[Y]                                      0.10421E+01 
c  Velocity[Z]                                      0.16821E-29 
c  Pressure     0.10562E-06     266   0.96886E-08   0.10615E+00 0.27953E+03 
c  nu_tilda     0.54214E-05      32   0.66091E-05   0.21543E-06 0.13303E+03 
c  TempC        0.33282E+02      27   0.39651E-03   0.36683E+01 0.19669E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0283          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1387          7.1658      0.00012215      0.00012215
v  Velocity[Z]       -1.0625e-014     1.0621e-014    -6.5652e-018    -6.5652e-018
v  ǁVelocityǁ         0.0011325          10.454          5.2591          5.2591
v  Pressure                -51.57          18.307         -9.4638         -9.4638
v  nu_tilda           4.3292e-007       0.0042695       0.0012234       0.0012234
v  TempC                       21          73.069          21.771          21.771
v  TurbVisc           3.0883e-014        0.005032       0.0014345       0.0014345
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1189:        0.15830E+01

===============================================================


 INSTANT    0.119000000E+04   TIME STEP NUMBER            1190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10327E-01 0.88958E+00
   Friction velocity        uk    :  0.10327E-01 0.88958E+00
   Dimensionless distance   yplus :  0.83136E-01 0.71617E+01
   Friction thermal sca.    tstar : -0.17320E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62029E-01 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82520E-02      32   0.28106E-03   0.22340E+01 0.10295E+03 
c  Velocity[X]                                      0.11679E+01 
c  Velocity[Y]                                      0.10661E+01 
c  Velocity[Z]                                      0.12377E-29 
c  Pressure     0.12609E-06     410   0.95719E-08   0.12460E+00 0.22755E+03 
c  nu_tilda     0.54232E-05      32   0.15737E-04   0.21565E-06 0.13308E+03 
c  TempC        0.33292E+02      27   0.33229E-03   0.53213E+01 0.25027E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0255          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1338           7.191      0.00011103      0.00011103
v  Velocity[Z]        -1.041e-014     1.0148e-014    -6.5548e-018    -6.5548e-018
v  ǁVelocityǁ        0.00094268          10.454          5.2591          5.2591
v  Pressure               -51.567           18.34         -9.4806         -9.4806
v  nu_tilda           4.3291e-007       0.0042695        0.001224        0.001224
v  TempC                       21          73.069          21.771          21.771
v  TurbVisc           3.0903e-014        0.005032       0.0014352       0.0014352
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1190:        0.19240E+01

===============================================================


 INSTANT    0.119100000E+04   TIME STEP NUMBER            1191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58177E-02 0.89101E+00
   Friction velocity        uk    :  0.58177E-02 0.89101E+00
   Dimensionless distance   yplus :  0.46836E-01 0.71733E+01
   Friction thermal sca.    tstar : -0.12982E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34945E-01 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82547E-02      32   0.29355E-03   0.22083E+01 0.10278E+03 
c  Velocity[X]                                      0.11543E+01 
c  Velocity[Y]                                      0.10540E+01 
c  Velocity[Z]                                      0.10714E-29 
c  Pressure     0.12520E-06     394   0.99817E-08   0.12218E+00 0.31638E+03 
c  nu_tilda     0.54249E-05      32   0.65906E-05   0.21586E-06 0.13313E+03 
c  TempC        0.33302E+02      26   0.44259E-03   0.52214E+01 0.22571E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0229          10.454          4.5729          4.5729
v  Velocity[Y]            -3.1299          7.1965      0.00010002      0.00010002
v  Velocity[Z]       -1.0223e-014     1.0649e-014    -6.5463e-018    -6.5463e-018
v  ǁVelocityǁ        0.00097949          10.454          5.2591          5.2591
v  Pressure               -51.536          18.343         -9.4711         -9.4711
v  nu_tilda           4.3289e-007       0.0042695       0.0012246       0.0012246
v  TempC                       21          73.069          21.772          21.772
v  TurbVisc             3.09e-014        0.005032       0.0014359       0.0014359
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1191:        0.18850E+01

===============================================================


 INSTANT    0.119200000E+04   TIME STEP NUMBER            1192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88915E-02 0.89085E+00
   Friction velocity        uk    :  0.88915E-02 0.89085E+00
   Dimensionless distance   yplus :  0.71582E-01 0.71720E+01
   Friction thermal sca.    tstar : -0.21264E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53408E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82574E-02      32   0.31961E-03   0.22064E+01 0.10279E+03 
c  Velocity[X]                                      0.11572E+01 
c  Velocity[Y]                                      0.10492E+01 
c  Velocity[Z]                                      0.11882E-29 
c  Pressure     0.10957E-06     457   0.95150E-08   0.11062E+00 0.76867E+03 
c  nu_tilda     0.54267E-05      32   0.15747E-04   0.21609E-06 0.13318E+03 
c  TempC        0.33313E+02      27   0.39291E-03   0.60948E+01 0.26314E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0202          10.453          4.5729          4.5729
v  Velocity[Y]            -3.1257          7.1717     8.8861e-005     8.8861e-005
v  Velocity[Z]       -1.0098e-014     1.0186e-014    -6.5387e-018    -6.5387e-018
v  ǁVelocityǁ         0.0011008          10.454          5.2591          5.2591
v  Pressure               -51.531          18.207         -9.5175         -9.5175
v  nu_tilda           4.3295e-007       0.0042695       0.0012252       0.0012252
v  TempC                       21          73.069          21.772          21.772
v  TurbVisc           3.0894e-014        0.005032       0.0014366       0.0014366
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1192:        0.20410E+01

===============================================================


 INSTANT    0.119300000E+04   TIME STEP NUMBER            1193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99727E-02 0.88968E+00
   Friction velocity        uk    :  0.99727E-02 0.88968E+00
   Dimensionless distance   yplus :  0.80287E-01 0.71625E+01
   Friction thermal sca.    tstar : -0.22857E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59903E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82601E-02      32   0.33017E-03   0.22098E+01 0.10294E+03 
c  Velocity[X]                                      0.11388E+01 
c  Velocity[Y]                                      0.10710E+01 
c  Velocity[Z]                                      0.13176E-29 
c  Pressure     0.11088E-06     473   0.93809E-08   0.10891E+00 0.93839E+03 
c  nu_tilda     0.54285E-05      32   0.65906E-05   0.21630E-06 0.13324E+03 
c  TempC        0.33323E+02      26   0.38899E-03   0.52842E+01 0.25179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0176          10.453          4.5729          4.5729
v  Velocity[Y]            -3.1214          7.1929     7.7916e-005     7.7916e-005
v  Velocity[Z]       -9.9754e-015     1.0622e-014    -6.5365e-018    -6.5365e-018
v  ǁVelocityǁ        0.00084811          10.454          5.2591          5.2591
v  Pressure               -51.497          18.378         -9.4707         -9.4707
v  nu_tilda           4.3296e-007       0.0042695       0.0012258       0.0012258
v  TempC                       21          73.069          21.773          21.773
v  TurbVisc           3.0912e-014        0.005032       0.0014373       0.0014373
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1193:        0.20570E+01

===============================================================


 INSTANT    0.119400000E+04   TIME STEP NUMBER            1194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46509E-02 0.89068E+00
   Friction velocity        uk    :  0.46509E-02 0.89068E+00
   Dimensionless distance   yplus :  0.37443E-01 0.71705E+01
   Friction thermal sca.    tstar : -0.14048E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27936E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82628E-02      32   0.31949E-03   0.22311E+01 0.10317E+03 
c  Velocity[X]                                      0.11694E+01 
c  Velocity[Y]                                      0.10617E+01 
c  Velocity[Z]                                      0.15385E-29 
c  Pressure     0.13740E-06     506   0.94081E-08   0.13428E+00 0.14003E+04 
c  nu_tilda     0.54302E-05      32   0.15742E-04   0.21653E-06 0.13329E+03 
c  TempC        0.33333E+02      26   0.31622E-03   0.58296E+01 0.24985E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0148          10.453          4.5729          4.5729
v  Velocity[Y]            -3.1172          7.1674     6.6826e-005     6.6826e-005
v  Velocity[Z]       -1.0171e-014     1.0147e-014    -6.5219e-018    -6.5219e-018
v  ǁVelocityǁ        0.00053175          10.454          5.2591          5.2591
v  Pressure               -51.494          18.114         -9.5522         -9.5522
v  nu_tilda           4.3303e-007       0.0042695       0.0012263       0.0012263
v  TempC                       21          73.069          21.773          21.773
v  TurbVisc           3.0913e-014        0.005032        0.001438        0.001438
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1194:        0.21280E+01

===============================================================


 INSTANT    0.119500000E+04   TIME STEP NUMBER            1195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44002E-02 0.89037E+00
   Friction velocity        uk    :  0.44002E-02 0.89037E+00
   Dimensionless distance   yplus :  0.35425E-01 0.71681E+01
   Friction thermal sca.    tstar : -0.26941E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26431E-01 0.53482E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82654E-02      32   0.31026E-03   0.22115E+01 0.10305E+03 
c  Velocity[X]                                      0.11531E+01 
c  Velocity[Y]                                      0.10584E+01 
c  Velocity[Z]                                      0.14981E-29 
c  Pressure     0.10314E-06     506   0.99853E-08   0.10206E+00 0.12181E+04 
c  nu_tilda     0.54320E-05      32   0.65752E-05   0.21673E-06 0.13333E+03 
c  TempC        0.33344E+02      26   0.28683E-03   0.46313E+01 0.21851E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0121          10.453          4.5729          4.5729
v  Velocity[Y]            -3.1117          7.1954     5.5629e-005     5.5629e-005
v  Velocity[Z]       -9.9656e-015     1.0648e-014    -6.5134e-018    -6.5134e-018
v  ǁVelocityǁ        0.00078429          10.454           5.259           5.259
v  Pressure               -51.465          18.353         -9.4921         -9.4921
v  nu_tilda           4.3307e-007       0.0042695        0.001227        0.001227
v  TempC                       21          73.069          21.773          21.773
v  TurbVisc           3.0936e-014        0.005032       0.0014387       0.0014387
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1195:        0.21330E+01

===============================================================


 INSTANT    0.119600000E+04   TIME STEP NUMBER            1196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46536E-02 0.89138E+00
   Friction velocity        uk    :  0.46536E-02 0.89138E+00
   Dimensionless distance   yplus :  0.37465E-01 0.71762E+01
   Friction thermal sca.    tstar : -0.14934E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27953E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82682E-02      32   0.30107E-03   0.22054E+01 0.10314E+03 
c  Velocity[X]                                      0.11257E+01 
c  Velocity[Y]                                      0.10797E+01 
c  Velocity[Z]                                      0.13983E-29 
c  Pressure     0.98696E-07     456   0.91460E-08   0.97366E-01 0.61139E+03 
c  nu_tilda     0.54338E-05      32   0.15755E-04   0.21695E-06 0.13338E+03 
c  TempC        0.33354E+02      26   0.44656E-03   0.43429E+01 0.21404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0093          10.453          4.5729          4.5729
v  Velocity[Y]            -3.1074          7.2031     4.4641e-005     4.4641e-005
v  Velocity[Z]       -1.0092e-014     1.0187e-014    -6.5097e-018    -6.5097e-018
v  ǁVelocityǁ         0.0015224          10.454           5.259           5.259
v  Pressure               -51.459          18.258         -9.5297         -9.5297
v  nu_tilda           4.3301e-007       0.0042695       0.0012275       0.0012275
v  TempC                       21          73.069          21.774          21.774
v  TurbVisc           3.0945e-014        0.005032       0.0014394       0.0014394
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1196:        0.20270E+01

===============================================================


 INSTANT    0.119700000E+04   TIME STEP NUMBER            1197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12736E-01 0.89106E+00
   Friction velocity        uk    :  0.12736E-01 0.89106E+00
   Dimensionless distance   yplus :  0.10254E+00 0.71737E+01
   Friction thermal sca.    tstar : -0.10769E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76504E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82708E-02      32   0.32072E-03   0.22355E+01 0.10335E+03 
c  Velocity[X]                                      0.11656E+01 
c  Velocity[Y]                                      0.10699E+01 
c  Velocity[Z]                                      0.13495E-29 
c  Pressure     0.13017E-06     424   0.96260E-08   0.12765E+00 0.39665E+03 
c  nu_tilda     0.54356E-05      32   0.65598E-05   0.21716E-06 0.13343E+03 
c  TempC        0.33365E+02      26   0.39865E-03   0.61025E+01 0.27317E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0064          10.453          4.5729          4.5729
v  Velocity[Y]            -3.1032           7.174     3.3601e-005     3.3601e-005
v  Velocity[Z]       -1.0063e-014     1.0622e-014    -6.5018e-018    -6.5018e-018
v  ǁVelocityǁ        0.00078275          10.454           5.259           5.259
v  Pressure               -51.425          18.168         -9.5438         -9.5438
v  nu_tilda             4.33e-007       0.0042695       0.0012281       0.0012281
v  TempC                       21          73.069          21.774          21.774
v  TurbVisc           3.0929e-014        0.005032       0.0014401       0.0014401
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1197:        0.19670E+01

===============================================================


 INSTANT    0.119800000E+04   TIME STEP NUMBER            1198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28202E-02 0.88982E+00
   Friction velocity        uk    :  0.28202E-02 0.88982E+00
   Dimensionless distance   yplus :  0.22704E-01 0.71637E+01
   Friction thermal sca.    tstar : -0.14046E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16940E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82735E-02      32   0.34932E-03   0.22509E+01 0.10358E+03 
c  Velocity[X]                                      0.11856E+01 
c  Velocity[Y]                                      0.10653E+01 
c  Velocity[Z]                                      0.11718E-29 
c  Pressure     0.11564E-06     266   0.97068E-08   0.11400E+00 0.19275E+03 
c  nu_tilda     0.54373E-05      32   0.15766E-04   0.21738E-06 0.13348E+03 
c  TempC        0.33375E+02      26   0.44116E-03   0.50841E+01 0.24422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0038          10.453          4.5729          4.5729
v  Velocity[Y]             -3.098          7.1959     2.2426e-005     2.2426e-005
v  Velocity[Z]       -1.0107e-014     1.0149e-014    -6.4963e-018    -6.4963e-018
v  ǁVelocityǁ         0.0013574          10.454           5.259           5.259
v  Pressure               -51.423           18.22         -9.5505         -9.5505
v  nu_tilda           4.3304e-007       0.0042695       0.0012287       0.0012287
v  TempC                       21          73.069          21.774          21.774
v  TurbVisc           3.0926e-014        0.005032       0.0014408       0.0014408
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1198:        0.15940E+01

===============================================================


 INSTANT    0.119900000E+04   TIME STEP NUMBER            1199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11758E-01 0.89107E+00
   Friction velocity        uk    :  0.11758E-01 0.89107E+00
   Dimensionless distance   yplus :  0.94661E-01 0.71737E+01
   Friction thermal sca.    tstar : -0.10583E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70628E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82762E-02      32   0.32370E-03   0.22421E+01 0.10366E+03 
c  Velocity[X]                                      0.11556E+01 
c  Velocity[Y]                                      0.10865E+01 
c  Velocity[Z]                                      0.10594E-29 
c  Pressure     0.11297E-06     249   0.95012E-08   0.11299E+00 0.26962E+03 
c  nu_tilda     0.54391E-05      32   0.65596E-05   0.21759E-06 0.13353E+03 
c  TempC        0.33385E+02      26   0.36610E-03   0.90601E+01 0.31037E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0011          10.453          4.5729          4.5729
v  Velocity[Y]            -3.0938          7.1765     1.1234e-005     1.1234e-005
v  Velocity[Z]       -1.0221e-014     1.0648e-014    -6.4896e-018    -6.4896e-018
v  ǁVelocityǁ        0.00087481          10.454           5.259           5.259
v  Pressure               -51.392           18.19         -9.5499         -9.5499
v  nu_tilda           4.3308e-007       0.0042695       0.0012293       0.0012293
v  TempC                       21          73.069          21.775          21.775
v  TurbVisc           3.0936e-014        0.005032       0.0014415       0.0014415
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1199:        0.15500E+01

===============================================================


 INSTANT    0.120000000E+04   TIME STEP NUMBER            1200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66061E-02 0.89018E+00
   Friction velocity        uk    :  0.66061E-02 0.89018E+00
   Dimensionless distance   yplus :  0.53184E-01 0.71666E+01
   Friction thermal sca.    tstar : -0.97465E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39681E-01 0.53471E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82788E-02      32   0.26735E-03   0.22266E+01 0.10354E+03 
c  Velocity[X]                                      0.11516E+01 
c  Velocity[Y]                                      0.10750E+01 
c  Velocity[Z]                                      0.12039E-29 
c  Pressure     0.11925E-06     425   0.94792E-08   0.11581E+00 0.42517E+03 
c  nu_tilda     0.54409E-05      32   0.15763E-04   0.21783E-06 0.13359E+03 
c  TempC        0.33396E+02      26   0.24912E-03   0.61038E+01 0.24937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9984          10.453          4.5729          4.5729
v  Velocity[Y]            -3.0885          7.1972     3.7341e-007     3.7341e-007
v  Velocity[Z]       -1.0488e-014     1.0186e-014    -6.4854e-018    -6.4854e-018
v  ǁVelocityǁ         0.0010308          10.454          5.2589          5.2589
v  Pressure               -51.387          18.151          -9.579          -9.579
v  nu_tilda           4.3314e-007       0.0042695       0.0012299       0.0012299
v  TempC                       21          73.069          21.775          21.775
v  TurbVisc            3.095e-014        0.005032       0.0014422       0.0014422
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1200:        0.19630E+01

===============================================================


 INSTANT    0.120100000E+04   TIME STEP NUMBER            1201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10263E-01 0.89190E+00
   Friction velocity        uk    :  0.10263E-01 0.89190E+00
   Dimensionless distance   yplus :  0.82624E-01 0.71804E+01
   Friction thermal sca.    tstar : -0.10069E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61647E-01 0.53574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82815E-02      32   0.34337E-03   0.22238E+01 0.10359E+03 
c  Velocity[X]                                      0.11498E+01 
c  Velocity[Y]                                      0.10741E+01 
c  Velocity[Z]                                      0.20402E-29 
c  Pressure     0.10741E-06     472   0.92155E-08   0.10579E+00 0.70830E+03 
c  nu_tilda     0.54427E-05      32   0.65402E-05   0.21805E-06 0.13364E+03 
c  TempC        0.33406E+02      27   0.41472E-03   0.27813E+01 0.16699E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9956          10.453          4.5729          4.5729
v  Velocity[Y]            -3.0838          7.2103    -1.0867e-005    -1.0867e-005
v  Velocity[Z]        -1.065e-014      1.062e-014     -6.485e-018     -6.485e-018
v  ǁVelocityǁ         0.0010732          10.454          5.2589          5.2589
v  Pressure               -51.352          18.259         -9.5438         -9.5438
v  nu_tilda           4.3319e-007       0.0042695       0.0012305       0.0012305
v  TempC                       21          73.069          21.776          21.776
v  TurbVisc           3.0967e-014        0.005032       0.0014429       0.0014429
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1201:        0.23420E+01

===============================================================


 INSTANT    0.120200000E+04   TIME STEP NUMBER            1202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92119E-02 0.89145E+00
   Friction velocity        uk    :  0.92119E-02 0.89145E+00
   Dimensionless distance   yplus :  0.74162E-01 0.71768E+01
   Friction thermal sca.    tstar : -0.93913E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55333E-01 0.53547E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82842E-02      32   0.31285E-03   0.22525E+01 0.10394E+03 
c  Velocity[X]                                      0.11587E+01 
c  Velocity[Y]                                      0.10937E+01 
c  Velocity[Z]                                      0.11388E-29 
c  Pressure     0.11974E-06     489   0.93394E-08   0.12025E+00 0.94185E+03 
c  nu_tilda     0.54444E-05      32   0.15782E-04   0.21829E-06 0.13369E+03 
c  TempC        0.33416E+02      27   0.38283E-03   0.70475E+01 0.27125E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9928          10.453          4.5729          4.5729
v  Velocity[Y]             -3.079          7.1827    -2.1994e-005    -2.1994e-005
v  Velocity[Z]       -1.0364e-014     1.0148e-014    -6.4737e-018    -6.4737e-018
v  ǁVelocityǁ        0.00098692          10.454          5.2589          5.2589
v  Pressure               -51.352          18.091         -9.6013         -9.6013
v  nu_tilda           4.3324e-007       0.0042695       0.0012311       0.0012311
v  TempC                       21          73.069          21.776          21.776
v  TurbVisc            3.098e-014        0.005032       0.0014436       0.0014436
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1202:        0.23070E+01

===============================================================


 INSTANT    0.120300000E+04   TIME STEP NUMBER            1203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82072E-02 0.89005E+00
   Friction velocity        uk    :  0.82072E-02 0.89005E+00
   Dimensionless distance   yplus :  0.66074E-01 0.71655E+01
   Friction thermal sca.    tstar : -0.98743E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49298E-01 0.53463E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82868E-02      32   0.32966E-03   0.22401E+01 0.10387E+03 
c  Velocity[X]                                      0.11572E+01 
c  Velocity[Y]                                      0.10830E+01 
c  Velocity[Z]                                      0.11950E-29 
c  Pressure     0.11620E-06     456   0.98677E-08   0.11275E+00 0.55255E+03 
c  nu_tilda     0.54462E-05      32   0.65214E-05   0.21850E-06 0.13374E+03 
c  TempC        0.33426E+02      26   0.39943E-03   0.58788E+01 0.24262E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9899          10.453          4.5729          4.5729
v  Velocity[Y]            -3.0743           7.201    -3.3072e-005    -3.3072e-005
v  Velocity[Z]       -1.0814e-014     1.0646e-014    -6.4705e-018    -6.4705e-018
v  ǁVelocityǁ         0.0013482          10.454          5.2589          5.2589
v  Pressure               -51.319          18.177         -9.5772         -9.5772
v  nu_tilda           4.3326e-007       0.0042695       0.0012317       0.0012317
v  TempC                       21          73.069          21.776          21.776
v  TurbVisc           3.0995e-014        0.005032       0.0014443       0.0014443
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1203:        0.20380E+01

===============================================================


 INSTANT    0.120400000E+04   TIME STEP NUMBER            1204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11341E-01 0.89124E+00
   Friction velocity        uk    :  0.11341E-01 0.89124E+00
   Dimensionless distance   yplus :  0.91299E-01 0.71751E+01
   Friction thermal sca.    tstar : -0.11950E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68119E-01 0.53534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82895E-02      32   0.36176E-03   0.22714E+01 0.10418E+03 
c  Velocity[X]                                      0.11913E+01 
c  Velocity[Y]                                      0.10801E+01 
c  Velocity[Z]                                      0.12142E-29 
c  Pressure     0.12374E-06     457   0.97014E-08   0.12364E+00 0.67299E+03 
c  nu_tilda     0.54480E-05      32   0.15782E-04   0.21873E-06 0.13379E+03 
c  TempC        0.33437E+02      26   0.38107E-03   0.51567E+01 0.25094E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9871          10.453          4.5729          4.5729
v  Velocity[Y]            -3.0691          7.1799    -4.4282e-005    -4.4282e-005
v  Velocity[Z]       -1.0906e-014     1.0185e-014      -6.47e-018      -6.47e-018
v  ǁVelocityǁ        0.00025352          10.454          5.2588          5.2588
v  Pressure               -51.314          18.058         -9.6168         -9.6168
v  nu_tilda           4.3326e-007       0.0042695       0.0012322       0.0012322
v  TempC                       21          73.069          21.777          21.777
v  TurbVisc              3.1e-014        0.005032        0.001445        0.001445
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1204:        0.20320E+01

===============================================================


 INSTANT    0.120500000E+04   TIME STEP NUMBER            1205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30328E-02 0.89052E+00
   Friction velocity        uk    :  0.30328E-02 0.89052E+00
   Dimensionless distance   yplus :  0.24416E-01 0.71693E+01
   Friction thermal sca.    tstar : -0.62263E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18217E-01 0.53491E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82921E-02      32   0.31083E-03   0.22763E+01 0.10439E+03 
c  Velocity[X]                                      0.11734E+01 
c  Velocity[Y]                                      0.11029E+01 
c  Velocity[Z]                                      0.11787E-29 
c  Pressure     0.11131E-06     504   0.91662E-08   0.10891E+00 0.88007E+03 
c  nu_tilda     0.54498E-05      32   0.65173E-05   0.21893E-06 0.13384E+03 
c  TempC        0.33447E+02      26   0.34354E-03   0.71972E+01 0.27824E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9844          10.453          4.5729          4.5729
v  Velocity[Y]             -3.063          7.2056    -5.5268e-005    -5.5268e-005
v  Velocity[Z]       -1.0937e-014     1.0618e-014    -6.4669e-018    -6.4669e-018
v  ǁVelocityǁ         0.0016424          10.454          5.2588          5.2588
v  Pressure               -51.284          18.227         -9.5755         -9.5755
v  nu_tilda            4.332e-007       0.0042695       0.0012329       0.0012329
v  TempC                       21          73.069          21.777          21.777
v  TurbVisc              3.1e-014        0.005032       0.0014457       0.0014457
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1205:        0.21310E+01

===============================================================


 INSTANT    0.120600000E+04   TIME STEP NUMBER            1206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12100E-01 0.89165E+00
   Friction velocity        uk    :  0.12100E-01 0.89165E+00
   Dimensionless distance   yplus :  0.97414E-01 0.71784E+01
   Friction thermal sca.    tstar : -0.12080E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72681E-01 0.53559E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82948E-02      32   0.28060E-03   0.22314E+01 0.10405E+03 
c  Velocity[X]                                      0.11404E+01 
c  Velocity[Y]                                      0.10909E+01 
c  Velocity[Z]                                      0.11965E-29 
c  Pressure     0.11102E-06     473   0.95505E-08   0.10803E+00 0.80926E+03 
c  nu_tilda     0.54516E-05      32   0.15784E-04   0.21916E-06 0.13389E+03 
c  TempC        0.33457E+02      26   0.40720E-03   0.54937E+01 0.22512E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9817          10.454          4.5729          4.5729
v  Velocity[Y]             -3.058          7.2097    -6.6502e-005    -6.6502e-005
v  Velocity[Z]       -1.0946e-014     1.0145e-014    -6.4639e-018    -6.4639e-018
v  ǁVelocityǁ        0.00094546          10.454          5.2588          5.2588
v  Pressure               -51.279          18.097         -9.6249         -9.6249
v  nu_tilda           4.3311e-007       0.0042695       0.0012334       0.0012334
v  TempC                       21           73.07          21.777          21.777
v  TurbVisc           3.0982e-014        0.005032       0.0014464       0.0014464
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1206:        0.20720E+01

===============================================================


 INSTANT    0.120700000E+04   TIME STEP NUMBER            1207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58005E-02 0.89140E+00
   Friction velocity        uk    :  0.58005E-02 0.89140E+00
   Dimensionless distance   yplus :  0.46698E-01 0.71764E+01
   Friction thermal sca.    tstar : -0.95173E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34842E-01 0.53544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82974E-02      32   0.34478E-03   0.22536E+01 0.10425E+03 
c  Velocity[X]                                      0.11646E+01 
c  Velocity[Y]                                      0.10889E+01 
c  Velocity[Z]                                      0.15555E-29 
c  Pressure     0.11950E-06     424   0.96533E-08   0.11986E+00 0.37291E+03 
c  nu_tilda     0.54534E-05      32   0.64965E-05   0.21938E-06 0.13395E+03 
c  TempC        0.33468E+02      27   0.35398E-03   0.54123E+01 0.22599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.979          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0528          7.1853    -7.7535e-005    -7.7535e-005
v  Velocity[Z]       -1.0951e-014     1.0642e-014    -6.4622e-018    -6.4622e-018
v  ǁVelocityǁ        0.00058541          10.454          5.2588          5.2588
v  Pressure               -51.242          18.092         -9.6108         -9.6108
v  nu_tilda           4.3305e-007       0.0042695        0.001234        0.001234
v  TempC                       21           73.07          21.778          21.778
v  TurbVisc           3.0957e-014        0.005032       0.0014471       0.0014471
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1207:        0.19630E+01

===============================================================


 INSTANT    0.120800000E+04   TIME STEP NUMBER            1208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63968E-02 0.89009E+00
   Friction velocity        uk    :  0.63968E-02 0.89009E+00
   Dimensionless distance   yplus :  0.51499E-01 0.71658E+01
   Friction thermal sca.    tstar : -0.10058E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38424E-01 0.53465E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83001E-02      32   0.33878E-03   0.22957E+01 0.10474E+03 
c  Velocity[X]                                      0.11837E+01 
c  Velocity[Y]                                      0.11120E+01 
c  Velocity[Z]                                      0.17896E-29 
c  Pressure     0.13204E-06     425   0.92958E-08   0.13027E+00 0.25941E+03 
c  nu_tilda     0.54552E-05      32   0.15803E-04   0.21963E-06 0.13400E+03 
c  TempC        0.33478E+02      27   0.35983E-03   0.44433E+01 0.21521E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9762          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0469          7.2045    -8.8831e-005    -8.8831e-005
v  Velocity[Z]       -1.0744e-014     1.0182e-014    -6.4526e-018    -6.4526e-018
v  ǁVelocityǁ         0.0012587          10.454          5.2587          5.2587
v  Pressure               -51.244          18.108         -9.6327         -9.6327
v  nu_tilda           4.3302e-007       0.0042695       0.0012346       0.0012346
v  TempC                       21           73.07          21.778          21.778
v  TurbVisc            3.094e-014        0.005032       0.0014478       0.0014478
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1208:        0.20160E+01

===============================================================


 INSTANT    0.120900000E+04   TIME STEP NUMBER            1209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10010E-01 0.89121E+00
   Friction velocity        uk    :  0.10010E-01 0.89121E+00
   Dimensionless distance   yplus :  0.80587E-01 0.71749E+01
   Friction thermal sca.    tstar : -0.97253E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60127E-01 0.53532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83027E-02      32   0.30210E-03   0.23041E+01 0.10481E+03 
c  Velocity[X]                                      0.12022E+01 
c  Velocity[Y]                                      0.11019E+01 
c  Velocity[Z]                                      0.13023E-29 
c  Pressure     0.13552E-06     442   0.94217E-08   0.13183E+00 0.50017E+03 
c  nu_tilda     0.54569E-05      32   0.64898E-05   0.21985E-06 0.13406E+03 
c  TempC        0.33488E+02      27   0.38277E-03   0.45517E+01 0.22388E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9733          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0424          7.1813    -9.9891e-005    -9.9891e-005
v  Velocity[Z]          -1.1e-014     1.0614e-014    -6.4527e-018    -6.4527e-018
v  ǁVelocityǁ         0.0010656          10.454          5.2587          5.2587
v  Pressure               -51.209          17.988         -9.6506         -9.6506
v  nu_tilda           4.3312e-007       0.0042695       0.0012352       0.0012352
v  TempC                       21          73.069          21.778          21.778
v  TurbVisc           3.0931e-014        0.005032       0.0014485       0.0014485
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1209:        0.20030E+01

===============================================================


 INSTANT    0.121000000E+04   TIME STEP NUMBER            1210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75382E-02 0.89079E+00
   Friction velocity        uk    :  0.75382E-02 0.89079E+00
   Dimensionless distance   yplus :  0.60688E-01 0.71715E+01
   Friction thermal sca.    tstar : -0.10527E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45280E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83054E-02      32   0.26400E-03   0.22628E+01 0.10455E+03 
c  Velocity[X]                                      0.11669E+01 
c  Velocity[Y]                                      0.10959E+01 
c  Velocity[Z]                                      0.12020E-29 
c  Pressure     0.10802E-06     440   0.93186E-08   0.10672E+00 0.37689E+03 
c  nu_tilda     0.54587E-05      32   0.15799E-04   0.22010E-06 0.13411E+03 
c  TempC        0.33499E+02      26   0.41633E-03   0.54613E+01 0.24308E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9704          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0358          7.2064     -0.00011098     -0.00011098
v  Velocity[Z]       -1.1113e-014     1.0144e-014    -6.4504e-018    -6.4504e-018
v  ǁVelocityǁ         0.0018317          10.454          5.2587          5.2587
v  Pressure               -51.208          18.101         -9.6441         -9.6441
v  nu_tilda           4.3317e-007       0.0042695       0.0012358       0.0012358
v  TempC                       21          73.069          21.779          21.779
v  TurbVisc           3.0959e-014        0.005032       0.0014492       0.0014492
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1210:        0.19860E+01

===============================================================


 INSTANT    0.121100000E+04   TIME STEP NUMBER            1211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13645E-01 0.89221E+00
   Friction velocity        uk    :  0.13645E-01 0.89221E+00
   Dimensionless distance   yplus :  0.10985E+00 0.71829E+01
   Friction thermal sca.    tstar : -0.99745E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81959E-01 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83080E-02      32   0.33134E-03   0.22549E+01 0.10467E+03 
c  Velocity[X]                                      0.11365E+01 
c  Velocity[Y]                                      0.11185E+01 
c  Velocity[Z]                                      0.12004E-29 
c  Pressure     0.10459E-06     426   0.93444E-08   0.10309E+00 0.36560E+03 
c  nu_tilda     0.54605E-05      32   0.64827E-05   0.22032E-06 0.13416E+03 
c  TempC        0.33509E+02      26   0.30955E-03   0.63559E+01 0.26127E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9675          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0303          7.2175     -0.00012219     -0.00012219
v  Velocity[Z]       -1.1161e-014     1.0639e-014    -6.4484e-018    -6.4484e-018
v  ǁVelocityǁ         0.0010748          10.454          5.2586          5.2586
v  Pressure               -51.175          18.126         -9.6308         -9.6308
v  nu_tilda           4.3316e-007       0.0042695       0.0012364       0.0012364
v  TempC                       21          73.069          21.779          21.779
v  TurbVisc           3.0974e-014        0.005032       0.0014499       0.0014499
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1211:        0.19700E+01

===============================================================


 INSTANT    0.121200000E+04   TIME STEP NUMBER            1212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53426E-02 0.89182E+00
   Friction velocity        uk    :  0.53426E-02 0.89182E+00
   Dimensionless distance   yplus :  0.43011E-01 0.71798E+01
   Friction thermal sca.    tstar : -0.99725E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32091E-01 0.53569E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83107E-02      32   0.30460E-03   0.23010E+01 0.10505E+03 
c  Velocity[X]                                      0.11919E+01 
c  Velocity[Y]                                      0.11091E+01 
c  Velocity[Z]                                      0.13581E-29 
c  Pressure     0.13753E-06     520   0.98908E-08   0.13427E+00 0.12393E+04 
c  nu_tilda     0.54623E-05      32   0.15812E-04   0.22055E-06 0.13422E+03 
c  TempC        0.33519E+02      26   0.31851E-03   0.42252E+01 0.21532E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9648          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0243          7.1867     -0.00013326     -0.00013326
v  Velocity[Z]       -1.1081e-014     1.0177e-014    -6.4433e-018    -6.4433e-018
v  ǁVelocityǁ         0.0014525          10.454          5.2586          5.2586
v  Pressure               -51.169          17.894         -9.7015         -9.7015
v  nu_tilda           4.3322e-007       0.0042695       0.0012369       0.0012369
v  TempC                       21          73.069           21.78           21.78
v  TurbVisc           3.0972e-014        0.005032       0.0014506       0.0014506
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1212:        0.21720E+01

===============================================================


 INSTANT    0.121300000E+04   TIME STEP NUMBER            1213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11187E-01 0.89092E+00
   Friction velocity        uk    :  0.11187E-01 0.89092E+00
   Dimensionless distance   yplus :  0.90065E-01 0.71725E+01
   Friction thermal sca.    tstar : -0.10787E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67198E-01 0.53515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83133E-02      32   0.30926E-03   0.22769E+01 0.10491E+03 
c  Velocity[X]                                      0.11689E+01 
c  Velocity[Y]                                      0.11080E+01 
c  Velocity[Z]                                      0.11892E-29 
c  Pressure     0.12109E-06     490   0.93873E-08   0.11884E+00 0.93490E+03 
c  nu_tilda     0.54641E-05      32   0.64714E-05   0.22077E-06 0.13427E+03 
c  TempC        0.33529E+02      27   0.44569E-03   0.33788E+01 0.19146E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9621          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0192            7.21     -0.00014459     -0.00014459
v  Velocity[Z]       -1.1071e-014     1.0609e-014    -6.4396e-018    -6.4396e-018
v  ǁVelocityǁ        0.00075269          10.454          5.2585          5.2585
v  Pressure               -51.139          18.068         -9.6566         -9.6566
v  nu_tilda           4.3326e-007       0.0042695       0.0012376       0.0012376
v  TempC                       21          73.069           21.78           21.78
v  TurbVisc           3.0989e-014        0.005032       0.0014513       0.0014513
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1213:        0.21140E+01

===============================================================


 INSTANT    0.121400000E+04   TIME STEP NUMBER            1214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68839E-02 0.89192E+00
   Friction velocity        uk    :  0.68839E-02 0.89192E+00
   Dimensionless distance   yplus :  0.55420E-01 0.71806E+01
   Friction thermal sca.    tstar : -0.10322E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41349E-01 0.53575E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83159E-02      32   0.31046E-03   0.22943E+01 0.10518E+03 
c  Velocity[X]                                      0.11658E+01 
c  Velocity[Y]                                      0.11286E+01 
c  Velocity[Z]                                      0.16017E-29 
c  Pressure     0.11050E-06     488   0.93841E-08   0.10981E+00 0.70746E+03 
c  nu_tilda     0.54659E-05      32   0.15817E-04   0.22101E-06 0.13432E+03 
c  TempC        0.33540E+02      28   0.33510E-03   0.44633E+01 0.22552E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9592          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0129          7.1883     -0.00015558     -0.00015558
v  Velocity[Z]       -1.1088e-014     1.0139e-014    -6.4418e-018    -6.4418e-018
v  ǁVelocityǁ        0.00094479          10.454          5.2585          5.2585
v  Pressure               -51.135          17.947          -9.699          -9.699
v  nu_tilda           4.3332e-007       0.0042695       0.0012381       0.0012381
v  TempC                       21          73.069           21.78           21.78
v  TurbVisc              3.1e-014        0.005032       0.0014519       0.0014519
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1214:        0.21170E+01

===============================================================


 INSTANT    0.121500000E+04   TIME STEP NUMBER            1215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48514E-02 0.89111E+00
   Friction velocity        uk    :  0.48514E-02 0.89111E+00
   Dimensionless distance   yplus :  0.39057E-01 0.71741E+01
   Friction thermal sca.    tstar : -0.10713E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29141E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83185E-02      32   0.32490E-03   0.22895E+01 0.10517E+03 
c  Velocity[X]                                      0.11722E+01 
c  Velocity[Y]                                      0.11173E+01 
c  Velocity[Z]                                      0.12238E-29 
c  Pressure     0.12893E-06     457   0.97654E-08   0.12378E+00 0.49613E+03 
c  nu_tilda     0.54677E-05      32   0.64751E-05   0.22123E-06 0.13437E+03 
c  TempC        0.33550E+02      27   0.28524E-03   0.40406E+01 0.19315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9564          10.454          4.5729          4.5729
v  Velocity[Y]            -3.0075          7.2109     -0.00016672     -0.00016672
v  Velocity[Z]       -1.1052e-014     1.0634e-014    -6.4405e-018    -6.4405e-018
v  ǁVelocityǁ         0.0018633          10.454          5.2585          5.2585
v  Pressure               -51.098          18.011         -9.6774         -9.6774
v  nu_tilda           4.3337e-007       0.0042695       0.0012387       0.0012387
v  TempC                       21          73.069          21.781          21.781
v  TurbVisc           3.1016e-014        0.005032       0.0014526       0.0014526
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1215:        0.20310E+01

===============================================================


 INSTANT    0.121600000E+04   TIME STEP NUMBER            1216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35367E-02 0.89261E+00
   Friction velocity        uk    :  0.35367E-02 0.89261E+00
   Dimensionless distance   yplus :  0.28473E-01 0.71861E+01
   Friction thermal sca.    tstar : -0.16980E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21244E-01 0.53617E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83212E-02      32   0.35568E-03   0.23009E+01 0.10541E+03 
c  Velocity[X]                                      0.11862E+01 
c  Velocity[Y]                                      0.11147E+01 
c  Velocity[Z]                                      0.11376E-29 
c  Pressure     0.11657E-06     424   0.98875E-08   0.11449E+00 0.28996E+03 
c  nu_tilda     0.54695E-05      32   0.15817E-04   0.22148E-06 0.13443E+03 
c  TempC        0.33560E+02      26   0.42355E-03   0.40406E+01 0.20936E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9535          10.454          4.5729          4.5729
v  Velocity[Y]             -3.001          7.2208     -0.00017799     -0.00017799
v  Velocity[Z]       -1.0869e-014     1.0174e-014    -6.4349e-018    -6.4349e-018
v  ǁVelocityǁ         0.0016238          10.454          5.2584          5.2584
v  Pressure                 -51.1          18.009         -9.7012         -9.7012
v  nu_tilda           4.3338e-007       0.0042695       0.0012393       0.0012393
v  TempC                       21          73.069          21.781          21.781
v  TurbVisc           3.1031e-014        0.005032       0.0014533       0.0014533
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1216:        0.19710E+01

===============================================================


 INSTANT    0.121700000E+04   TIME STEP NUMBER            1217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99249E-02 0.89217E+00
   Friction velocity        uk    :  0.99249E-02 0.89217E+00
   Dimensionless distance   yplus :  0.79902E-01 0.71826E+01
   Friction thermal sca.    tstar : -0.10250E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59616E-01 0.53590E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83238E-02      32   0.31307E-03   0.23260E+01 0.10571E+03 
c  Velocity[X]                                      0.11891E+01 
c  Velocity[Y]                                      0.11369E+01 
c  Velocity[Z]                                      0.14711E-29 
c  Pressure     0.11964E-06     426   0.92242E-08   0.11928E+00 0.40860E+03 
c  nu_tilda     0.54713E-05      32   0.64575E-05   0.22172E-06 0.13449E+03 
c  TempC        0.33570E+02      27   0.32872E-03   0.58652E+01 0.26892E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9505          10.454          4.5729          4.5729
v  Velocity[Y]            -2.9954          7.1956     -0.00018933     -0.00018933
v  Velocity[Z]       -1.0897e-014     1.0604e-014    -6.4397e-018    -6.4397e-018
v  ǁVelocityǁ          0.001497          10.454          5.2584          5.2584
v  Pressure               -51.064          17.911          -9.712          -9.712
v  nu_tilda           4.3341e-007       0.0042695       0.0012399       0.0012399
v  TempC                       21          73.069          21.781          21.781
v  TurbVisc           3.1035e-014        0.005032        0.001454        0.001454
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1217:        0.19660E+01

===============================================================


 INSTANT    0.121800000E+04   TIME STEP NUMBER            1218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78016E-02 0.89090E+00
   Friction velocity        uk    :  0.78016E-02 0.89090E+00
   Dimensionless distance   yplus :  0.62809E-01 0.71723E+01
   Friction thermal sca.    tstar : -0.11001E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46862E-01 0.53514E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83264E-02      32   0.31116E-03   0.23013E+01 0.10548E+03 
c  Velocity[X]                                      0.11772E+01 
c  Velocity[Y]                                      0.11242E+01 
c  Velocity[Z]                                      0.13025E-29 
c  Pressure     0.13519E-06     393   0.95665E-08   0.12937E+00 0.23326E+03 
c  nu_tilda     0.54731E-05      32   0.15837E-04   0.22196E-06 0.13454E+03 
c  TempC        0.33581E+02      27   0.38549E-03   0.39627E+01 0.21137E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9477          10.454          4.5729          4.5729
v  Velocity[Y]            -2.9892          7.2111     -0.00020054     -0.00020054
v  Velocity[Z]       -1.0736e-014     1.0135e-014    -6.4366e-018    -6.4366e-018
v  ǁVelocityǁ         0.0015448          10.454          5.2583          5.2583
v  Pressure                -51.06          17.936         -9.7273         -9.7273
v  nu_tilda           4.3341e-007       0.0042695       0.0012405       0.0012405
v  TempC                       21          73.069          21.782          21.782
v  TurbVisc           3.1044e-014        0.005032       0.0014547       0.0014547
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1218:        0.18870E+01

===============================================================


 INSTANT    0.121900000E+04   TIME STEP NUMBER            1219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11157E-01 0.89214E+00
   Friction velocity        uk    :  0.11157E-01 0.89214E+00
   Dimensionless distance   yplus :  0.89822E-01 0.71823E+01
   Friction thermal sca.    tstar : -0.10618E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67017E-01 0.53588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83290E-02      32   0.32098E-03   0.23211E+01 0.10572E+03 
c  Velocity[X]                                      0.11979E+01 
c  Velocity[Y]                                      0.11232E+01 
c  Velocity[Z]                                      0.15355E-29 
c  Pressure     0.10729E-06     345   0.97312E-08   0.10676E+00 0.28913E+03 
c  nu_tilda     0.54749E-05      32   0.64408E-05   0.22219E-06 0.13460E+03 
c  TempC        0.33591E+02      26   0.40580E-03   0.48962E+01 0.20670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.945          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9839          7.1938     -0.00021185     -0.00021185
v  Velocity[Z]       -1.0479e-014     1.0628e-014    -6.4348e-018    -6.4348e-018
v  ǁVelocityǁ         0.0011993          10.454          5.2583          5.2583
v  Pressure               -51.028          17.898         -9.7244         -9.7244
v  nu_tilda           4.3346e-007       0.0042695       0.0012411       0.0012411
v  TempC                       21          73.068          21.782          21.782
v  TurbVisc           3.1043e-014        0.005032       0.0014554       0.0014554
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1219:        0.17560E+01

===============================================================


 INSTANT    0.122000000E+04   TIME STEP NUMBER            1220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60306E-02 0.89143E+00
   Friction velocity        uk    :  0.60306E-02 0.89143E+00
   Dimensionless distance   yplus :  0.48551E-01 0.71766E+01
   Friction thermal sca.    tstar : -0.11298E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36224E-01 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83316E-02      32   0.24733E-03   0.23113E+01 0.10580E+03 
c  Velocity[X]                                      0.11683E+01 
c  Velocity[Y]                                      0.11430E+01 
c  Velocity[Z]                                      0.12028E-29 
c  Pressure     0.10756E-06     296   0.96705E-08   0.10584E+00 0.21090E+03 
c  nu_tilda     0.54767E-05      32   0.15834E-04   0.22243E-06 0.13465E+03 
c  TempC        0.33601E+02      26   0.31065E-03   0.50874E+01 0.23403E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9421          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9776          7.2182     -0.00022303     -0.00022303
v  Velocity[Z]       -1.0236e-014      1.017e-014    -6.4377e-018    -6.4377e-018
v  ǁVelocityǁ        0.00041646          10.454          5.2582          5.2582
v  Pressure               -51.026          17.962         -9.7312         -9.7312
v  nu_tilda           4.3346e-007       0.0042695       0.0012416       0.0012416
v  TempC                       21          73.069          21.782          21.782
v  TurbVisc           3.1056e-014        0.005032       0.0014561       0.0014561
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1220:        0.16530E+01

===============================================================


 INSTANT    0.122100000E+04   TIME STEP NUMBER            1221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43296E-02 0.89276E+00
   Friction velocity        uk    :  0.43296E-02 0.89276E+00
   Dimensionless distance   yplus :  0.34856E-01 0.71873E+01
   Friction thermal sca.    tstar : -0.10614E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26007E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83342E-02      32   0.32615E-03   0.22874E+01 0.10567E+03 
c  Velocity[X]                                      0.11540E+01 
c  Velocity[Y]                                      0.11334E+01 
c  Velocity[Z]                                      0.13835E-29 
c  Pressure     0.11290E-06     345   0.97856E-08   0.10904E+00 0.29145E+03 
c  nu_tilda     0.54785E-05      32   0.64425E-05   0.22266E-06 0.13471E+03 
c  TempC        0.33611E+02      26   0.29096E-03   0.43314E+01 0.21858E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9392          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9727          7.2254     -0.00023432     -0.00023432
v  Velocity[Z]       -1.0082e-014     1.0599e-014    -6.4343e-018    -6.4343e-018
v  ǁVelocityǁ        0.00096409          10.454          5.2582          5.2582
v  Pressure               -50.991          17.925         -9.7348         -9.7348
v  nu_tilda           4.3339e-007       0.0042695       0.0012423       0.0012423
v  TempC                       21          73.069          21.783          21.783
v  TurbVisc           3.1056e-014        0.005032       0.0014568       0.0014568
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1221:        0.17700E+01

===============================================================


 INSTANT    0.122200000E+04   TIME STEP NUMBER            1222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51325E-02 0.89254E+00
   Friction velocity        uk    :  0.51325E-02 0.89254E+00
   Dimensionless distance   yplus :  0.41320E-01 0.71855E+01
   Friction thermal sca.    tstar : -0.10596E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30830E-01 0.53612E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83369E-02      32   0.34806E-03   0.23374E+01 0.10609E+03 
c  Velocity[X]                                      0.12071E+01 
c  Velocity[Y]                                      0.11303E+01 
c  Velocity[Z]                                      0.15483E-29 
c  Pressure     0.13043E-06     458   0.96554E-08   0.13004E+00 0.65756E+03 
c  nu_tilda     0.54803E-05      32   0.15842E-04   0.22290E-06 0.13476E+03 
c  TempC        0.33622E+02      26   0.52187E-03   0.46986E+01 0.23001E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9363          10.453          4.5729          4.5729
v  Velocity[Y]             -2.971          7.1996      -0.0002457      -0.0002457
v  Velocity[Z]       -9.9002e-015     1.0129e-014    -6.4433e-018    -6.4433e-018
v  ǁVelocityǁ         0.0014356          10.454          5.2581          5.2581
v  Pressure               -50.984          17.805         -9.7725         -9.7725
v  nu_tilda           4.3339e-007       0.0042695       0.0012428       0.0012428
v  TempC                       21          73.069          21.783          21.783
v  TurbVisc           3.1038e-014        0.005032       0.0014575       0.0014575
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1222:        0.20420E+01

===============================================================


 INSTANT    0.122300000E+04   TIME STEP NUMBER            1223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11673E-01 0.89129E+00
   Friction velocity        uk    :  0.11673E-01 0.89129E+00
   Dimensionless distance   yplus :  0.93979E-01 0.71755E+01
   Friction thermal sca.    tstar : -0.11465E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70119E-01 0.53537E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83394E-02      32   0.31228E-03   0.23419E+01 0.10633E+03 
c  Velocity[X]                                      0.11892E+01 
c  Velocity[Y]                                      0.11527E+01 
c  Velocity[Z]                                      0.11184E-29 
c  Pressure     0.10939E-06     489   0.95886E-08   0.10653E+00 0.90357E+03 
c  nu_tilda     0.54821E-05      32   0.64219E-05   0.22313E-06 0.13482E+03 
c  TempC        0.33632E+02      27   0.33782E-03   0.91344E+01 0.33009E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9334          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9694          7.2209     -0.00025685     -0.00025685
v  Velocity[Z]       -9.7963e-015      1.062e-014     -6.445e-018     -6.445e-018
v  ǁVelocityǁ         0.0026824          10.454          5.2581          5.2581
v  Pressure               -50.954          17.977         -9.7297         -9.7297
v  nu_tilda           4.3336e-007       0.0042695       0.0012434       0.0012434
v  TempC                       21          73.069          21.783          21.783
v  TurbVisc           3.1038e-014        0.005032       0.0014582       0.0014582
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1223:        0.21160E+01

===============================================================


 INSTANT    0.122400000E+04   TIME STEP NUMBER            1224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17710E-01 0.89221E+00
   Friction velocity        uk    :  0.17710E-01 0.89221E+00
   Dimensionless distance   yplus :  0.14258E+00 0.71829E+01
   Friction thermal sca.    tstar : -0.11398E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10638E+00 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83421E-02      32   0.31579E-03   0.23255E+01 0.10621E+03 
c  Velocity[X]                                      0.11841E+01 
c  Velocity[Y]                                      0.11414E+01 
c  Velocity[Z]                                      0.10457E-29 
c  Pressure     0.12326E-06     520   0.94541E-08   0.11994E+00 0.13489E+04 
c  nu_tilda     0.54839E-05      32   0.15853E-04   0.22338E-06 0.13487E+03 
c  TempC        0.33642E+02      26   0.38129E-03   0.45104E+01 0.22796E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9304          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9677          7.1952     -0.00026819     -0.00026819
v  Velocity[Z]       -9.7057e-015      1.016e-014    -6.4438e-018    -6.4438e-018
v  ǁVelocityǁ         0.0038133          10.454           5.258           5.258
v  Pressure               -50.951          17.727         -9.8079         -9.8079
v  nu_tilda           4.3344e-007       0.0042695        0.001244        0.001244
v  TempC                       21          73.069          21.784          21.784
v  TurbVisc           3.1029e-014        0.005032       0.0014589       0.0014589
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1224:        0.21910E+01

===============================================================


 INSTANT    0.122500000E+04   TIME STEP NUMBER            1225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20666E-01 0.89171E+00
   Friction velocity        uk    :  0.20666E-01 0.89171E+00
   Dimensionless distance   yplus :  0.16638E+00 0.71788E+01
   Friction thermal sca.    tstar : -0.11939E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12413E+00 0.53562E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83446E-02      32   0.31781E-03   0.23403E+01 0.10636E+03 
c  Velocity[X]                                      0.12000E+01 
c  Velocity[Y]                                      0.11403E+01 
c  Velocity[Z]                                      0.13207E-29 
c  Pressure     0.10729E-06     521   0.97810E-08   0.10512E+00 0.12099E+04 
c  nu_tilda     0.54857E-05      32   0.64124E-05   0.22362E-06 0.13493E+03 
c  TempC        0.33652E+02      26   0.38444E-03   0.50557E+01 0.24900E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9276          10.453          4.5729          4.5729
v  Velocity[Y]             -2.966          7.2227     -0.00027946     -0.00027946
v  Velocity[Z]       -1.0193e-014     1.0588e-014    -6.4529e-018    -6.4529e-018
v  ǁVelocityǁ         0.0018021          10.454           5.258           5.258
v  Pressure               -50.918          17.953          -9.746          -9.746
v  nu_tilda           4.3349e-007       0.0042695       0.0012446       0.0012446
v  TempC                       21          73.069          21.784          21.784
v  TurbVisc           3.1052e-014        0.005032       0.0014596       0.0014596
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1225:        0.22010E+01

===============================================================


 INSTANT    0.122600000E+04   TIME STEP NUMBER            1226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54295E-02 0.89277E+00
   Friction velocity        uk    :  0.54295E-02 0.89277E+00
   Dimensionless distance   yplus :  0.43711E-01 0.71874E+01
   Friction thermal sca.    tstar : -0.10829E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32614E-01 0.53626E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83473E-02      32   0.32009E-03   0.23200E+01 0.10638E+03 
c  Velocity[X]                                      0.11600E+01 
c  Velocity[Y]                                      0.11600E+01 
c  Velocity[Z]                                      0.15438E-29 
c  Pressure     0.97611E-07     489   0.99403E-08   0.95543E-01 0.65862E+03 
c  nu_tilda     0.54875E-05      32   0.15848E-04   0.22388E-06 0.13499E+03 
c  TempC        0.33663E+02      27   0.44981E-03   0.49307E+01 0.24257E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9248          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9643          7.2289     -0.00029077     -0.00029077
v  Velocity[Z]       -1.0208e-014     1.0122e-014    -6.4522e-018    -6.4522e-018
v  ǁVelocityǁ        0.00043592          10.453          5.2579          5.2579
v  Pressure               -50.916          17.855         -9.7887         -9.7887
v  nu_tilda           4.3346e-007       0.0042695       0.0012451       0.0012451
v  TempC                       21          73.069          21.784          21.784
v  TurbVisc           3.1067e-014        0.005032       0.0014603       0.0014603
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1226:        0.21020E+01

===============================================================


 INSTANT    0.122700000E+04   TIME STEP NUMBER            1227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58634E-02 0.89239E+00
   Friction velocity        uk    :  0.58634E-02 0.89239E+00
   Dimensionless distance   yplus :  0.47204E-01 0.71843E+01
   Friction thermal sca.    tstar : -0.10849E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35220E-01 0.53603E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83498E-02      32   0.31642E-03   0.23499E+01 0.10658E+03 
c  Velocity[X]                                      0.11986E+01 
c  Velocity[Y]                                      0.11513E+01 
c  Velocity[Z]                                      0.14331E-29 
c  Pressure     0.13657E-06     426   0.98924E-08   0.13247E+00 0.45128E+03 
c  nu_tilda     0.54893E-05      32   0.64082E-05   0.22412E-06 0.13505E+03 
c  TempC        0.33673E+02      27   0.40778E-03   0.59117E+01 0.24812E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9219          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9627          7.2004     -0.00030207     -0.00030207
v  Velocity[Z]       -1.0406e-014     1.0613e-014    -6.4582e-018    -6.4582e-018
v  ǁVelocityǁ         0.0016239          10.453          5.2579          5.2579
v  Pressure               -50.877          17.754         -9.8014         -9.8014
v  nu_tilda            4.335e-007       0.0042695       0.0012458       0.0012458
v  TempC                       21          73.069          21.785          21.785
v  TurbVisc           3.1057e-014        0.005032        0.001461        0.001461
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1227:        0.19670E+01

===============================================================


 INSTANT    0.122800000E+04   TIME STEP NUMBER            1228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62399E-02 0.89129E+00
   Friction velocity        uk    :  0.62399E-02 0.89129E+00
   Dimensionless distance   yplus :  0.50236E-01 0.71755E+01
   Friction thermal sca.    tstar : -0.11725E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37482E-01 0.53537E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83524E-02      32   0.31909E-03   0.23459E+01 0.10666E+03 
c  Velocity[X]                                      0.11988E+01 
c  Velocity[Y]                                      0.11470E+01 
c  Velocity[Z]                                      0.11429E-29 
c  Pressure     0.10624E-06     346   0.92793E-08   0.10388E+00 0.23888E+03 
c  nu_tilda     0.54911E-05      32   0.15868E-04   0.22437E-06 0.13510E+03 
c  TempC        0.33683E+02      26   0.41207E-03   0.56760E+01 0.25335E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.919          10.453          4.5729          4.5729
v  Velocity[Y]             -2.961          7.2217     -0.00031388     -0.00031388
v  Velocity[Z]       -1.0406e-014     1.0156e-014    -6.4563e-018    -6.4563e-018
v  ǁVelocityǁ         0.0030544          10.453          5.2578          5.2578
v  Pressure               -50.878          17.828         -9.8052         -9.8052
v  nu_tilda           4.3354e-007       0.0042695       0.0012463       0.0012463
v  TempC                       21          73.069          21.785          21.785
v  TurbVisc           3.1068e-014        0.005032       0.0014616       0.0014616
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1228:        0.17830E+01

===============================================================


 INSTANT    0.122900000E+04   TIME STEP NUMBER            1229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12219E-01 0.89248E+00
   Friction velocity        uk    :  0.12219E-01 0.89248E+00
   Dimensionless distance   yplus :  0.98369E-01 0.71850E+01
   Friction thermal sca.    tstar : -0.11146E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73394E-01 0.53608E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83550E-02      32   0.31549E-03   0.23544E+01 0.10686E+03 
c  Velocity[X]                                      0.11860E+01 
c  Velocity[Y]                                      0.11684E+01 
c  Velocity[Z]                                      0.14452E-29 
c  Pressure     0.11111E-06     377   0.90402E-08   0.10994E+00 0.34679E+03 
c  nu_tilda     0.54930E-05      32   0.63905E-05   0.22459E-06 0.13516E+03 
c  TempC        0.33693E+02      27   0.41828E-03   0.50421E+01 0.24516E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9161          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9593          7.2014     -0.00032558     -0.00032558
v  Velocity[Z]       -1.0667e-014     1.0582e-014    -6.4701e-018    -6.4701e-018
v  ǁVelocityǁ         0.0033665          10.453          5.2577          5.2577
v  Pressure               -50.838          17.788         -9.7989         -9.7989
v  nu_tilda           4.3355e-007       0.0042695       0.0012469       0.0012469
v  TempC                       21          73.069          21.785          21.785
v  TurbVisc           3.1081e-014        0.005032       0.0014623       0.0014623
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1229:        0.18560E+01

===============================================================


 INSTANT    0.123000000E+04   TIME STEP NUMBER            1230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20621E-01 0.89161E+00
   Friction velocity        uk    :  0.20621E-01 0.89161E+00
   Dimensionless distance   yplus :  0.16601E+00 0.71781E+01
   Friction thermal sca.    tstar : -0.11618E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12386E+00 0.53556E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83576E-02      32   0.24828E-03   0.23463E+01 0.10680E+03 
c  Velocity[X]                                      0.11879E+01 
c  Velocity[Y]                                      0.11584E+01 
c  Velocity[Z]                                      0.12304E-29 
c  Pressure     0.12129E-06     440   0.97713E-08   0.11678E+00 0.42437E+03 
c  nu_tilda     0.54948E-05      32   0.15867E-04   0.22484E-06 0.13521E+03 
c  TempC        0.33704E+02      26   0.29451E-03   0.51129E+01 0.24152E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9131          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9576          7.2227     -0.00033737     -0.00033737
v  Velocity[Z]       -1.0578e-014     1.0115e-014    -6.4672e-018    -6.4672e-018
v  ǁVelocityǁ         0.0024637          10.453          5.2577          5.2577
v  Pressure               -50.836          17.765         -9.8302         -9.8302
v  nu_tilda           4.3356e-007       0.0042695       0.0012475       0.0012475
v  TempC                       21          73.069          21.786          21.786
v  TurbVisc           3.1083e-014        0.005032        0.001463        0.001463
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1230:        0.19940E+01

===============================================================


 INSTANT    0.123100000E+04   TIME STEP NUMBER            1231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15689E-01 0.89308E+00
   Friction velocity        uk    :  0.15689E-01 0.89308E+00
   Dimensionless distance   yplus :  0.12631E+00 0.71899E+01
   Friction thermal sca.    tstar : -0.11409E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94240E-01 0.53645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83602E-02      32   0.35555E-03   0.23215E+01 0.10673E+03 
c  Velocity[X]                                      0.11651E+01 
c  Velocity[Y]                                      0.11564E+01 
c  Velocity[Z]                                      0.10419E-29 
c  Pressure     0.91566E-07     456   0.91505E-08   0.89489E-01 0.55300E+03 
c  nu_tilda     0.54966E-05      32   0.63840E-05   0.22508E-06 0.13527E+03 
c  TempC        0.33714E+02      26   0.42173E-03   0.44395E+01 0.21574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9101          10.453          4.5729          4.5729
v  Velocity[Y]             -2.956          7.2332     -0.00034953     -0.00034953
v  Velocity[Z]       -1.0595e-014     1.0604e-014    -6.4672e-018    -6.4672e-018
v  ǁVelocityǁ         0.0016217          10.453          5.2576          5.2576
v  Pressure               -50.804          17.834         -9.8039         -9.8039
v  nu_tilda           4.3358e-007       0.0042695       0.0012481       0.0012481
v  TempC                       21          73.069          21.786          21.786
v  TurbVisc           3.1085e-014        0.005032       0.0014637       0.0014637
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1231:        0.20320E+01

===============================================================


 INSTANT    0.123200000E+04   TIME STEP NUMBER            1232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11266E-01 0.89276E+00
   Friction velocity        uk    :  0.11266E-01 0.89276E+00
   Dimensionless distance   yplus :  0.90695E-01 0.71873E+01
   Friction thermal sca.    tstar : -0.11218E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67669E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83628E-02      32   0.33769E-03   0.24089E+01 0.10755E+03 
c  Velocity[X]                                      0.12291E+01 
c  Velocity[Y]                                      0.11797E+01 
c  Velocity[Z]                                      0.15821E-29 
c  Pressure     0.13731E-06     472   0.97759E-08   0.13542E+00 0.85115E+03 
c  nu_tilda     0.54984E-05      32   0.15869E-04   0.22534E-06 0.13533E+03 
c  TempC        0.33724E+02      26   0.35173E-03   0.54934E+01 0.26805E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9073          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9543           7.206     -0.00036144     -0.00036144
v  Velocity[Z]       -1.0601e-014     1.0148e-014    -6.4748e-018    -6.4748e-018
v  ǁVelocityǁ        0.00066216          10.453          5.2576          5.2576
v  Pressure               -50.799          17.684         -9.8544         -9.8544
v  nu_tilda           4.3366e-007       0.0042695       0.0012486       0.0012486
v  TempC                       21          73.068          21.786          21.786
v  TurbVisc           3.1091e-014        0.005032       0.0014644       0.0014644
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1232:        0.23080E+01

===============================================================


 INSTANT    0.123300000E+04   TIME STEP NUMBER            1233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87663E-02 0.89149E+00
   Friction velocity        uk    :  0.87663E-02 0.89149E+00
   Dimensionless distance   yplus :  0.70575E-01 0.71771E+01
   Friction thermal sca.    tstar : -0.11935E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52657E-01 0.53549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83653E-02      32   0.29401E-03   0.23687E+01 0.10732E+03 
c  Velocity[X]                                      0.11992E+01 
c  Velocity[Y]                                      0.11694E+01 
c  Velocity[Z]                                      0.18648E-29 
c  Pressure     0.95527E-07     442   0.94615E-08   0.92354E-01 0.54623E+03 
c  nu_tilda     0.55002E-05      32   0.63665E-05   0.22559E-06 0.13539E+03 
c  TempC        0.33734E+02      27   0.34599E-03   0.56081E+01 0.24683E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9045          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9527          7.2299     -0.00037377     -0.00037377
v  Velocity[Z]       -1.0651e-014     1.0573e-014    -6.4736e-018    -6.4736e-018
v  ǁVelocityǁ        0.00077063          10.453          5.2575          5.2575
v  Pressure               -50.766           17.77         -9.8304         -9.8304
v  nu_tilda           4.3369e-007       0.0042695       0.0012492       0.0012492
v  TempC                       21          73.069          21.787          21.787
v  TurbVisc           3.1116e-014        0.005032       0.0014651       0.0014651
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1233:        0.22770E+01

===============================================================


 INSTANT    0.123400000E+04   TIME STEP NUMBER            1234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12495E-01 0.89275E+00
   Friction velocity        uk    :  0.12495E-01 0.89275E+00
   Dimensionless distance   yplus :  0.10059E+00 0.71872E+01
   Friction thermal sca.    tstar : -0.11606E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75054E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83679E-02      32   0.35213E-03   0.23701E+01 0.10732E+03 
c  Velocity[X]                                      0.12066E+01 
c  Velocity[Y]                                      0.11636E+01 
c  Velocity[Z]                                      0.11637E-29 
c  Pressure     0.12786E-06     489   0.99254E-08   0.12429E+00 0.80081E+03 
c  nu_tilda     0.55020E-05      32   0.15887E-04   0.22585E-06 0.13545E+03 
c  TempC        0.33744E+02      26   0.36995E-03   0.44966E+01 0.22028E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9015          10.453          4.5729          4.5729
v  Velocity[Y]             -2.951           7.204      -0.0003858      -0.0003858
v  Velocity[Z]        -1.073e-014     1.0106e-014    -6.4783e-018    -6.4783e-018
v  ǁVelocityǁ        0.00071129          10.453          5.2574          5.2574
v  Pressure               -50.761          17.632         -9.8781         -9.8781
v  nu_tilda           4.3376e-007       0.0042695       0.0012498       0.0012498
v  TempC                       21          73.068          21.787          21.787
v  TurbVisc           3.1124e-014        0.005032       0.0014658       0.0014658
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1234:        0.21170E+01

===============================================================


 INSTANT    0.123500000E+04   TIME STEP NUMBER            1235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17961E-01 0.89215E+00
   Friction velocity        uk    :  0.17961E-01 0.89215E+00
   Dimensionless distance   yplus :  0.14460E+00 0.71824E+01
   Friction thermal sca.    tstar : -0.12316E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10789E+00 0.53589E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83705E-02      32   0.23434E-03   0.23916E+01 0.10762E+03 
c  Velocity[X]                                      0.12044E+01 
c  Velocity[Y]                                      0.11872E+01 
c  Velocity[Z]                                      0.10240E-29 
c  Pressure     0.12215E-06     488   0.96355E-08   0.11925E+00 0.77245E+03 
c  nu_tilda     0.55039E-05      32   0.63479E-05   0.22609E-06 0.13551E+03 
c  TempC        0.33754E+02      26   0.36277E-03   0.48466E+01 0.23225E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8985          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9493          7.2305      -0.0003984      -0.0003984
v  Velocity[Z]       -1.0823e-014     1.0592e-014      -6.48e-018      -6.48e-018
v  ǁVelocityǁ        0.00062886          10.453          5.2573          5.2573
v  Pressure               -50.729          17.763         -9.8408         -9.8408
v  nu_tilda           4.3382e-007       0.0042695       0.0012504       0.0012504
v  TempC                       21          73.068          21.787          21.787
v  TurbVisc           3.1142e-014        0.005032       0.0014665       0.0014665
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1235:        0.21170E+01

===============================================================


 INSTANT    0.123600000E+04   TIME STEP NUMBER            1236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20618E-01 0.89376E+00
   Friction velocity        uk    :  0.20618E-01 0.89376E+00
   Dimensionless distance   yplus :  0.16599E+00 0.71954E+01
   Friction thermal sca.    tstar : -0.12700E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12385E+00 0.53686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83731E-02      32   0.28791E-03   0.23498E+01 0.10741E+03 
c  Velocity[X]                                      0.11723E+01 
c  Velocity[Y]                                      0.11775E+01 
c  Velocity[Z]                                      0.12131E-29 
c  Pressure     0.10591E-06     458   0.99629E-08   0.10226E+00 0.47609E+03 
c  nu_tilda     0.55057E-05      32   0.15882E-04   0.22634E-06 0.13556E+03 
c  TempC        0.33765E+02      26   0.40488E-03   0.55735E+01 0.24164E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8955          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9476          7.2398     -0.00041066     -0.00041066
v  Velocity[Z]       -1.0839e-014     1.0137e-014    -6.4817e-018    -6.4817e-018
v  ǁVelocityǁ        0.00058756          10.453          5.2573          5.2573
v  Pressure               -50.721           17.72         -9.8714         -9.8714
v  nu_tilda           4.3379e-007       0.0042695       0.0012509       0.0012509
v  TempC                       21          73.069          21.788          21.788
v  TurbVisc            3.116e-014        0.005032       0.0014672       0.0014672
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1236:        0.20460E+01

===============================================================


 INSTANT    0.123700000E+04   TIME STEP NUMBER            1237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66007E-02 0.89324E+00
   Friction velocity        uk    :  0.66007E-02 0.89324E+00
   Dimensionless distance   yplus :  0.53140E-01 0.71912E+01
   Friction thermal sca.    tstar : -0.11647E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39648E-01 0.53654E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83756E-02      32   0.35021E-03   0.23727E+01 0.10761E+03 
c  Velocity[X]                                      0.12001E+01 
c  Velocity[Y]                                      0.11727E+01 
c  Velocity[Z]                                      0.13288E-29 
c  Pressure     0.12171E-06     425   0.93077E-08   0.11875E+00 0.41903E+03 
c  nu_tilda     0.55075E-05      32   0.63337E-05   0.22658E-06 0.13562E+03 
c  TempC        0.33775E+02      26   0.34977E-03   0.52130E+01 0.23821E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8925          10.453          4.5729          4.5729
v  Velocity[Y]             -2.946          7.2122     -0.00042325     -0.00042325
v  Velocity[Z]       -1.0753e-014      1.056e-014    -6.4825e-018    -6.4825e-018
v  ǁVelocityǁ        0.00060085          10.453          5.2572          5.2572
v  Pressure               -50.688          17.612         -9.8804         -9.8804
v  nu_tilda           4.3377e-007       0.0042695       0.0012516       0.0012516
v  TempC                       21          73.068          21.788          21.788
v  TurbVisc           3.1152e-014        0.005032       0.0014678       0.0014678
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1237:        0.19800E+01

===============================================================


 INSTANT    0.123800000E+04   TIME STEP NUMBER            1238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18302E-01 0.89220E+00
   Friction velocity        uk    :  0.18302E-01 0.89220E+00
   Dimensionless distance   yplus :  0.14735E+00 0.71828E+01
   Friction thermal sca.    tstar : -0.12891E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10994E+00 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83782E-02      32   0.33684E-03   0.24071E+01 0.10807E+03 
c  Velocity[X]                                      0.12093E+01 
c  Velocity[Y]                                      0.11978E+01 
c  Velocity[Z]                                      0.96654E-30 
c  Pressure     0.11338E-06     313   0.91872E-08   0.11050E+00 0.26756E+03 
c  nu_tilda     0.55093E-05      32   0.15897E-04   0.22683E-06 0.13568E+03 
c  TempC        0.33785E+02      26   0.42482E-03   0.42898E+01 0.22087E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8896          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9443          7.2305     -0.00043576     -0.00043576
v  Velocity[Z]       -1.0653e-014     1.0096e-014    -6.4785e-018    -6.4785e-018
v  ǁVelocityǁ        0.00063938          10.453          5.2571          5.2571
v  Pressure                -50.69          17.702         -9.8876         -9.8876
v  nu_tilda           4.3372e-007       0.0042695       0.0012521       0.0012521
v  TempC                       21          73.069          21.789          21.789
v  TurbVisc           3.1145e-014        0.005032       0.0014685       0.0014685
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1238:        0.17210E+01

===============================================================


 INSTANT    0.123900000E+04   TIME STEP NUMBER            1239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12786E-01 0.89310E+00
   Friction velocity        uk    :  0.12786E-01 0.89310E+00
   Dimensionless distance   yplus :  0.10293E+00 0.71900E+01
   Friction thermal sca.    tstar : -0.11671E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76800E-01 0.53646E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83807E-02      32   0.30731E-03   0.24044E+01 0.10808E+03 
c  Velocity[X]                                      0.12169E+01 
c  Velocity[Y]                                      0.11875E+01 
c  Velocity[Z]                                      0.10870E-29 
c  Pressure     0.11715E-06     438   0.91620E-08   0.11488E+00 0.48168E+03 
c  nu_tilda     0.55112E-05      32   0.63160E-05   0.22707E-06 0.13574E+03 
c  TempC        0.33795E+02      26   0.31756E-03   0.76551E+01 0.27475E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8868          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9427          7.2124     -0.00044837     -0.00044837
v  Velocity[Z]       -1.0631e-014     1.0582e-014    -6.4843e-018    -6.4843e-018
v  ǁVelocityǁ        0.00046856          10.453          5.2571          5.2571
v  Pressure                -50.65           17.59         -9.8975         -9.8975
v  nu_tilda           4.3381e-007       0.0042695       0.0012527       0.0012527
v  TempC                       21          73.068          21.789          21.789
v  TurbVisc           3.1131e-014        0.005032       0.0014692       0.0014692
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1239:        0.20040E+01

===============================================================


 INSTANT    0.124000000E+04   TIME STEP NUMBER            1240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83324E-02 0.89238E+00
   Friction velocity        uk    :  0.83324E-02 0.89238E+00
   Dimensionless distance   yplus :  0.67081E-01 0.71843E+01
   Friction thermal sca.    tstar : -0.13049E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50050E-01 0.53603E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83833E-02      32   0.25640E-03   0.23858E+01 0.10793E+03 
c  Velocity[X]                                      0.12051E+01 
c  Velocity[Y]                                      0.11807E+01 
c  Velocity[Z]                                      0.16326E-29 
c  Pressure     0.12000E-06     328   0.97335E-08   0.11487E+00 0.23416E+03 
c  nu_tilda     0.55130E-05      32   0.15900E-04   0.22734E-06 0.13580E+03 
c  TempC        0.33805E+02      27   0.36607E-03   0.47782E+01 0.22578E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8838          10.453          4.5729          4.5729
v  Velocity[Y]             -2.941          7.2325     -0.00046074     -0.00046074
v  Velocity[Z]       -1.0426e-014     1.0128e-014    -6.4828e-018    -6.4828e-018
v  ǁVelocityǁ        0.00066563          10.453           5.257           5.257
v  Pressure               -50.652          17.665         -9.9031         -9.9031
v  nu_tilda            4.339e-007       0.0042695       0.0012533       0.0012533
v  TempC                       21          73.068          21.789          21.789
v  TurbVisc           3.1158e-014        0.005032       0.0014699       0.0014699
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1240:        0.17390E+01

===============================================================


 INSTANT    0.124100000E+04   TIME STEP NUMBER            1241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15930E-01 0.89371E+00
   Friction velocity        uk    :  0.15930E-01 0.89371E+00
   Dimensionless distance   yplus :  0.12825E+00 0.71950E+01
   Friction thermal sca.    tstar : -0.11962E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95687E-01 0.53683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83858E-02      32   0.33410E-03   0.23779E+01 0.10806E+03 
c  Velocity[X]                                      0.11735E+01 
c  Velocity[Y]                                      0.12045E+01 
c  Velocity[Z]                                      0.11090E-29 
c  Pressure     0.10122E-06     440   0.97025E-08   0.98251E-01 0.44977E+03 
c  nu_tilda     0.55148E-05      32   0.63230E-05   0.22759E-06 0.13586E+03 
c  TempC        0.33816E+02      27   0.45071E-03   0.46404E+01 0.22784E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8809          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9393          7.2413      -0.0004735      -0.0004735
v  Velocity[Z]       -1.0241e-014     1.0551e-014    -6.4838e-018    -6.4838e-018
v  ǁVelocityǁ        0.00042016          10.453          5.2569          5.2569
v  Pressure               -50.614          17.699         -9.8828         -9.8828
v  nu_tilda           4.3387e-007       0.0042695       0.0012539       0.0012539
v  TempC                       21          73.068           21.79           21.79
v  TurbVisc           3.1184e-014        0.005032       0.0014706       0.0014706
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1241:        0.20020E+01

===============================================================


 INSTANT    0.124200000E+04   TIME STEP NUMBER            1242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12000E-01 0.89344E+00
   Friction velocity        uk    :  0.12000E-01 0.89344E+00
   Dimensionless distance   yplus :  0.96609E-01 0.71928E+01
   Friction thermal sca.    tstar : -0.11831E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72081E-01 0.53667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83884E-02      32   0.31861E-03   0.24296E+01 0.10854E+03 
c  Velocity[X]                                      0.12330E+01 
c  Velocity[Y]                                      0.11966E+01 
c  Velocity[Z]                                      0.12425E-29 
c  Pressure     0.13116E-06     505   0.99967E-08   0.12901E+00 0.10826E+04 
c  nu_tilda     0.55166E-05      32   0.15898E-04   0.22786E-06 0.13592E+03 
c  TempC        0.33826E+02      26   0.30582E-03   0.73345E+01 0.29040E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8778          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9376          7.2158     -0.00048606     -0.00048606
v  Velocity[Z]        -1.005e-014     1.0086e-014    -6.4805e-018    -6.4805e-018
v  ǁVelocityǁ        0.00070745          10.453          5.2568          5.2568
v  Pressure               -50.612          17.516         -9.9484         -9.9484
v  nu_tilda            4.339e-007       0.0042695       0.0012544       0.0012544
v  TempC                       21          73.068           21.79           21.79
v  TurbVisc           3.1175e-014        0.005032       0.0014713       0.0014713
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1242:        0.21510E+01

===============================================================


 INSTANT    0.124300000E+04   TIME STEP NUMBER            1243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20648E-01 0.89212E+00
   Friction velocity        uk    :  0.20648E-01 0.89212E+00
   Dimensionless distance   yplus :  0.16623E+00 0.71821E+01
   Friction thermal sca.    tstar : -0.12756E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12403E+00 0.53587E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83909E-02      32   0.31914E-03   0.24064E+01 0.10837E+03 
c  Velocity[X]                                      0.12169E+01 
c  Velocity[Y]                                      0.11895E+01 
c  Velocity[Z]                                      0.11053E-29 
c  Pressure     0.13156E-06     488   0.97432E-08   0.12608E+00 0.85067E+03 
c  nu_tilda     0.55185E-05      32   0.63037E-05   0.22811E-06 0.13598E+03 
c  TempC        0.33836E+02      27   0.43906E-03   0.46243E+01 0.20939E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8748          10.453          4.5729          4.5729
v  Velocity[Y]             -2.936          7.2334     -0.00049889     -0.00049889
v  Velocity[Z]        -9.894e-015      1.057e-014     -6.481e-018     -6.481e-018
v  ǁVelocityǁ        0.00036568          10.453          5.2567          5.2567
v  Pressure               -50.573          17.645          -9.903          -9.903
v  nu_tilda           4.3395e-007       0.0042695        0.001255        0.001255
v  TempC                       21          73.068           21.79           21.79
v  TurbVisc           3.1183e-014        0.005032        0.001472        0.001472
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1243:        0.21020E+01

===============================================================


 INSTANT    0.124400000E+04   TIME STEP NUMBER            1244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20008E-01 0.89351E+00
   Friction velocity        uk    :  0.20008E-01 0.89351E+00
   Dimensionless distance   yplus :  0.16108E+00 0.71934E+01
   Friction thermal sca.    tstar : -0.13960E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12018E+00 0.53671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83935E-02      32   0.32727E-03   0.23966E+01 0.10842E+03 
c  Velocity[X]                                      0.12038E+01 
c  Velocity[Y]                                      0.11928E+01 
c  Velocity[Z]                                      0.14574E-29 
c  Pressure     0.11762E-06     506   0.92839E-08   0.11574E+00 0.72814E+03 
c  nu_tilda     0.55203E-05      32   0.15913E-04   0.22837E-06 0.13604E+03 
c  TempC        0.33846E+02      27   0.43084E-03   0.56127E+01 0.25737E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8718          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9343          7.2131     -0.00051142     -0.00051142
v  Velocity[Z]        -9.669e-015     1.0119e-014    -6.4783e-018    -6.4783e-018
v  ǁVelocityǁ        0.00056752          10.453          5.2567          5.2567
v  Pressure               -50.573           17.53         -9.9495         -9.9495
v  nu_tilda           4.3402e-007       0.0042695       0.0012556       0.0012556
v  TempC                       21          73.068          21.791          21.791
v  TurbVisc           3.1198e-014        0.005032       0.0014726       0.0014726
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1244:        0.21430E+01

===============================================================


 INSTANT    0.124500000E+04   TIME STEP NUMBER            1245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14462E-01 0.89275E+00
   Friction velocity        uk    :  0.14462E-01 0.89275E+00
   Dimensionless distance   yplus :  0.11643E+00 0.71873E+01
   Friction thermal sca.    tstar : -0.25890E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86870E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83960E-02      32   0.27760E-03   0.24162E+01 0.10869E+03 
c  Velocity[X]                                      0.11971E+01 
c  Velocity[Y]                                      0.12191E+01 
c  Velocity[Z]                                      0.11837E-29 
c  Pressure     0.11253E-06     456   0.98194E-08   0.10892E+00 0.54506E+03 
c  nu_tilda     0.55221E-05      32   0.62824E-05   0.22861E-06 0.13610E+03 
c  TempC        0.33856E+02      27   0.36717E-03   0.66489E+01 0.27073E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.869          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9326          7.2389     -0.00052421     -0.00052421
v  Velocity[Z]       -9.4808e-015     1.0539e-014    -6.4719e-018    -6.4719e-018
v  ǁVelocityǁ        0.00032527          10.453          5.2566          5.2566
v  Pressure               -50.538           17.61         -9.9247         -9.9247
v  nu_tilda           4.3404e-007       0.0042695       0.0012562       0.0012562
v  TempC                       21          73.068          21.791          21.791
v  TurbVisc           3.1218e-014        0.005032       0.0014733       0.0014733
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1245:        0.20340E+01

===============================================================


 INSTANT    0.124600000E+04   TIME STEP NUMBER            1246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41633E-02 0.89424E+00
   Friction velocity        uk    :  0.41633E-02 0.89424E+00
   Dimensionless distance   yplus :  0.33518E-01 0.71993E+01
   Friction thermal sca.    tstar : -0.18906E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25008E-01 0.53714E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.83986E-02      32   0.31736E-03   0.24188E+01 0.10875E+03 
c  Velocity[X]                                      0.12111E+01 
c  Velocity[Y]                                      0.12077E+01 
c  Velocity[Z]                                      0.98284E-30 
c  Pressure     0.13282E-06     456   0.92992E-08   0.12683E+00 0.48427E+03 
c  nu_tilda     0.55240E-05      32   0.15911E-04   0.22887E-06 0.13616E+03 
c  TempC        0.33866E+02      26   0.31733E-03   0.49562E+01 0.23946E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.866          10.453          4.5729          4.5729
v  Velocity[Y]             -2.931          7.2439     -0.00053684     -0.00053684
v  Velocity[Z]       -9.3331e-015     1.0077e-014    -6.4687e-018    -6.4687e-018
v  ǁVelocityǁ        0.00029644          10.453          5.2565          5.2565
v  Pressure               -50.535           17.55         -9.9568         -9.9568
v  nu_tilda           4.3401e-007       0.0042695       0.0012567       0.0012567
v  TempC                       21          73.068          21.791          21.791
v  TurbVisc           3.1224e-014        0.005032        0.001474        0.001474
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1246:        0.20200E+01

===============================================================


 INSTANT    0.124700000E+04   TIME STEP NUMBER            1247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14384E-01 0.89421E+00
   Friction velocity        uk    :  0.14384E-01 0.89421E+00
   Dimensionless distance   yplus :  0.11580E+00 0.71990E+01
   Friction thermal sca.    tstar : -0.18748E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86402E-01 0.53713E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84011E-02      32   0.31704E-03   0.24425E+01 0.10902E+03 
c  Velocity[X]                                      0.12372E+01 
c  Velocity[Y]                                      0.12053E+01 
c  Velocity[Z]                                      0.16029E-29 
c  Pressure     0.11506E-06     282   0.92675E-08   0.11385E+00 0.30635E+03 
c  nu_tilda     0.55258E-05      32   0.62859E-05   0.22912E-06 0.13622E+03 
c  TempC        0.33876E+02      26   0.29242E-03   0.48718E+01 0.22615E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8631          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9293          7.2218     -0.00054973     -0.00054973
v  Velocity[Z]       -9.1891e-015     1.0558e-014    -6.4667e-018    -6.4667e-018
v  ǁVelocityǁ        0.00060309          10.453          5.2564          5.2564
v  Pressure               -50.502          17.502         -9.9556         -9.9556
v  nu_tilda           4.3403e-007       0.0042695       0.0012573       0.0012573
v  TempC                       21          73.068          21.792          21.792
v  TurbVisc           3.1215e-014        0.005032       0.0014747       0.0014747
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1247:        0.16330E+01

===============================================================


 INSTANT    0.124800000E+04   TIME STEP NUMBER            1248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20659E-01 0.89295E+00
   Friction velocity        uk    :  0.20659E-01 0.89295E+00
   Dimensionless distance   yplus :  0.16632E+00 0.71888E+01
   Friction thermal sca.    tstar : -0.14799E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12410E+00 0.53637E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84036E-02      32   0.30154E-03   0.24295E+01 0.10908E+03 
c  Velocity[X]                                      0.12019E+01 
c  Velocity[Y]                                      0.12275E+01 
c  Velocity[Z]                                      0.15532E-29 
c  Pressure     0.95270E-07     378   0.94050E-08   0.91234E-01 0.22231E+03 
c  nu_tilda     0.55276E-05      32   0.15915E-04   0.22940E-06 0.13628E+03 
c  TempC        0.33887E+02      26   0.44243E-03   0.44584E+01 0.22164E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.86          10.453          4.5729          4.5729
v  Velocity[Y]            -2.9276          7.2404     -0.00056244     -0.00056244
v  Velocity[Z]       -9.0887e-015     1.0106e-014    -6.4619e-018    -6.4619e-018
v  ǁVelocityǁ        0.00066553          10.453          5.2563          5.2563
v  Pressure               -50.498          17.553         -9.9685         -9.9685
v  nu_tilda           4.3401e-007       0.0042695       0.0012579       0.0012579
v  TempC                       21          73.068          21.792          21.792
v  TurbVisc           3.1221e-014        0.005032       0.0014754       0.0014754
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1248:        0.18480E+01

===============================================================


 INSTANT    0.124900000E+04   TIME STEP NUMBER            1249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17980E-01 0.89388E+00
   Friction velocity        uk    :  0.17980E-01 0.89388E+00
   Dimensionless distance   yplus :  0.14475E+00 0.71963E+01
   Friction thermal sca.    tstar : -0.13497E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10800E+00 0.53693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84062E-02      32   0.33150E-03   0.24278E+01 0.10908E+03 
c  Velocity[X]                                      0.12111E+01 
c  Velocity[Y]                                      0.12168E+01 
c  Velocity[Z]                                      0.10623E-29 
c  Pressure     0.12183E-06     378   0.97738E-08   0.11777E+00 0.42338E+03 
c  nu_tilda     0.55295E-05      32   0.62631E-05   0.22966E-06 0.13634E+03 
c  TempC        0.33897E+02      26   0.31488E-03   0.60913E+01 0.27444E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.857          10.453          4.5729          4.5729
v  Velocity[Y]             -2.926          7.2168     -0.00057518     -0.00057518
v  Velocity[Z]       -9.2192e-015     1.0524e-014    -6.4586e-018    -6.4586e-018
v  ǁVelocityǁ        0.00029156          10.453          5.2562          5.2562
v  Pressure               -50.458          17.454         -9.9729         -9.9729
v  nu_tilda           4.3405e-007       0.0042695       0.0012585       0.0012585
v  TempC                       21          73.068          21.792          21.792
v  TurbVisc           3.1215e-014        0.005032       0.0014761       0.0014761
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1249:        0.18590E+01

===============================================================


 INSTANT    0.125000000E+04   TIME STEP NUMBER            1250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19358E-01 0.89330E+00
   Friction velocity        uk    :  0.19358E-01 0.89330E+00
   Dimensionless distance   yplus :  0.15584E+00 0.71916E+01
   Friction thermal sca.    tstar : -0.14355E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11628E+00 0.53658E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84087E-02      32   0.34516E-03   0.24555E+01 0.10941E+03 
c  Velocity[X]                                      0.12422E+01 
c  Velocity[Y]                                      0.12132E+01 
c  Velocity[Z]                                      0.98772E-30 
c  Pressure     0.11537E-06     346   0.94596E-08   0.11180E+00 0.26517E+03 
c  nu_tilda     0.55313E-05      32   0.15930E-04   0.22993E-06 0.13640E+03 
c  TempC        0.33907E+02      26   0.31294E-03   0.38894E+01 0.21071E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8539          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9243          7.2434     -0.00058788     -0.00058788
v  Velocity[Z]       -8.8635e-015     1.0063e-014    -6.4519e-018    -6.4519e-018
v  ǁVelocityǁ        0.00034625          10.453          5.2561          5.2561
v  Pressure               -50.462          17.542         -9.9799         -9.9799
v  nu_tilda           4.3414e-007       0.0042695        0.001259        0.001259
v  TempC                       21          73.068          21.793          21.793
v  TurbVisc           3.1228e-014        0.005032       0.0014767       0.0014767
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1250:        0.17880E+01

===============================================================


 INSTANT    0.125100000E+04   TIME STEP NUMBER            1251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89109E-02 0.89457E+00
   Friction velocity        uk    :  0.89109E-02 0.89457E+00
   Dimensionless distance   yplus :  0.71739E-01 0.72019E+01
   Friction thermal sca.    tstar : -0.12876E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53525E-01 0.53734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84112E-02      32   0.31943E-03   0.24298E+01 0.10934E+03 
c  Velocity[X]                                      0.11955E+01 
c  Velocity[Y]                                      0.12344E+01 
c  Velocity[Z]                                      0.12022E-29 
c  Pressure     0.10501E-06     394   0.91878E-08   0.10129E+00 0.32527E+03 
c  nu_tilda     0.55331E-05      32   0.62486E-05   0.23018E-06 0.13646E+03 
c  TempC        0.33917E+02      27   0.50418E-03   0.34279E+01 0.18263E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8511          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9226          7.2536       -0.000601       -0.000601
v  Velocity[Z]       -9.3019e-015     1.0543e-014    -6.4478e-018    -6.4478e-018
v  ǁVelocityǁ        0.00024426          10.453           5.256           5.256
v  Pressure               -50.425          17.534         -9.9725         -9.9725
v  nu_tilda           4.3413e-007       0.0042695       0.0012596       0.0012596
v  TempC                       21          73.068          21.793          21.793
v  TurbVisc           3.1252e-014        0.005032       0.0014774       0.0014774
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1251:        0.18870E+01

===============================================================


 INSTANT    0.125200000E+04   TIME STEP NUMBER            1252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30328E-02 0.89417E+00
   Friction velocity        uk    :  0.30328E-02 0.89417E+00
   Dimensionless distance   yplus :  0.24416E-01 0.71987E+01
   Friction thermal sca.    tstar : -0.12891E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18217E-01 0.53710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84138E-02      32   0.31973E-03   0.24547E+01 0.10952E+03 
c  Velocity[X]                                      0.12303E+01 
c  Velocity[Y]                                      0.12244E+01 
c  Velocity[Z]                                      0.11975E-29 
c  Pressure     0.12957E-06     473   0.98596E-08   0.12480E+00 0.77552E+03 
c  nu_tilda     0.55350E-05      32   0.15926E-04   0.23045E-06 0.13652E+03 
c  TempC        0.33927E+02      28   0.35831E-03   0.54881E+01 0.24974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8481          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9209          7.2216     -0.00061353     -0.00061353
v  Velocity[Z]       -9.4182e-015     1.0093e-014    -6.4442e-018    -6.4442e-018
v  ǁVelocityǁ        0.00072048          10.453           5.256           5.256
v  Pressure               -50.421          17.396         -10.018         -10.018
v  nu_tilda            4.342e-007       0.0042695       0.0012602       0.0012602
v  TempC                       21          73.068          21.794          21.794
v  TurbVisc           3.1251e-014        0.005032       0.0014781       0.0014781
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1252:        0.20840E+01

===============================================================


 INSTANT    0.125300000E+04   TIME STEP NUMBER            1253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13333E-01 0.89297E+00
   Friction velocity        uk    :  0.13333E-01 0.89297E+00
   Dimensionless distance   yplus :  0.10734E+00 0.71890E+01
   Friction thermal sca.    tstar : -0.13960E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80085E-01 0.53638E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84163E-02      32   0.34034E-03   0.24511E+01 0.10959E+03 
c  Velocity[X]                                      0.12279E+01 
c  Velocity[Y]                                      0.12232E+01 
c  Velocity[Z]                                      0.13203E-29 
c  Pressure     0.10086E-06     489   0.92470E-08   0.97678E-01 0.73121E+03 
c  nu_tilda     0.55368E-05      32   0.62431E-05   0.23070E-06 0.13658E+03 
c  TempC        0.33937E+02      27   0.40884E-03   0.53847E+01 0.24520E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8452          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9193          7.2461     -0.00062658     -0.00062658
v  Velocity[Z]        -9.496e-015     1.0511e-014      -6.44e-018      -6.44e-018
v  ǁVelocityǁ         0.0003409          10.453          5.2559          5.2559
v  Pressure               -50.387          17.519         -9.9828         -9.9828
v  nu_tilda           4.3423e-007       0.0042695       0.0012608       0.0012608
v  TempC                       21          73.068          21.794          21.794
v  TurbVisc            3.127e-014        0.005032       0.0014788       0.0014788
v  total_pressure     1.0127e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1253:        0.21050E+01

===============================================================


 INSTANT    0.125400000E+04   TIME STEP NUMBER            1254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20154E-01 0.89416E+00
   Friction velocity        uk    :  0.20154E-01 0.89416E+00
   Dimensionless distance   yplus :  0.16225E+00 0.71986E+01
   Friction thermal sca.    tstar : -0.13322E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12106E+00 0.53709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84188E-02      32   0.32529E-03   0.24597E+01 0.10981E+03 
c  Velocity[X]                                      0.12168E+01 
c  Velocity[Y]                                      0.12429E+01 
c  Velocity[Z]                                      0.14746E-29 
c  Pressure     0.11604E-06     490   0.93543E-08   0.11329E+00 0.88401E+03 
c  nu_tilda     0.55387E-05      32   0.15937E-04   0.23097E-06 0.13665E+03 
c  TempC        0.33947E+02      26   0.34240E-03   0.60581E+01 0.26819E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8421          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9176          7.2231      -0.0006393      -0.0006393
v  Velocity[Z]       -9.5399e-015     1.0051e-014     -6.432e-018     -6.432e-018
v  ǁVelocityǁ        0.00018028          10.452          5.2558          5.2558
v  Pressure               -50.383          17.374         -10.035         -10.035
v  nu_tilda           4.3423e-007       0.0042695       0.0012613       0.0012613
v  TempC                       21          73.068          21.794          21.794
v  TurbVisc           3.1279e-014        0.005032       0.0014795       0.0014795
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1254:        0.21080E+01

===============================================================


 INSTANT    0.125500000E+04   TIME STEP NUMBER            1255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13293E-01 0.89323E+00
   Friction velocity        uk    :  0.13293E-01 0.89323E+00
   Dimensionless distance   yplus :  0.10702E+00 0.71911E+01
   Friction thermal sca.    tstar : -0.14004E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79848E-01 0.53654E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84213E-02      32   0.31709E-03   0.24507E+01 0.10981E+03 
c  Velocity[X]                                      0.12162E+01 
c  Velocity[Y]                                      0.12345E+01 
c  Velocity[Z]                                      0.12215E-29 
c  Pressure     0.11369E-06     473   0.92223E-08   0.10817E+00 0.63321E+03 
c  nu_tilda     0.55405E-05      32   0.62287E-05   0.23123E-06 0.13671E+03 
c  TempC        0.33957E+02      27   0.36306E-03   0.62539E+01 0.25897E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8391          10.452          4.5729          4.5729
v  Velocity[Y]             -2.916          7.2459     -0.00065204     -0.00065204
v  Velocity[Z]       -9.6947e-015     1.0529e-014    -6.4268e-018    -6.4268e-018
v  ǁVelocityǁ        0.00049083          10.452          5.2557          5.2557
v  Pressure                -50.35          17.467         -10.005         -10.005
v  nu_tilda           4.3424e-007       0.0042695       0.0012619       0.0012619
v  TempC                       21          73.068          21.795          21.795
v  TurbVisc            3.128e-014        0.005032       0.0014801       0.0014801
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1255:        0.20730E+01

===============================================================


 INSTANT    0.125600000E+04   TIME STEP NUMBER            1256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16499E-01 0.89477E+00
   Friction velocity        uk    :  0.16499E-01 0.89477E+00
   Dimensionless distance   yplus :  0.13283E+00 0.72035E+01
   Friction thermal sca.    tstar : -0.14754E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99105E-01 0.53746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84238E-02      32   0.34819E-03   0.24431E+01 0.10986E+03 
c  Velocity[X]                                      0.12120E+01 
c  Velocity[Y]                                      0.12311E+01 
c  Velocity[Z]                                      0.12604E-29 
c  Pressure     0.10638E-06     410   0.93706E-08   0.10235E+00 0.28603E+03 
c  nu_tilda     0.55424E-05      32   0.15938E-04   0.23152E-06 0.13677E+03 
c  TempC        0.33967E+02      26   0.37856E-03   0.47439E+01 0.21996E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8359          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9143          7.2557     -0.00066497     -0.00066497
v  Velocity[Z]       -9.9475e-015     1.0082e-014    -6.4239e-018    -6.4239e-018
v  ǁVelocityǁ         0.0008157          10.452          5.2556          5.2556
v  Pressure               -50.348          17.463         -10.026         -10.026
v  nu_tilda            4.342e-007       0.0042695       0.0012625       0.0012625
v  TempC                       21          73.068          21.795          21.795
v  TurbVisc           3.1281e-014        0.005032       0.0014808       0.0014808
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1256:        0.19230E+01

===============================================================


 INSTANT    0.125700000E+04   TIME STEP NUMBER            1257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13406E-01 0.89438E+00
   Friction velocity        uk    :  0.13406E-01 0.89438E+00
   Dimensionless distance   yplus :  0.10793E+00 0.72004E+01
   Friction thermal sca.    tstar : -0.13318E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80528E-01 0.53723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84263E-02      33   0.30694E-03   0.24915E+01 0.11035E+03 
c  Velocity[X]                                      0.12374E+01 
c  Velocity[Y]                                      0.12541E+01 
c  Velocity[Z]                                      0.10964E-29 
c  Pressure     0.12295E-06     409   0.98607E-08   0.11998E+00 0.45762E+03 
c  nu_tilda     0.55442E-05      32   0.62284E-05   0.23178E-06 0.13684E+03 
c  TempC        0.33978E+02      26   0.34029E-03   0.50961E+01 0.24352E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.833          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9126          7.2301     -0.00067769     -0.00067769
v  Velocity[Z]       -1.0199e-014     1.0497e-014    -6.4184e-018    -6.4184e-018
v  ǁVelocityǁ        0.00031265          10.452          5.2555          5.2555
v  Pressure               -50.306          17.367         -10.035         -10.035
v  nu_tilda           4.3422e-007       0.0042695       0.0012631       0.0012631
v  TempC                       21          73.068          21.795          21.795
v  TurbVisc            3.127e-014        0.005032       0.0014815       0.0014815
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1257:        0.19350E+01

===============================================================


 INSTANT    0.125800000E+04   TIME STEP NUMBER            1258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55757E-02 0.89303E+00
   Friction velocity        uk    :  0.55757E-02 0.89303E+00
   Dimensionless distance   yplus :  0.44889E-01 0.71895E+01
   Friction thermal sca.    tstar : -0.14446E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33492E-01 0.53642E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84289E-02      33   0.30571E-03   0.24625E+01 0.11015E+03 
c  Velocity[X]                                      0.12199E+01 
c  Velocity[Y]                                      0.12426E+01 
c  Velocity[Z]                                      0.11504E-29 
c  Pressure     0.11122E-06     394   0.99479E-08   0.10585E+00 0.19811E+03 
c  nu_tilda     0.55461E-05      32   0.15942E-04   0.23206E-06 0.13690E+03 
c  TempC        0.33988E+02      26   0.34588E-03   0.55985E+01 0.25082E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8301          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9109          7.2462     -0.00069035     -0.00069035
v  Velocity[Z]       -1.0089e-014     1.0039e-014    -6.4129e-018    -6.4129e-018
v  ǁVelocityǁ        0.00055638          10.452          5.2554          5.2554
v  Pressure               -50.307          17.394          -10.05          -10.05
v  nu_tilda           4.3427e-007       0.0042695       0.0012636       0.0012636
v  TempC                       21          73.068          21.796          21.796
v  TurbVisc           3.1276e-014        0.005032       0.0014822       0.0014822
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1258:        0.18990E+01

===============================================================


 INSTANT    0.125900000E+04   TIME STEP NUMBER            1259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12746E-01 0.89433E+00
   Friction velocity        uk    :  0.12746E-01 0.89433E+00
   Dimensionless distance   yplus :  0.10262E+00 0.72000E+01
   Friction thermal sca.    tstar : -0.13916E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76564E-01 0.53720E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84314E-02      33   0.33356E-03   0.24919E+01 0.11045E+03 
c  Velocity[X]                                      0.12493E+01 
c  Velocity[Y]                                      0.12426E+01 
c  Velocity[Z]                                      0.11533E-29 
c  Pressure     0.11191E-06     393   0.92510E-08   0.10972E+00 0.33381E+03 
c  nu_tilda     0.55479E-05      32   0.62085E-05   0.23232E-06 0.13696E+03 
c  TempC        0.33998E+02      26   0.45021E-03   0.61331E+01 0.24472E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8272          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9093          7.2283     -0.00070328     -0.00070328
v  Velocity[Z]       -1.0037e-014     1.0515e-014    -6.4088e-018    -6.4088e-018
v  ǁVelocityǁ        0.00024155          10.452          5.2553          5.2553
v  Pressure               -50.269          17.361         -10.044         -10.044
v  nu_tilda           4.3435e-007       0.0042695       0.0012642       0.0012642
v  TempC                       21          73.067          21.796          21.796
v  TurbVisc           3.1291e-014        0.005032       0.0014829       0.0014829
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1259:        0.18900E+01

===============================================================


 INSTANT    0.126000000E+04   TIME STEP NUMBER            1260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47334E-02 0.89358E+00
   Friction velocity        uk    :  0.47334E-02 0.89358E+00
   Dimensionless distance   yplus :  0.38107E-01 0.71939E+01
   Friction thermal sca.    tstar : -0.14980E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28432E-01 0.53675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84339E-02      33   0.25509E-03   0.24866E+01 0.11058E+03 
c  Velocity[X]                                      0.12236E+01 
c  Velocity[Y]                                      0.12629E+01 
c  Velocity[Z]                                      0.12558E-29 
c  Pressure     0.10616E-06     425   0.92571E-08   0.10161E+00 0.29714E+03 
c  nu_tilda     0.55498E-05      32   0.15956E-04   0.23259E-06 0.13702E+03 
c  TempC        0.34008E+02      26   0.33260E-03   0.63714E+01 0.28656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8241          10.452          4.5729          4.5729
v  Velocity[Y]            -2.9076          7.2526      -0.0007159      -0.0007159
v  Velocity[Z]       -9.9438e-015     1.0067e-014    -6.4019e-018    -6.4019e-018
v  ǁVelocityǁ        0.00011657          10.452          5.2552          5.2552
v  Pressure                -50.27          17.379         -10.067         -10.067
v  nu_tilda           4.3441e-007       0.0042695       0.0012648       0.0012648
v  TempC                       21          73.068          21.796          21.796
v  TurbVisc           3.1314e-014        0.005032       0.0014835       0.0014835
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1260:        0.19630E+01

===============================================================


 INSTANT    0.126100000E+04   TIME STEP NUMBER            1261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71618E-02 0.89503E+00
   Friction velocity        uk    :  0.71618E-02 0.89503E+00
   Dimensionless distance   yplus :  0.57657E-01 0.72056E+01
   Friction thermal sca.    tstar : -0.13760E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43019E-01 0.53762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84364E-02      33   0.30424E-03   0.24549E+01 0.11038E+03 
c  Velocity[X]                                      0.12019E+01 
c  Velocity[Y]                                      0.12530E+01 
c  Velocity[Z]                                      0.14904E-29 
c  Pressure     0.10270E-06     441   0.93649E-08   0.98109E-01 0.42894E+03 
c  nu_tilda     0.55516E-05      32   0.61988E-05   0.23285E-06 0.13709E+03 
c  TempC        0.34018E+02      26   0.32873E-03   0.54637E+01 0.24712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8211          10.452          4.5729          4.5729
v  Velocity[Y]             -2.906          7.2602     -0.00072867     -0.00072867
v  Velocity[Z]       -1.0027e-014     1.0481e-014    -6.3981e-018    -6.3981e-018
v  ǁVelocityǁ        0.00038537          10.452          5.2551          5.2551
v  Pressure               -50.234            17.4         -10.048         -10.048
v  nu_tilda           4.3439e-007       0.0042695       0.0012654       0.0012654
v  TempC                       21          73.068          21.797          21.797
v  TurbVisc            3.133e-014        0.005032       0.0014842       0.0014842
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1261:        0.20080E+01

===============================================================


 INSTANT    0.126200000E+04   TIME STEP NUMBER            1262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14118E-01 0.89481E+00
   Friction velocity        uk    :  0.14118E-01 0.89481E+00
   Dimensionless distance   yplus :  0.11366E+00 0.72038E+01
   Friction thermal sca.    tstar : -0.13824E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84804E-01 0.53748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84389E-02      33   0.34817E-03   0.24790E+01 0.11067E+03 
c  Velocity[X]                                      0.12278E+01 
c  Velocity[Y]                                      0.12513E+01 
c  Velocity[Z]                                      0.12049E-29 
c  Pressure     0.10799E-06     490   0.91878E-08   0.10585E+00 0.83119E+03 
c  nu_tilda     0.55535E-05      32   0.15953E-04   0.23313E-06 0.13715E+03 
c  TempC        0.34028E+02      26   0.40977E-03   0.47150E+01 0.22293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8179          10.451          4.5729          4.5729
v  Velocity[Y]            -2.9043          7.2334     -0.00074138     -0.00074138
v  Velocity[Z]       -1.0096e-014     1.0024e-014    -6.3951e-018    -6.3951e-018
v  ǁVelocityǁ        0.00067427          10.452           5.255           5.255
v  Pressure               -50.233          17.262           -10.1           -10.1
v  nu_tilda           4.3445e-007       0.0042695       0.0012659       0.0012659
v  TempC                       21          73.067          21.797          21.797
v  TurbVisc           3.1325e-014        0.005032       0.0014849       0.0014849
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1262:        0.21110E+01

===============================================================


 INSTANT    0.126300000E+04   TIME STEP NUMBER            1263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16485E-01 0.89345E+00
   Friction velocity        uk    :  0.16485E-01 0.89345E+00
   Dimensionless distance   yplus :  0.13272E+00 0.71929E+01
   Friction thermal sca.    tstar : -0.15099E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99023E-01 0.53667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84413E-02      33   0.33712E-03   0.25268E+01 0.11113E+03 
c  Velocity[X]                                      0.12520E+01 
c  Velocity[Y]                                      0.12749E+01 
c  Velocity[Z]                                      0.13864E-29 
c  Pressure     0.13622E-06     473   0.98836E-08   0.13050E+00 0.70991E+03 
c  nu_tilda     0.55553E-05      32   0.61874E-05   0.23340E-06 0.13721E+03 
c  TempC        0.34038E+02      26   0.35046E-03   0.77004E+01 0.28648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8149          10.451          4.5729          4.5729
v  Velocity[Y]            -2.9026          7.2553     -0.00075414     -0.00075414
v  Velocity[Z]       -1.0213e-014     1.0497e-014     -6.389e-018     -6.389e-018
v  ǁVelocityǁ        0.00024058          10.452          5.2548          5.2548
v  Pressure               -50.193          17.374         -10.064         -10.064
v  nu_tilda           4.3449e-007       0.0042695       0.0012665       0.0012665
v  TempC                       21          73.067          21.797          21.797
v  TurbVisc           3.1341e-014        0.005032       0.0014856       0.0014856
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1263:        0.20720E+01

===============================================================


 INSTANT    0.126400000E+04   TIME STEP NUMBER            1264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51276E-02 0.89456E+00
   Friction velocity        uk    :  0.51276E-02 0.89456E+00
   Dimensionless distance   yplus :  0.41281E-01 0.72018E+01
   Friction thermal sca.    tstar : -0.14289E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30800E-01 0.53734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84439E-02      33   0.30645E-03   0.25338E+01 0.11120E+03 
c  Velocity[X]                                      0.12705E+01 
c  Velocity[Y]                                      0.12634E+01 
c  Velocity[Z]                                      0.11974E-29 
c  Pressure     0.13921E-06     489   0.95358E-08   0.13292E+00 0.86650E+03 
c  nu_tilda     0.55572E-05      32   0.15965E-04   0.23368E-06 0.13728E+03 
c  TempC        0.34048E+02      26   0.38603E-03   0.56773E+01 0.25123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.812          10.451          4.5729          4.5729
v  Velocity[Y]             -2.901          7.2278     -0.00076665     -0.00076665
v  Velocity[Z]       -1.0096e-014     1.0051e-014    -6.3845e-018    -6.3845e-018
v  ǁVelocityǁ         0.0010767          10.451          5.2547          5.2547
v  Pressure               -50.192          17.217         -10.115         -10.115
v  nu_tilda           4.3453e-007       0.0042695       0.0012671       0.0012671
v  TempC                       21          73.067          21.798          21.798
v  TurbVisc           3.1353e-014        0.005032       0.0014863       0.0014863
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1264:        0.23680E+01

===============================================================


 INSTANT    0.126500000E+04   TIME STEP NUMBER            1265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12749E-01 0.89400E+00
   Friction velocity        uk    :  0.12749E-01 0.89400E+00
   Dimensionless distance   yplus :  0.10264E+00 0.71973E+01
   Friction thermal sca.    tstar : -0.16197E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76578E-01 0.53700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84463E-02      33   0.26149E-03   0.24948E+01 0.11100E+03 
c  Velocity[X]                                      0.12342E+01 
c  Velocity[Y]                                      0.12605E+01 
c  Velocity[Z]                                      0.10264E-29 
c  Pressure     0.10979E-06     488   0.95900E-08   0.10559E+00 0.91330E+03 
c  nu_tilda     0.55590E-05      32   0.61704E-05   0.23395E-06 0.13734E+03 
c  TempC        0.34058E+02      27   0.36838E-03   0.49532E+01 0.23899E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.809          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8993          7.2557     -0.00077937     -0.00077937
v  Velocity[Z]       -1.0008e-014     1.0463e-014    -6.3804e-018    -6.3804e-018
v  ǁVelocityǁ        0.00083515          10.451          5.2546          5.2546
v  Pressure               -50.157          17.382          -10.07          -10.07
v  nu_tilda           4.3452e-007       0.0042695       0.0012677       0.0012677
v  TempC                       21          73.067          21.798          21.798
v  TurbVisc           3.1366e-014        0.005032       0.0014869       0.0014869
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1265:        0.22910E+01

===============================================================


 INSTANT    0.126600000E+04   TIME STEP NUMBER            1266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10106E-01 0.89538E+00
   Friction velocity        uk    :  0.10106E-01 0.89538E+00
   Dimensionless distance   yplus :  0.81364E-01 0.72084E+01
   Friction thermal sca.    tstar : -0.14440E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60707E-01 0.53783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84488E-02      33   0.33364E-03   0.24873E+01 0.11116E+03 
c  Velocity[X]                                      0.12052E+01 
c  Velocity[Y]                                      0.12821E+01 
c  Velocity[Z]                                      0.11699E-29 
c  Pressure     0.99317E-07     489   0.93937E-08   0.95134E-01 0.70359E+03 
c  nu_tilda     0.55609E-05      32   0.15963E-04   0.23423E-06 0.13741E+03 
c  TempC        0.34068E+02      27   0.37431E-03   0.53069E+01 0.24522E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.806          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8977          7.2639     -0.00079197     -0.00079197
v  Velocity[Z]       -9.9079e-015     1.0007e-014    -6.3715e-018    -6.3715e-018
v  ǁVelocityǁ        0.00060077          10.451          5.2545          5.2545
v  Pressure               -50.155           17.29         -10.116         -10.116
v  nu_tilda           4.3446e-007       0.0042695       0.0012682       0.0012682
v  TempC                       21          73.067          21.798          21.798
v  TurbVisc           3.1362e-014        0.005032       0.0014876       0.0014876
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1266:        0.21100E+01

===============================================================


 INSTANT    0.126700000E+04   TIME STEP NUMBER            1267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20625E-01 0.89499E+00
   Friction velocity        uk    :  0.20625E-01 0.89499E+00
   Dimensionless distance   yplus :  0.16604E+00 0.72053E+01
   Friction thermal sca.    tstar : -0.14066E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12389E+00 0.53759E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84513E-02      33   0.30482E-03   0.25331E+01 0.11149E+03 
c  Velocity[X]                                      0.12589E+01 
c  Velocity[Y]                                      0.12742E+01 
c  Velocity[Z]                                      0.11239E-29 
c  Pressure     0.13854E-06     280   0.92572E-08   0.13239E+00 0.38314E+03 
c  nu_tilda     0.55628E-05      32   0.61802E-05   0.23450E-06 0.13747E+03 
c  TempC        0.34078E+02      27   0.39274E-03   0.46498E+01 0.21633E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8029          10.451          4.5729          4.5729
v  Velocity[Y]             -2.896          7.2341     -0.00080451     -0.00080451
v  Velocity[Z]       -9.7461e-015     1.0479e-014    -6.3678e-018    -6.3678e-018
v  ǁVelocityǁ         0.0003794          10.451          5.2544          5.2544
v  Pressure               -50.118          17.212         -10.115         -10.115
v  nu_tilda           4.3453e-007       0.0042695       0.0012688       0.0012688
v  TempC                       21          73.067          21.799          21.799
v  TurbVisc           3.1345e-014        0.005032       0.0014883       0.0014883
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1267:        0.16380E+01

===============================================================


 INSTANT    0.126800000E+04   TIME STEP NUMBER            1268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19725E-01 0.89401E+00
   Friction velocity        uk    :  0.19725E-01 0.89401E+00
   Dimensionless distance   yplus :  0.15880E+00 0.71974E+01
   Friction thermal sca.    tstar : -0.16552E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11848E+00 0.53701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84538E-02      33   0.31864E-03   0.25023E+01 0.11140E+03 
c  Velocity[X]                                      0.12319E+01 
c  Velocity[Y]                                      0.12704E+01 
c  Velocity[Z]                                      0.13384E-29 
c  Pressure     0.10735E-06     329   0.99557E-08   0.10288E+00 0.26829E+03 
c  nu_tilda     0.55646E-05      32   0.15969E-04   0.23478E-06 0.13753E+03 
c  TempC        0.34088E+02      27   0.32775E-03   0.45704E+01 0.21478E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7998          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8944          7.2563     -0.00081717     -0.00081717
v  Velocity[Z]       -9.5474e-015     1.0036e-014    -6.3642e-018    -6.3642e-018
v  ǁVelocityǁ         0.0001818          10.451          5.2543          5.2543
v  Pressure                -50.12          17.299         -10.121         -10.121
v  nu_tilda           4.3458e-007       0.0042695       0.0012694       0.0012694
v  TempC                       21          73.067          21.799          21.799
v  TurbVisc           3.1366e-014        0.005032        0.001489        0.001489
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1268:        0.17460E+01

===============================================================


 INSTANT    0.126900000E+04   TIME STEP NUMBER            1269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40709E-02 0.89500E+00
   Friction velocity        uk    :  0.40709E-02 0.89500E+00
   Dimensionless distance   yplus :  0.32773E-01 0.72053E+01
   Friction thermal sca.    tstar : -0.14521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24453E-01 0.53760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84563E-02      33   0.31295E-03   0.25305E+01 0.11171E+03 
c  Velocity[X]                                      0.12362E+01 
c  Velocity[Y]                                      0.12944E+01 
c  Velocity[Z]                                      0.13726E-29 
c  Pressure     0.11742E-06     410   0.94486E-08   0.11336E+00 0.50635E+03 
c  nu_tilda     0.55665E-05      32   0.61661E-05   0.23504E-06 0.13760E+03 
c  TempC        0.34098E+02      26   0.43567E-03   0.49583E+01 0.24232E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7967          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8927          7.2373     -0.00082964     -0.00082964
v  Velocity[Z]       -9.3657e-015     1.0446e-014    -6.3573e-018    -6.3573e-018
v  ǁVelocityǁ        2.397e-005          10.451          5.2542          5.2542
v  Pressure               -50.077          17.186          -10.13          -10.13
v  nu_tilda           4.3464e-007       0.0042695         0.00127         0.00127
v  TempC                       21          73.067            21.8            21.8
v  TurbVisc           3.1378e-014        0.005032       0.0014896       0.0014896
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1269:        0.19140E+01

===============================================================


 INSTANT    0.127000000E+04   TIME STEP NUMBER            1270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62095E-02 0.89438E+00
   Friction velocity        uk    :  0.62095E-02 0.89438E+00
   Dimensionless distance   yplus :  0.49991E-01 0.72004E+01
   Friction thermal sca.    tstar : -0.18208E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37299E-01 0.53723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84588E-02      33   0.27413E-03   0.25341E+01 0.11178E+03 
c  Velocity[X]                                      0.12508E+01 
c  Velocity[Y]                                      0.12833E+01 
c  Velocity[Z]                                      0.11040E-29 
c  Pressure     0.11913E-06     373   0.88900E-08   0.11287E+00 0.20857E+03 
c  nu_tilda     0.55683E-05      32   0.15978E-04   0.23533E-06 0.13766E+03 
c  TempC        0.34108E+02      26   0.35191E-03   0.62245E+01 0.28160E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7938          10.451          4.5729          4.5729
v  Velocity[Y]             -2.891          7.2578     -0.00084188     -0.00084188
v  Velocity[Z]       -9.1009e-015     9.9941e-015     -6.351e-018     -6.351e-018
v  ǁVelocityǁ        0.00019546          10.451          5.2541          5.2541
v  Pressure               -50.079          17.239         -10.142         -10.142
v  nu_tilda           4.3472e-007       0.0042695       0.0012705       0.0012705
v  TempC                       21          73.067            21.8            21.8
v  TurbVisc           3.1396e-014        0.005032       0.0014903       0.0014903
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1270:        0.20550E+01

===============================================================


 INSTANT    0.127100000E+04   TIME STEP NUMBER            1271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12209E-01 0.89593E+00
   Friction velocity        uk    :  0.12209E-01 0.89593E+00
   Dimensionless distance   yplus :  0.98289E-01 0.72128E+01
   Friction thermal sca.    tstar : -0.15553E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73335E-01 0.53816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84612E-02      33   0.33023E-03   0.25409E+01 0.11197E+03 
c  Velocity[X]                                      0.12585E+01 
c  Velocity[Y]                                      0.12824E+01 
c  Velocity[Z]                                      0.12922E-29 
c  Pressure     0.12186E-06     426   0.96795E-08   0.11720E+00 0.41294E+03 
c  nu_tilda     0.55702E-05      32   0.61516E-05   0.23560E-06 0.13773E+03 
c  TempC        0.34118E+02      26   0.36375E-03   0.60493E+01 0.24529E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7908          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8893           7.272     -0.00085464     -0.00085464
v  Velocity[Z]       -8.9588e-015     1.0463e-014    -6.3472e-018    -6.3472e-018
v  ǁVelocityǁ        0.00040035          10.451          5.2539          5.2539
v  Pressure               -50.045           17.27         -10.125         -10.125
v  nu_tilda            4.347e-007       0.0042695       0.0012711       0.0012711
v  TempC                       21          73.067            21.8            21.8
v  TurbVisc           3.1421e-014        0.005032        0.001491        0.001491
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1271:        0.22980E+01

===============================================================


 INSTANT    0.127200000E+04   TIME STEP NUMBER            1272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14242E-01 0.89568E+00
   Friction velocity        uk    :  0.14242E-01 0.89568E+00
   Dimensionless distance   yplus :  0.11466E+00 0.72108E+01
   Friction thermal sca.    tstar : -0.15285E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85550E-01 0.53801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84637E-02      33   0.30293E-03   0.25522E+01 0.11217E+03 
c  Velocity[X]                                      0.12498E+01 
c  Velocity[Y]                                      0.13023E+01 
c  Velocity[Z]                                      0.12849E-29 
c  Pressure     0.12384E-06     473   0.94651E-08   0.11929E+00 0.91886E+03 
c  nu_tilda     0.55721E-05      32   0.15976E-04   0.23590E-06 0.13779E+03 
c  TempC        0.34129E+02      26   0.40247E-03   0.51768E+01 0.24404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7878          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8877          7.2433     -0.00086691     -0.00086691
v  Velocity[Z]       -8.8245e-015      1.002e-014    -6.3373e-018    -6.3373e-018
v  ǁVelocityǁ        0.00057329          10.451          5.2538          5.2538
v  Pressure               -50.038           17.12         -10.179         -10.179
v  nu_tilda           4.3473e-007       0.0042695       0.0012716       0.0012716
v  TempC                       21          73.067          21.801          21.801
v  TurbVisc           3.1415e-014        0.005032       0.0014917       0.0014917
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1272:        0.26500E+01

===============================================================


 INSTANT    0.127300000E+04   TIME STEP NUMBER            1273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76873E-02 0.89419E+00
   Friction velocity        uk    :  0.76873E-02 0.89419E+00
   Dimensionless distance   yplus :  0.61888E-01 0.71988E+01
   Friction thermal sca.    tstar : -0.16441E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46175E-01 0.53711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84662E-02      33   0.30309E-03   0.25252E+01 0.11201E+03 
c  Velocity[X]                                      0.12329E+01 
c  Velocity[Y]                                      0.12924E+01 
c  Velocity[Z]                                      0.10630E-29 
c  Pressure     0.10966E-06     473   0.98710E-08   0.10342E+00 0.68809E+03 
c  nu_tilda     0.55739E-05      32   0.61416E-05   0.23617E-06 0.13786E+03 
c  TempC        0.34139E+02      26   0.30359E-03   0.51956E+01 0.24299E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7847          10.451          4.5729          4.5729
v  Velocity[Y]             -2.886          7.2619      -0.0008792      -0.0008792
v  Velocity[Z]       -8.6826e-015     1.0428e-014    -6.3322e-018    -6.3322e-018
v  ǁVelocityǁ        0.00074556          10.451          5.2537          5.2537
v  Pressure               -50.004          17.217         -10.145         -10.145
v  nu_tilda            4.348e-007       0.0042695       0.0012722       0.0012722
v  TempC                       21          73.067          21.801          21.801
v  TurbVisc           3.1423e-014        0.005032       0.0014923       0.0014923
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1273:        0.25310E+01

===============================================================


 INSTANT    0.127400000E+04   TIME STEP NUMBER            1274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13677E-01 0.89554E+00
   Friction velocity        uk    :  0.13677E-01 0.89554E+00
   Dimensionless distance   yplus :  0.11011E+00 0.72097E+01
   Friction thermal sca.    tstar : -0.16346E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82154E-01 0.53793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84687E-02      33   0.33313E-03   0.25496E+01 0.11227E+03 
c  Velocity[X]                                      0.12601E+01 
c  Velocity[Y]                                      0.12895E+01 
c  Velocity[Z]                                      0.13764E-29 
c  Pressure     0.11481E-06     473   0.92906E-08   0.11169E+00 0.61644E+03 
c  nu_tilda     0.55758E-05      32   0.15988E-04   0.23646E-06 0.13793E+03 
c  TempC        0.34149E+02      26   0.46086E-03   0.48371E+01 0.23932E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7816          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8844          7.2413     -0.00089152     -0.00089152
v  Velocity[Z]       -8.4967e-015     9.9775e-015     -6.328e-018     -6.328e-018
v  ǁVelocityǁ        0.00087682          10.451          5.2536          5.2536
v  Pressure               -50.002          17.126         -10.183         -10.183
v  nu_tilda            4.348e-007       0.0042695       0.0012728       0.0012728
v  TempC                       21          73.067          21.801          21.801
v  TurbVisc           3.1443e-014        0.005032        0.001493        0.001493
v  total_pressure     1.0127e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1274:        0.21530E+01

===============================================================


 INSTANT    0.127500000E+04   TIME STEP NUMBER            1275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11125E-01 0.89464E+00
   Friction velocity        uk    :  0.11125E-01 0.89464E+00
   Dimensionless distance   yplus :  0.89564E-01 0.72025E+01
   Friction thermal sca.    tstar : -0.17104E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66825E-01 0.53739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84711E-02      33   0.31358E-03   0.25559E+01 0.11246E+03 
c  Velocity[X]                                      0.12428E+01 
c  Velocity[Y]                                      0.13132E+01 
c  Velocity[Z]                                      0.16706E-29 
c  Pressure     0.11370E-06     456   0.98808E-08   0.10802E+00 0.56011E+03 
c  nu_tilda     0.55777E-05      32   0.61241E-05   0.23673E-06 0.13799E+03 
c  TempC        0.34159E+02      26   0.34190E-03   0.73206E+01 0.30246E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7784          10.451          4.5729          4.5729
v  Velocity[Y]            -2.8827          7.2676     -0.00090391     -0.00090391
v  Velocity[Z]       -8.3168e-015     1.0444e-014    -6.3192e-018    -6.3192e-018
v  ǁVelocityǁ        0.00047853          10.451          5.2535          5.2535
v  Pressure               -49.965           17.21         -10.158         -10.158
v  nu_tilda           4.3476e-007       0.0042695       0.0012734       0.0012734
v  TempC                       21          73.067          21.802          21.802
v  TurbVisc           3.1444e-014        0.005032       0.0014937       0.0014937
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1275:        0.21200E+01

===============================================================


 INSTANT    0.127600000E+04   TIME STEP NUMBER            1276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77073E-02 0.89592E+00
   Friction velocity        uk    :  0.77073E-02 0.89592E+00
   Dimensionless distance   yplus :  0.62049E-01 0.72128E+01
   Friction thermal sca.    tstar : -0.15827E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46296E-01 0.53816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84736E-02      33   0.33225E-03   0.25362E+01 0.11236E+03 
c  Velocity[X]                                      0.12348E+01 
c  Velocity[Y]                                      0.13014E+01 
c  Velocity[Z]                                      0.12267E-29 
c  Pressure     0.12242E-06     442   0.97399E-08   0.11504E+00 0.37498E+03 
c  nu_tilda     0.55795E-05      32   0.15985E-04   0.23701E-06 0.13806E+03 
c  TempC        0.34169E+02      26   0.38378E-03   0.46340E+01 0.22937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7755          10.451          4.5729          4.5729
v  Velocity[Y]             -2.881          7.2709     -0.00091592     -0.00091592
v  Velocity[Z]       -8.1194e-015     1.0003e-014    -6.3115e-018    -6.3115e-018
v  ǁVelocityǁ         0.0010411          10.451          5.2533          5.2533
v  Pressure               -49.964          17.177         -10.184         -10.184
v  nu_tilda           4.3473e-007       0.0042695       0.0012739       0.0012739
v  TempC                       21          73.067          21.802          21.802
v  TurbVisc            3.143e-014        0.005032       0.0014944       0.0014944
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1276:        0.19860E+01

===============================================================


 INSTANT    0.127700000E+04   TIME STEP NUMBER            1277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11371E-01 0.89558E+00
   Friction velocity        uk    :  0.11371E-01 0.89558E+00
   Dimensionless distance   yplus :  0.91548E-01 0.72100E+01
   Friction thermal sca.    tstar : -0.15173E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68305E-01 0.53795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84760E-02      33   0.32121E-03   0.25854E+01 0.11281E+03 
c  Velocity[X]                                      0.12836E+01 
c  Velocity[Y]                                      0.13018E+01 
c  Velocity[Z]                                      0.12141E-29 
c  Pressure     0.12621E-06     346   0.97503E-08   0.12246E+00 0.37244E+03 
c  nu_tilda     0.55814E-05      32   0.61194E-05   0.23729E-06 0.13812E+03 
c  TempC        0.34179E+02      27   0.38360E-03   0.54048E+01 0.24840E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7726           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8794          7.2478     -0.00092823     -0.00092823
v  Velocity[Z]       -7.9751e-015     1.0409e-014     -6.307e-018     -6.307e-018
v  ǁVelocityǁ         0.0012962          10.451          5.2532          5.2532
v  Pressure               -49.927          17.097         -10.187         -10.187
v  nu_tilda           4.3483e-007       0.0042695       0.0012745       0.0012745
v  TempC                       21          73.067          21.802          21.802
v  TurbVisc           3.1423e-014        0.005032        0.001495        0.001495
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1277:        0.17660E+01

===============================================================


 INSTANT    0.127800000E+04   TIME STEP NUMBER            1278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66695E-02 0.89441E+00
   Friction velocity        uk    :  0.66695E-02 0.89441E+00
   Dimensionless distance   yplus :  0.53694E-01 0.72006E+01
   Friction thermal sca.    tstar : -0.19774E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40062E-01 0.53725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84785E-02      33   0.30552E-03   0.25648E+01 0.11284E+03 
c  Velocity[X]                                      0.12434E+01 
c  Velocity[Y]                                      0.13214E+01 
c  Velocity[Z]                                      0.11213E-29 
c  Pressure     0.10590E-06     393   0.90971E-08   0.10074E+00 0.24225E+03 
c  nu_tilda     0.55833E-05      32   0.15989E-04   0.23758E-06 0.13819E+03 
c  TempC        0.34189E+02      27   0.39911E-03   0.49670E+01 0.24717E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7695           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8778          7.2667     -0.00094028     -0.00094028
v  Velocity[Z]       -7.8045e-015     9.9582e-015    -6.2973e-018    -6.2973e-018
v  ǁVelocityǁ         0.0012778          10.451          5.2531          5.2531
v  Pressure               -49.923          17.151         -10.201         -10.201
v  nu_tilda           4.3486e-007       0.0042695       0.0012751       0.0012751
v  TempC                       21          73.067          21.803          21.803
v  TurbVisc           3.1451e-014        0.005032       0.0014957       0.0014957
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1278:        0.18930E+01

===============================================================


 INSTANT    0.127900000E+04   TIME STEP NUMBER            1279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76645E-02 0.89535E+00
   Friction velocity        uk    :  0.76645E-02 0.89535E+00
   Dimensionless distance   yplus :  0.61705E-01 0.72082E+01
   Friction thermal sca.    tstar : -0.15881E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46039E-01 0.53781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84810E-02      33   0.31974E-03   0.25615E+01 0.11284E+03 
c  Velocity[X]                                      0.12492E+01 
c  Velocity[Y]                                      0.13124E+01 
c  Velocity[Z]                                      0.13305E-29 
c  Pressure     0.11682E-06     392   0.91782E-08   0.11148E+00 0.40606E+03 
c  nu_tilda     0.55852E-05      32   0.61067E-05   0.23786E-06 0.13826E+03 
c  TempC        0.34199E+02      26   0.37482E-03   0.64300E+01 0.26565E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7664           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8761           7.243     -0.00095224     -0.00095224
v  Velocity[Z]       -7.6435e-015     1.0422e-014    -6.2924e-018    -6.2924e-018
v  ǁVelocityǁ         0.0011675          10.451           5.253           5.253
v  Pressure               -49.887          17.053         -10.206         -10.206
v  nu_tilda           4.3489e-007       0.0042695       0.0012757       0.0012757
v  TempC                       21          73.066          21.803          21.803
v  TurbVisc            3.146e-014        0.005032       0.0014964       0.0014964
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1279:        0.18980E+01

===============================================================


 INSTANT    0.128000000E+04   TIME STEP NUMBER            1280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16732E-01 0.89481E+00
   Friction velocity        uk    :  0.16732E-01 0.89481E+00
   Dimensionless distance   yplus :  0.13470E+00 0.72038E+01
   Friction thermal sca.    tstar : -0.19237E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10050E+00 0.53749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84834E-02      33   0.32425E-03   0.25805E+01 0.11311E+03 
c  Velocity[X]                                      0.12686E+01 
c  Velocity[Y]                                      0.13119E+01 
c  Velocity[Z]                                      0.11750E-29 
c  Pressure     0.10931E-06     314   0.99878E-08   0.10385E+00 0.25416E+03 
c  nu_tilda     0.55870E-05      32   0.16001E-04   0.23816E-06 0.13832E+03 
c  TempC        0.34209E+02      26   0.37002E-03   0.55633E+01 0.24637E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7633           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8745          7.2687     -0.00096426     -0.00096426
v  Velocity[Z]        -7.507e-015     9.9834e-015    -6.2862e-018    -6.2862e-018
v  ǁVelocityǁ         0.0011149           10.45          5.2528          5.2528
v  Pressure               -49.888          17.133         -10.213         -10.213
v  nu_tilda           4.3495e-007       0.0042695       0.0012762       0.0012762
v  TempC                       21          73.066          21.803          21.803
v  TurbVisc           3.1469e-014        0.005032       0.0014971       0.0014971
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1280:        0.17000E+01

===============================================================


 INSTANT    0.128100000E+04   TIME STEP NUMBER            1281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16758E-01 0.89606E+00
   Friction velocity        uk    :  0.16758E-01 0.89606E+00
   Dimensionless distance   yplus :  0.13492E+00 0.72139E+01
   Friction thermal sca.    tstar : -0.16184E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10066E+00 0.53824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84859E-02      33   0.31170E-03   0.25632E+01 0.11313E+03 
c  Velocity[X]                                      0.12301E+01 
c  Velocity[Y]                                      0.13332E+01 
c  Velocity[Z]                                      0.12416E-29 
c  Pressure     0.10126E-06     424   0.97460E-08   0.96321E-01 0.35838E+03 
c  nu_tilda     0.55889E-05      32   0.61013E-05   0.23843E-06 0.13839E+03 
c  TempC        0.34219E+02      26   0.42587E-03   0.45668E+01 0.23085E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7601           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8728          7.2801     -0.00097614     -0.00097614
v  Velocity[Z]       -7.3722e-015     1.0387e-014    -6.2776e-018    -6.2776e-018
v  ǁVelocityǁ        0.00051984           10.45          5.2527          5.2527
v  Pressure               -49.851          17.147         -10.201         -10.201
v  nu_tilda           4.3495e-007       0.0042695       0.0012768       0.0012768
v  TempC                       21          73.067          21.804          21.804
v  TurbVisc           3.1486e-014        0.005032       0.0014977       0.0014977
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1281:        0.19600E+01

===============================================================


 INSTANT    0.128200000E+04   TIME STEP NUMBER            1282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80353E-02 0.89562E+00
   Friction velocity        uk    :  0.80353E-02 0.89562E+00
   Dimensionless distance   yplus :  0.64690E-01 0.72103E+01
   Friction thermal sca.    tstar : -0.16749E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48266E-01 0.53797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84883E-02      33   0.28907E-03   0.25827E+01 0.11329E+03 
c  Velocity[X]                                      0.12594E+01 
c  Velocity[Y]                                      0.13233E+01 
c  Velocity[Z]                                      0.15405E-29 
c  Pressure     0.10963E-06     504   0.94105E-08   0.10535E+00 0.96912E+03 
c  nu_tilda     0.55908E-05      32   0.15995E-04   0.23872E-06 0.13846E+03 
c  TempC        0.34229E+02      26   0.39099E-03   0.48057E+01 0.23754E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7572           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8712          7.2472     -0.00098799     -0.00098799
v  Velocity[Z]       -7.2669e-015     9.9393e-015     -6.273e-018     -6.273e-018
v  ǁVelocityǁ        0.00096258           10.45          5.2526          5.2526
v  Pressure               -49.849          16.968         -10.257         -10.257
v  nu_tilda             4.35e-007       0.0042695       0.0012773       0.0012773
v  TempC                       21          73.066          21.804          21.804
v  TurbVisc           3.1486e-014        0.005032       0.0014984       0.0014984
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1282:        0.21490E+01

===============================================================


 INSTANT    0.128300000E+04   TIME STEP NUMBER            1283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11522E-01 0.89435E+00
   Friction velocity        uk    :  0.11522E-01 0.89435E+00
   Dimensionless distance   yplus :  0.92761E-01 0.72001E+01
   Friction thermal sca.    tstar : -0.21893E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69210E-01 0.53721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84907E-02      33   0.35038E-03   0.25610E+01 0.11321E+03 
c  Velocity[X]                                      0.12408E+01 
c  Velocity[Y]                                      0.13202E+01 
c  Velocity[Z]                                      0.99502E-30 
c  Pressure     0.97326E-07     488   0.90137E-08   0.93032E-01 0.10233E+04 
c  nu_tilda     0.55927E-05      32   0.60811E-05   0.23900E-06 0.13852E+03 
c  TempC        0.34239E+02      26   0.32872E-03   0.40416E+01 0.21289E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7542           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8695            7.27     -0.00099964     -0.00099964
v  Velocity[Z]       -7.1294e-015     1.0401e-014    -6.2685e-018    -6.2685e-018
v  ǁVelocityǁ        0.00092593           10.45          5.2524          5.2524
v  Pressure                -49.81          17.142         -10.204         -10.204
v  nu_tilda           4.3503e-007       0.0042695       0.0012779       0.0012779
v  TempC                       21          73.066          21.804          21.804
v  TurbVisc           3.1501e-014        0.005032       0.0014991       0.0014991
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1283:        0.21050E+01

===============================================================


 INSTANT    0.128400000E+04   TIME STEP NUMBER            1284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19231E-01 0.89558E+00
   Friction velocity        uk    :  0.19231E-01 0.89558E+00
   Dimensionless distance   yplus :  0.15482E+00 0.72101E+01
   Friction thermal sca.    tstar : -0.20178E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11551E+00 0.53795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84932E-02      33   0.35497E-03   0.26295E+01 0.11389E+03 
c  Velocity[X]                                      0.12856E+01 
c  Velocity[Y]                                      0.13440E+01 
c  Velocity[Z]                                      0.13319E-29 
c  Pressure     0.13676E-06     474   0.99464E-08   0.13075E+00 0.11661E+04 
c  nu_tilda     0.55946E-05      32   0.16007E-04   0.23930E-06 0.13859E+03 
c  TempC        0.34249E+02      27   0.29373E-03   0.36741E+01 0.19179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7512           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8679           7.249      -0.0010112      -0.0010112
v  Velocity[Z]       -6.9928e-015     9.9641e-015    -6.2605e-018    -6.2605e-018
v  ǁVelocityǁ        0.00087279           10.45          5.2523          5.2523
v  Pressure               -49.808          16.943         -10.273         -10.273
v  nu_tilda           4.3512e-007       0.0042695       0.0012785       0.0012785
v  TempC                       21          73.066          21.805          21.805
v  TurbVisc           3.1511e-014        0.005032       0.0014997       0.0014997
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1284:        0.21830E+01

===============================================================


 INSTANT    0.128500000E+04   TIME STEP NUMBER            1285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36737E-02 0.89495E+00
   Friction velocity        uk    :  0.36737E-02 0.89495E+00
   Dimensionless distance   yplus :  0.29576E-01 0.72050E+01
   Friction thermal sca.    tstar : -0.19594E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22067E-01 0.53757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84956E-02      33   0.23348E-03   0.26314E+01 0.11393E+03 
c  Velocity[X]                                      0.12965E+01 
c  Velocity[Y]                                      0.13349E+01 
c  Velocity[Z]                                      0.12508E-29 
c  Pressure     0.12853E-06     458   0.96569E-08   0.12050E+00 0.89904E+03 
c  nu_tilda     0.55964E-05      32   0.60612E-05   0.23957E-06 0.13866E+03 
c  TempC        0.34259E+02      26   0.42711E-03   0.37688E+01 0.20419E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7481           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8662          7.2719      -0.0010229      -0.0010229
v  Velocity[Z]       -6.9287e-015     1.0366e-014     -6.254e-018     -6.254e-018
v  ǁVelocityǁ        0.00084122           10.45          5.2522          5.2522
v  Pressure               -49.771          17.088         -10.226         -10.226
v  nu_tilda           4.3516e-007       0.0042695       0.0012791       0.0012791
v  TempC                       21          73.066          21.805          21.805
v  TurbVisc           3.1536e-014        0.005032       0.0015004       0.0015004
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1285:        0.21770E+01

===============================================================


 INSTANT    0.128600000E+04   TIME STEP NUMBER            1286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17915E-01 0.89665E+00
   Friction velocity        uk    :  0.17915E-01 0.89665E+00
   Dimensionless distance   yplus :  0.14423E+00 0.72186E+01
   Friction thermal sca.    tstar : -0.19439E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10761E+00 0.53859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84981E-02      33   0.31856E-03   0.25745E+01 0.11360E+03 
c  Velocity[X]                                      0.12447E+01 
c  Velocity[Y]                                      0.13297E+01 
c  Velocity[Z]                                      0.10856E-29 
c  Pressure     0.10478E-06     457   0.97015E-08   0.10017E+00 0.46212E+03 
c  nu_tilda     0.55983E-05      32   0.16005E-04   0.23987E-06 0.13873E+03 
c  TempC        0.34269E+02      26   0.39138E-03   0.76151E+01 0.30111E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.745           10.45          4.5729          4.5729
v  Velocity[Y]            -2.8646          7.2811      -0.0010343      -0.0010343
v  Velocity[Z]       -6.9287e-015     9.9217e-015    -6.2483e-018    -6.2483e-018
v  ǁVelocityǁ        0.00082627           10.45           5.252           5.252
v  Pressure               -49.773          17.044         -10.259         -10.259
v  nu_tilda            4.351e-007       0.0042695       0.0012796       0.0012796
v  TempC                       21          73.066          21.805          21.805
v  TurbVisc           3.1547e-014        0.005032       0.0015011       0.0015011
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1286:        0.20330E+01

===============================================================


 INSTANT    0.128700000E+04   TIME STEP NUMBER            1287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74455E-02 0.89631E+00
   Friction velocity        uk    :  0.74455E-02 0.89631E+00
   Dimensionless distance   yplus :  0.59942E-01 0.72159E+01
   Friction thermal sca.    tstar : -0.17219E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44723E-01 0.53838E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85005E-02      33   0.31985E-03   0.26161E+01 0.11405E+03 
c  Velocity[X]                                      0.12616E+01 
c  Velocity[Y]                                      0.13545E+01 
c  Velocity[Z]                                      0.13354E-29 
c  Pressure     0.12174E-06     362   0.95887E-08   0.11709E+00 0.42474E+03 
c  nu_tilda     0.56002E-05      32   0.60631E-05   0.24016E-06 0.13879E+03 
c  TempC        0.34279E+02      27   0.36587E-03   0.58738E+01 0.26145E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7418          10.449          4.5729          4.5729
v  Velocity[Y]             -2.863          7.2564       -0.001046       -0.001046
v  Velocity[Z]       -6.9287e-015     1.0381e-014    -6.2396e-018    -6.2396e-018
v  ǁVelocityǁ        0.00028715           10.45          5.2519          5.2519
v  Pressure               -49.732           16.96         -10.266         -10.266
v  nu_tilda           4.3507e-007       0.0042695       0.0012802       0.0012802
v  TempC                       21          73.066          21.806          21.806
v  TurbVisc           3.1529e-014        0.005032       0.0015018       0.0015018
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1287:        0.18140E+01

===============================================================


 INSTANT    0.128800000E+04   TIME STEP NUMBER            1288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59360E-02 0.89498E+00
   Friction velocity        uk    :  0.59360E-02 0.89498E+00
   Dimensionless distance   yplus :  0.47789E-01 0.72052E+01
   Friction thermal sca.    tstar : -0.20043E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35656E-01 0.53759E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85030E-02      33   0.31911E-03   0.26155E+01 0.11415E+03 
c  Velocity[X]                                      0.12712E+01 
c  Velocity[Y]                                      0.13443E+01 
c  Velocity[Z]                                      0.11618E-29 
c  Pressure     0.11859E-06     378   0.94121E-08   0.11106E+00 0.19949E+03 
c  nu_tilda     0.56021E-05      32   0.16010E-04   0.24046E-06 0.13886E+03 
c  TempC        0.34289E+02      26   0.39468E-03   0.48355E+01 0.23515E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7388          10.449          4.5729          4.5729
v  Velocity[Y]            -2.8614          7.2773      -0.0010571      -0.0010571
v  Velocity[Z]       -6.9287e-015     9.9455e-015    -6.2335e-018    -6.2335e-018
v  ǁVelocityǁ        0.00079569           10.45          5.2517          5.2517
v  Pressure               -49.734          16.998         -10.278         -10.278
v  nu_tilda           4.3509e-007       0.0042695       0.0012807       0.0012807
v  TempC                       21          73.066          21.806          21.806
v  TurbVisc           3.1521e-014        0.005032       0.0015024       0.0015024
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1288:        0.18520E+01

===============================================================


 INSTANT    0.128900000E+04   TIME STEP NUMBER            1289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12669E-01 0.89621E+00
   Friction velocity        uk    :  0.12669E-01 0.89621E+00
   Dimensionless distance   yplus :  0.10199E+00 0.72151E+01
   Friction thermal sca.    tstar : -0.18116E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76096E-01 0.53833E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85054E-02      33   0.33247E-03   0.26216E+01 0.11418E+03 
c  Velocity[X]                                      0.12806E+01 
c  Velocity[Y]                                      0.13410E+01 
c  Velocity[Z]                                      0.13094E-29 
c  Pressure     0.12628E-06     393   0.94422E-08   0.11966E+00 0.37475E+03 
c  nu_tilda     0.56040E-05      32   0.60381E-05   0.24074E-06 0.13893E+03 
c  TempC        0.34299E+02      26   0.32595E-03   0.56150E+01 0.24933E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7359          10.449          4.5729          4.5729
v  Velocity[Y]            -2.8597          7.2538      -0.0010684      -0.0010684
v  Velocity[Z]       -6.9287e-015     1.0344e-014    -6.2294e-018    -6.2294e-018
v  ǁVelocityǁ        0.00080027          10.449          5.2516          5.2516
v  Pressure               -49.693          16.952          -10.27          -10.27
v  nu_tilda           4.3514e-007       0.0042695       0.0012813       0.0012813
v  TempC                       21          73.066          21.806          21.806
v  TurbVisc           3.1528e-014        0.005032       0.0015031       0.0015031
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1289:        0.19010E+01

===============================================================


 INSTANT    0.129000000E+04   TIME STEP NUMBER            1290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14520E-01 0.89555E+00
   Friction velocity        uk    :  0.14520E-01 0.89555E+00
   Dimensionless distance   yplus :  0.11690E+00 0.72098E+01
   Friction thermal sca.    tstar : -0.24003E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87217E-01 0.53793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85078E-02      33   0.22455E-03   0.26367E+01 0.11449E+03 
c  Velocity[X]                                      0.12710E+01 
c  Velocity[Y]                                      0.13657E+01 
c  Velocity[Z]                                      0.99830E-30 
c  Pressure     0.11246E-06     425   0.93013E-08   0.10665E+00 0.36642E+03 
c  nu_tilda     0.56059E-05      32   0.16018E-04   0.24104E-06 0.13900E+03 
c  TempC        0.34309E+02      27   0.40034E-03   0.41255E+01 0.21553E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7328          10.449          4.5729          4.5729
v  Velocity[Y]            -2.8581          7.2773      -0.0010797      -0.0010797
v  Velocity[Z]       -6.9287e-015     9.8985e-015    -6.2214e-018    -6.2214e-018
v  ǁVelocityǁ        0.00079493          10.449          5.2515          5.2515
v  Pressure               -49.696          16.964         -10.299         -10.299
v  nu_tilda           4.3516e-007       0.0042695       0.0012819       0.0012819
v  TempC                       21          73.066          21.807          21.807
v  TurbVisc           3.1541e-014        0.005032       0.0015038       0.0015038
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1290:        0.19530E+01

===============================================================


 INSTANT    0.129100000E+04   TIME STEP NUMBER            1291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16754E-01 0.89693E+00
   Friction velocity        uk    :  0.16754E-01 0.89693E+00
   Dimensionless distance   yplus :  0.13488E+00 0.72209E+01
   Friction thermal sca.    tstar : -0.18427E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10064E+00 0.53876E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85103E-02      33   0.33270E-03   0.26232E+01 0.11447E+03 
c  Velocity[X]                                      0.12677E+01 
c  Velocity[Y]                                      0.13555E+01 
c  Velocity[Z]                                      0.92965E-30 
c  Pressure     0.12243E-06     425   0.96944E-08   0.11476E+00 0.53837E+03 
c  nu_tilda     0.56078E-05      32   0.60363E-05   0.24132E-06 0.13907E+03 
c  TempC        0.34319E+02      27   0.34451E-03   0.40274E+01 0.21999E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7297          10.449          4.5729          4.5729
v  Velocity[Y]            -2.8564          7.2859      -0.0010908      -0.0010908
v  Velocity[Z]       -6.9287e-015     1.0356e-014    -6.2147e-018    -6.2147e-018
v  ǁVelocityǁ         0.0007952          10.449          5.2513          5.2513
v  Pressure               -49.658           17.01         -10.272         -10.272
v  nu_tilda            4.352e-007       0.0042695       0.0012825       0.0012825
v  TempC                       21          73.066          21.807          21.807
v  TurbVisc           3.1548e-014        0.005032       0.0015044       0.0015044
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1291:        0.19700E+01

===============================================================


 INSTANT    0.129200000E+04   TIME STEP NUMBER            1292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12570E-01 0.89671E+00
   Friction velocity        uk    :  0.12570E-01 0.89671E+00
   Dimensionless distance   yplus :  0.10120E+00 0.72192E+01
   Friction thermal sca.    tstar : -0.18201E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75506E-01 0.53863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85127E-02      33   0.33101E-03   0.26732E+01 0.11492E+03 
c  Velocity[X]                                      0.13202E+01 
c  Velocity[Y]                                      0.13531E+01 
c  Velocity[Z]                                      0.14221E-29 
c  Pressure     0.12561E-06     489   0.96593E-08   0.12099E+00 0.93280E+03 
c  nu_tilda     0.56097E-05      32   0.16015E-04   0.24163E-06 0.13914E+03 
c  TempC        0.34328E+02      27   0.39539E-03   0.43142E+01 0.20844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7266          10.449          4.5729          4.5729
v  Velocity[Y]            -2.8548          7.2595      -0.0011019      -0.0011019
v  Velocity[Z]       -6.9287e-015     9.9228e-015    -6.2108e-018    -6.2108e-018
v  ǁVelocityǁ        0.00084092          10.449          5.2512          5.2512
v  Pressure               -49.655          16.844         -10.327         -10.327
v  nu_tilda           4.3532e-007       0.0042695        0.001283        0.001283
v  TempC                       21          73.065          21.807          21.807
v  TurbVisc           3.1558e-014        0.005032       0.0015051       0.0015051
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1292:        0.21260E+01

===============================================================


 INSTANT    0.129300000E+04   TIME STEP NUMBER            1293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25787E-02 0.89549E+00
   Friction velocity        uk    :  0.25787E-02 0.89549E+00
   Dimensionless distance   yplus :  0.20761E-01 0.72093E+01
   Friction thermal sca.    tstar : -0.32530E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15490E-01 0.53789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85151E-02      33   0.30302E-03   0.26444E+01 0.11486E+03 
c  Velocity[X]                                      0.12684E+01 
c  Velocity[Y]                                      0.13760E+01 
c  Velocity[Z]                                      0.12642E-29 
c  Pressure     0.10842E-06     457   0.94457E-08   0.10174E+00 0.80973E+03 
c  nu_tilda     0.56116E-05      32   0.60259E-05   0.24192E-06 0.13920E+03 
c  TempC        0.34338E+02      27   0.31687E-03   0.51018E+01 0.22056E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7234          10.449          4.5729          4.5729
v  Velocity[Y]            -2.8532          7.2809      -0.0011128      -0.0011128
v  Velocity[Z]       -6.9287e-015      1.032e-014    -6.2018e-018    -6.2018e-018
v  ǁVelocityǁ        0.00010223          10.449           5.251           5.251
v  Pressure               -49.618          16.995         -10.288         -10.288
v  nu_tilda           4.3534e-007       0.0042695       0.0012836       0.0012836
v  TempC                       21          73.066          21.808          21.808
v  TurbVisc           3.1593e-014        0.005032       0.0015058       0.0015058
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1293:        0.20100E+01

===============================================================


 INSTANT    0.129400000E+04   TIME STEP NUMBER            1294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13917E-02 0.89641E+00
   Friction velocity        uk    :  0.13917E-02 0.89641E+00
   Dimensionless distance   yplus :  0.11204E-01 0.72167E+01
   Friction thermal sca.    tstar : -0.19544E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83593E-02 0.53845E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85175E-02      33   0.31827E-03   0.26379E+01 0.11484E+03 
c  Velocity[X]                                      0.12729E+01 
c  Velocity[Y]                                      0.13650E+01 
c  Velocity[Z]                                      0.11899E-29 
c  Pressure     0.12083E-06     473   0.98418E-08   0.11375E+00 0.97919E+03 
c  nu_tilda     0.56135E-05      32   0.16025E-04   0.24222E-06 0.13928E+03 
c  TempC        0.34348E+02      26   0.40370E-03   0.34412E+01 0.20156E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7204          10.448          4.5729          4.5729
v  Velocity[Y]            -2.8515          7.2549      -0.0011237      -0.0011237
v  Velocity[Z]       -6.9287e-015     9.8787e-015     -6.198e-018     -6.198e-018
v  ǁVelocityǁ        0.00091628          10.449          5.2509          5.2509
v  Pressure               -49.618          16.806         -10.343         -10.343
v  nu_tilda           4.3539e-007       0.0042695       0.0012841       0.0012841
v  TempC                       21          73.065          21.808          21.808
v  TurbVisc           3.1599e-014        0.005032       0.0015064       0.0015064
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1294:        0.20700E+01

===============================================================


 INSTANT    0.129500000E+04   TIME STEP NUMBER            1295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23243E-02 0.89593E+00
   Friction velocity        uk    :  0.23243E-02 0.89593E+00
   Dimensionless distance   yplus :  0.18712E-01 0.72129E+01
   Friction thermal sca.    tstar : -0.26098E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13961E-01 0.53816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85199E-02      33   0.25849E-03   0.26556E+01 0.11506E+03 
c  Velocity[X]                                      0.12913E+01 
c  Velocity[Y]                                      0.13643E+01 
c  Velocity[Z]                                      0.11366E-29 
c  Pressure     0.11516E-06     488   0.98168E-08   0.10886E+00 0.10529E+04 
c  nu_tilda     0.56153E-05      32   0.60010E-05   0.24251E-06 0.13934E+03 
c  TempC        0.34358E+02      26   0.30827E-03   0.51056E+01 0.24440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7175          10.448          4.5729          4.5729
v  Velocity[Y]            -2.8499          7.2835      -0.0011345      -0.0011345
v  Velocity[Z]       -6.9287e-015     1.0333e-014    -6.1929e-018    -6.1929e-018
v  ǁVelocityǁ        0.00096932          10.448          5.2507          5.2507
v  Pressure               -49.577              17         -10.289         -10.289
v  nu_tilda           4.3541e-007       0.0042695       0.0012847       0.0012847
v  TempC                       21          73.065          21.808          21.808
v  TurbVisc           3.1615e-014        0.005032       0.0015071       0.0015071
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1295:        0.23910E+01

===============================================================


 INSTANT    0.129600000E+04   TIME STEP NUMBER            1296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76721E-02 0.89725E+00
   Friction velocity        uk    :  0.76721E-02 0.89725E+00
   Dimensionless distance   yplus :  0.61766E-01 0.72234E+01
   Friction thermal sca.    tstar : -0.19238E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46084E-01 0.53895E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85224E-02      33   0.30409E-03   0.26376E+01 0.11513E+03 
c  Velocity[X]                                      0.12527E+01 
c  Velocity[Y]                                      0.13849E+01 
c  Velocity[Z]                                      0.11949E-29 
c  Pressure     0.10498E-06     473   0.93892E-08   0.98975E-01 0.77790E+03 
c  nu_tilda     0.56172E-05      32   0.16021E-04   0.24282E-06 0.13941E+03 
c  TempC        0.34368E+02      27   0.31620E-03   0.37939E+01 0.20490E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7144          10.448          4.5729          4.5729
v  Velocity[Y]            -2.8482          7.2919      -0.0011451      -0.0011451
v  Velocity[Z]       -6.9287e-015     9.9009e-015    -6.1842e-018    -6.1842e-018
v  ǁVelocityǁ          0.001011          10.448          5.2506          5.2506
v  Pressure                -49.58          16.898         -10.341         -10.341
v  nu_tilda           4.3535e-007       0.0042695       0.0012852       0.0012852
v  TempC                       21          73.066          21.809          21.809
v  TurbVisc           3.1621e-014        0.005032       0.0015078       0.0015078
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1296:        0.22450E+01

===============================================================


 INSTANT    0.129700000E+04   TIME STEP NUMBER            1297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17009E-01 0.89672E+00
   Friction velocity        uk    :  0.17009E-01 0.89672E+00
   Dimensionless distance   yplus :  0.13694E+00 0.72192E+01
   Friction thermal sca.    tstar : -0.18048E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10217E+00 0.53863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85248E-02      33   0.32468E-03   0.26606E+01 0.11528E+03 
c  Velocity[X]                                      0.12852E+01 
c  Velocity[Y]                                      0.13754E+01 
c  Velocity[Z]                                      0.15413E-29 
c  Pressure     0.12280E-06     376   0.90003E-08   0.11543E+00 0.37708E+03 
c  nu_tilda     0.56191E-05      32   0.60015E-05   0.24311E-06 0.13948E+03 
c  TempC        0.34378E+02      26   0.41657E-03   0.36410E+01 0.19456E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7113          10.448          4.5729          4.5729
v  Velocity[Y]            -2.8466          7.2616      -0.0011558      -0.0011558
v  Velocity[Z]       -6.9287e-015     1.0296e-014    -6.1804e-018    -6.1804e-018
v  ǁVelocityǁ         0.0010651          10.448          5.2504          5.2504
v  Pressure               -49.543           16.83         -10.336         -10.336
v  nu_tilda           4.3537e-007       0.0042695       0.0012858       0.0012858
v  TempC                       21          73.066          21.809          21.809
v  TurbVisc           3.1604e-014        0.005032       0.0015084       0.0015084
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1297:        0.18600E+01

===============================================================


 INSTANT    0.129800000E+04   TIME STEP NUMBER            1298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95823E-02 0.89561E+00
   Friction velocity        uk    :  0.95823E-02 0.89561E+00
   Dimensionless distance   yplus :  0.77144E-01 0.72102E+01
   Friction thermal sca.    tstar : -0.25151E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57558E-01 0.53796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85272E-02      33   0.32841E-03   0.26750E+01 0.11555E+03 
c  Velocity[X]                                      0.13013E+01 
c  Velocity[Y]                                      0.13738E+01 
c  Velocity[Z]                                      0.10962E-29 
c  Pressure     0.12238E-06     328   0.95410E-08   0.11548E+00 0.23880E+03 
c  nu_tilda     0.56210E-05      32   0.16028E-04   0.24342E-06 0.13955E+03 
c  TempC        0.34388E+02      27   0.32889E-03   0.44469E+01 0.22530E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7082          10.448          4.5729          4.5729
v  Velocity[Y]             -2.845          7.2839      -0.0011662      -0.0011662
v  Velocity[Z]       -6.9287e-015     9.8575e-015    -6.1753e-018    -6.1753e-018
v  ǁVelocityǁ         0.0011659          10.448          5.2503          5.2503
v  Pressure                -49.54          16.898         -10.342         -10.342
v  nu_tilda           4.3536e-007       0.0042695       0.0012864       0.0012864
v  TempC                       21          73.066           21.81           21.81
v  TurbVisc           3.1608e-014        0.005032       0.0015091       0.0015091
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1298:        0.18140E+01

===============================================================


 INSTANT    0.129900000E+04   TIME STEP NUMBER            1299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13064E-01 0.89683E+00
   Friction velocity        uk    :  0.13064E-01 0.89683E+00
   Dimensionless distance   yplus :  0.10517E+00 0.72201E+01
   Friction thermal sca.    tstar : -0.20123E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78470E-01 0.53870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85296E-02      33   0.31861E-03   0.27021E+01 0.11582E+03 
c  Velocity[X]                                      0.13044E+01 
c  Velocity[Y]                                      0.13977E+01 
c  Velocity[Z]                                      0.13992E-29 
c  Pressure     0.12816E-06     392   0.97647E-08   0.12059E+00 0.46233E+03 
c  nu_tilda     0.56229E-05      32   0.59803E-05   0.24370E-06 0.13962E+03 
c  TempC        0.34398E+02      27   0.34847E-03   0.38097E+01 0.20344E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.705          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8434          7.2578      -0.0011767      -0.0011767
v  Velocity[Z]       -6.9287e-015     1.0309e-014    -6.1668e-018    -6.1668e-018
v  ǁVelocityǁ        0.00038444          10.448          5.2501          5.2501
v  Pressure               -49.501          16.803         -10.353         -10.353
v  nu_tilda           4.3539e-007       0.0042695        0.001287        0.001287
v  TempC                       21          73.065           21.81           21.81
v  TurbVisc           3.1605e-014        0.005032       0.0015098       0.0015098
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1299:        0.20770E+01

===============================================================


 INSTANT    0.130000000E+04   TIME STEP NUMBER            1300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66284E-02 0.89612E+00
   Friction velocity        uk    :  0.66284E-02 0.89612E+00
   Dimensionless distance   yplus :  0.53363E-01 0.72144E+01
   Friction thermal sca.    tstar : -0.23889E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39815E-01 0.53827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85320E-02      33   0.21206E-03   0.26751E+01 0.11569E+03 
c  Velocity[X]                                      0.12875E+01 
c  Velocity[Y]                                      0.13876E+01 
c  Velocity[Z]                                      0.12752E-29 
c  Pressure     0.10597E-06     296   0.96540E-08   0.10035E+00 0.21445E+03 
c  nu_tilda     0.56248E-05      32   0.16035E-04   0.24401E-06 0.13969E+03 
c  TempC        0.34408E+02      27   0.36758E-03   0.37889E+01 0.20386E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.702          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8417          7.2847      -0.0011868      -0.0011868
v  Velocity[Z]       -6.9287e-015     9.8799e-015    -6.1624e-018    -6.1624e-018
v  ǁVelocityǁ         0.0013288          10.448            5.25            5.25
v  Pressure               -49.502          16.857         -10.361         -10.361
v  nu_tilda           4.3544e-007       0.0042695       0.0012875       0.0012875
v  TempC                       21          73.065           21.81           21.81
v  TurbVisc           3.1614e-014        0.005032       0.0015105       0.0015105
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1300:        0.16840E+01

===============================================================


 INSTANT    0.130100000E+04   TIME STEP NUMBER            1301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11522E-01 0.89763E+00
   Friction velocity        uk    :  0.11522E-01 0.89763E+00
   Dimensionless distance   yplus :  0.92759E-01 0.72265E+01
   Friction thermal sca.    tstar : -0.20917E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69209E-01 0.53918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85344E-02      33   0.34982E-03   0.26376E+01 0.11556E+03 
c  Velocity[X]                                      0.12535E+01 
c  Velocity[Y]                                      0.13841E+01 
c  Velocity[Z]                                      0.11882E-29 
c  Pressure     0.11108E-06     457   0.94878E-08   0.10440E+00 0.64874E+03 
c  nu_tilda     0.56268E-05      32   0.59654E-05   0.24430E-06 0.13976E+03 
c  TempC        0.34418E+02      27   0.32957E-03   0.57830E+01 0.23445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6991          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8401          7.2983      -0.0011969      -0.0011969
v  Velocity[Z]       -6.9287e-015     1.0272e-014    -6.1581e-018    -6.1581e-018
v  ǁVelocityǁ         0.0014408          10.447          5.2498          5.2498
v  Pressure               -49.462          16.939         -10.327         -10.327
v  nu_tilda           4.3541e-007       0.0042695       0.0012881       0.0012881
v  TempC                       21          73.065          21.811          21.811
v  TurbVisc           3.1627e-014        0.005032       0.0015111       0.0015111
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1301:        0.20650E+01

===============================================================


 INSTANT    0.130200000E+04   TIME STEP NUMBER            1302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51947E-02 0.89715E+00
   Friction velocity        uk    :  0.51947E-02 0.89715E+00
   Dimensionless distance   yplus :  0.41821E-01 0.72227E+01
   Friction thermal sca.    tstar : -0.19927E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31203E-01 0.53889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85369E-02      33   0.32061E-03   0.27243E+01 0.11631E+03 
c  Velocity[X]                                      0.13135E+01 
c  Velocity[Y]                                      0.14108E+01 
c  Velocity[Z]                                      0.14097E-29 
c  Pressure     0.14203E-06     504   0.92003E-08   0.13295E+00 0.15541E+04 
c  nu_tilda     0.56287E-05      32   0.16028E-04   0.24462E-06 0.13984E+03 
c  TempC        0.34428E+02      26   0.40804E-03   0.54533E+01 0.25001E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.696          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8385          7.2646       -0.001207       -0.001207
v  Velocity[Z]       -6.9287e-015     9.8334e-015    -6.1514e-018    -6.1514e-018
v  ǁVelocityǁ         0.0015099          10.447          5.2496          5.2496
v  Pressure               -49.463          16.654         -10.417         -10.417
v  nu_tilda           4.3549e-007       0.0042695       0.0012886       0.0012886
v  TempC                       21          73.065          21.811          21.811
v  TurbVisc            3.162e-014        0.005032       0.0015118       0.0015118
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1302:        0.21690E+01

===============================================================


 INSTANT    0.130300000E+04   TIME STEP NUMBER            1303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11072E-01 0.89618E+00
   Friction velocity        uk    :  0.11072E-01 0.89618E+00
   Dimensionless distance   yplus :  0.89141E-01 0.72149E+01
   Friction thermal sca.    tstar : -0.30155E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66509E-01 0.53831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85392E-02      33   0.28191E-03   0.26964E+01 0.11620E+03 
c  Velocity[X]                                      0.12945E+01 
c  Velocity[Y]                                      0.14019E+01 
c  Velocity[Z]                                      0.11312E-29 
c  Pressure     0.11567E-06     504   0.95540E-08   0.10882E+00 0.14135E+04 
c  nu_tilda     0.56306E-05      32   0.59600E-05   0.24492E-06 0.13991E+03 
c  TempC        0.34438E+02      26   0.40768E-03   0.56497E+01 0.26419E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6929          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8369          7.2883       -0.001217       -0.001217
v  Velocity[Z]       -6.9287e-015     1.0283e-014    -6.1471e-018    -6.1471e-018
v  ǁVelocityǁ         0.0016097          10.447          5.2495          5.2495
v  Pressure               -49.428          16.918         -10.344         -10.344
v  nu_tilda           4.3557e-007       0.0042695       0.0012892       0.0012892
v  TempC                       21          73.065          21.811          21.811
v  TurbVisc           3.1644e-014        0.005032       0.0015124       0.0015124
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1303:        0.21690E+01

===============================================================


 INSTANT    0.130400000E+04   TIME STEP NUMBER            1304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64194E-02 0.89698E+00
   Friction velocity        uk    :  0.64194E-02 0.89698E+00
   Dimensionless distance   yplus :  0.51681E-01 0.72213E+01
   Friction thermal sca.    tstar : -0.20702E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38560E-01 0.53879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85417E-02      33   0.35353E-03   0.26758E+01 0.11612E+03 
c  Velocity[X]                                      0.12823E+01 
c  Velocity[Y]                                      0.13935E+01 
c  Velocity[Z]                                      0.14792E-29 
c  Pressure     0.11718E-06     490   0.99158E-08   0.11123E+00 0.12062E+04 
c  nu_tilda     0.56325E-05      32   0.16038E-04   0.24523E-06 0.13998E+03 
c  TempC        0.34448E+02      26   0.29665E-03   0.53343E+01 0.24609E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6897          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8352          7.2675      -0.0012266      -0.0012266
v  Velocity[Z]       -6.9287e-015     9.8567e-015    -6.1455e-018    -6.1455e-018
v  ǁVelocityǁ         0.0013148          10.447          5.2493          5.2493
v  Pressure               -49.423          16.693         -10.411         -10.411
v  nu_tilda           4.3569e-007       0.0042695       0.0012897       0.0012897
v  TempC                       21          73.065          21.812          21.812
v  TurbVisc           3.1667e-014        0.005032       0.0015131       0.0015131
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1304:        0.21080E+01

===============================================================


 INSTANT    0.130500000E+04   TIME STEP NUMBER            1305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69654E-02 0.89627E+00
   Friction velocity        uk    :  0.69654E-02 0.89627E+00
   Dimensionless distance   yplus :  0.56076E-01 0.72156E+01
   Friction thermal sca.    tstar : -0.29364E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41839E-01 0.53836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85440E-02      33   0.32683E-03   0.27121E+01 0.11647E+03 
c  Velocity[X]                                      0.12934E+01 
c  Velocity[Y]                                      0.14187E+01 
c  Velocity[Z]                                      0.13128E-29 
c  Pressure     0.12441E-06     457   0.91522E-08   0.11472E+00 0.70452E+03 
c  nu_tilda     0.56344E-05      32   0.59424E-05   0.24552E-06 0.14005E+03 
c  TempC        0.34458E+02      27   0.39618E-03   0.37972E+01 0.19521E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6865          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8336          7.2882      -0.0012362      -0.0012362
v  Velocity[Z]       -6.9287e-015     1.0247e-014    -6.1377e-018    -6.1377e-018
v  ǁVelocityǁ        0.00054355          10.447          5.2492          5.2492
v  Pressure               -49.386          16.819         -10.378         -10.378
v  nu_tilda           4.3573e-007       0.0042695       0.0012903       0.0012903
v  TempC                       21          73.065          21.812          21.812
v  TurbVisc             3.17e-014        0.005032       0.0015138       0.0015138
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1305:        0.20390E+01

===============================================================


 INSTANT    0.130600000E+04   TIME STEP NUMBER            1306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80219E-02 0.89754E+00
   Friction velocity        uk    :  0.80219E-02 0.89754E+00
   Dimensionless distance   yplus :  0.64582E-01 0.72258E+01
   Friction thermal sca.    tstar : -0.23218E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48185E-01 0.53913E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85464E-02      33   0.30458E-03   0.26910E+01 0.11647E+03 
c  Velocity[X]                                      0.12837E+01 
c  Velocity[Y]                                      0.14073E+01 
c  Velocity[Z]                                      0.11788E-29 
c  Pressure     0.10851E-06     440   0.95167E-08   0.10097E+00 0.41784E+03 
c  nu_tilda     0.56363E-05      32   0.16035E-04   0.24583E-06 0.14012E+03 
c  TempC        0.34468E+02      27   0.31559E-03   0.40115E+01 0.22023E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6836          10.447          4.5729          4.5729
v  Velocity[Y]             -2.832          7.2964       -0.001246       -0.001246
v  Velocity[Z]       -6.9287e-015     9.8111e-015    -6.1358e-018    -6.1358e-018
v  ǁVelocityǁ         0.0012728          10.447           5.249           5.249
v  Pressure               -49.386          16.769         -10.406         -10.406
v  nu_tilda            4.357e-007       0.0042695       0.0012909       0.0012909
v  TempC                       21          73.065          21.812          21.812
v  TurbVisc           3.1714e-014        0.005032       0.0015145       0.0015145
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1306:        0.20120E+01

===============================================================


 INSTANT    0.130700000E+04   TIME STEP NUMBER            1307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15111E-01 0.89746E+00
   Friction velocity        uk    :  0.15111E-01 0.89746E+00
   Dimensionless distance   yplus :  0.12165E+00 0.72252E+01
   Friction thermal sca.    tstar : -0.22099E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90767E-01 0.53908E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85488E-02      33   0.32292E-03   0.27041E+01 0.11660E+03 
c  Velocity[X]                                      0.12988E+01 
c  Velocity[Y]                                      0.14053E+01 
c  Velocity[Z]                                      0.13459E-29 
c  Pressure     0.12526E-06     392   0.95270E-08   0.11867E+00 0.38340E+03 
c  nu_tilda     0.56382E-05      32   0.59327E-05   0.24613E-06 0.14019E+03 
c  TempC        0.34477E+02      27   0.37377E-03   0.32879E+01 0.19272E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6806          10.447          4.5729          4.5729
v  Velocity[Y]            -2.8303          7.2736      -0.0012553      -0.0012553
v  Velocity[Z]       -6.9287e-015     1.0258e-014    -6.1299e-018    -6.1299e-018
v  ǁVelocityǁ         0.0011553          10.447          5.2488          5.2488
v  Pressure               -49.344           16.72         -10.401         -10.401
v  nu_tilda           4.3572e-007       0.0042695       0.0012915       0.0012915
v  TempC                       21          73.065          21.813          21.813
v  TurbVisc           3.1703e-014        0.005032       0.0015151       0.0015151
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1307:        0.18960E+01

===============================================================


 INSTANT    0.130800000E+04   TIME STEP NUMBER            1308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11333E-01 0.89612E+00
   Friction velocity        uk    :  0.11333E-01 0.89612E+00
   Dimensionless distance   yplus :  0.91239E-01 0.72144E+01
   Friction thermal sca.    tstar : -0.28920E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68075E-01 0.53827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85512E-02      33   0.29269E-03   0.27187E+01 0.11688E+03 
c  Velocity[X]                                      0.12882E+01 
c  Velocity[Y]                                      0.14304E+01 
c  Velocity[Z]                                      0.11310E-29 
c  Pressure     0.11139E-06     409   0.94989E-08   0.10346E+00 0.23233E+03 
c  nu_tilda     0.56401E-05      32   0.16038E-04   0.24645E-06 0.14026E+03 
c  TempC        0.34487E+02      26   0.45156E-03   0.62026E+01 0.26110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6775          10.446          4.5729          4.5729
v  Velocity[Y]            -2.8287          7.2875      -0.0012647      -0.0012647
v  Velocity[Z]       -6.9287e-015      9.832e-015    -6.1274e-018    -6.1274e-018
v  ǁVelocityǁ         0.0010149          10.447          5.2487          5.2487
v  Pressure               -49.349          16.745         -10.421         -10.421
v  nu_tilda           4.3576e-007       0.0042695        0.001292        0.001292
v  TempC                       21          73.065          21.813          21.813
v  TurbVisc            3.171e-014        0.005032       0.0015158       0.0015158
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1308:        0.19340E+01

===============================================================


 INSTANT    0.130900000E+04   TIME STEP NUMBER            1309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12131E-01 0.89730E+00
   Friction velocity        uk    :  0.12131E-01 0.89730E+00
   Dimensionless distance   yplus :  0.97663E-01 0.72239E+01
   Friction thermal sca.    tstar : -0.22800E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72868E-01 0.53898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85536E-02      33   0.33228E-03   0.27184E+01 0.11696E+03 
c  Velocity[X]                                      0.12967E+01 
c  Velocity[Y]                                      0.14216E+01 
c  Velocity[Z]                                      0.14916E-29 
c  Pressure     0.12039E-06     410   0.94879E-08   0.11313E+00 0.36722E+03 
c  nu_tilda     0.56420E-05      32   0.59117E-05   0.24675E-06 0.14033E+03 
c  TempC        0.34497E+02      26   0.33451E-03   0.65932E+01 0.28586E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6744          10.446          4.5729          4.5729
v  Velocity[Y]            -2.8271          7.2699       -0.001274       -0.001274
v  Velocity[Z]       -6.9287e-015      1.022e-014    -6.1255e-018    -6.1255e-018
v  ǁVelocityǁ        0.00089431          10.447          5.2485          5.2485
v  Pressure               -49.311          16.708         -10.411         -10.411
v  nu_tilda           4.3581e-007       0.0042695       0.0012926       0.0012926
v  TempC                       21          73.064          21.813          21.813
v  TurbVisc           3.1722e-014        0.005032       0.0015164       0.0015164
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1309:        0.19220E+01

===============================================================


 INSTANT    0.131000000E+04   TIME STEP NUMBER            1310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95916E-02 0.89671E+00
   Friction velocity        uk    :  0.95916E-02 0.89671E+00
   Dimensionless distance   yplus :  0.77219E-01 0.72191E+01
   Friction thermal sca.    tstar : -0.36374E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57614E-01 0.53863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85560E-02      33   0.28239E-03   0.27471E+01 0.11725E+03 
c  Velocity[X]                                      0.13295E+01 
c  Velocity[Y]                                      0.14177E+01 
c  Velocity[Z]                                      0.11318E-29 
c  Pressure     0.12802E-06     441   0.93606E-08   0.11889E+00 0.40999E+03 
c  nu_tilda     0.56439E-05      32   0.16045E-04   0.24707E-06 0.14041E+03 
c  TempC        0.34507E+02      26   0.44398E-03   0.36028E+01 0.22298E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6712          10.446          4.5729          4.5729
v  Velocity[Y]            -2.8255          7.2979      -0.0012829      -0.0012829
v  Velocity[Z]       -6.9287e-015      9.787e-015    -6.1194e-018    -6.1194e-018
v  ǁVelocityǁ        0.00074259          10.446          5.2483          5.2483
v  Pressure               -49.307          16.707         -10.439         -10.439
v  nu_tilda           4.3584e-007       0.0042695       0.0012931       0.0012931
v  TempC                       21          73.065          21.814          21.814
v  TurbVisc           3.1738e-014        0.005032       0.0015171       0.0015171
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1310:        0.20040E+01

===============================================================


 INSTANT    0.131100000E+04   TIME STEP NUMBER            1311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90590E-02 0.89827E+00
   Friction velocity        uk    :  0.90590E-02 0.89827E+00
   Dimensionless distance   yplus :  0.72932E-01 0.72317E+01
   Friction thermal sca.    tstar : -0.24769E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54415E-01 0.53957E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85584E-02      33   0.30429E-03   0.27428E+01 0.11731E+03 
c  Velocity[X]                                      0.13014E+01 
c  Velocity[Y]                                      0.14414E+01 
c  Velocity[Z]                                      0.99003E-30 
c  Pressure     0.12811E-06     472   0.98103E-08   0.11784E+00 0.58671E+03 
c  nu_tilda     0.56459E-05      32   0.59004E-05   0.24736E-06 0.14048E+03 
c  TempC        0.34517E+02      27   0.39502E-03   0.75251E+01 0.29210E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6681          10.446          4.5729          4.5729
v  Velocity[Y]            -2.8238          7.3039      -0.0012918      -0.0012918
v  Velocity[Z]       -6.9287e-015     1.0231e-014    -6.1151e-018    -6.1151e-018
v  ǁVelocityǁ        0.00060501          10.446          5.2482          5.2482
v  Pressure               -49.272          16.768          -10.41          -10.41
v  nu_tilda           4.3577e-007       0.0042695       0.0012937       0.0012937
v  TempC                       21          73.065          21.814          21.814
v  TurbVisc           3.1745e-014        0.005032       0.0015178       0.0015178
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1311:        0.20670E+01

===============================================================


 INSTANT    0.131200000E+04   TIME STEP NUMBER            1312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10166E-01 0.89803E+00
   Friction velocity        uk    :  0.10166E-01 0.89803E+00
   Dimensionless distance   yplus :  0.81845E-01 0.72298E+01
   Friction thermal sca.    tstar : -0.23341E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61066E-01 0.53942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85608E-02      33   0.27615E-03   0.27428E+01 0.11739E+03 
c  Velocity[X]                                      0.13127E+01 
c  Velocity[Y]                                      0.14302E+01 
c  Velocity[Z]                                      0.13460E-29 
c  Pressure     0.11210E-06     489   0.99883E-08   0.10573E+00 0.11050E+04 
c  nu_tilda     0.56478E-05      32   0.16042E-04   0.24768E-06 0.14055E+03 
c  TempC        0.34527E+02      26   0.37669E-03   0.56146E+01 0.26454E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6651          10.446          4.5729          4.5729
v  Velocity[Y]            -2.8222          7.2761      -0.0013007      -0.0013007
v  Velocity[Z]       -6.9287e-015     9.8067e-015    -6.1116e-018    -6.1116e-018
v  ǁVelocityǁ        0.00046393          10.446           5.248           5.248
v  Pressure               -49.268          16.581         -10.474         -10.474
v  nu_tilda           4.3577e-007       0.0042695       0.0012942       0.0012942
v  TempC                       21          73.065          21.814          21.814
v  TurbVisc           3.1724e-014        0.005032       0.0015184       0.0015184
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1312:        0.21090E+01

===============================================================


 INSTANT    0.131300000E+04   TIME STEP NUMBER            1313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10369E-01 0.89657E+00
   Friction velocity        uk    :  0.10369E-01 0.89657E+00
   Dimensionless distance   yplus :  0.83481E-01 0.72180E+01
   Friction thermal sca.    tstar : -0.31634E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62286E-01 0.53854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85631E-02      33   0.35266E-03   0.27186E+01 0.11733E+03 
c  Velocity[X]                                      0.12914E+01 
c  Velocity[Y]                                      0.14272E+01 
c  Velocity[Z]                                      0.11612E-29 
c  Pressure     0.10709E-06     490   0.96714E-08   0.99012E-01 0.11398E+04 
c  nu_tilda     0.56497E-05      32   0.58840E-05   0.24799E-06 0.14062E+03 
c  TempC        0.34537E+02      26   0.39789E-03   0.52574E+01 0.24725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6621          10.446          4.5729          4.5729
v  Velocity[Y]            -2.8206             7.3      -0.0013092      -0.0013092
v  Velocity[Z]       -6.9287e-015     1.0192e-014    -6.1082e-018    -6.1082e-018
v  ǁVelocityǁ        0.00032596          10.446          5.2478          5.2478
v  Pressure               -49.229          16.772         -10.414         -10.414
v  nu_tilda           4.3579e-007       0.0042695       0.0012948       0.0012948
v  TempC                       21          73.065          21.815          21.815
v  TurbVisc           3.1725e-014        0.005032       0.0015191       0.0015191
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1313:        0.20930E+01

===============================================================


 INSTANT    0.131400000E+04   TIME STEP NUMBER            1314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49432E-02 0.89757E+00
   Friction velocity        uk    :  0.49432E-02 0.89757E+00
   Dimensionless distance   yplus :  0.39796E-01 0.72261E+01
   Friction thermal sca.    tstar : -0.25960E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29692E-01 0.53915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85655E-02      33   0.33844E-03   0.27838E+01 0.11797E+03 
c  Velocity[X]                                      0.13282E+01 
c  Velocity[Y]                                      0.14556E+01 
c  Velocity[Z]                                      0.12227E-29 
c  Pressure     0.14866E-06     489   0.97445E-08   0.13745E+00 0.11942E+04 
c  nu_tilda     0.56516E-05      32   0.16051E-04   0.24831E-06 0.14070E+03 
c  TempC        0.34547E+02      27   0.35421E-03   0.48279E+01 0.23929E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.659          10.446          4.5729          4.5729
v  Velocity[Y]             -2.819           7.271      -0.0013177      -0.0013177
v  Velocity[Z]       -6.9287e-015      9.761e-015    -6.1086e-018    -6.1086e-018
v  ǁVelocityǁ        0.00028125          10.446          5.2476          5.2476
v  Pressure               -49.232          16.556         -10.484         -10.484
v  nu_tilda           4.3588e-007       0.0042695       0.0012954       0.0012954
v  TempC                       21          73.064          21.815          21.815
v  TurbVisc            3.173e-014        0.005032       0.0015198       0.0015198
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1314:        0.21170E+01

===============================================================


 INSTANT    0.131500000E+04   TIME STEP NUMBER            1315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75049E-02 0.89712E+00
   Friction velocity        uk    :  0.75049E-02 0.89712E+00
   Dimensionless distance   yplus :  0.60419E-01 0.72224E+01
   Friction thermal sca.    tstar : -0.44515E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45079E-01 0.53887E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85679E-02      33   0.22230E-03   0.27632E+01 0.11791E+03 
c  Velocity[X]                                      0.13184E+01 
c  Velocity[Y]                                      0.14448E+01 
c  Velocity[Z]                                      0.11513E-29 
c  Pressure     0.11380E-06     490   0.98685E-08   0.10590E+00 0.86763E+03 
c  nu_tilda     0.56535E-05      32   0.58717E-05   0.24861E-06 0.14077E+03 
c  TempC        0.34557E+02      27   0.42431E-03   0.47379E+01 0.23227E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6559          10.445          4.5729          4.5729
v  Velocity[Y]            -2.8174          7.3013      -0.0013261      -0.0013261
v  Velocity[Z]       -6.9287e-015     1.0203e-014    -6.1075e-018    -6.1075e-018
v  ǁVelocityǁ        0.00033189          10.446          5.2475          5.2475
v  Pressure               -49.193          16.716         -10.442         -10.442
v  nu_tilda             4.36e-007       0.0042695       0.0012959       0.0012959
v  TempC                       21          73.064          21.815          21.815
v  TurbVisc           3.1758e-014        0.005032       0.0015204       0.0015204
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1315:        0.21540E+01

===============================================================


 INSTANT    0.131600000E+04   TIME STEP NUMBER            1316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12479E-01 0.89852E+00
   Friction velocity        uk    :  0.12479E-01 0.89852E+00
   Dimensionless distance   yplus :  0.10047E+00 0.72337E+01
   Friction thermal sca.    tstar : -0.26273E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74960E-01 0.53971E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85703E-02      33   0.34744E-03   0.27216E+01 0.11767E+03 
c  Velocity[X]                                      0.12824E+01 
c  Velocity[Y]                                      0.14392E+01 
c  Velocity[Z]                                      0.13248E-29 
c  Pressure     0.11513E-06     425   0.94390E-08   0.10662E+00 0.34052E+03 
c  nu_tilda     0.56555E-05      32   0.16046E-04   0.24894E-06 0.14084E+03 
c  TempC        0.34566E+02      26   0.38495E-03   0.58294E+01 0.27634E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6528          10.445          4.5729          4.5729
v  Velocity[Y]            -2.8157          7.3122      -0.0013343      -0.0013343
v  Velocity[Z]       -6.9287e-015     9.7836e-015    -6.1087e-018    -6.1087e-018
v  ǁVelocityǁ        0.00036887          10.445          5.2473          5.2473
v  Pressure               -49.192          16.684         -10.464         -10.464
v  nu_tilda             4.36e-007       0.0042695       0.0012965       0.0012965
v  TempC                       21          73.064          21.816          21.816
v  TurbVisc           3.1791e-014        0.005032       0.0015211       0.0015211
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1316:        0.19680E+01

===============================================================


 INSTANT    0.131700000E+04   TIME STEP NUMBER            1317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19201E-02 0.89815E+00
   Friction velocity        uk    :  0.19201E-02 0.89815E+00
   Dimensionless distance   yplus :  0.15458E-01 0.72307E+01
   Friction thermal sca.    tstar : -0.23264E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11533E-01 0.53949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85727E-02      33   0.33719E-03   0.27862E+01 0.11821E+03 
c  Velocity[X]                                      0.13224E+01 
c  Velocity[Y]                                      0.14638E+01 
c  Velocity[Z]                                      0.14419E-29 
c  Pressure     0.13633E-06     440   0.95539E-08   0.12558E+00 0.54861E+03 
c  nu_tilda     0.56574E-05      32   0.58722E-05   0.24924E-06 0.14091E+03 
c  TempC        0.34576E+02      26   0.31295E-03   0.54756E+01 0.23688E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6496          10.445          4.5729          4.5729
v  Velocity[Y]            -2.8141          7.2805      -0.0013423      -0.0013423
v  Velocity[Z]       -6.9287e-015     1.0166e-014    -6.1078e-018    -6.1078e-018
v  ǁVelocityǁ        0.00065195          10.445          5.2471          5.2471
v  Pressure               -49.153          16.564         -10.481         -10.481
v  nu_tilda           4.3604e-007       0.0042695       0.0012971       0.0012971
v  TempC                       21          73.064          21.816          21.816
v  TurbVisc           3.1793e-014        0.005032       0.0015217       0.0015217
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1317:        0.20400E+01

===============================================================


 INSTANT    0.131800000E+04   TIME STEP NUMBER            1318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82670E-02 0.89684E+00
   Friction velocity        uk    :  0.82670E-02 0.89684E+00
   Dimensionless distance   yplus :  0.66555E-01 0.72202E+01
   Friction thermal sca.    tstar : -0.42218E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49658E-01 0.53871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85750E-02      33   0.30830E-03   0.27956E+01 0.11842E+03 
c  Velocity[X]                                      0.13427E+01 
c  Velocity[Y]                                      0.14529E+01 
c  Velocity[Z]                                      0.96120E-30 
c  Pressure     0.12021E-06     377   0.93061E-08   0.11095E+00 0.25144E+03 
c  nu_tilda     0.56593E-05      32   0.16052E-04   0.24956E-06 0.14099E+03 
c  TempC        0.34586E+02      27   0.43225E-03   0.37693E+01 0.19973E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6466          10.445          4.5729          4.5729
v  Velocity[Y]            -2.8125          7.3013      -0.0013503      -0.0013503
v  Velocity[Z]       -6.9287e-015     9.7362e-015    -6.1101e-018    -6.1101e-018
v  ǁVelocityǁ        0.00088989          10.445          5.2469          5.2469
v  Pressure               -49.154          16.637         -10.485         -10.485
v  nu_tilda           4.3609e-007       0.0042695       0.0012976       0.0012976
v  TempC                       21          73.064          21.816          21.816
v  TurbVisc           3.1804e-014        0.005032       0.0015224       0.0015224
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1318:        0.18600E+01

===============================================================


 INSTANT    0.131900000E+04   TIME STEP NUMBER            1319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12449E-01 0.89794E+00
   Friction velocity        uk    :  0.12449E-01 0.89794E+00
   Dimensionless distance   yplus :  0.10022E+00 0.72290E+01
   Friction thermal sca.    tstar : -0.26840E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74777E-01 0.53937E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85774E-02      33   0.33672E-03   0.27703E+01 0.11833E+03 
c  Velocity[X]                                      0.13217E+01 
c  Velocity[Y]                                      0.14486E+01 
c  Velocity[Z]                                      0.14040E-29 
c  Pressure     0.12363E-06     440   0.99951E-08   0.11579E+00 0.40773E+03 
c  nu_tilda     0.56612E-05      32   0.58490E-05   0.24986E-06 0.14106E+03 
c  TempC        0.34596E+02      27   0.38271E-03   0.46374E+01 0.23979E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6436          10.445          4.5729          4.5729
v  Velocity[Y]            -2.8109          7.2835      -0.0013578      -0.0013578
v  Velocity[Z]       -6.9287e-015     1.0174e-014    -6.1153e-018    -6.1153e-018
v  ǁVelocityǁ         0.0011161          10.445          5.2468          5.2468
v  Pressure               -49.112          16.615          -10.47          -10.47
v  nu_tilda           4.3615e-007       0.0042695       0.0012982       0.0012982
v  TempC                       21          73.064          21.817          21.817
v  TurbVisc           3.1818e-014        0.005032       0.0015231       0.0015231
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1319:        0.19980E+01

===============================================================


 INSTANT    0.132000000E+04   TIME STEP NUMBER            1320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81166E-02 0.89709E+00
   Friction velocity        uk    :  0.81166E-02 0.89709E+00
   Dimensionless distance   yplus :  0.65345E-01 0.72221E+01
   Friction thermal sca.    tstar : -0.40404E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48754E-01 0.53885E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85798E-02      33   0.23635E-03   0.27815E+01 0.11852E+03 
c  Velocity[X]                                      0.13165E+01 
c  Velocity[Y]                                      0.14651E+01 
c  Velocity[Z]                                      0.12663E-29 
c  Pressure     0.12201E-06     456   0.99804E-08   0.11144E+00 0.53515E+03 
c  nu_tilda     0.56632E-05      32   0.16055E-04   0.25019E-06 0.14113E+03 
c  TempC        0.34606E+02      27   0.37195E-03   0.44410E+01 0.22195E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6405          10.445          4.5729          4.5729
v  Velocity[Y]            -2.8093          7.3013      -0.0013654      -0.0013654
v  Velocity[Z]       -6.9287e-015     9.7543e-015    -6.1111e-018    -6.1111e-018
v  ǁVelocityǁ         0.0013348          10.445          5.2466          5.2466
v  Pressure               -49.115          16.583          -10.51          -10.51
v  nu_tilda           4.3617e-007       0.0042695       0.0012987       0.0012987
v  TempC                       21          73.064          21.817          21.817
v  TurbVisc           3.1834e-014        0.005032       0.0015237       0.0015237
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1320:        0.20170E+01

===============================================================


 INSTANT    0.132100000E+04   TIME STEP NUMBER            1321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12411E-01 0.89843E+00
   Friction velocity        uk    :  0.12411E-01 0.89843E+00
   Dimensionless distance   yplus :  0.99917E-01 0.72330E+01
   Friction thermal sca.    tstar : -0.26435E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74549E-01 0.53966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85821E-02      33   0.31818E-03   0.27501E+01 0.11841E+03 
c  Velocity[X]                                      0.12879E+01 
c  Velocity[Y]                                      0.14622E+01 
c  Velocity[Z]                                      0.11713E-29 
c  Pressure     0.10384E-06     488   0.93031E-08   0.95419E-01 0.77421E+03 
c  nu_tilda     0.56651E-05      32   0.58427E-05   0.25050E-06 0.14121E+03 
c  TempC        0.34616E+02      26   0.34429E-03   0.49729E+01 0.23138E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6374          10.444          4.5729          4.5729
v  Velocity[Y]            -2.8077          7.3128       -0.001373       -0.001373
v  Velocity[Z]       -6.9287e-015     1.0135e-014    -6.1162e-018    -6.1162e-018
v  ǁVelocityǁ         0.0010788          10.445          5.2464          5.2464
v  Pressure               -49.078          16.686         -10.469         -10.469
v  nu_tilda           4.3611e-007       0.0042695       0.0012993       0.0012993
v  TempC                       21          73.064          21.817          21.817
v  TurbVisc           3.1841e-014        0.005032       0.0015244       0.0015244
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1321:        0.21150E+01

===============================================================


 INSTANT    0.132200000E+04   TIME STEP NUMBER            1322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11146E-01 0.89804E+00
   Friction velocity        uk    :  0.11146E-01 0.89804E+00
   Dimensionless distance   yplus :  0.89729E-01 0.72298E+01
   Friction thermal sca.    tstar : -0.25322E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66948E-01 0.53943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85845E-02      33   0.35204E-03   0.28141E+01 0.11892E+03 
c  Velocity[X]                                      0.13543E+01 
c  Velocity[Y]                                      0.14598E+01 
c  Velocity[Z]                                      0.14838E-29 
c  Pressure     0.15341E-06     504   0.92128E-08   0.14259E+00 0.11936E+04 
c  nu_tilda     0.56670E-05      32   0.16051E-04   0.25083E-06 0.14128E+03 
c  TempC        0.34626E+02      26   0.32151E-03   0.49172E+01 0.24600E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6342          10.444          4.5729          4.5729
v  Velocity[Y]             -2.806          7.2863      -0.0013802      -0.0013802
v  Velocity[Z]       -6.9287e-015     9.7092e-015     -6.114e-018     -6.114e-018
v  ǁVelocityǁ        0.00058934          10.444          5.2462          5.2462
v  Pressure               -49.074          16.474         -10.536         -10.536
v  nu_tilda            4.361e-007       0.0042695       0.0012998       0.0012998
v  TempC                       21          73.064          21.818          21.818
v  TurbVisc           3.1822e-014        0.005032       0.0015251       0.0015251
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1322:        0.21480E+01

===============================================================


 INSTANT    0.132300000E+04   TIME STEP NUMBER            1323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28865E-02 0.89683E+00
   Friction velocity        uk    :  0.28865E-02 0.89683E+00
   Dimensionless distance   yplus :  0.23238E-01 0.72201E+01
   Friction thermal sca.    tstar : -0.59060E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17338E-01 0.53870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85868E-02      33   0.30898E-03   0.28135E+01 0.11899E+03 
c  Velocity[X]                                      0.13376E+01 
c  Velocity[Y]                                      0.14759E+01 
c  Velocity[Z]                                      0.13782E-29 
c  Pressure     0.12410E-06     488   0.96464E-08   0.11302E+00 0.91801E+03 
c  nu_tilda     0.56690E-05      32   0.58351E-05   0.25115E-06 0.14136E+03 
c  TempC        0.34635E+02      26   0.44290E-03   0.56831E+01 0.24848E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6311          10.444          4.5729          4.5729
v  Velocity[Y]            -2.8044          7.3023      -0.0013872      -0.0013872
v  Velocity[Z]       -6.9287e-015     1.0145e-014    -6.1173e-018    -6.1173e-018
v  ǁVelocityǁ         0.0015077          10.444           5.246           5.246
v  Pressure               -49.039          16.627          -10.49          -10.49
v  nu_tilda           4.3612e-007       0.0042695       0.0013004       0.0013004
v  TempC                       21          73.064          21.818          21.818
v  TurbVisc            3.182e-014        0.005032       0.0015257       0.0015257
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1323:        0.21140E+01

===============================================================


 INSTANT    0.132400000E+04   TIME STEP NUMBER            1324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10811E-01 0.89807E+00
   Friction velocity        uk    :  0.10811E-01 0.89807E+00
   Dimensionless distance   yplus :  0.87035E-01 0.72301E+01
   Friction thermal sca.    tstar : -0.28835E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64938E-01 0.53945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85892E-02      33   0.31175E-03   0.27954E+01 0.11900E+03 
c  Velocity[X]                                      0.13231E+01 
c  Velocity[Y]                                      0.14723E+01 
c  Velocity[Z]                                      0.13370E-29 
c  Pressure     0.11524E-06     488   0.90927E-08   0.10783E+00 0.84643E+03 
c  nu_tilda     0.56709E-05      32   0.16059E-04   0.25147E-06 0.14143E+03 
c  TempC        0.34645E+02      27   0.33168E-03   0.65408E+01 0.28631E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6281          10.444          4.5729          4.5729
v  Velocity[Y]            -2.8028          7.2804      -0.0013941      -0.0013941
v  Velocity[Z]       -6.9287e-015      9.728e-015    -6.1197e-018    -6.1197e-018
v  ǁVelocityǁ         0.0012418          10.444          5.2458          5.2458
v  Pressure               -49.038          16.485          -10.54          -10.54
v  nu_tilda            4.362e-007       0.0042695       0.0013009       0.0013009
v  TempC                       21          73.064          21.818          21.818
v  TurbVisc           3.1827e-014        0.005032       0.0015264       0.0015264
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1324:        0.21240E+01

===============================================================


 INSTANT    0.132500000E+04   TIME STEP NUMBER            1325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77592E-02 0.89734E+00
   Friction velocity        uk    :  0.77592E-02 0.89734E+00
   Dimensionless distance   yplus :  0.62467E-01 0.72242E+01
   Friction thermal sca.    tstar : -0.42291E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46608E-01 0.53900E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85916E-02      33   0.30125E-03   0.27997E+01 0.11915E+03 
c  Velocity[X]                                      0.13255E+01 
c  Velocity[Y]                                      0.14742E+01 
c  Velocity[Z]                                      0.10695E-29 
c  Pressure     0.11740E-06     488   0.93680E-08   0.10744E+00 0.72127E+03 
c  nu_tilda     0.56728E-05      32   0.58232E-05   0.25178E-06 0.14150E+03 
c  TempC        0.34655E+02      27   0.40165E-03   0.40564E+01 0.22327E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6251          10.443          4.5729          4.5729
v  Velocity[Y]            -2.8012          7.3104      -0.0014007      -0.0014007
v  Velocity[Z]       -6.9287e-015     1.0105e-014    -6.1217e-018    -6.1217e-018
v  ǁVelocityǁ        0.00099783          10.444          5.2456          5.2456
v  Pressure               -48.996          16.597         -10.504         -10.504
v  nu_tilda           4.3627e-007       0.0042695       0.0013015       0.0013015
v  TempC                       21          73.064          21.819          21.819
v  TurbVisc           3.1851e-014        0.005032        0.001527        0.001527
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1325:        0.20940E+01

===============================================================


 INSTANT    0.132600000E+04   TIME STEP NUMBER            1326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10819E-01 0.89887E+00
   Friction velocity        uk    :  0.10819E-01 0.89887E+00
   Dimensionless distance   yplus :  0.87101E-01 0.72365E+01
   Friction thermal sca.    tstar : -0.32265E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64987E-01 0.53992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85939E-02      33   0.31176E-03   0.28252E+01 0.11950E+03 
c  Velocity[X]                                      0.13278E+01 
c  Velocity[Y]                                      0.14974E+01 
c  Velocity[Z]                                      0.10050E-29 
c  Pressure     0.14106E-06     457   0.94936E-08   0.12755E+00 0.63024E+03 
c  nu_tilda     0.56748E-05      32   0.16053E-04   0.25211E-06 0.14158E+03 
c  TempC        0.34665E+02      26   0.40266E-03   0.65984E+01 0.27397E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.622          10.443          4.5729          4.5729
v  Velocity[Y]            -2.7996           7.314      -0.0014074      -0.0014074
v  Velocity[Z]       -6.9287e-015     9.6795e-015    -6.1193e-018    -6.1193e-018
v  ǁVelocityǁ        0.00074588          10.443          5.2455          5.2455
v  Pressure               -49.001          16.507         -10.547         -10.547
v  nu_tilda           4.3633e-007       0.0042695       0.0013021       0.0013021
v  TempC                       21          73.064          21.819          21.819
v  TurbVisc           3.1871e-014        0.005032       0.0015277       0.0015277
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1326:        0.23050E+01

===============================================================


 INSTANT    0.132700000E+04   TIME STEP NUMBER            1327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99124E-02 0.89897E+00
   Friction velocity        uk    :  0.99124E-02 0.89897E+00
   Dimensionless distance   yplus :  0.79802E-01 0.72373E+01
   Friction thermal sca.    tstar : -0.33721E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59541E-01 0.53998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85963E-02      33   0.27864E-03   0.28261E+01 0.11954E+03 
c  Velocity[X]                                      0.13372E+01 
c  Velocity[Y]                                      0.14889E+01 
c  Velocity[Z]                                      0.13044E-29 
c  Pressure     0.12994E-06     410   0.96040E-08   0.12108E+00 0.37507E+03 
c  nu_tilda     0.56767E-05      32   0.58248E-05   0.25243E-06 0.14165E+03 
c  TempC        0.34675E+02      26   0.37814E-03   0.54185E+01 0.25202E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6189          10.443          4.5729          4.5729
v  Velocity[Y]             -2.798          7.2896      -0.0014138      -0.0014138
v  Velocity[Z]       -6.9287e-015     1.0112e-014    -6.1213e-018    -6.1213e-018
v  ǁVelocityǁ        0.00054186          10.443          5.2453          5.2453
v  Pressure                -48.96          16.498         -10.536         -10.536
v  nu_tilda           4.3641e-007       0.0042695       0.0013026       0.0013026
v  TempC                       21          73.063          21.819          21.819
v  TurbVisc           3.1889e-014        0.005032       0.0015283       0.0015283
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1327:        0.21260E+01

===============================================================


 INSTANT    0.132800000E+04   TIME STEP NUMBER            1328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72348E-02 0.89732E+00
   Friction velocity        uk    :  0.72348E-02 0.89732E+00
   Dimensionless distance   yplus :  0.58245E-01 0.72240E+01
   Friction thermal sca.    tstar : -0.40244E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43457E-01 0.53899E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.85986E-02      33   0.35565E-03   0.27950E+01 0.11940E+03 
c  Velocity[X]                                      0.13119E+01 
c  Velocity[Y]                                      0.14831E+01 
c  Velocity[Z]                                      0.99847E-30 
c  Pressure     0.11574E-06     344   0.94647E-08   0.10605E+00 0.19699E+03 
c  nu_tilda     0.56786E-05      32   0.16058E-04   0.25276E-06 0.14173E+03 
c  TempC        0.34685E+02      26   0.32096E-03   0.43599E+01 0.23752E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6157          10.443          4.5729          4.5729
v  Velocity[Y]            -2.7964          7.3114        -0.00142        -0.00142
v  Velocity[Z]       -6.9287e-015     9.6996e-015    -6.1201e-018    -6.1201e-018
v  ǁVelocityǁ        0.00034859          10.443          5.2451          5.2451
v  Pressure               -48.961          16.531         -10.545         -10.545
v  nu_tilda           4.3643e-007       0.0042695       0.0013032       0.0013032
v  TempC                       21          73.064           21.82           21.82
v  TurbVisc           3.1913e-014        0.005032        0.001529        0.001529
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1328:        0.17840E+01

===============================================================


 INSTANT    0.132900000E+04   TIME STEP NUMBER            1329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10219E-01 0.89844E+00
   Friction velocity        uk    :  0.10219E-01 0.89844E+00
   Dimensionless distance   yplus :  0.82270E-01 0.72331E+01
   Friction thermal sca.    tstar : -0.32062E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61383E-01 0.53967E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86010E-02      33   0.35802E-03   0.28415E+01 0.11984E+03 
c  Velocity[X]                                      0.13341E+01 
c  Velocity[Y]                                      0.15074E+01 
c  Velocity[Z]                                      0.11893E-29 
c  Pressure     0.13573E-06     361   0.92699E-08   0.12410E+00 0.37066E+03 
c  nu_tilda     0.56806E-05      32   0.58049E-05   0.25308E-06 0.14180E+03 
c  TempC        0.34694E+02      26   0.32152E-03   0.42965E+01 0.22511E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6126          10.443          4.5729          4.5729
v  Velocity[Y]            -2.7947          7.2851      -0.0014259      -0.0014259
v  Velocity[Z]       -6.9287e-015     1.0074e-014    -6.1224e-018    -6.1224e-018
v  ǁVelocityǁ        0.00037916          10.443          5.2449          5.2449
v  Pressure               -48.923          16.471         -10.544         -10.544
v  nu_tilda           4.3648e-007       0.0042695       0.0013038       0.0013038
v  TempC                       21          73.063           21.82           21.82
v  TurbVisc           3.1918e-014        0.005032       0.0015297       0.0015297
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1329:        0.18210E+01

===============================================================


 INSTANT    0.133000000E+04   TIME STEP NUMBER            1330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41696E-02 0.89773E+00
   Friction velocity        uk    :  0.41696E-02 0.89773E+00
   Dimensionless distance   yplus :  0.33568E-01 0.72273E+01
   Friction thermal sca.    tstar : -0.78873E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25046E-01 0.53924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86033E-02      33   0.25962E-03   0.28690E+01 0.12017E+03 
c  Velocity[X]                                      0.13698E+01 
c  Velocity[Y]                                      0.14992E+01 
c  Velocity[Z]                                      0.12692E-29 
c  Pressure     0.12509E-06     426   0.96711E-08   0.11436E+00 0.44011E+03 
c  nu_tilda     0.56825E-05      32   0.16063E-04   0.25341E-06 0.14188E+03 
c  TempC        0.34704E+02      27   0.47711E-03   0.40247E+01 0.22151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6096          10.442          4.5729          4.5729
v  Velocity[Y]            -2.7931          7.3122      -0.0014317      -0.0014317
v  Velocity[Z]       -6.9287e-015     9.6514e-015    -6.1179e-018    -6.1179e-018
v  ǁVelocityǁ        0.00059269          10.442          5.2447          5.2447
v  Pressure               -48.921          16.455         -10.576         -10.576
v  nu_tilda           4.3657e-007       0.0042695       0.0013043       0.0013043
v  TempC                       21          73.063           21.82           21.82
v  TurbVisc           3.1931e-014        0.005032       0.0015303       0.0015303
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1330:        0.20230E+01

===============================================================


 INSTANT    0.133100000E+04   TIME STEP NUMBER            1331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57779E-02 0.89939E+00
   Friction velocity        uk    :  0.57779E-02 0.89939E+00
   Dimensionless distance   yplus :  0.46516E-01 0.72407E+01
   Friction thermal sca.    tstar : -0.40945E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34706E-01 0.54024E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86057E-02      33   0.32779E-03   0.28179E+01 0.11994E+03 
c  Velocity[X]                                      0.13222E+01 
c  Velocity[Y]                                      0.14957E+01 
c  Velocity[Z]                                      0.10193E-29 
c  Pressure     0.11204E-06     474   0.95095E-08   0.10272E+00 0.91190E+03 
c  nu_tilda     0.56845E-05      32   0.57943E-05   0.25372E-06 0.14195E+03 
c  TempC        0.34714E+02      27   0.31832E-03   0.66254E+01 0.29106E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6066          10.442          4.5729          4.5729
v  Velocity[Y]            -2.7915          7.3261      -0.0014373      -0.0014373
v  Velocity[Z]       -6.9287e-015     1.0081e-014    -6.1155e-018    -6.1155e-018
v  ǁVelocityǁ        0.00088779          10.442          5.2445          5.2445
v  Pressure               -48.881          16.589         -10.526         -10.526
v  nu_tilda           4.3653e-007       0.0042695       0.0013049       0.0013049
v  TempC                       21          73.063          21.821          21.821
v  TurbVisc           3.1958e-014        0.005032        0.001531        0.001531
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1331:        0.20980E+01

===============================================================


 INSTANT    0.133200000E+04   TIME STEP NUMBER            1332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75568E-02 0.89886E+00
   Friction velocity        uk    :  0.75568E-02 0.89886E+00
   Dimensionless distance   yplus :  0.60838E-01 0.72364E+01
   Friction thermal sca.    tstar : -0.26464E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45392E-01 0.53992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86081E-02      33   0.28997E-03   0.28635E+01 0.12037E+03 
c  Velocity[X]                                      0.13423E+01 
c  Velocity[Y]                                      0.15211E+01 
c  Velocity[Z]                                      0.12907E-29 
c  Pressure     0.12005E-06     506   0.96942E-08   0.11041E+00 0.14572E+04 
c  nu_tilda     0.56864E-05      32   0.16057E-04   0.25406E-06 0.14203E+03 
c  TempC        0.34724E+02      26   0.33270E-03   0.44982E+01 0.22290E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6035          10.442          4.5729          4.5729
v  Velocity[Y]            -2.7899          7.2918      -0.0014428      -0.0014428
v  Velocity[Z]       -6.9287e-015     9.6674e-015    -6.1104e-018    -6.1104e-018
v  ǁVelocityǁ         0.0011672          10.442          5.2443          5.2443
v  Pressure               -48.883          16.325         -10.611         -10.611
v  nu_tilda           4.3654e-007       0.0042695       0.0013054       0.0013054
v  TempC                       21          73.063          21.821          21.821
v  TurbVisc           3.1946e-014        0.005032       0.0015316       0.0015316
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1332:        0.21750E+01

===============================================================


 INSTANT    0.133300000E+04   TIME STEP NUMBER            1333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17233E-02 0.89755E+00
   Friction velocity        uk    :  0.17233E-02 0.89755E+00
   Dimensionless distance   yplus :  0.13874E-01 0.72259E+01
   Friction thermal sca.    tstar : -0.18977E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10351E-01 0.53913E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86104E-02      33   0.31990E-03   0.28319E+01 0.12021E+03 
c  Velocity[X]                                      0.13201E+01 
c  Velocity[Y]                                      0.15118E+01 
c  Velocity[Z]                                      0.10510E-29 
c  Pressure     0.10651E-06     506   0.94388E-08   0.96791E-01 0.12937E+04 
c  nu_tilda     0.56884E-05      32   0.57862E-05   0.25438E-06 0.14210E+03 
c  TempC        0.34734E+02      27   0.37342E-03   0.47565E+01 0.21834E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6003          10.441          4.5729          4.5729
v  Velocity[Y]            -2.7883           7.314      -0.0014481      -0.0014481
v  Velocity[Z]       -6.9287e-015      1.004e-014    -6.1107e-018    -6.1107e-018
v  ǁVelocityǁ        0.00058796          10.442          5.2441          5.2441
v  Pressure               -48.846          16.557         -10.544         -10.544
v  nu_tilda           4.3655e-007       0.0042695        0.001306        0.001306
v  TempC                       21          73.063          21.821          21.821
v  TurbVisc           3.1949e-014        0.005032       0.0015323       0.0015323
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1333:        0.21580E+01

===============================================================


 INSTANT    0.133400000E+04   TIME STEP NUMBER            1334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67817E-02 0.89856E+00
   Friction velocity        uk    :  0.67817E-02 0.89856E+00
   Dimensionless distance   yplus :  0.54597E-01 0.72341E+01
   Friction thermal sca.    tstar : -0.32985E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40736E-01 0.53974E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86127E-02      33   0.37010E-03   0.28750E+01 0.12061E+03 
c  Velocity[X]                                      0.13684E+01 
c  Velocity[Y]                                      0.15065E+01 
c  Velocity[Z]                                      0.13894E-29 
c  Pressure     0.13622E-06     520   0.98531E-08   0.12538E+00 0.13529E+04 
c  nu_tilda     0.56903E-05      32   0.16064E-04   0.25472E-06 0.14218E+03 
c  TempC        0.34744E+02      26   0.35331E-03   0.49997E+01 0.24328E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5971          10.441          4.5729          4.5729
v  Velocity[Y]            -2.7867          7.2938       -0.001453       -0.001453
v  Velocity[Z]       -6.9287e-015     9.6207e-015    -6.1052e-018    -6.1052e-018
v  ǁVelocityǁ          0.001815          10.441          5.2439          5.2439
v  Pressure               -48.842          16.315         -10.619         -10.619
v  nu_tilda           4.3659e-007       0.0042695       0.0013065       0.0013065
v  TempC                       21          73.063          21.822          21.822
v  TurbVisc           3.1952e-014        0.005032        0.001533        0.001533
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1334:        0.22200E+01

===============================================================


 INSTANT    0.133500000E+04   TIME STEP NUMBER            1335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51413E-02 0.89788E+00
   Friction velocity        uk    :  0.51413E-02 0.89788E+00
   Dimensionless distance   yplus :  0.41391E-01 0.72285E+01
   Friction thermal sca.    tstar : -0.65112E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30882E-01 0.53933E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86150E-02      33   0.24945E-03   0.29089E+01 0.12096E+03 
c  Velocity[X]                                      0.13754E+01 
c  Velocity[Y]                                      0.15335E+01 
c  Velocity[Z]                                      0.10836E-29 
c  Pressure     0.13422E-06     504   0.92070E-08   0.12066E+00 0.11361E+04 
c  nu_tilda     0.56923E-05      32   0.57732E-05   0.25503E-06 0.14226E+03 
c  TempC        0.34753E+02      27   0.38941E-03   0.47882E+01 0.23165E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.594          10.441          4.5729          4.5729
v  Velocity[Y]            -2.7851          7.3135      -0.0014577      -0.0014577
v  Velocity[Z]       -6.9287e-015     1.0047e-014    -6.1056e-018    -6.1056e-018
v  ǁVelocityǁ         0.0015914          10.441          5.2437          5.2437
v  Pressure               -48.807          16.515         -10.561         -10.561
v  nu_tilda           4.3654e-007       0.0042695       0.0013071       0.0013071
v  TempC                       21          73.063          21.822          21.822
v  TurbVisc           3.1963e-014        0.005032       0.0015336       0.0015336
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1335:        0.21500E+01

===============================================================


 INSTANT    0.133600000E+04   TIME STEP NUMBER            1336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44488E-02 0.89933E+00
   Friction velocity        uk    :  0.44488E-02 0.89933E+00
   Dimensionless distance   yplus :  0.35816E-01 0.72403E+01
   Friction thermal sca.    tstar : -0.34821E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26723E-01 0.54020E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86174E-02      33   0.28281E-03   0.28456E+01 0.12063E+03 
c  Velocity[X]                                      0.13257E+01 
c  Velocity[Y]                                      0.15199E+01 
c  Velocity[Z]                                      0.96799E-30 
c  Pressure     0.10134E-06     488   0.91969E-08   0.92370E-01 0.72395E+03 
c  nu_tilda     0.56942E-05      32   0.16059E-04   0.25538E-06 0.14233E+03 
c  TempC        0.34763E+02      26   0.35786E-03   0.50898E+01 0.25056E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5911          10.441          4.5729          4.5729
v  Velocity[Y]            -2.7835          7.3229      -0.0014626      -0.0014626
v  Velocity[Z]       -6.9287e-015     9.6383e-015    -6.0966e-018    -6.0966e-018
v  ǁVelocityǁ         0.0012561          10.441          5.2435          5.2435
v  Pressure               -48.805           16.42         -10.606         -10.606
v  nu_tilda           4.3645e-007       0.0042695       0.0013076       0.0013076
v  TempC                       21          73.063          21.822          21.822
v  TurbVisc           3.1949e-014        0.005032       0.0015343       0.0015343
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1336:        0.21220E+01

===============================================================


 INSTANT    0.133700000E+04   TIME STEP NUMBER            1337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10740E-01 0.89900E+00
   Friction velocity        uk    :  0.10740E-01 0.89900E+00
   Dimensionless distance   yplus :  0.86464E-01 0.72375E+01
   Friction thermal sca.    tstar : -0.30551E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64512E-01 0.54000E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86197E-02      33   0.34856E-03   0.28600E+01 0.12078E+03 
c  Velocity[X]                                      0.13422E+01 
c  Velocity[Y]                                      0.15178E+01 
c  Velocity[Z]                                      0.16859E-29 
c  Pressure     0.13447E-06     457   0.95699E-08   0.12359E+00 0.47128E+03 
c  nu_tilda     0.56962E-05      32   0.57697E-05   0.25569E-06 0.14241E+03 
c  TempC        0.34773E+02      27   0.39115E-03   0.52677E+01 0.24752E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.588          10.441          4.5729          4.5729
v  Velocity[Y]            -2.7819          7.2989      -0.0014668      -0.0014668
v  Velocity[Z]       -6.9287e-015     1.0008e-014    -6.0906e-018    -6.0906e-018
v  ǁVelocityǁ         0.0009235          10.441          5.2433          5.2433
v  Pressure               -48.764          16.414         -10.585         -10.585
v  nu_tilda           4.3651e-007       0.0042695       0.0013082       0.0013082
v  TempC                       21          73.063          21.822          21.822
v  TurbVisc           3.1924e-014        0.005032       0.0015349       0.0015349
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1337:        0.20380E+01

===============================================================


 INSTANT    0.133800000E+04   TIME STEP NUMBER            1338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26741E-02 0.89765E+00
   Friction velocity        uk    :  0.26741E-02 0.89765E+00
   Dimensionless distance   yplus :  0.21529E-01 0.72267E+01
   Friction thermal sca.    tstar : -0.91385E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16063E-01 0.53919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86221E-02      33   0.34267E-03   0.28931E+01 0.12121E+03 
c  Velocity[X]                                      0.13474E+01 
c  Velocity[Y]                                      0.15457E+01 
c  Velocity[Z]                                      0.11397E-29 
c  Pressure     0.13662E-06     425   0.96121E-08   0.12362E+00 0.25776E+03 
c  nu_tilda     0.56981E-05      32   0.16061E-04   0.25603E-06 0.14249E+03 
c  TempC        0.34783E+02      27   0.32333E-03   0.56179E+01 0.25462E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5849          10.441          4.5729          4.5729
v  Velocity[Y]            -2.7803          7.3184      -0.0014712      -0.0014712
v  Velocity[Z]       -6.9287e-015     9.5902e-015    -6.0869e-018    -6.0869e-018
v  ǁVelocityǁ        0.00060429          10.441          5.2431          5.2431
v  Pressure                -48.77          16.439         -10.606         -10.606
v  nu_tilda           4.3661e-007       0.0042695       0.0013087       0.0013087
v  TempC                       21          73.063          21.823          21.823
v  TurbVisc           3.1941e-014        0.005032       0.0015356       0.0015356
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1338:        0.19700E+01

===============================================================


 INSTANT    0.133900000E+04   TIME STEP NUMBER            1339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80245E-02 0.89888E+00
   Friction velocity        uk    :  0.80245E-02 0.89888E+00
   Dimensionless distance   yplus :  0.64603E-01 0.72366E+01
   Friction thermal sca.    tstar : -0.32605E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48201E-01 0.53993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86244E-02      33   0.30242E-03   0.29047E+01 0.12131E+03 
c  Velocity[X]                                      0.13709E+01 
c  Velocity[Y]                                      0.15338E+01 
c  Velocity[Z]                                      0.12062E-29 
c  Pressure     0.13283E-06     425   0.99097E-08   0.12042E+00 0.59471E+03 
c  nu_tilda     0.57001E-05      32   0.57533E-05   0.25635E-06 0.14256E+03 
c  TempC        0.34793E+02      26   0.27660E-03   0.47099E+01 0.23054E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5817           10.44          4.5729          4.5729
v  Velocity[Y]            -2.7787          7.2948      -0.0014751      -0.0014751
v  Velocity[Z]       -6.9287e-015     1.0014e-014    -6.0857e-018    -6.0857e-018
v  ǁVelocityǁ        0.00040904          10.441          5.2429          5.2429
v  Pressure               -48.726          16.314         -10.622         -10.622
v  nu_tilda           4.3674e-007       0.0042695       0.0013093       0.0013093
v  TempC                       21          73.063          21.823          21.823
v  TurbVisc           3.1969e-014        0.005032       0.0015362       0.0015362
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1339:        0.19810E+01

===============================================================


 INSTANT    0.134000000E+04   TIME STEP NUMBER            1340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50060E-02 0.89823E+00
   Friction velocity        uk    :  0.50060E-02 0.89823E+00
   Dimensionless distance   yplus :  0.40301E-01 0.72313E+01
   Friction thermal sca.    tstar : -0.65138E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30069E-01 0.53954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86267E-02      33   0.26097E-03   0.28797E+01 0.12125E+03 
c  Velocity[X]                                      0.13510E+01 
c  Velocity[Y]                                      0.15288E+01 
c  Velocity[Z]                                      0.12507E-29 
c  Pressure     0.11689E-06     394   0.92829E-08   0.10676E+00 0.31438E+03 
c  nu_tilda     0.57020E-05      32   0.16067E-04   0.25670E-06 0.14264E+03 
c  TempC        0.34802E+02      26   0.41945E-03   0.39271E+01 0.22172E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5786           10.44          4.5729          4.5729
v  Velocity[Y]            -2.7772          7.3209      -0.0014788      -0.0014788
v  Velocity[Z]       -6.9287e-015      9.607e-015    -6.0766e-018    -6.0766e-018
v  ǁVelocityǁ         0.0004411           10.44          5.2427          5.2427
v  Pressure               -48.727          16.404         -10.622         -10.622
v  nu_tilda           4.3684e-007       0.0042695       0.0013098       0.0013098
v  TempC                       21          73.062          21.823          21.823
v  TurbVisc           3.2008e-014        0.005032       0.0015369       0.0015369
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1340:        0.19010E+01

===============================================================


 INSTANT    0.134100000E+04   TIME STEP NUMBER            1341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87932E-02 0.89960E+00
   Friction velocity        uk    :  0.87932E-02 0.89960E+00
   Dimensionless distance   yplus :  0.70792E-01 0.72424E+01
   Friction thermal sca.    tstar : -0.37028E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52818E-01 0.54036E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86291E-02      33   0.34761E-03   0.28914E+01 0.12148E+03 
c  Velocity[X]                                      0.13372E+01 
c  Velocity[Y]                                      0.15543E+01 
c  Velocity[Z]                                      0.13137E-29 
c  Pressure     0.13227E-06     409   0.92899E-08   0.11823E+00 0.36196E+03 
c  nu_tilda     0.57040E-05      32   0.57419E-05   0.25701E-06 0.14271E+03 
c  TempC        0.34812E+02      26   0.33623E-03   0.60703E+01 0.28171E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5755           10.44          4.5729          4.5729
v  Velocity[Y]            -2.7756          7.3269      -0.0014825      -0.0014825
v  Velocity[Z]       -6.9287e-015      9.973e-015    -6.0773e-018    -6.0773e-018
v  ǁVelocityǁ        0.00068968           10.44          5.2425          5.2425
v  Pressure               -48.688          16.399         -10.612         -10.612
v  nu_tilda           4.3685e-007       0.0042695       0.0013104       0.0013104
v  TempC                       21          73.063          21.824          21.824
v  TurbVisc           3.2038e-014        0.005032       0.0015375       0.0015375
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1341:        0.19290E+01

===============================================================


 INSTANT    0.134200000E+04   TIME STEP NUMBER            1342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72238E-02 0.89938E+00
   Friction velocity        uk    :  0.72238E-02 0.89938E+00
   Dimensionless distance   yplus :  0.58156E-01 0.72406E+01
   Friction thermal sca.    tstar : -0.38296E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43391E-01 0.54023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86314E-02      33   0.31025E-03   0.29393E+01 0.12190E+03 
c  Velocity[X]                                      0.13952E+01 
c  Velocity[Y]                                      0.15442E+01 
c  Velocity[Z]                                      0.14224E-29 
c  Pressure     0.13319E-06     473   0.93800E-08   0.12253E+00 0.70220E+03 
c  nu_tilda     0.57059E-05      32   0.16061E-04   0.25736E-06 0.14279E+03 
c  TempC        0.34822E+02      27   0.37824E-03   0.42812E+01 0.22375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5725           10.44          4.5729          4.5729
v  Velocity[Y]             -2.774          7.2993      -0.0014858      -0.0014858
v  Velocity[Z]       -6.9287e-015     9.5585e-015    -6.0704e-018    -6.0704e-018
v  ǁVelocityǁ         0.0010651           10.44          5.2423          5.2423
v  Pressure               -48.689          16.278         -10.655         -10.655
v  nu_tilda            4.369e-007       0.0042695       0.0013109       0.0013109
v  TempC                       21          73.063          21.824          21.824
v  TurbVisc           3.2041e-014        0.005032       0.0015382       0.0015382
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1342:        0.20970E+01

===============================================================


 INSTANT    0.134300000E+04   TIME STEP NUMBER            1343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35292E-02 0.89806E+00
   Friction velocity        uk    :  0.35292E-02 0.89806E+00
   Dimensionless distance   yplus :  0.28413E-01 0.72300E+01
   Friction thermal sca.    tstar : -0.92870E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21199E-01 0.53944E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86337E-02      33   0.32042E-03   0.28943E+01 0.12170E+03 
c  Velocity[X]                                      0.13524E+01 
c  Velocity[Y]                                      0.15419E+01 
c  Velocity[Z]                                      0.11138E-29 
c  Pressure     0.11354E-06     488   0.89111E-08   0.10302E+00 0.10998E+04 
c  nu_tilda     0.57079E-05      32   0.57297E-05   0.25768E-06 0.14287E+03 
c  TempC        0.34832E+02      26   0.37517E-03   0.54270E+01 0.23475E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5695           10.44          4.5729          4.5729
v  Velocity[Y]            -2.7724          7.3237      -0.0014888      -0.0014888
v  Velocity[Z]       -6.9287e-015     9.9791e-015    -6.0629e-018    -6.0629e-018
v  ǁVelocityǁ         0.0013196           10.44          5.2421          5.2421
v  Pressure               -48.649          16.463         -10.596         -10.596
v  nu_tilda           4.3691e-007       0.0042695       0.0013115       0.0013115
v  TempC                       21          73.062          21.824          21.824
v  TurbVisc           3.2054e-014        0.005032       0.0015389       0.0015389
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1343:        0.21260E+01

===============================================================


 INSTANT    0.134400000E+04   TIME STEP NUMBER            1344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83629E-02 0.89912E+00
   Friction velocity        uk    :  0.83629E-02 0.89912E+00
   Dimensionless distance   yplus :  0.67327E-01 0.72385E+01
   Friction thermal sca.    tstar : -0.39034E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50234E-01 0.54007E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86361E-02      33   0.32860E-03   0.29151E+01 0.12196E+03 
c  Velocity[X]                                      0.13580E+01 
c  Velocity[Y]                                      0.15570E+01 
c  Velocity[Z]                                      0.14339E-29 
c  Pressure     0.12545E-06     489   0.96044E-08   0.11346E+00 0.15928E+04 
c  nu_tilda     0.57098E-05      32   0.16066E-04   0.25803E-06 0.14295E+03 
c  TempC        0.34841E+02      27   0.34327E-03   0.51314E+01 0.24385E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5663          10.439          4.5729          4.5729
v  Velocity[Y]            -2.7708          7.2951      -0.0014917      -0.0014917
v  Velocity[Z]       -6.9287e-015     9.5732e-015    -6.0638e-018    -6.0638e-018
v  ǁVelocityǁ        0.00064652          10.439          5.2419          5.2419
v  Pressure                -48.65          16.186         -10.688         -10.688
v  nu_tilda           4.3695e-007       0.0042695        0.001312        0.001312
v  TempC                       21          73.062          21.825          21.825
v  TurbVisc           3.2057e-014        0.005032       0.0015395       0.0015395
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1344:        0.21190E+01

===============================================================


 INSTANT    0.134500000E+04   TIME STEP NUMBER            1345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53245E-02 0.89855E+00
   Friction velocity        uk    :  0.53245E-02 0.89855E+00
   Dimensionless distance   yplus :  0.42866E-01 0.72339E+01
   Friction thermal sca.    tstar : -0.43981E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31983E-01 0.53973E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86384E-02      33   0.28432E-03   0.29221E+01 0.12209E+03 
c  Velocity[X]                                      0.13673E+01 
c  Velocity[Y]                                      0.15548E+01 
c  Velocity[Z]                                      0.11230E-29 
c  Pressure     0.11649E-06     521   0.98568E-08   0.10480E+00 0.13180E+04 
c  nu_tilda     0.57118E-05      32   0.57211E-05   0.25835E-06 0.14302E+03 
c  TempC        0.34851E+02      27   0.40088E-03   0.43116E+01 0.22477E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5631          10.439          4.5729          4.5729
v  Velocity[Y]            -2.7692          7.3245      -0.0014944      -0.0014944
v  Velocity[Z]       -6.9287e-015     9.9374e-015    -6.0625e-018    -6.0625e-018
v  ǁVelocityǁ         0.0016358          10.439          5.2417          5.2417
v  Pressure               -48.612          16.419          -10.62          -10.62
v  nu_tilda           4.3693e-007       0.0042695       0.0013126       0.0013126
v  TempC                       21          73.062          21.825          21.825
v  TurbVisc           3.2069e-014        0.005032       0.0015402       0.0015402
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1345:        0.22030E+01

===============================================================


 INSTANT    0.134600000E+04   TIME STEP NUMBER            1346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71199E-02 0.89982E+00
   Friction velocity        uk    :  0.71199E-02 0.89982E+00
   Dimensionless distance   yplus :  0.57320E-01 0.72442E+01
   Friction thermal sca.    tstar : -0.45994E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42767E-01 0.54050E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86407E-02      33   0.32811E-03   0.28832E+01 0.12195E+03 
c  Velocity[X]                                      0.13329E+01 
c  Velocity[Y]                                      0.15503E+01 
c  Velocity[Z]                                      0.10035E-29 
c  Pressure     0.10503E-06     474   0.93698E-08   0.94626E-01 0.80475E+03 
c  nu_tilda     0.57138E-05      32   0.16061E-04   0.25871E-06 0.14310E+03 
c  TempC        0.34861E+02      26   0.33353E-03   0.46913E+01 0.23938E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5599          10.439          4.5729          4.5729
v  Velocity[Y]            -2.7677          7.3338      -0.0014968      -0.0014968
v  Velocity[Z]       -6.9287e-015     9.5257e-015    -6.0467e-018    -6.0467e-018
v  ǁVelocityǁ         0.0012366          10.439          5.2415          5.2415
v  Pressure               -48.609          16.308         -10.669         -10.669
v  nu_tilda           4.3688e-007       0.0042695       0.0013131       0.0013131
v  TempC                       21          73.063          21.825          21.825
v  TurbVisc           3.2065e-014        0.005032       0.0015408       0.0015408
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1346:        0.20790E+01

===============================================================


 INSTANT    0.134700000E+04   TIME STEP NUMBER            1347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91797E-02 0.89943E+00
   Friction velocity        uk    :  0.91797E-02 0.89943E+00
   Dimensionless distance   yplus :  0.73903E-01 0.72410E+01
   Friction thermal sca.    tstar : -0.35788E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55140E-01 0.54026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86430E-02      33   0.34431E-03   0.29419E+01 0.12241E+03 
c  Velocity[X]                                      0.13724E+01 
c  Velocity[Y]                                      0.15695E+01 
c  Velocity[Z]                                      0.11921E-29 
c  Pressure     0.12760E-06     440   0.91480E-08   0.11574E+00 0.40088E+03 
c  nu_tilda     0.57157E-05      32   0.57173E-05   0.25903E-06 0.14318E+03 
c  TempC        0.34871E+02      26   0.35339E-03   0.50924E+01 0.23064E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5569          10.439          4.5729          4.5729
v  Velocity[Y]            -2.7661          7.3026       -0.001499       -0.001499
v  Velocity[Z]       -6.9287e-015     9.9429e-015    -6.0518e-018    -6.0518e-018
v  ǁVelocityǁ        0.00087387          10.439          5.2412          5.2412
v  Pressure               -48.573          16.281         -10.654         -10.654
v  nu_tilda           4.3687e-007       0.0042695       0.0013137       0.0013137
v  TempC                       21          73.062          21.826          21.826
v  TurbVisc           3.2049e-014        0.005032       0.0015415       0.0015415
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1347:        0.19990E+01

===============================================================


 INSTANT    0.134800000E+04   TIME STEP NUMBER            1348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52174E-02 0.89820E+00
   Friction velocity        uk    :  0.52174E-02 0.89820E+00
   Dimensionless distance   yplus :  0.42004E-01 0.72311E+01
   Friction thermal sca.    tstar : -0.66600E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31339E-01 0.53952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86453E-02      33   0.30174E-03   0.29542E+01 0.12267E+03 
c  Velocity[X]                                      0.13870E+01 
c  Velocity[Y]                                      0.15672E+01 
c  Velocity[Z]                                      0.14687E-29 
c  Pressure     0.13594E-06     424   0.91189E-08   0.12214E+00 0.34257E+03 
c  nu_tilda     0.57177E-05      32   0.16065E-04   0.25938E-06 0.14326E+03 
c  TempC        0.34881E+02      27   0.45447E-03   0.46096E+01 0.21993E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5539          10.438          4.5729          4.5729
v  Velocity[Y]            -2.7645          7.3241      -0.0015012      -0.0015012
v  Velocity[Z]       -6.9287e-015     9.5408e-015    -6.0403e-018    -6.0403e-018
v  ǁVelocityǁ        0.00052263          10.439           5.241           5.241
v  Pressure               -48.573          16.287         -10.679         -10.679
v  nu_tilda           4.3689e-007       0.0042695       0.0013142       0.0013142
v  TempC                       21          73.063          21.826          21.826
v  TurbVisc           3.2047e-014        0.005032       0.0015421       0.0015421
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1348:        0.19660E+01

===============================================================


 INSTANT    0.134900000E+04   TIME STEP NUMBER            1349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53325E-02 0.89942E+00
   Friction velocity        uk    :  0.53325E-02 0.89942E+00
   Dimensionless distance   yplus :  0.42930E-01 0.72410E+01
   Friction thermal sca.    tstar : -0.62463E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32031E-01 0.54026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86476E-02      33   0.32059E-03   0.29305E+01 0.12256E+03 
c  Velocity[X]                                      0.13668E+01 
c  Velocity[Y]                                      0.15638E+01 
c  Velocity[Z]                                      0.13185E-29 
c  Pressure     0.13080E-06     442   0.92645E-08   0.11873E+00 0.49051E+03 
c  nu_tilda     0.57197E-05      32   0.56973E-05   0.25970E-06 0.14333E+03 
c  TempC        0.34890E+02      27   0.31829E-03   0.48722E+01 0.23205E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5508          10.438          4.5729          4.5729
v  Velocity[Y]            -2.7629           7.305      -0.0015026      -0.0015026
v  Velocity[Z]       -6.9287e-015     9.9017e-015    -6.0452e-018    -6.0452e-018
v  ǁVelocityǁ        0.00040396          10.438          5.2408          5.2408
v  Pressure               -48.531            16.3         -10.656         -10.656
v  nu_tilda           4.3689e-007       0.0042695       0.0013148       0.0013148
v  TempC                       21          73.062          21.826          21.826
v  TurbVisc           3.2051e-014        0.005032       0.0015428       0.0015428
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1349:        0.20170E+01

===============================================================


 INSTANT    0.135000000E+04   TIME STEP NUMBER            1350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25685E-02 0.89846E+00
   Friction velocity        uk    :  0.25685E-02 0.89846E+00
   Dimensionless distance   yplus :  0.20678E-01 0.72332E+01
   Friction thermal sca.    tstar : -0.12779E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15428E-01 0.53968E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86500E-02      33   0.24157E-03   0.29371E+01 0.12274E+03 
c  Velocity[X]                                      0.13575E+01 
c  Velocity[Y]                                      0.15796E+01 
c  Velocity[Z]                                      0.11162E-29 
c  Pressure     0.12356E-06     457   0.97538E-08   0.11047E+00 0.66633E+03 
c  nu_tilda     0.57216E-05      32   0.16068E-04   0.26005E-06 0.14341E+03 
c  TempC        0.34900E+02      27   0.28873E-03   0.31877E+01 0.18971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5477          10.438          4.5729          4.5729
v  Velocity[Y]            -2.7613          7.3248      -0.0015042      -0.0015042
v  Velocity[Z]       -6.9287e-015     9.4916e-015    -6.0492e-018    -6.0492e-018
v  ǁVelocityǁ        0.00064764          10.438          5.2406          5.2406
v  Pressure               -48.535          16.229         -10.702         -10.702
v  nu_tilda           4.3692e-007       0.0042695       0.0013154       0.0013154
v  TempC                       21          73.062          21.827          21.827
v  TurbVisc           3.2052e-014        0.005032       0.0015434       0.0015434
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1350:        0.20290E+01

===============================================================


 INSTANT    0.135100000E+04   TIME STEP NUMBER            1351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39771E-02 0.90015E+00
   Friction velocity        uk    :  0.39771E-02 0.90015E+00
   Dimensionless distance   yplus :  0.32018E-01 0.72468E+01
   Friction thermal sca.    tstar : -0.82515E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23889E-01 0.54069E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86523E-02      33   0.32460E-03   0.29120E+01 0.12270E+03 
c  Velocity[X]                                      0.13338E+01 
c  Velocity[Y]                                      0.15783E+01 
c  Velocity[Z]                                      0.11496E-29 
c  Pressure     0.10114E-06     488   0.95767E-08   0.91292E-01 0.89436E+03 
c  nu_tilda     0.57236E-05      32   0.56897E-05   0.26038E-06 0.14349E+03 
c  TempC        0.34910E+02      26   0.44981E-03   0.41819E+01 0.22152E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5445          10.438          4.5729          4.5729
v  Velocity[Y]            -2.7598          7.3374      -0.0015053      -0.0015053
v  Velocity[Z]       -6.9287e-015     9.9065e-015    -6.0473e-018    -6.0473e-018
v  ǁVelocityǁ         0.0010233          10.438          5.2404          5.2404
v  Pressure               -48.497          16.364         -10.655         -10.655
v  nu_tilda           4.3693e-007       0.0042695       0.0013159       0.0013159
v  TempC                       21          73.062          21.827          21.827
v  TurbVisc            3.206e-014        0.005032       0.0015441       0.0015441
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1351:        0.21190E+01

===============================================================


 INSTANT    0.135200000E+04   TIME STEP NUMBER            1352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97573E-02 0.89976E+00
   Friction velocity        uk    :  0.97573E-02 0.89976E+00
   Dimensionless distance   yplus :  0.78553E-01 0.72437E+01
   Friction thermal sca.    tstar : -0.35565E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58610E-01 0.54046E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86546E-02      33   0.36068E-03   0.29799E+01 0.12323E+03 
c  Velocity[X]                                      0.14011E+01 
c  Velocity[Y]                                      0.15787E+01 
c  Velocity[Z]                                      0.14715E-29 
c  Pressure     0.13932E-06     506   0.96258E-08   0.12699E+00 0.12602E+04 
c  nu_tilda     0.57256E-05      32   0.16062E-04   0.26074E-06 0.14357E+03 
c  TempC        0.34920E+02      26   0.44218E-03   0.62647E+01 0.28588E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5413          10.437          4.5729          4.5729
v  Velocity[Y]            -2.7582          7.3113      -0.0015062      -0.0015062
v  Velocity[Z]       -6.9287e-015     9.5073e-015    -6.0487e-018    -6.0487e-018
v  ǁVelocityǁ         0.0014623          10.438          5.2402          5.2402
v  Pressure               -48.493          16.134         -10.725         -10.725
v  nu_tilda           4.3703e-007       0.0042695       0.0013165       0.0013165
v  TempC                       21          73.062          21.827          21.827
v  TurbVisc           3.2065e-014        0.005032       0.0015447       0.0015447
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1352:        0.21560E+01

===============================================================


 INSTANT    0.135300000E+04   TIME STEP NUMBER            1353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78831E-02 0.89845E+00
   Friction velocity        uk    :  0.78831E-02 0.89845E+00
   Dimensionless distance   yplus :  0.63465E-01 0.72331E+01
   Friction thermal sca.    tstar : -0.42177E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47352E-01 0.53967E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86569E-02      33   0.31287E-03   0.30044E+01 0.12350E+03 
c  Velocity[X]                                      0.14019E+01 
c  Velocity[Y]                                      0.16025E+01 
c  Velocity[Z]                                      0.10967E-29 
c  Pressure     0.13669E-06     489   0.99984E-08   0.12075E+00 0.11750E+04 
c  nu_tilda     0.57275E-05      32   0.56790E-05   0.26107E-06 0.14365E+03 
c  TempC        0.34929E+02      27   0.30284E-03   0.61052E+01 0.25191E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5383          10.437          4.5729          4.5729
v  Velocity[Y]            -2.7566          7.3257       -0.001507       -0.001507
v  Velocity[Z]       -6.9287e-015     9.8648e-015    -6.0512e-018    -6.0512e-018
v  ǁVelocityǁ         0.0019107          10.437          5.2399          5.2399
v  Pressure               -48.458          16.336         -10.665         -10.665
v  nu_tilda           4.3708e-007       0.0042695        0.001317        0.001317
v  TempC                       21          73.062          21.828          21.828
v  TurbVisc           3.2092e-014        0.005032       0.0015454       0.0015454
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1353:        0.21140E+01

===============================================================


 INSTANT    0.135400000E+04   TIME STEP NUMBER            1354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29169E-02 0.89963E+00
   Friction velocity        uk    :  0.29169E-02 0.89963E+00
   Dimensionless distance   yplus :  0.23483E-01 0.72427E+01
   Friction thermal sca.    tstar : -0.55250E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17521E-01 0.54038E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86592E-02      33   0.29732E-03   0.29677E+01 0.12336E+03 
c  Velocity[X]                                      0.13753E+01 
c  Velocity[Y]                                      0.15924E+01 
c  Velocity[Z]                                      0.11198E-29 
c  Pressure     0.12035E-06     506   0.98370E-08   0.10982E+00 0.10905E+04 
c  nu_tilda     0.57295E-05      32   0.16069E-04   0.26142E-06 0.14373E+03 
c  TempC        0.34939E+02      27   0.43172E-03   0.36206E+01 0.20671E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5353          10.437          4.5729          4.5729
v  Velocity[Y]             -2.755          7.3041      -0.0015076      -0.0015076
v  Velocity[Z]       -6.9287e-015     9.4575e-015    -6.0551e-018    -6.0551e-018
v  ǁVelocityǁ         0.0013736          10.437          5.2397          5.2397
v  Pressure               -48.457          16.148         -10.728         -10.728
v  nu_tilda           4.3717e-007       0.0042695       0.0013176       0.0013176
v  TempC                       21          73.062          21.828          21.828
v  TurbVisc           3.2107e-014        0.005032        0.001546        0.001546
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1354:        0.21430E+01

===============================================================


 INSTANT    0.135500000E+04   TIME STEP NUMBER            1355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81416E-02 0.89892E+00
   Friction velocity        uk    :  0.81416E-02 0.89892E+00
   Dimensionless distance   yplus :  0.65546E-01 0.72369E+01
   Friction thermal sca.    tstar : -0.40301E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48905E-01 0.53996E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86615E-02      33   0.29594E-03   0.29545E+01 0.12336E+03 
c  Velocity[X]                                      0.13649E+01 
c  Velocity[Y]                                      0.15896E+01 
c  Velocity[Z]                                      0.12899E-29 
c  Pressure     0.12076E-06     488   0.90106E-08   0.10765E+00 0.87528E+03 
c  nu_tilda     0.57315E-05      32   0.56679E-05   0.26175E-06 0.14381E+03 
c  TempC        0.34949E+02      27   0.30080E-03   0.49368E+01 0.23128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5322          10.437          4.5729          4.5729
v  Velocity[Y]            -2.7534          7.3328       -0.001508       -0.001508
v  Velocity[Z]        -9.123e-015     9.8686e-015    -6.0685e-018    -6.0685e-018
v  ǁVelocityǁ        0.00096883          10.437          5.2395          5.2395
v  Pressure               -48.414          16.299         -10.683         -10.683
v  nu_tilda           4.3722e-007       0.0042695       0.0013181       0.0013181
v  TempC                       21          73.062          21.828          21.828
v  TurbVisc           3.2134e-014        0.005032       0.0015467       0.0015467
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1355:        0.21070E+01

===============================================================


 INSTANT    0.135600000E+04   TIME STEP NUMBER            1356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68285E-02 0.90019E+00
   Friction velocity        uk    :  0.68285E-02 0.90019E+00
   Dimensionless distance   yplus :  0.54974E-01 0.72472E+01
   Friction thermal sca.    tstar : -0.50815E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41017E-01 0.54072E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86638E-02      33   0.32776E-03   0.29859E+01 0.12375E+03 
c  Velocity[X]                                      0.13718E+01 
c  Velocity[Y]                                      0.16141E+01 
c  Velocity[Z]                                      0.12354E-29 
c  Pressure     0.15247E-06     456   0.99596E-08   0.13415E+00 0.60921E+03 
c  nu_tilda     0.57335E-05      32   0.16062E-04   0.26210E-06 0.14389E+03 
c  TempC        0.34958E+02      27   0.36852E-03   0.32755E+01 0.18878E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.529          10.436          4.5729          4.5729
v  Velocity[Y]            -2.7519          7.3353      -0.0015079      -0.0015079
v  Velocity[Z]       -8.6073e-015     9.4719e-015      -6.08e-018      -6.08e-018
v  ǁVelocityǁ        0.00069763          10.436          5.2393          5.2393
v  Pressure               -48.419          16.205         -10.723         -10.723
v  nu_tilda            4.372e-007       0.0042695       0.0013187       0.0013187
v  TempC                       21          73.062          21.829          21.829
v  TurbVisc           3.2148e-014        0.005032       0.0015473       0.0015473
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1356:        0.21250E+01

===============================================================


 INSTANT    0.135700000E+04   TIME STEP NUMBER            1357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31412E-02 0.90021E+00
   Friction velocity        uk    :  0.31412E-02 0.90021E+00
   Dimensionless distance   yplus :  0.25289E-01 0.72473E+01
   Friction thermal sca.    tstar : -0.10583E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18868E-01 0.54073E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86661E-02      33   0.28599E-03   0.29992E+01 0.12393E+03 
c  Velocity[X]                                      0.13951E+01 
c  Velocity[Y]                                      0.16041E+01 
c  Velocity[Z]                                      0.13462E-29 
c  Pressure     0.14613E-06     424   0.97414E-08   0.13126E+00 0.38176E+03 
c  nu_tilda     0.57354E-05      32   0.56634E-05   0.26244E-06 0.14396E+03 
c  TempC        0.34968E+02      28   0.32374E-03   0.36239E+01 0.21028E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5259          10.436          4.5729          4.5729
v  Velocity[Y]            -2.7503          7.3111      -0.0015078      -0.0015078
v  Velocity[Z]       -1.0243e-014     9.8269e-015    -6.0967e-018    -6.0967e-018
v  ǁVelocityǁ        0.00043141          10.436          5.2391          5.2391
v  Pressure               -48.376          16.186         -10.714         -10.714
v  nu_tilda           4.3725e-007       0.0042695       0.0013192       0.0013192
v  TempC                       21          73.062          21.829          21.829
v  TurbVisc           3.2144e-014        0.005032        0.001548        0.001548
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1357:        0.22690E+01

===============================================================


 INSTANT    0.135800000E+04   TIME STEP NUMBER            1358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58509E-02 0.89870E+00
   Friction velocity        uk    :  0.58509E-02 0.89870E+00
   Dimensionless distance   yplus :  0.47104E-01 0.72352E+01
   Friction thermal sca.    tstar : -0.56051E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35145E-01 0.53983E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86684E-02      33   0.34920E-03   0.29633E+01 0.12376E+03 
c  Velocity[X]                                      0.13629E+01 
c  Velocity[Y]                                      0.16003E+01 
c  Velocity[Z]                                      0.13847E-29 
c  Pressure     0.11783E-06     393   0.95715E-08   0.10464E+00 0.20429E+03 
c  nu_tilda     0.57374E-05      32   0.16065E-04   0.26280E-06 0.14404E+03 
c  TempC        0.34978E+02      26   0.31350E-03   0.47995E+01 0.23763E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5227          10.436          4.5729          4.5729
v  Velocity[Y]            -2.7487          7.3332      -0.0015072      -0.0015072
v  Velocity[Z]       -9.4879e-015     9.4228e-015    -6.1044e-018    -6.1044e-018
v  ǁVelocityǁ         0.0005686          10.436          5.2388          5.2388
v  Pressure               -48.383          16.221         -10.727         -10.727
v  nu_tilda            4.373e-007       0.0042695       0.0013198       0.0013198
v  TempC                       21          73.062          21.829          21.829
v  TurbVisc           3.2158e-014        0.005032       0.0015487       0.0015487
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1358:        0.19700E+01

===============================================================


 INSTANT    0.135900000E+04   TIME STEP NUMBER            1359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34157E-02 0.89991E+00
   Friction velocity        uk    :  0.34157E-02 0.89991E+00
   Dimensionless distance   yplus :  0.27499E-01 0.72449E+01
   Friction thermal sca.    tstar : -0.96723E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20517E-01 0.54055E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86707E-02      33   0.35151E-03   0.30110E+01 0.12420E+03 
c  Velocity[X]                                      0.13863E+01 
c  Velocity[Y]                                      0.16247E+01 
c  Velocity[Z]                                      0.13096E-29 
c  Pressure     0.13824E-06     394   0.97091E-08   0.12281E+00 0.52059E+03 
c  nu_tilda     0.57394E-05      32   0.56462E-05   0.26314E-06 0.14412E+03 
c  TempC        0.34988E+02      27   0.39713E-03   0.44533E+01 0.22089E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5197          10.435          4.5729          4.5729
v  Velocity[Y]            -2.7472          7.3076      -0.0015063      -0.0015063
v  Velocity[Z]        -1.102e-014     9.8301e-015    -6.1203e-018    -6.1203e-018
v  ǁVelocityǁ        0.00093123          10.435          5.2386          5.2386
v  Pressure               -48.338          16.123         -10.736         -10.736
v  nu_tilda            4.373e-007       0.0042695       0.0013203       0.0013203
v  TempC                       21          73.061           21.83           21.83
v  TurbVisc           3.2171e-014        0.005032       0.0015493       0.0015493
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1359:        0.19040E+01

===============================================================


 INSTANT    0.136000000E+04   TIME STEP NUMBER            1360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89414E-02 0.89922E+00
   Friction velocity        uk    :  0.89414E-02 0.89922E+00
   Dimensionless distance   yplus :  0.71984E-01 0.72393E+01
   Friction thermal sca.    tstar : -0.36672E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53708E-01 0.54013E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86730E-02      33   0.25636E-03   0.30318E+01 0.12447E+03 
c  Velocity[X]                                      0.14163E+01 
c  Velocity[Y]                                      0.16155E+01 
c  Velocity[Z]                                      0.10337E-29 
c  Pressure     0.13016E-06     328   0.97345E-08   0.11567E+00 0.23612E+03 
c  nu_tilda     0.57414E-05      32   0.16069E-04   0.26349E-06 0.14420E+03 
c  TempC        0.34997E+02      27   0.38232E-03   0.65803E+01 0.27474E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5166          10.435          4.5729          4.5729
v  Velocity[Y]            -2.7456          7.3348      -0.0015053      -0.0015053
v  Velocity[Z]       -1.1397e-014     9.4352e-015    -6.1264e-018    -6.1264e-018
v  ǁVelocityǁ        0.00076759          10.435          5.2384          5.2384
v  Pressure               -48.342          16.182         -10.744         -10.744
v  nu_tilda           4.3732e-007       0.0042695       0.0013209       0.0013209
v  TempC                       21          73.061           21.83           21.83
v  TurbVisc           3.2173e-014        0.005032         0.00155         0.00155
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1360:        0.17820E+01

===============================================================


 INSTANT    0.136100000E+04   TIME STEP NUMBER            1361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77829E-03 0.90089E+00
   Friction velocity        uk    :  0.77829E-03 0.90089E+00
   Dimensionless distance   yplus :  0.62657E-02 0.72528E+01
   Friction thermal sca.    tstar : -0.72202E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46749E-02 0.54114E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86753E-02      33   0.31944E-03   0.29713E+01 0.12416E+03 
c  Velocity[X]                                      0.13600E+01 
c  Velocity[Y]                                      0.16112E+01 
c  Velocity[Z]                                      0.12895E-29 
c  Pressure     0.11611E-06     472   0.93444E-08   0.10244E+00 0.56914E+03 
c  nu_tilda     0.57434E-05      32   0.56375E-05   0.26383E-06 0.14428E+03 
c  TempC        0.35007E+02      26   0.29773E-03   0.64347E+01 0.27360E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5136          10.435          4.5729          4.5729
v  Velocity[Y]             -2.744          7.3481      -0.0015036      -0.0015036
v  Velocity[Z]       -1.3311e-014     9.7861e-015     -6.145e-018     -6.145e-018
v  ǁVelocityǁ         0.0019128          10.435          5.2381          5.2381
v  Pressure               -48.299          16.249         -10.716         -10.716
v  nu_tilda           4.3728e-007       0.0042695       0.0013214       0.0013214
v  TempC                       21          73.061           21.83           21.83
v  TurbVisc           3.2177e-014        0.005032       0.0015506       0.0015506
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1361:        0.21060E+01

===============================================================


 INSTANT    0.136200000E+04   TIME STEP NUMBER            1362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81085E-02 0.90032E+00
   Friction velocity        uk    :  0.81085E-02 0.90032E+00
   Dimensionless distance   yplus :  0.65279E-01 0.72482E+01
   Friction thermal sca.    tstar : -0.40175E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48706E-01 0.54080E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86776E-02      33   0.33788E-03   0.30188E+01 0.12458E+03 
c  Velocity[X]                                      0.13908E+01 
c  Velocity[Y]                                      0.16280E+01 
c  Velocity[Z]                                      0.12152E-29 
c  Pressure     0.13095E-06     504   0.95750E-08   0.11629E+00 0.10124E+04 
c  nu_tilda     0.57453E-05      32   0.16062E-04   0.26419E-06 0.14436E+03 
c  TempC        0.35017E+02      26   0.48866E-03   0.54488E+01 0.24901E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5104          10.434          4.5729          4.5729
v  Velocity[Y]            -2.7425          7.3137      -0.0015021      -0.0015021
v  Velocity[Z]       -1.2355e-014     9.4225e-015    -6.1567e-018    -6.1567e-018
v  ǁVelocityǁ         0.0015803          10.434          5.2379          5.2379
v  Pressure               -48.303          16.057         -10.775         -10.775
v  nu_tilda            4.373e-007       0.0042695        0.001322        0.001322
v  TempC                       21          73.061           21.83           21.83
v  TurbVisc           3.2166e-014        0.005032       0.0015513       0.0015513
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1362:        0.21560E+01

===============================================================


 INSTANT    0.136300000E+04   TIME STEP NUMBER            1363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93765E-02 0.89918E+00
   Friction velocity        uk    :  0.93765E-02 0.89918E+00
   Dimensionless distance   yplus :  0.75487E-01 0.72391E+01
   Friction thermal sca.    tstar : -0.34986E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56322E-01 0.54011E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86799E-02      33   0.29309E-03   0.30263E+01 0.12475E+03 
c  Velocity[X]                                      0.13975E+01 
c  Velocity[Y]                                      0.16288E+01 
c  Velocity[Z]                                      0.10692E-29 
c  Pressure     0.12346E-06     505   0.99821E-08   0.10973E+00 0.12170E+04 
c  nu_tilda     0.57473E-05      32   0.56307E-05   0.26453E-06 0.14444E+03 
c  TempC        0.35026E+02      27   0.37756E-03   0.71098E+01 0.30548E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5072          10.434          4.5729          4.5729
v  Velocity[Y]            -2.7409          7.3388      -0.0015002      -0.0015002
v  Velocity[Z]       -1.3721e-014     9.7875e-015    -6.1757e-018    -6.1757e-018
v  ǁVelocityǁ         0.0010985          10.434          5.2377          5.2377
v  Pressure               -48.263          16.275         -10.712         -10.712
v  nu_tilda           4.3732e-007       0.0042695       0.0013225       0.0013225
v  TempC                       21          73.061          21.831          21.831
v  TurbVisc           3.2172e-014        0.005032       0.0015519       0.0015519
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1363:        0.21570E+01

===============================================================


 INSTANT    0.136400000E+04   TIME STEP NUMBER            1364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61464E-02 0.90017E+00
   Friction velocity        uk    :  0.61464E-02 0.90017E+00
   Dimensionless distance   yplus :  0.49482E-01 0.72470E+01
   Friction thermal sca.    tstar : -0.53173E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36919E-01 0.54071E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86822E-02      33   0.33806E-03   0.30119E+01 0.12474E+03 
c  Velocity[X]                                      0.13876E+01 
c  Velocity[Y]                                      0.16243E+01 
c  Velocity[Z]                                      0.14816E-29 
c  Pressure     0.11807E-06     536   0.90135E-08   0.10576E+00 0.15779E+04 
c  nu_tilda     0.57493E-05      32   0.16066E-04   0.26489E-06 0.14452E+03 
c  TempC        0.35036E+02      27   0.36381E-03   0.54873E+01 0.24028E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5041          10.434          4.5729          4.5729
v  Velocity[Y]            -2.7393           7.317      -0.0014983      -0.0014983
v  Velocity[Z]       -1.3085e-014     9.3947e-015    -6.1855e-018    -6.1855e-018
v  ǁVelocityǁ        0.00067591          10.434          5.2375          5.2375
v  Pressure               -48.263          16.001         -10.802         -10.802
v  nu_tilda           4.3741e-007       0.0042695       0.0013231       0.0013231
v  TempC                       21          73.061          21.831          21.831
v  TurbVisc           3.2177e-014        0.005032       0.0015526       0.0015526
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1364:        0.22200E+01

===============================================================


 INSTANT    0.136500000E+04   TIME STEP NUMBER            1365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95368E-02 0.89933E+00
   Friction velocity        uk    :  0.95368E-02 0.89933E+00
   Dimensionless distance   yplus :  0.76777E-01 0.72403E+01
   Friction thermal sca.    tstar : -0.34388E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57285E-01 0.54020E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86845E-02      33   0.30394E-03   0.30345E+01 0.12498E+03 
c  Velocity[X]                                      0.13927E+01 
c  Velocity[Y]                                      0.16418E+01 
c  Velocity[Z]                                      0.12995E-29 
c  Pressure     0.12733E-06     536   0.95670E-08   0.11136E+00 0.12637E+04 
c  nu_tilda     0.57513E-05      32   0.56191E-05   0.26523E-06 0.14460E+03 
c  TempC        0.35046E+02      26   0.39333E-03   0.50969E+01 0.24574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5011          10.433          4.5729          4.5729
v  Velocity[Y]            -2.7377          7.3373      -0.0014955      -0.0014955
v  Velocity[Z]        -1.454e-014      9.744e-015    -6.2017e-018    -6.2017e-018
v  ǁVelocityǁ        0.00042594          10.433          5.2372          5.2372
v  Pressure               -48.224          16.219         -10.736         -10.736
v  nu_tilda           4.3746e-007       0.0042695       0.0013236       0.0013236
v  TempC                       21          73.061          21.831          21.831
v  TurbVisc           3.2204e-014        0.005032       0.0015532       0.0015532
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1365:        0.22320E+01

===============================================================


 INSTANT    0.136600000E+04   TIME STEP NUMBER            1366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54765E-02 0.90052E+00
   Friction velocity        uk    :  0.54765E-02 0.90052E+00
   Dimensionless distance   yplus :  0.44090E-01 0.72498E+01
   Friction thermal sca.    tstar : -0.63787E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32896E-01 0.54091E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86868E-02      33   0.32257E-03   0.30004E+01 0.12489E+03 
c  Velocity[X]                                      0.13645E+01 
c  Velocity[Y]                                      0.16359E+01 
c  Velocity[Z]                                      0.11014E-29 
c  Pressure     0.10772E-06     473   0.95656E-08   0.95068E-01 0.72776E+03 
c  nu_tilda     0.57533E-05      32   0.16062E-04   0.26559E-06 0.14468E+03 
c  TempC        0.35056E+02      26   0.35277E-03   0.54904E+01 0.24742E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.498          10.433          4.5729          4.5729
v  Velocity[Y]            -2.7362           7.345      -0.0014926      -0.0014926
v  Velocity[Z]       -1.5067e-014     9.3759e-015    -6.2151e-018    -6.2151e-018
v  ǁVelocityǁ        0.00070709          10.433           5.237           5.237
v  Pressure               -48.222          16.117          -10.78          -10.78
v  nu_tilda           4.3747e-007       0.0042695       0.0013241       0.0013241
v  TempC                       21          73.061          21.832          21.832
v  TurbVisc           3.2219e-014        0.005032       0.0015538       0.0015538
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1366:        0.20660E+01

===============================================================


 INSTANT    0.136700000E+04   TIME STEP NUMBER            1367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58532E-02 0.90024E+00
   Friction velocity        uk    :  0.58532E-02 0.90024E+00
   Dimensionless distance   yplus :  0.47122E-01 0.72476E+01
   Friction thermal sca.    tstar : -0.57243E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35158E-01 0.54075E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86891E-02      33   0.34956E-03   0.30584E+01 0.12540E+03 
c  Velocity[X]                                      0.14191E+01 
c  Velocity[Y]                                      0.16393E+01 
c  Velocity[Z]                                      0.16360E-29 
c  Pressure     0.14388E-06     440   0.92427E-08   0.12899E+00 0.39954E+03 
c  nu_tilda     0.57553E-05      32   0.56145E-05   0.26593E-06 0.14476E+03 
c  TempC        0.35065E+02      26   0.43226E-03   0.69741E+01 0.27325E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4948          10.433          4.5729          4.5729
v  Velocity[Y]            -2.7346          7.3218      -0.0014896      -0.0014896
v  Velocity[Z]       -1.3634e-014     9.7485e-015    -6.2242e-018    -6.2242e-018
v  ǁVelocityǁ         0.0011576          10.433          5.2368          5.2368
v  Pressure               -48.187          16.106         -10.765         -10.765
v  nu_tilda           4.3754e-007       0.0042695       0.0013247       0.0013247
v  TempC                       21          73.061          21.832          21.832
v  TurbVisc           3.2222e-014        0.005032       0.0015545       0.0015545
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1367:        0.20090E+01

===============================================================


 INSTANT    0.136800000E+04   TIME STEP NUMBER            1368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74268E-02 0.89889E+00
   Friction velocity        uk    :  0.74268E-02 0.89889E+00
   Dimensionless distance   yplus :  0.59790E-01 0.72367E+01
   Friction thermal sca.    tstar : -0.44297E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44610E-01 0.53994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86914E-02      33   0.30827E-03   0.30747E+01 0.12566E+03 
c  Velocity[X]                                      0.14144E+01 
c  Velocity[Y]                                      0.16602E+01 
c  Velocity[Z]                                      0.13163E-29 
c  Pressure     0.14074E-06     457   0.92203E-08   0.12233E+00 0.43401E+03 
c  nu_tilda     0.57573E-05      32   0.16063E-04   0.26629E-06 0.14485E+03 
c  TempC        0.35075E+02      26   0.29611E-03   0.69467E+01 0.29525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4916          10.432          4.5729          4.5729
v  Velocity[Y]            -2.7331           7.334      -0.0014867      -0.0014867
v  Velocity[Z]       -1.4654e-014     9.3596e-015    -6.2387e-018    -6.2387e-018
v  ǁVelocityǁ         0.0016528          10.432          5.2365          5.2365
v  Pressure               -48.186          16.079         -10.795         -10.795
v  nu_tilda           4.3762e-007       0.0042695       0.0013252       0.0013252
v  TempC                       21          73.061          21.832          21.832
v  TurbVisc           3.2242e-014        0.005032       0.0015551       0.0015551
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1368:        0.20400E+01

===============================================================


 INSTANT    0.136900000E+04   TIME STEP NUMBER            1369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51431E-02 0.90029E+00
   Friction velocity        uk    :  0.51431E-02 0.90029E+00
   Dimensionless distance   yplus :  0.41405E-01 0.72479E+01
   Friction thermal sca.    tstar : -0.63863E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30893E-01 0.54078E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86937E-02      33   0.29062E-03   0.30462E+01 0.12551E+03 
c  Velocity[X]                                      0.13943E+01 
c  Velocity[Y]                                      0.16519E+01 
c  Velocity[Z]                                      0.13444E-29 
c  Pressure     0.12565E-06     424   0.98727E-08   0.11189E+00 0.47316E+03 
c  nu_tilda     0.57593E-05      32   0.55983E-05   0.26664E-06 0.14493E+03 
c  TempC        0.35085E+02      26   0.31935E-03   0.40469E+01 0.21772E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4884          10.432          4.5729          4.5729
v  Velocity[Y]            -2.7315          7.3151      -0.0014839      -0.0014839
v  Velocity[Z]       -1.5907e-014     9.7047e-015    -6.2592e-018    -6.2592e-018
v  ǁVelocityǁ         0.0019092          10.432          5.2363          5.2363
v  Pressure               -48.143          16.093         -10.774         -10.774
v  nu_tilda           4.3768e-007       0.0042695       0.0013258       0.0013258
v  TempC                       21          73.061          21.833          21.833
v  TurbVisc           3.2267e-014        0.005032       0.0015558       0.0015558
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1369:        0.19690E+01

===============================================================


 INSTANT    0.137000000E+04   TIME STEP NUMBER            1370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77387E-02 0.89943E+00
   Friction velocity        uk    :  0.77387E-02 0.89943E+00
   Dimensionless distance   yplus :  0.62302E-01 0.72410E+01
   Friction thermal sca.    tstar : -0.42517E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46484E-01 0.54026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86960E-02      33   0.30471E-03   0.30337E+01 0.12555E+03 
c  Velocity[X]                                      0.13869E+01 
c  Velocity[Y]                                      0.16469E+01 
c  Velocity[Z]                                      0.10661E-29 
c  Pressure     0.10375E-06     441   0.99884E-08   0.91283E-01 0.47982E+03 
c  nu_tilda     0.57613E-05      32   0.16066E-04   0.26700E-06 0.14501E+03 
c  TempC        0.35094E+02      26   0.36831E-03   0.42032E+01 0.21734E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4854          10.432          4.5729          4.5729
v  Velocity[Y]            -2.7299          7.3427      -0.0014804      -0.0014804
v  Velocity[Z]       -1.5473e-014     9.4253e-015    -6.2633e-018    -6.2633e-018
v  ǁVelocityǁ         0.0013785          10.432           5.236           5.236
v  Pressure               -48.145          16.058         -10.808         -10.808
v  nu_tilda           4.3773e-007       0.0042695       0.0013263       0.0013263
v  TempC                       21           73.06          21.833          21.833
v  TurbVisc           3.2285e-014        0.005032       0.0015564       0.0015564
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1370:        0.20070E+01

===============================================================


 INSTANT    0.137100000E+04   TIME STEP NUMBER            1371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47480E-02 0.90116E+00
   Friction velocity        uk    :  0.47480E-02 0.90116E+00
   Dimensionless distance   yplus :  0.38224E-01 0.72550E+01
   Friction thermal sca.    tstar : -0.69000E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28520E-01 0.54130E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86982E-02      33   0.33394E-03   0.30787E+01 0.12596E+03 
c  Velocity[X]                                      0.14042E+01 
c  Velocity[Y]                                      0.16745E+01 
c  Velocity[Z]                                      0.12535E-29 
c  Pressure     0.14258E-06     488   0.91304E-08   0.12392E+00 0.75189E+03 
c  nu_tilda     0.57633E-05      32   0.55943E-05   0.26734E-06 0.14509E+03 
c  TempC        0.35104E+02      26   0.33732E-03   0.46244E+01 0.24263E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4823          10.431          4.5729          4.5729
v  Velocity[Y]            -2.7283          7.3501      -0.0014769      -0.0014769
v  Velocity[Z]       -1.6278e-014     9.7055e-015    -6.2882e-018    -6.2882e-018
v  ǁVelocityǁ        0.00092798          10.432          5.2358          5.2358
v  Pressure               -48.105          16.146         -10.767         -10.767
v  nu_tilda           4.3772e-007       0.0042695       0.0013269       0.0013269
v  TempC                       21           73.06          21.833          21.833
v  TurbVisc             3.23e-014        0.005032       0.0015571       0.0015571
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1371:        0.21240E+01

===============================================================


 INSTANT    0.137200000E+04   TIME STEP NUMBER            1372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34453E-02 0.90115E+00
   Friction velocity        uk    :  0.34453E-02 0.90115E+00
   Dimensionless distance   yplus :  0.27737E-01 0.72549E+01
   Friction thermal sca.    tstar : -0.94741E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20695E-01 0.54130E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87005E-02      33   0.28819E-03   0.30958E+01 0.12618E+03 
c  Velocity[X]                                      0.14300E+01 
c  Velocity[Y]                                      0.16658E+01 
c  Velocity[Z]                                      0.16283E-29 
c  Pressure     0.13325E-06     472   0.91408E-08   0.11858E+00 0.94552E+03 
c  nu_tilda     0.57652E-05      32   0.16059E-04   0.26771E-06 0.14517E+03 
c  TempC        0.35114E+02      26   0.39112E-03   0.48310E+01 0.23817E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4793          10.431          4.5729          4.5729
v  Velocity[Y]            -2.7268           7.322      -0.0014735      -0.0014735
v  Velocity[Z]        -1.614e-014     9.4013e-015    -6.2949e-018    -6.2949e-018
v  ǁVelocityǁ        0.00051525          10.431          5.2356          5.2356
v  Pressure               -48.101          15.993         -10.822         -10.822
v  nu_tilda           4.3774e-007       0.0042695       0.0013274       0.0013274
v  TempC                       21          73.061          21.834          21.834
v  TurbVisc           3.2297e-014        0.005032       0.0015577       0.0015577
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1372:        0.20840E+01

===============================================================


 INSTANT    0.137300000E+04   TIME STEP NUMBER            1373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84903E-02 0.89963E+00
   Friction velocity        uk    :  0.84903E-02 0.89963E+00
   Dimensionless distance   yplus :  0.68353E-01 0.72426E+01
   Friction thermal sca.    tstar : -0.38392E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50999E-01 0.54038E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87028E-02      33   0.34095E-03   0.30479E+01 0.12596E+03 
c  Velocity[X]                                      0.13873E+01 
c  Velocity[Y]                                      0.16606E+01 
c  Velocity[Z]                                      0.11659E-29 
c  Pressure     0.10271E-06     489   0.99659E-08   0.89885E-01 0.92363E+03 
c  nu_tilda     0.57672E-05      32   0.55928E-05   0.26806E-06 0.14525E+03 
c  TempC        0.35123E+02      26   0.40636E-03   0.68730E+01 0.28124E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4761          10.431          4.5729          4.5729
v  Velocity[Y]            -2.7252          7.3467      -0.0014698      -0.0014698
v  Velocity[Z]       -1.5694e-014     9.6615e-015    -6.3124e-018    -6.3124e-018
v  ǁVelocityǁ        0.00051308          10.431          5.2353          5.2353
v  Pressure               -48.064          16.143         -10.775         -10.775
v  nu_tilda           4.3771e-007       0.0042695        0.001328        0.001328
v  TempC                       21           73.06          21.834          21.834
v  TurbVisc           3.2301e-014        0.005032       0.0015584       0.0015584
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1373:        0.21460E+01

===============================================================


 INSTANT    0.137400000E+04   TIME STEP NUMBER            1374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21910E-02 0.90064E+00
   Friction velocity        uk    :  0.21910E-02 0.90064E+00
   Dimensionless distance   yplus :  0.17639E-01 0.72508E+01
   Friction thermal sca.    tstar : -0.15033E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13161E-01 0.54099E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87051E-02      33   0.31977E-03   0.30975E+01 0.12642E+03 
c  Velocity[X]                                      0.14132E+01 
c  Velocity[Y]                                      0.16843E+01 
c  Velocity[Z]                                      0.11383E-29 
c  Pressure     0.13575E-06     506   0.94651E-08   0.11842E+00 0.13199E+04 
c  nu_tilda     0.57692E-05      32   0.16064E-04   0.26843E-06 0.14533E+03 
c  TempC        0.35133E+02      26   0.37372E-03   0.61596E+01 0.26709E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4729          10.431          4.5729          4.5729
v  Velocity[Y]            -2.7237          7.3173      -0.0014658      -0.0014658
v  Velocity[Z]       -1.5533e-014     9.3755e-015    -6.3252e-018    -6.3252e-018
v  ǁVelocityǁ        0.00091938          10.431          5.2351          5.2351
v  Pressure               -48.062          15.908         -10.849         -10.849
v  nu_tilda           4.3776e-007       0.0042695       0.0013285       0.0013285
v  TempC                       21           73.06          21.834          21.834
v  TurbVisc           3.2292e-014        0.005032        0.001559        0.001559
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1374:        0.21620E+01

===============================================================


 INSTANT    0.137500000E+04   TIME STEP NUMBER            1375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11631E-01 0.90013E+00
   Friction velocity        uk    :  0.11631E-01 0.90013E+00
   Dimensionless distance   yplus :  0.93634E-01 0.72467E+01
   Friction thermal sca.    tstar : -0.28212E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69861E-01 0.54068E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87073E-02      33   0.21504E-03   0.30735E+01 0.12636E+03 
c  Velocity[X]                                      0.13978E+01 
c  Velocity[Y]                                      0.16757E+01 
c  Velocity[Z]                                      0.11191E-29 
c  Pressure     0.10809E-06     504   0.93759E-08   0.95189E-01 0.13863E+04 
c  nu_tilda     0.57712E-05      32   0.55764E-05   0.26877E-06 0.14541E+03 
c  TempC        0.35143E+02      26   0.34930E-03   0.46865E+01 0.24650E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4697           10.43          4.5729          4.5729
v  Velocity[Y]            -2.7221           7.347      -0.0014614      -0.0014614
v  Velocity[Z]       -1.5584e-014     9.6618e-015    -6.3372e-018    -6.3372e-018
v  ǁVelocityǁ           0.00142          10.431          5.2349          5.2349
v  Pressure               -48.027          16.159         -10.779         -10.779
v  nu_tilda           4.3776e-007       0.0042695       0.0013291       0.0013291
v  TempC                       21           73.06          21.834          21.834
v  TurbVisc           3.2307e-014        0.005032       0.0015597       0.0015597
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1375:        0.22550E+01

===============================================================


 INSTANT    0.137600000E+04   TIME STEP NUMBER            1376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21863E-02 0.90145E+00
   Friction velocity        uk    :  0.21863E-02 0.90145E+00
   Dimensionless distance   yplus :  0.17601E-01 0.72573E+01
   Friction thermal sca.    tstar : -0.14948E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13132E-01 0.54147E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87096E-02      33   0.35526E-03   0.30500E+01 0.12633E+03 
c  Velocity[X]                                      0.13788E+01 
c  Velocity[Y]                                      0.16711E+01 
c  Velocity[Z]                                      0.13997E-29 
c  Pressure     0.10320E-06     474   0.93734E-08   0.90489E-01 0.85816E+03 
c  nu_tilda     0.57732E-05      32   0.16057E-04   0.26915E-06 0.14550E+03 
c  TempC        0.35152E+02      27   0.33030E-03   0.57865E+01 0.26887E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4667           10.43          4.5729          4.5729
v  Velocity[Y]            -2.7206          7.3576      -0.0014568      -0.0014568
v  Velocity[Z]       -1.6018e-014     9.2801e-015    -6.3505e-018    -6.3505e-018
v  ǁVelocityǁ        0.00096312           10.43          5.2346          5.2346
v  Pressure               -48.026          16.037         -10.831         -10.831
v  nu_tilda           4.3765e-007       0.0042695       0.0013296       0.0013296
v  TempC                       21           73.06          21.835          21.835
v  TurbVisc           3.2307e-014        0.005032       0.0015603       0.0015603
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1376:        0.20760E+01

===============================================================


 INSTANT    0.137700000E+04   TIME STEP NUMBER            1377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53987E-02 0.90098E+00
   Friction velocity        uk    :  0.53987E-02 0.90098E+00
   Dimensionless distance   yplus :  0.43463E-01 0.72535E+01
   Friction thermal sca.    tstar : -0.60427E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32428E-01 0.54119E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87119E-02      33   0.33665E-03   0.31285E+01 0.12689E+03 
c  Velocity[X]                                      0.14262E+01 
c  Velocity[Y]                                      0.17023E+01 
c  Velocity[Z]                                      0.12346E-29 
c  Pressure     0.13660E-06     458   0.97597E-08   0.11933E+00 0.52981E+03 
c  nu_tilda     0.57753E-05      32   0.55807E-05   0.26950E-06 0.14558E+03 
c  TempC        0.35162E+02      27   0.44338E-03   0.52131E+01 0.24621E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4637           10.43          4.5729          4.5729
v  Velocity[Y]             -2.719          7.3252       -0.001452       -0.001452
v  Velocity[Z]       -1.6349e-014     9.6184e-015    -6.3695e-018    -6.3695e-018
v  ǁVelocityǁ         0.0015815           10.43          5.2344          5.2344
v  Pressure               -47.984          16.035         -10.804         -10.804
v  nu_tilda           4.3766e-007       0.0042695       0.0013302       0.0013302
v  TempC                       21           73.06          21.835          21.835
v  TurbVisc           3.2276e-014        0.005032        0.001561        0.001561
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1377:        0.20670E+01

===============================================================


 INSTANT    0.137800000E+04   TIME STEP NUMBER            1378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93201E-02 0.89975E+00
   Friction velocity        uk    :  0.93201E-02 0.89975E+00
   Dimensionless distance   yplus :  0.75033E-01 0.72436E+01
   Friction thermal sca.    tstar : -0.34697E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55983E-01 0.54045E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87142E-02      33   0.29528E-03   0.31296E+01 0.12709E+03 
c  Velocity[X]                                      0.14404E+01 
c  Velocity[Y]                                      0.16891E+01 
c  Velocity[Z]                                      0.11989E-29 
c  Pressure     0.12675E-06     472   0.98790E-08   0.11074E+00 0.63461E+03 
c  nu_tilda     0.57773E-05      32   0.16061E-04   0.26987E-06 0.14566E+03 
c  TempC        0.35172E+02      27   0.33100E-03   0.62728E+01 0.28622E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4605          10.429          4.5729          4.5729
v  Velocity[Y]            -2.7174          7.3463      -0.0014472      -0.0014472
v  Velocity[Z]       -1.5915e-014     9.3934e-015    -6.3762e-018    -6.3762e-018
v  ǁVelocityǁ          0.001066           10.43          5.2341          5.2341
v  Pressure               -47.988          15.995         -10.849         -10.849
v  nu_tilda           4.3775e-007       0.0042695       0.0013307       0.0013307
v  TempC                       21           73.06          21.835          21.835
v  TurbVisc           3.2278e-014        0.005032       0.0015616       0.0015616
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1378:        0.20820E+01

===============================================================


 INSTANT    0.137900000E+04   TIME STEP NUMBER            1379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27509E-02 0.90088E+00
   Friction velocity        uk    :  0.27509E-02 0.90088E+00
   Dimensionless distance   yplus :  0.22146E-01 0.72527E+01
   Friction thermal sca.    tstar : -0.11956E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16524E-01 0.54113E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87165E-02      33   0.32905E-03   0.30986E+01 0.12696E+03 
c  Velocity[X]                                      0.14133E+01 
c  Velocity[Y]                                      0.16853E+01 
c  Velocity[Z]                                      0.12187E-29 
c  Pressure     0.12020E-06     440   0.93642E-08   0.10624E+00 0.49808E+03 
c  nu_tilda     0.57793E-05      32   0.55648E-05   0.27021E-06 0.14574E+03 
c  TempC        0.35181E+02      26   0.32061E-03   0.50512E+01 0.24832E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4573          10.429          4.5729          4.5729
v  Velocity[Y]            -2.7159          7.3281      -0.0014417      -0.0014417
v  Velocity[Z]       -1.6885e-014      9.618e-015    -6.3995e-018    -6.3995e-018
v  ǁVelocityǁ        0.00061394          10.429          5.2339          5.2339
v  Pressure               -47.947              16         -10.826         -10.826
v  nu_tilda           4.3787e-007       0.0042695       0.0013313       0.0013313
v  TempC                       21           73.06          21.836          21.836
v  TurbVisc           3.2307e-014        0.005032       0.0015623       0.0015623
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1379:        0.20130E+01

===============================================================


 INSTANT    0.138000000E+04   TIME STEP NUMBER            1380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95981E-02 0.89996E+00
   Friction velocity        uk    :  0.95981E-02 0.89996E+00
   Dimensionless distance   yplus :  0.77271E-01 0.72453E+01
   Friction thermal sca.    tstar : -0.36248E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57653E-01 0.54058E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87187E-02      33   0.23803E-03   0.31184E+01 0.12721E+03 
c  Velocity[X]                                      0.14089E+01 
c  Velocity[Y]                                      0.17095E+01 
c  Velocity[Z]                                      0.10576E-29 
c  Pressure     0.12061E-06     425   0.98805E-08   0.10464E+00 0.40710E+03 
c  nu_tilda     0.57813E-05      32   0.16061E-04   0.27059E-06 0.14582E+03 
c  TempC        0.35191E+02      26   0.37226E-03   0.39910E+01 0.21852E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4541          10.429          4.5729          4.5729
v  Velocity[Y]            -2.7143          7.3461      -0.0014358      -0.0014358
v  Velocity[Z]       -1.7167e-014     9.4082e-015      -6.41e-018      -6.41e-018
v  ǁVelocityǁ        0.00050205          10.429          5.2336          5.2336
v  Pressure               -47.947          15.986         -10.853         -10.853
v  nu_tilda           4.3798e-007       0.0042695       0.0013318       0.0013318
v  TempC                       21           73.06          21.836          21.836
v  TurbVisc           3.2341e-014        0.005032       0.0015629       0.0015629
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1380:        0.20780E+01

===============================================================


 INSTANT    0.138100000E+04   TIME STEP NUMBER            1381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39993E-02 0.90144E+00
   Friction velocity        uk    :  0.39993E-02 0.90144E+00
   Dimensionless distance   yplus :  0.32197E-01 0.72572E+01
   Friction thermal sca.    tstar : -0.83388E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24022E-01 0.54147E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87210E-02      33   0.31713E-03   0.30898E+01 0.12712E+03 
c  Velocity[X]                                      0.13866E+01 
c  Velocity[Y]                                      0.17032E+01 
c  Velocity[Z]                                      0.10708E-29 
c  Pressure     0.10901E-06     504   0.91786E-08   0.95726E-01 0.81505E+03 
c  nu_tilda     0.57833E-05      32   0.55665E-05   0.27094E-06 0.14591E+03 
c  TempC        0.35201E+02      26   0.33976E-03   0.47871E+01 0.23784E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4509          10.429          4.5729          4.5729
v  Velocity[Y]            -2.7128          7.3588      -0.0014299      -0.0014299
v  Velocity[Z]       -1.7393e-014     9.5725e-015     -6.421e-018     -6.421e-018
v  ǁVelocityǁ        0.00091663          10.429          5.2334          5.2334
v  Pressure               -47.909          16.097         -10.811         -10.811
v  nu_tilda           4.3802e-007       0.0042695       0.0013324       0.0013324
v  TempC                       21           73.06          21.836          21.836
v  TurbVisc           3.2374e-014        0.005032       0.0015635       0.0015635
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1381:        0.21370E+01

===============================================================


 INSTANT    0.138200000E+04   TIME STEP NUMBER            1382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31272E-02 0.90107E+00
   Friction velocity        uk    :  0.31272E-02 0.90107E+00
   Dimensionless distance   yplus :  0.25176E-01 0.72543E+01
   Friction thermal sca.    tstar : -0.60614E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18784E-01 0.54125E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87233E-02      33   0.35986E-03   0.31511E+01 0.12762E+03 
c  Velocity[X]                                      0.14524E+01 
c  Velocity[Y]                                      0.16987E+01 
c  Velocity[Z]                                      0.14094E-29 
c  Pressure     0.13401E-06     506   0.99589E-08   0.11873E+00 0.13589E+04 
c  nu_tilda     0.57853E-05      32   0.16055E-04   0.27132E-06 0.14599E+03 
c  TempC        0.35210E+02      26   0.39610E-03   0.54102E+01 0.25631E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4479          10.428          4.5729          4.5729
v  Velocity[Y]            -2.7112          7.3321       -0.001424       -0.001424
v  Velocity[Z]       -1.7586e-014     9.3745e-015    -6.4308e-018    -6.4308e-018
v  ǁVelocityǁ         0.0014788          10.428          5.2331          5.2331
v  Pressure               -47.908          15.858         -10.887         -10.887
v  nu_tilda            4.381e-007       0.0042695       0.0013329       0.0013329
v  TempC                       21           73.06          21.837          21.837
v  TurbVisc           3.2384e-014        0.005032       0.0015642       0.0015642
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1382:        0.21560E+01

===============================================================


 INSTANT    0.138300000E+04   TIME STEP NUMBER            1383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10178E-01 0.89978E+00
   Friction velocity        uk    :  0.10178E-01 0.89978E+00
   Dimensionless distance   yplus :  0.81940E-01 0.72438E+01
   Friction thermal sca.    tstar : -0.32282E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61136E-01 0.54047E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87255E-02      33   0.31089E-03   0.31740E+01 0.12789E+03 
c  Velocity[X]                                      0.14517E+01 
c  Velocity[Y]                                      0.17223E+01 
c  Velocity[Z]                                      0.10132E-29 
c  Pressure     0.13721E-06     520   0.94881E-08   0.11860E+00 0.12961E+04 
c  nu_tilda     0.57873E-05      32   0.55607E-05   0.27167E-06 0.14607E+03 
c  TempC        0.35220E+02      27   0.33259E-03   0.48528E+01 0.23648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4448          10.428          4.5729          4.5729
v  Velocity[Y]            -2.7097          7.3472       -0.001417       -0.001417
v  Velocity[Z]       -1.7737e-014     9.5706e-015    -6.4503e-018    -6.4503e-018
v  ǁVelocityǁ         0.0020573          10.428          5.2329          5.2329
v  Pressure               -47.867          16.071         -10.818         -10.818
v  nu_tilda           4.3814e-007       0.0042695       0.0013335       0.0013335
v  TempC                       21           73.06          21.837          21.837
v  TurbVisc           3.2407e-014        0.005032       0.0015648       0.0015648
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1383:        0.21760E+01

===============================================================


 INSTANT    0.138400000E+04   TIME STEP NUMBER            1384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55515E-02 0.90100E+00
   Friction velocity        uk    :  0.55515E-02 0.90100E+00
   Dimensionless distance   yplus :  0.44693E-01 0.72537E+01
   Friction thermal sca.    tstar : -0.62594E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33346E-01 0.54121E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87278E-02      33   0.30092E-03   0.31391E+01 0.12777E+03 
c  Velocity[X]                                      0.14284E+01 
c  Velocity[Y]                                      0.17107E+01 
c  Velocity[Z]                                      0.13502E-29 
c  Pressure     0.10957E-06     522   0.97489E-08   0.96577E-01 0.12174E+04 
c  nu_tilda     0.57893E-05      32   0.16060E-04   0.27205E-06 0.14615E+03 
c  TempC        0.35229E+02      27   0.36184E-03   0.36797E+01 0.20748E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4417          10.428          4.5729          4.5729
v  Velocity[Y]            -2.7081          7.3248      -0.0014101      -0.0014101
v  Velocity[Z]       -1.7527e-014     9.1935e-015    -6.4602e-018    -6.4602e-018
v  ǁVelocityǁ         0.0014831          10.428          5.2326          5.2326
v  Pressure               -47.871          15.872         -10.891         -10.891
v  nu_tilda           4.3819e-007       0.0042695        0.001334        0.001334
v  TempC                       21          73.059          21.837          21.837
v  TurbVisc           3.2421e-014        0.005032       0.0015655       0.0015655
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1384:        0.21980E+01

===============================================================


 INSTANT    0.138500000E+04   TIME STEP NUMBER            1385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10019E-01 0.90023E+00
   Friction velocity        uk    :  0.10019E-01 0.90023E+00
   Dimensionless distance   yplus :  0.80659E-01 0.72474E+01
   Friction thermal sca.    tstar : -0.33228E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60181E-01 0.54074E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87301E-02      33   0.34939E-03   0.31234E+01 0.12775E+03 
c  Velocity[X]                                      0.14122E+01 
c  Velocity[Y]                                      0.17112E+01 
c  Velocity[Z]                                      0.12892E-29 
c  Pressure     0.10724E-06     520   0.99205E-08   0.92822E-01 0.12778E+04 
c  nu_tilda     0.57913E-05      32   0.55427E-05   0.27240E-06 0.14624E+03 
c  TempC        0.35239E+02      27   0.37532E-03   0.52747E+01 0.24878E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4385          10.427          4.5729          4.5729
v  Velocity[Y]            -2.7066           7.354      -0.0014027      -0.0014027
v  Velocity[Z]       -1.8144e-014     9.5251e-015    -6.4805e-018    -6.4805e-018
v  ǁVelocityǁ        0.00091702          10.427          5.2324          5.2324
v  Pressure               -47.832          16.085         -10.823         -10.823
v  nu_tilda           4.3817e-007       0.0042695       0.0013346       0.0013346
v  TempC                       21          73.059          21.837          21.837
v  TurbVisc           3.2436e-014        0.005032       0.0015661       0.0015661
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1385:        0.21760E+01

===============================================================


 INSTANT    0.138600000E+04   TIME STEP NUMBER            1386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26459E-02 0.90154E+00
   Friction velocity        uk    :  0.26459E-02 0.90154E+00
   Dimensionless distance   yplus :  0.21301E-01 0.72580E+01
   Friction thermal sca.    tstar : -0.12416E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15893E-01 0.54153E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87324E-02      33   0.32879E-03   0.31573E+01 0.12817E+03 
c  Velocity[X]                                      0.14208E+01 
c  Velocity[Y]                                      0.17365E+01 
c  Velocity[Z]                                      0.11526E-29 
c  Pressure     0.14741E-06     521   0.93554E-08   0.12618E+00 0.11406E+04 
c  nu_tilda     0.57933E-05      32   0.16053E-04   0.27278E-06 0.14632E+03 
c  TempC        0.35249E+02      26   0.41747E-03   0.56333E+01 0.25968E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4352          10.427          4.5729          4.5729
v  Velocity[Y]             -2.705          7.3559      -0.0013952      -0.0013952
v  Velocity[Z]       -1.8483e-014     9.3822e-015    -6.4933e-018    -6.4933e-018
v  ǁVelocityǁ        0.00049192          10.427          5.2321          5.2321
v  Pressure               -47.829           15.91          -10.89          -10.89
v  nu_tilda           4.3814e-007       0.0042695       0.0013351       0.0013351
v  TempC                       21          73.059          21.838          21.838
v  TurbVisc           3.2431e-014        0.005032       0.0015668       0.0015668
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1386:        0.22220E+01

===============================================================


 INSTANT    0.138700000E+04   TIME STEP NUMBER            1387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46348E-02 0.90153E+00
   Friction velocity        uk    :  0.46348E-02 0.90153E+00
   Dimensionless distance   yplus :  0.37313E-01 0.72579E+01
   Friction thermal sca.    tstar : -0.70876E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27840E-01 0.54152E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87346E-02      33   0.28585E-03   0.31690E+01 0.12832E+03 
c  Velocity[X]                                      0.14439E+01 
c  Velocity[Y]                                      0.17251E+01 
c  Velocity[Z]                                      0.12610E-29 
c  Pressure     0.13590E-06     474   0.95364E-08   0.11991E+00 0.60573E+03 
c  nu_tilda     0.57953E-05      32   0.55400E-05   0.27313E-06 0.14640E+03 
c  TempC        0.35258E+02      27   0.37677E-03   0.70524E+01 0.28276E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4322          10.426          4.5729          4.5729
v  Velocity[Y]            -2.7035          7.3321      -0.0013872      -0.0013872
v  Velocity[Z]       -1.8637e-014      9.525e-015    -6.5117e-018    -6.5117e-018
v  ǁVelocityǁ        0.00065363          10.427          5.2319          5.2319
v  Pressure               -47.792          15.956         -10.859         -10.859
v  nu_tilda           4.3817e-007       0.0042695       0.0013356       0.0013356
v  TempC                       21          73.059          21.838          21.838
v  TurbVisc           3.2421e-014        0.005032       0.0015674       0.0015674
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1387:        0.23820E+01

===============================================================


 INSTANT    0.138800000E+04   TIME STEP NUMBER            1388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85511E-02 0.90005E+00
   Friction velocity        uk    :  0.85511E-02 0.90005E+00
   Dimensionless distance   yplus :  0.68843E-01 0.72460E+01
   Friction thermal sca.    tstar : -0.40633E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51364E-01 0.54064E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87369E-02      33   0.35428E-03   0.31315E+01 0.12817E+03 
c  Velocity[X]                                      0.14128E+01 
c  Velocity[Y]                                      0.17187E+01 
c  Velocity[Z]                                      0.11459E-29 
c  Pressure     0.10570E-06     456   0.93303E-08   0.91477E-01 0.45653E+03 
c  nu_tilda     0.57974E-05      32   0.16055E-04   0.27351E-06 0.14649E+03 
c  TempC        0.35268E+02      27   0.35718E-03   0.54709E+01 0.25697E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4291          10.426          4.5729          4.5729
v  Velocity[Y]             -2.702          7.3536      -0.0013787      -0.0013787
v  Velocity[Z]       -1.8684e-014     9.3951e-015    -6.5229e-018    -6.5229e-018
v  ǁVelocityǁ         0.0012177          10.426          5.2316          5.2316
v  Pressure               -47.792          15.932         -10.891         -10.891
v  nu_tilda           4.3819e-007       0.0042695       0.0013361       0.0013361
v  TempC                       21          73.059          21.838          21.838
v  TurbVisc            3.243e-014        0.005032       0.0015681       0.0015681
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1388:        0.20960E+01

===============================================================


 INSTANT    0.138900000E+04   TIME STEP NUMBER            1389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33424E-02 0.90117E+00
   Friction velocity        uk    :  0.33424E-02 0.90117E+00
   Dimensionless distance   yplus :  0.26909E-01 0.72550E+01
   Friction thermal sca.    tstar : -0.84828E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20077E-01 0.54130E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87391E-02      33   0.32134E-03   0.31992E+01 0.12864E+03 
c  Velocity[X]                                      0.14512E+01 
c  Velocity[Y]                                      0.17480E+01 
c  Velocity[Z]                                      0.11824E-29 
c  Pressure     0.15363E-06     456   0.90507E-08   0.13327E+00 0.48064E+03 
c  nu_tilda     0.57994E-05      32   0.55284E-05   0.27387E-06 0.14657E+03 
c  TempC        0.35278E+02      26   0.32608E-03   0.52529E+01 0.24071E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.426          10.426          4.5729          4.5729
v  Velocity[Y]            -2.7004          7.3278      -0.0013701      -0.0013701
v  Velocity[Z]        -1.885e-014     9.4793e-015    -6.5368e-018    -6.5368e-018
v  ǁVelocityǁ         0.0018435          10.426          5.2314          5.2314
v  Pressure               -47.749          15.914          -10.87          -10.87
v  nu_tilda           4.3825e-007       0.0042695       0.0013367       0.0013367
v  TempC                       21          73.059          21.839          21.839
v  TurbVisc           3.2435e-014        0.005032       0.0015687       0.0015687
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1389:        0.20520E+01

===============================================================


 INSTANT    0.139000000E+04   TIME STEP NUMBER            1390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10832E-01 0.90063E+00
   Friction velocity        uk    :  0.10832E-01 0.90063E+00
   Dimensionless distance   yplus :  0.87207E-01 0.72507E+01
   Friction thermal sca.    tstar : -0.30313E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65066E-01 0.54098E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87414E-02      33   0.21137E-03   0.31709E+01 0.12860E+03 
c  Velocity[X]                                      0.14339E+01 
c  Velocity[Y]                                      0.17371E+01 
c  Velocity[Z]                                      0.97489E-30 
c  Pressure     0.11140E-06     440   0.97182E-08   0.97144E-01 0.40364E+03 
c  nu_tilda     0.58014E-05      32   0.16057E-04   0.27425E-06 0.14665E+03 
c  TempC        0.35287E+02      26   0.28903E-03   0.57334E+01 0.24774E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4228          10.425          4.5729          4.5729
v  Velocity[Y]            -2.6989          7.3551      -0.0013614      -0.0013614
v  Velocity[Z]       -1.8457e-014      9.361e-015    -6.5424e-018    -6.5424e-018
v  ǁVelocityǁ          0.001701          10.425          5.2311          5.2311
v  Pressure               -47.752          15.917           -10.9           -10.9
v  nu_tilda           4.3827e-007       0.0042695       0.0013372       0.0013372
v  TempC                       21          73.059          21.839          21.839
v  TurbVisc           3.2452e-014        0.005032       0.0015693       0.0015693
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1390:        0.20020E+01

===============================================================


 INSTANT    0.139100000E+04   TIME STEP NUMBER            1391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61708E-02 0.90219E+00
   Friction velocity        uk    :  0.61708E-02 0.90219E+00
   Dimensionless distance   yplus :  0.49679E-01 0.72633E+01
   Friction thermal sca.    tstar : -0.53604E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37066E-01 0.54192E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87436E-02      33   0.34802E-03   0.31363E+01 0.12853E+03 
c  Velocity[X]                                      0.14020E+01 
c  Velocity[Y]                                      0.17342E+01 
c  Velocity[Z]                                      0.11560E-29 
c  Pressure     0.10954E-06     506   0.97842E-08   0.95448E-01 0.90779E+03 
c  nu_tilda     0.58034E-05      32   0.55232E-05   0.27460E-06 0.14674E+03 
c  TempC        0.35297E+02      26   0.41380E-03   0.41871E+01 0.23413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4196          10.425          4.5729          4.5729
v  Velocity[Y]            -2.6973          7.3691      -0.0013517      -0.0013517
v  Velocity[Z]       -1.8325e-014     9.4767e-015     -6.557e-018     -6.557e-018
v  ǁVelocityǁ         0.0010853          10.425          5.2309          5.2309
v  Pressure               -47.711          16.044         -10.851         -10.851
v  nu_tilda           4.3819e-007       0.0042695       0.0013378       0.0013378
v  TempC                       21          73.059          21.839          21.839
v  TurbVisc           3.2457e-014        0.005032         0.00157         0.00157
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1391:        0.21560E+01

===============================================================


 INSTANT    0.139200000E+04   TIME STEP NUMBER            1392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34390E-02 0.90158E+00
   Friction velocity        uk    :  0.34390E-02 0.90158E+00
   Dimensionless distance   yplus :  0.27687E-01 0.72583E+01
   Friction thermal sca.    tstar : -0.46272E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20657E-01 0.54155E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87459E-02      33   0.32228E-03   0.32207E+01 0.12922E+03 
c  Velocity[X]                                      0.14600E+01 
c  Velocity[Y]                                      0.17607E+01 
c  Velocity[Z]                                      0.14457E-29 
c  Pressure     0.13241E-06     506   0.95251E-08   0.11500E+00 0.14877E+04 
c  nu_tilda     0.58054E-05      32   0.16050E-04   0.27499E-06 0.14682E+03 
c  TempC        0.35306E+02      26   0.43271E-03   0.60027E+01 0.28094E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4164          10.425          4.5729          4.5729
v  Velocity[Y]            -2.6958          7.3346      -0.0013421      -0.0013421
v  Velocity[Z]       -1.8169e-014     9.1056e-015    -6.5667e-018    -6.5667e-018
v  ǁVelocityǁ        0.00058091          10.425          5.2306          5.2306
v  Pressure               -47.713          15.774         -10.936         -10.936
v  nu_tilda           4.3824e-007       0.0042695       0.0013383       0.0013383
v  TempC                       21          73.059          21.839          21.839
v  TurbVisc           3.2435e-014        0.005032       0.0015706       0.0015706
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1392:        0.21470E+01

===============================================================


 INSTANT    0.139300000E+04   TIME STEP NUMBER            1393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10922E-01 0.90039E+00
   Friction velocity        uk    :  0.10922E-01 0.90039E+00
   Dimensionless distance   yplus :  0.87930E-01 0.72487E+01
   Friction thermal sca.    tstar : -0.29918E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65606E-01 0.54084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87481E-02      33   0.28427E-03   0.31859E+01 0.12908E+03 
c  Velocity[X]                                      0.14367E+01 
c  Velocity[Y]                                      0.17493E+01 
c  Velocity[Z]                                      0.11445E-29 
c  Pressure     0.11026E-06     537   0.94624E-08   0.94948E-01 0.15122E+04 
c  nu_tilda     0.58075E-05      32   0.55138E-05   0.27535E-06 0.14691E+03 
c  TempC        0.35316E+02      27   0.30400E-03   0.60919E+01 0.26522E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4134          10.424          4.5729          4.5729
v  Velocity[Y]            -2.6943          7.3563      -0.0013319      -0.0013319
v  Velocity[Z]       -1.8045e-014     9.4285e-015    -6.5842e-018    -6.5842e-018
v  ǁVelocityǁ        0.00058348          10.424          5.2304          5.2304
v  Pressure               -47.675          16.043         -10.857         -10.857
v  nu_tilda           4.3828e-007       0.0042695       0.0013389       0.0013389
v  TempC                       21          73.059           21.84           21.84
v  TurbVisc            3.245e-014        0.005032       0.0015713       0.0015713
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1393:        0.22310E+01

===============================================================


 INSTANT    0.139400000E+04   TIME STEP NUMBER            1394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47018E-02 0.90136E+00
   Friction velocity        uk    :  0.47018E-02 0.90136E+00
   Dimensionless distance   yplus :  0.37853E-01 0.72566E+01
   Friction thermal sca.    tstar : -0.69375E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28243E-01 0.54142E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87504E-02      33   0.34736E-03   0.31850E+01 0.12916E+03 
c  Velocity[X]                                      0.14382E+01 
c  Velocity[Y]                                      0.17468E+01 
c  Velocity[Z]                                      0.12591E-29 
c  Pressure     0.12134E-06     521   0.96149E-08   0.10625E+00 0.15540E+04 
c  nu_tilda     0.58095E-05      32   0.16055E-04   0.27573E-06 0.14699E+03 
c  TempC        0.35326E+02      27   0.41006E-03   0.39172E+01 0.21056E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4103          10.424          4.5729          4.5729
v  Velocity[Y]            -2.6928          7.3356      -0.0013217      -0.0013217
v  Velocity[Z]       -1.7806e-014     9.3676e-015    -6.5948e-018    -6.5948e-018
v  ǁVelocityǁ         0.0011171          10.424          5.2301          5.2301
v  Pressure               -47.674          15.772         -10.944         -10.944
v  nu_tilda           4.3837e-007       0.0042695       0.0013394       0.0013394
v  TempC                       21          73.058           21.84           21.84
v  TurbVisc           3.2461e-014        0.005032       0.0015719       0.0015719
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1394:        0.21750E+01

===============================================================


 INSTANT    0.139500000E+04   TIME STEP NUMBER            1395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10573E-01 0.90055E+00
   Friction velocity        uk    :  0.10573E-01 0.90055E+00
   Dimensionless distance   yplus :  0.85122E-01 0.72500E+01
   Friction thermal sca.    tstar : -0.31061E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63511E-01 0.54093E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87527E-02      33   0.29072E-03   0.32260E+01 0.12953E+03 
c  Velocity[X]                                      0.14548E+01 
c  Velocity[Y]                                      0.17712E+01 
c  Velocity[Z]                                      0.12601E-29 
c  Pressure     0.14089E-06     521   0.96419E-08   0.12029E+00 0.12841E+04 
c  nu_tilda     0.58115E-05      32   0.54950E-05   0.27609E-06 0.14707E+03 
c  TempC        0.35335E+02      27   0.39497E-03   0.76214E+01 0.29430E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4071          10.423          4.5729          4.5729
v  Velocity[Y]            -2.6912          7.3555      -0.0013105      -0.0013105
v  Velocity[Z]       -1.6428e-014     9.4249e-015    -6.6055e-018    -6.6055e-018
v  ǁVelocityǁ         0.0017794          10.424          5.2298          5.2298
v  Pressure               -47.633          15.986         -10.876         -10.876
v  nu_tilda           4.3844e-007       0.0042695         0.00134         0.00134
v  TempC                       21          73.059           21.84           21.84
v  TurbVisc            3.249e-014        0.005032       0.0015725       0.0015725
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1395:        0.22000E+01

===============================================================


 INSTANT    0.139600000E+04   TIME STEP NUMBER            1396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15419E-02 0.90202E+00
   Friction velocity        uk    :  0.15419E-02 0.90202E+00
   Dimensionless distance   yplus :  0.12413E-01 0.72619E+01
   Friction thermal sca.    tstar : -0.21220E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92618E-02 0.54182E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87549E-02      33   0.32929E-03   0.32142E+01 0.12964E+03 
c  Velocity[X]                                      0.14539E+01 
c  Velocity[Y]                                      0.17603E+01 
c  Velocity[Z]                                      0.12455E-29 
c  Pressure     0.11320E-06     504   0.92156E-08   0.97605E-01 0.79854E+03 
c  nu_tilda     0.58135E-05      32   0.16048E-04   0.27647E-06 0.14716E+03 
c  TempC        0.35345E+02      26   0.36410E-03   0.61171E+01 0.26773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4039          10.423          4.5729          4.5729
v  Velocity[Y]            -2.6897          7.3645      -0.0012993      -0.0012993
v  Velocity[Z]       -1.6665e-014     9.3786e-015    -6.6121e-018    -6.6121e-018
v  ǁVelocityǁ         0.0012318          10.423          5.2296          5.2296
v  Pressure               -47.636           15.88         -10.927         -10.927
v  nu_tilda           4.3843e-007       0.0042695       0.0013405       0.0013405
v  TempC                       21          73.059          21.841          21.841
v  TurbVisc           3.2509e-014        0.005032       0.0015732       0.0015732
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1396:        0.21420E+01

===============================================================


 INSTANT    0.139700000E+04   TIME STEP NUMBER            1397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40402E-02 0.90172E+00
   Friction velocity        uk    :  0.40402E-02 0.90172E+00
   Dimensionless distance   yplus :  0.32527E-01 0.72595E+01
   Friction thermal sca.    tstar : -0.81263E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24268E-01 0.54164E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87572E-02      33   0.32479E-03   0.32244E+01 0.12974E+03 
c  Velocity[X]                                      0.14640E+01 
c  Velocity[Y]                                      0.17605E+01 
c  Velocity[Z]                                      0.14090E-29 
c  Pressure     0.13313E-06     457   0.97477E-08   0.11642E+00 0.54201E+03 
c  nu_tilda     0.58156E-05      32   0.54946E-05   0.27684E-06 0.14724E+03 
c  TempC        0.35354E+02      26   0.34372E-03   0.41285E+01 0.23372E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4007          10.423          4.5729          4.5729
v  Velocity[Y]            -2.6882          7.3391      -0.0012878      -0.0012878
v  Velocity[Z]       -1.6537e-014     9.3789e-015    -6.6195e-018    -6.6195e-018
v  ǁVelocityǁ         0.0011265          10.423          5.2293          5.2293
v  Pressure               -47.593          15.895           -10.9           -10.9
v  nu_tilda           4.3848e-007       0.0042695       0.0013411       0.0013411
v  TempC                       21          73.058          21.841          21.841
v  TurbVisc           3.2506e-014        0.005032       0.0015738       0.0015738
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1397:        0.20420E+01

===============================================================


 INSTANT    0.139800000E+04   TIME STEP NUMBER            1398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69779E-02 0.90036E+00
   Friction velocity        uk    :  0.69779E-02 0.90036E+00
   Dimensionless distance   yplus :  0.56177E-01 0.72485E+01
   Friction thermal sca.    tstar : -0.50493E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41914E-01 0.54082E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87594E-02      33   0.34528E-03   0.32037E+01 0.12977E+03 
c  Velocity[X]                                      0.14287E+01 
c  Velocity[Y]                                      0.17750E+01 
c  Velocity[Z]                                      0.12034E-29 
c  Pressure     0.10783E-06     458   0.91812E-08   0.92914E-01 0.58748E+03 
c  nu_tilda     0.58176E-05      32   0.16049E-04   0.27722E-06 0.14733E+03 
c  TempC        0.35364E+02      26   0.30037E-03   0.73522E+01 0.28519E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3975          10.422          4.5729          4.5729
v  Velocity[Y]            -2.6867          7.3598      -0.0012761      -0.0012761
v  Velocity[Z]       -1.5035e-014     9.3422e-015    -6.6274e-018    -6.6274e-018
v  ǁVelocityǁ        0.00057216          10.422           5.229           5.229
v  Pressure               -47.597          15.849         -10.942         -10.942
v  nu_tilda           4.3856e-007       0.0042695       0.0013416       0.0013416
v  TempC                       21          73.058          21.841          21.841
v  TurbVisc           3.2522e-014        0.005032       0.0015745       0.0015745
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1398:        0.20600E+01

===============================================================


 INSTANT    0.139900000E+04   TIME STEP NUMBER            1399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24860E-02 0.90159E+00
   Friction velocity        uk    :  0.24860E-02 0.90159E+00
   Dimensionless distance   yplus :  0.20014E-01 0.72584E+01
   Friction thermal sca.    tstar : -0.13496E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14933E-01 0.54156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87617E-02      33   0.29225E-03   0.32339E+01 0.12998E+03 
c  Velocity[X]                                      0.14629E+01 
c  Velocity[Y]                                      0.17710E+01 
c  Velocity[Z]                                      0.12424E-29 
c  Pressure     0.13145E-06     441   0.92710E-08   0.11361E+00 0.51087E+03 
c  nu_tilda     0.58196E-05      32   0.54880E-05   0.27759E-06 0.14741E+03 
c  TempC        0.35374E+02      27   0.45180E-03   0.45757E+01 0.22338E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3945          10.422          4.5729          4.5729
v  Velocity[Y]            -2.6851          7.3361      -0.0012636      -0.0012636
v  Velocity[Z]       -1.5562e-014     9.3749e-015    -6.6431e-018    -6.6431e-018
v  ǁVelocityǁ        0.00060172          10.422          5.2288          5.2288
v  Pressure               -47.556          15.849         -10.917         -10.917
v  nu_tilda           4.3864e-007       0.0042695       0.0013422       0.0013422
v  TempC                       21          73.058          21.841          21.841
v  TurbVisc           3.2546e-014        0.005032       0.0015751       0.0015751
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1399:        0.19890E+01

===============================================================


 INSTANT    0.140000000E+04   TIME STEP NUMBER            1400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94759E-02 0.90086E+00
   Friction velocity        uk    :  0.94759E-02 0.90086E+00
   Dimensionless distance   yplus :  0.76287E-01 0.72525E+01
   Friction thermal sca.    tstar : -0.34767E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56919E-01 0.54112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87639E-02      33   0.26595E-03   0.32099E+01 0.12996E+03 
c  Velocity[X]                                      0.14423E+01 
c  Velocity[Y]                                      0.17675E+01 
c  Velocity[Z]                                      0.13497E-29 
c  Pressure     0.10168E-06     424   0.96803E-08   0.87520E-01 0.34260E+03 
c  nu_tilda     0.58217E-05      32   0.16050E-04   0.27798E-06 0.14750E+03 
c  TempC        0.35383E+02      28   0.33546E-03   0.58240E+01 0.25604E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3914          10.421          4.5729          4.5729
v  Velocity[Y]            -2.6836          7.3606      -0.0012507      -0.0012507
v  Velocity[Z]       -1.4175e-014     9.0129e-015    -6.6451e-018    -6.6451e-018
v  ǁVelocityǁ         0.0012279          10.421          5.2285          5.2285
v  Pressure               -47.556          15.858         -10.941         -10.941
v  nu_tilda           4.3869e-007       0.0042695       0.0013427       0.0013427
v  TempC                       21          73.058          21.842          21.842
v  TurbVisc            3.257e-014        0.005032       0.0015757       0.0015757
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1400:        0.19890E+01

===============================================================


 INSTANT    0.140100000E+04   TIME STEP NUMBER            1401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38399E-02 0.90238E+00
   Friction velocity        uk    :  0.38399E-02 0.90238E+00
   Dimensionless distance   yplus :  0.30914E-01 0.72648E+01
   Friction thermal sca.    tstar : -0.85716E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23065E-01 0.54204E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87662E-02      33   0.34251E-03   0.32061E+01 0.13011E+03 
c  Velocity[X]                                      0.14192E+01 
c  Velocity[Y]                                      0.17869E+01 
c  Velocity[Z]                                      0.13638E-29 
c  Pressure     0.11660E-06     490   0.91234E-08   0.10046E+00 0.91136E+03 
c  nu_tilda     0.58237E-05      32   0.54796E-05   0.27834E-06 0.14758E+03 
c  TempC        0.35393E+02      27   0.27509E-03   0.53043E+01 0.24354E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3882          10.421          4.5729          4.5729
v  Velocity[Y]            -2.6821          7.3731      -0.0012376      -0.0012376
v  Velocity[Z]       -1.4728e-014      9.327e-015    -6.6653e-018    -6.6653e-018
v  ǁVelocityǁ        0.00031069          10.421          5.2283          5.2283
v  Pressure                -47.52          15.991         -10.894         -10.894
v  nu_tilda           4.3863e-007       0.0042695       0.0013432       0.0013432
v  TempC                       21          73.059          21.842          21.842
v  TurbVisc           3.2584e-014        0.005032       0.0015764       0.0015764
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1401:        0.21100E+01

===============================================================


 INSTANT    0.140200000E+04   TIME STEP NUMBER            1402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33505E-02 0.90179E+00
   Friction velocity        uk    :  0.33505E-02 0.90179E+00
   Dimensionless distance   yplus :  0.26974E-01 0.72600E+01
   Friction thermal sca.    tstar : -0.38400E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20126E-01 0.54168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87685E-02      33   0.33019E-03   0.32611E+01 0.13057E+03 
c  Velocity[X]                                      0.14762E+01 
c  Velocity[Y]                                      0.17849E+01 
c  Velocity[Z]                                      0.13919E-29 
c  Pressure     0.13810E-06     521   0.99935E-08   0.11873E+00 0.17286E+04 
c  nu_tilda     0.58257E-05      32   0.16043E-04   0.27873E-06 0.14767E+03 
c  TempC        0.35402E+02      26   0.48834E-03   0.49648E+01 0.24099E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3849           10.42          4.5729          4.5729
v  Velocity[Y]            -2.6805          7.3387      -0.0012244      -0.0012244
v  Velocity[Z]       -1.3424e-014      9.349e-015    -6.6712e-018    -6.6712e-018
v  ǁVelocityǁ         0.0015355          10.421           5.228           5.228
v  Pressure               -47.519          15.679         -10.989         -10.989
v  nu_tilda           4.3867e-007       0.0042695       0.0013437       0.0013437
v  TempC                       21          73.058          21.842          21.842
v  TurbVisc           3.2566e-014        0.005032        0.001577        0.001577
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1402:        0.21730E+01

===============================================================


 INSTANT    0.140300000E+04   TIME STEP NUMBER            1403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10867E-01 0.90067E+00
   Friction velocity        uk    :  0.10867E-01 0.90067E+00
   Dimensionless distance   yplus :  0.87491E-01 0.72510E+01
   Friction thermal sca.    tstar : -0.30177E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65278E-01 0.54101E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87707E-02      33   0.32948E-03   0.32607E+01 0.13067E+03 
c  Velocity[X]                                      0.14747E+01 
c  Velocity[Y]                                      0.17859E+01 
c  Velocity[Z]                                      0.11082E-29 
c  Pressure     0.12448E-06     490   0.94476E-08   0.10783E+00 0.14206E+04 
c  nu_tilda     0.58278E-05      32   0.54693E-05   0.27910E-06 0.14775E+03 
c  TempC        0.35412E+02      27   0.39653E-03   0.78591E+01 0.29956E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3817           10.42          4.5729          4.5729
v  Velocity[Y]             -2.679          7.3628      -0.0012102      -0.0012102
v  Velocity[Z]       -1.4006e-014     9.3691e-015    -6.6811e-018    -6.6811e-018
v  ǁVelocityǁ        0.00070654           10.42          5.2277          5.2277
v  Pressure               -47.476          15.929         -10.914         -10.914
v  nu_tilda           4.3873e-007       0.0042695       0.0013443       0.0013443
v  TempC                       21          73.058          21.843          21.843
v  TurbVisc           3.2577e-014        0.005032       0.0015777       0.0015777
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1403:        0.21230E+01

===============================================================


 INSTANT    0.140400000E+04   TIME STEP NUMBER            1404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32673E-02 0.90176E+00
   Friction velocity        uk    :  0.32673E-02 0.90176E+00
   Dimensionless distance   yplus :  0.26304E-01 0.72598E+01
   Friction thermal sca.    tstar : -0.10004E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19626E-01 0.54166E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87729E-02      33   0.31415E-03   0.32580E+01 0.13079E+03 
c  Velocity[X]                                      0.14545E+01 
c  Velocity[Y]                                      0.18035E+01 
c  Velocity[Z]                                      0.14079E-29 
c  Pressure     0.11151E-06     506   0.91707E-08   0.96755E-01 0.12207E+04 
c  nu_tilda     0.58298E-05      32   0.16047E-04   0.27949E-06 0.14784E+03 
c  TempC        0.35421E+02      27   0.40770E-03   0.52113E+01 0.25687E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3786           10.42          4.5729          4.5729
v  Velocity[Y]            -2.6775          7.3388      -0.0011959      -0.0011959
v  Velocity[Z]        -1.263e-014     9.3579e-015    -6.6916e-018    -6.6916e-018
v  ǁVelocityǁ        0.00048929           10.42          5.2275          5.2275
v  Pressure                -47.48          15.717         -10.986         -10.986
v  nu_tilda           4.3881e-007       0.0042695       0.0013448       0.0013448
v  TempC                       21          73.058          21.843          21.843
v  TurbVisc           3.2594e-014        0.005032       0.0015783       0.0015783
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1404:        0.21560E+01

===============================================================


 INSTANT    0.140500000E+04   TIME STEP NUMBER            1405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71755E-02 0.90104E+00
   Friction velocity        uk    :  0.71755E-02 0.90104E+00
   Dimensionless distance   yplus :  0.57768E-01 0.72540E+01
   Friction thermal sca.    tstar : -0.33259E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43101E-01 0.54123E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87751E-02      33   0.32145E-03   0.32569E+01 0.13077E+03 
c  Velocity[X]                                      0.14587E+01 
c  Velocity[Y]                                      0.17982E+01 
c  Velocity[Z]                                      0.12104E-29 
c  Pressure     0.13450E-06     505   0.95580E-08   0.11363E+00 0.13559E+04 
c  nu_tilda     0.58318E-05      32   0.54640E-05   0.27985E-06 0.14792E+03 
c  TempC        0.35431E+02      26   0.38145E-03   0.57285E+01 0.27365E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3755          10.419          4.5729          4.5729
v  Velocity[Y]             -2.676           7.361      -0.0011811      -0.0011811
v  Velocity[Z]       -1.3228e-014     9.3381e-015    -6.7051e-018    -6.7051e-018
v  ǁVelocityǁ        0.00080794          10.419          5.2272          5.2272
v  Pressure                -47.44          15.942         -10.913         -10.913
v  nu_tilda           4.3888e-007       0.0042695       0.0013454       0.0013454
v  TempC                       21          73.058          21.843          21.843
v  TurbVisc            3.262e-014        0.005032       0.0015789       0.0015789
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1405:        0.21460E+01

===============================================================


 INSTANT    0.140600000E+04   TIME STEP NUMBER            1406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37160E-02 0.90243E+00
   Friction velocity        uk    :  0.37160E-02 0.90243E+00
   Dimensionless distance   yplus :  0.29916E-01 0.72652E+01
   Friction thermal sca.    tstar : -0.88182E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22321E-01 0.54206E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87774E-02      33   0.32908E-03   0.32604E+01 0.13098E+03 
c  Velocity[X]                                      0.14639E+01 
c  Velocity[Y]                                      0.17964E+01 
c  Velocity[Z]                                      0.11807E-29 
c  Pressure     0.11618E-06     490   0.98775E-08   0.99712E-01 0.99712E+03 
c  nu_tilda     0.58339E-05      32   0.16039E-04   0.28025E-06 0.14801E+03 
c  TempC        0.35441E+02      26   0.35707E-03   0.61378E+01 0.26096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3724          10.419          4.5729          4.5729
v  Velocity[Y]            -2.6745          7.3714      -0.0011662      -0.0011662
v  Velocity[Z]        -1.175e-014     9.3221e-015     -6.712e-018     -6.712e-018
v  ǁVelocityǁ         0.0012768          10.419          5.2269          5.2269
v  Pressure               -47.438          15.799         -10.973         -10.973
v  nu_tilda           4.3896e-007       0.0042695       0.0013459       0.0013459
v  TempC                       21          73.058          21.843          21.843
v  TurbVisc           3.2641e-014        0.005032       0.0015796       0.0015796
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1406:        0.21620E+01

===============================================================


 INSTANT    0.140700000E+04   TIME STEP NUMBER            1407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14905E-02 0.90221E+00
   Friction velocity        uk    :  0.14905E-02 0.90221E+00
   Dimensionless distance   yplus :  0.12000E-01 0.72634E+01
   Friction thermal sca.    tstar : -0.17676E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89531E-02 0.54193E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87796E-02      33   0.29650E-03   0.32821E+01 0.13126E+03 
c  Velocity[X]                                      0.14622E+01 
c  Velocity[Y]                                      0.18199E+01 
c  Velocity[Z]                                      0.13423E-29 
c  Pressure     0.12301E-06     456   0.92795E-08   0.10676E+00 0.54744E+03 
c  nu_tilda     0.58359E-05      32   0.54692E-05   0.28062E-06 0.14809E+03 
c  TempC        0.35450E+02      26   0.35654E-03   0.45879E+01 0.23613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3692          10.418          4.5729          4.5729
v  Velocity[Y]            -2.6729          7.3451      -0.0011504      -0.0011504
v  Velocity[Z]       -1.2359e-014     9.3078e-015    -6.7323e-018    -6.7323e-018
v  ǁVelocityǁ         0.0018786          10.419          5.2267          5.2267
v  Pressure                 -47.4          15.827         -10.945         -10.945
v  nu_tilda           4.3904e-007       0.0042695       0.0013465       0.0013465
v  TempC                       21          73.058          21.844          21.844
v  TurbVisc           3.2665e-014        0.005032       0.0015802       0.0015802
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1407:        0.20450E+01

===============================================================


 INSTANT    0.140800000E+04   TIME STEP NUMBER            1408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64556E-02 0.90075E+00
   Friction velocity        uk    :  0.64556E-02 0.90075E+00
   Dimensionless distance   yplus :  0.51972E-01 0.72517E+01
   Friction thermal sca.    tstar : -0.51967E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38777E-01 0.54105E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87819E-02      33   0.31965E-03   0.32632E+01 0.13124E+03 
c  Velocity[X]                                      0.14551E+01 
c  Velocity[Y]                                      0.18080E+01 
c  Velocity[Z]                                      0.13575E-29 
c  Pressure     0.12254E-06     456   0.94069E-08   0.10409E+00 0.59012E+03 
c  nu_tilda     0.58380E-05      32   0.16040E-04   0.28101E-06 0.14818E+03 
c  TempC        0.35460E+02      26   0.28477E-03   0.60077E+01 0.26702E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.366          10.418          4.5729          4.5729
v  Velocity[Y]            -2.6714          7.3607      -0.0011342      -0.0011342
v  Velocity[Z]        -1.097e-014      8.912e-015     -6.741e-018     -6.741e-018
v  ǁVelocityǁ         0.0012762          10.418          5.2264          5.2264
v  Pressure               -47.401           15.77         -10.985         -10.985
v  nu_tilda           4.3907e-007       0.0042695        0.001347        0.001347
v  TempC                       21          73.058          21.844          21.844
v  TurbVisc           3.2688e-014        0.005032       0.0015809       0.0015809
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1408:        0.20700E+01

===============================================================


 INSTANT    0.140900000E+04   TIME STEP NUMBER            1409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41981E-02 0.90206E+00
   Friction velocity        uk    :  0.41981E-02 0.90206E+00
   Dimensionless distance   yplus :  0.33797E-01 0.72622E+01
   Friction thermal sca.    tstar : -0.78468E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25217E-01 0.54184E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87841E-02      33   0.35836E-03   0.33046E+01 0.13158E+03 
c  Velocity[X]                                      0.14941E+01 
c  Velocity[Y]                                      0.18105E+01 
c  Velocity[Z]                                      0.13596E-29 
c  Pressure     0.14121E-06     457   0.91287E-08   0.12320E+00 0.59514E+03 
c  nu_tilda     0.58400E-05      32   0.54603E-05   0.28139E-06 0.14826E+03 
c  TempC        0.35469E+02      27   0.46190E-03   0.44848E+01 0.23463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3627          10.418          4.5729          4.5729
v  Velocity[Y]            -2.6699          7.3427      -0.0011181      -0.0011181
v  Velocity[Z]        -1.163e-014     9.2184e-015    -6.7587e-018    -6.7587e-018
v  ǁVelocityǁ        0.00065178          10.418          5.2261          5.2261
v  Pressure               -47.363          15.811         -10.955         -10.955
v  nu_tilda            4.391e-007       0.0042695       0.0013475       0.0013475
v  TempC                       21          73.057          21.844          21.844
v  TurbVisc           3.2697e-014        0.005032       0.0015815       0.0015815
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1409:        0.20370E+01

===============================================================


 INSTANT    0.141000000E+04   TIME STEP NUMBER            1410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81755E-02 0.90125E+00
   Friction velocity        uk    :  0.81755E-02 0.90125E+00
   Dimensionless distance   yplus :  0.65818E-01 0.72557E+01
   Friction thermal sca.    tstar : -0.40233E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49108E-01 0.54136E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87864E-02      33   0.25814E-03   0.33057E+01 0.13179E+03 
c  Velocity[X]                                      0.14720E+01 
c  Velocity[Y]                                      0.18337E+01 
c  Velocity[Z]                                      0.11592E-29 
c  Pressure     0.11964E-06     457   0.93580E-08   0.10329E+00 0.57811E+03 
c  nu_tilda     0.58421E-05      32   0.16041E-04   0.28178E-06 0.14835E+03 
c  TempC        0.35479E+02      27   0.33073E-03   0.79005E+01 0.31139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3597          10.417          4.5729          4.5729
v  Velocity[Y]            -2.6684          7.3675      -0.0011014      -0.0011014
v  Velocity[Z]       -1.0302e-014     9.3278e-015    -6.7663e-018    -6.7663e-018
v  ǁVelocityǁ        0.00059139          10.417          5.2258          5.2258
v  Pressure               -47.363           15.77         -10.994         -10.994
v  nu_tilda           4.3912e-007       0.0042695        0.001348        0.001348
v  TempC                       21          73.057          21.845          21.845
v  TurbVisc           3.2707e-014        0.005032       0.0015821       0.0015821
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1410:        0.20610E+01

===============================================================


 INSTANT    0.141100000E+04   TIME STEP NUMBER            1411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20813E-02 0.90282E+00
   Friction velocity        uk    :  0.20813E-02 0.90282E+00
   Dimensionless distance   yplus :  0.16756E-01 0.72683E+01
   Friction thermal sca.    tstar : -0.15835E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12502E-01 0.54230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87886E-02      33   0.31188E-03   0.32713E+01 0.13157E+03 
c  Velocity[X]                                      0.14496E+01 
c  Velocity[Y]                                      0.18216E+01 
c  Velocity[Z]                                      0.12720E-29 
c  Pressure     0.13513E-06     474   0.99454E-08   0.11542E+00 0.93748E+03 
c  nu_tilda     0.58441E-05      32   0.54591E-05   0.28215E-06 0.14843E+03 
c  TempC        0.35488E+02      27   0.28874E-03   0.54520E+01 0.25701E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3566          10.417          4.5729          4.5729
v  Velocity[Y]            -2.6669          7.3757      -0.0010839      -0.0010839
v  Velocity[Z]       -9.8385e-015     9.3468e-015    -6.7874e-018    -6.7874e-018
v  ǁVelocityǁ         0.0012399          10.417          5.2256          5.2256
v  Pressure               -47.322          15.893         -10.943         -10.943
v  nu_tilda           4.3901e-007       0.0042695       0.0013486       0.0013486
v  TempC                       21          73.057          21.845          21.845
v  TurbVisc           3.2711e-014        0.005032       0.0015828       0.0015828
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1411:        0.20770E+01

===============================================================


 INSTANT    0.141200000E+04   TIME STEP NUMBER            1412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22236E-02 0.90250E+00
   Friction velocity        uk    :  0.22236E-02 0.90250E+00
   Dimensionless distance   yplus :  0.17901E-01 0.72658E+01
   Friction thermal sca.    tstar : -0.43201E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13356E-01 0.54211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87909E-02      33   0.31949E-03   0.33150E+01 0.13196E+03 
c  Velocity[X]                                      0.14952E+01 
c  Velocity[Y]                                      0.18198E+01 
c  Velocity[Z]                                      0.16538E-29 
c  Pressure     0.11900E-06     505   0.94150E-08   0.10408E+00 0.13169E+04 
c  nu_tilda     0.58461E-05      32   0.16035E-04   0.28255E-06 0.14852E+03 
c  TempC        0.35498E+02      27   0.43751E-03   0.36688E+01 0.21089E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3534          10.416          4.5729          4.5729
v  Velocity[Y]            -2.6654          7.3482      -0.0010662      -0.0010662
v  Velocity[Z]       -1.0703e-014     9.3339e-015     -6.807e-018     -6.807e-018
v  ǁVelocityǁ          0.001935          10.417          5.2253          5.2253
v  Pressure               -47.327          15.666         -11.021         -11.021
v  nu_tilda           4.3901e-007       0.0042695       0.0013491       0.0013491
v  TempC                       21          73.057          21.845          21.845
v  TurbVisc           3.2679e-014        0.005032       0.0015834       0.0015834
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1412:        0.21410E+01

===============================================================


 INSTANT    0.141300000E+04   TIME STEP NUMBER            1413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83836E-02 0.90110E+00
   Friction velocity        uk    :  0.83836E-02 0.90110E+00
   Dimensionless distance   yplus :  0.67494E-01 0.72545E+01
   Friction thermal sca.    tstar : -0.39287E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50358E-01 0.54126E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87931E-02      33   0.31664E-03   0.33029E+01 0.13206E+03 
c  Velocity[X]                                      0.14573E+01 
c  Velocity[Y]                                      0.18456E+01 
c  Velocity[Z]                                      0.12357E-29 
c  Pressure     0.11567E-06     505   0.97488E-08   0.10001E+00 0.13311E+04 
c  nu_tilda     0.58482E-05      32   0.54588E-05   0.28292E-06 0.14861E+03 
c  TempC        0.35507E+02      28   0.36200E-03   0.52545E+01 0.24237E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3502          10.416          4.5729          4.5729
v  Velocity[Y]            -2.6638          7.3692      -0.0010481      -0.0010481
v  Velocity[Z]       -9.5128e-015     9.3136e-015    -6.8227e-018    -6.8227e-018
v  ǁVelocityǁ         0.0015005          10.416           5.225           5.225
v  Pressure               -47.287          15.897         -10.951         -10.951
v  nu_tilda           4.3901e-007       0.0042695       0.0013497       0.0013497
v  TempC                       21          73.058          21.845          21.845
v  TurbVisc           3.2679e-014        0.005032        0.001584        0.001584
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1413:        0.21500E+01

===============================================================


 INSTANT    0.141400000E+04   TIME STEP NUMBER            1414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79794E-02 0.90194E+00
   Friction velocity        uk    :  0.79794E-02 0.90194E+00
   Dimensionless distance   yplus :  0.64239E-01 0.72612E+01
   Friction thermal sca.    tstar : -0.40934E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47930E-01 0.54177E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87953E-02      33   0.33287E-03   0.33056E+01 0.13216E+03 
c  Velocity[X]                                      0.14712E+01 
c  Velocity[Y]                                      0.18344E+01 
c  Velocity[Z]                                      0.11894E-29 
c  Pressure     0.13058E-06     520   0.97127E-08   0.11297E+00 0.15692E+04 
c  nu_tilda     0.58502E-05      32   0.16037E-04   0.28332E-06 0.14869E+03 
c  TempC        0.35517E+02      27   0.30189E-03   0.58108E+01 0.24761E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3469          10.416          4.5729          4.5729
v  Velocity[Y]            -2.6623          7.3418      -0.0010297      -0.0010297
v  Velocity[Z]       -9.1055e-015     9.2975e-015    -6.8371e-018    -6.8371e-018
v  ǁVelocityǁ         0.0007883          10.416          5.2248          5.2248
v  Pressure               -47.285          15.614         -11.037         -11.037
v  nu_tilda           4.3906e-007       0.0042695       0.0013502       0.0013502
v  TempC                       21          73.057          21.846          21.846
v  TurbVisc            3.268e-014        0.005032       0.0015847       0.0015847
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1414:        0.21850E+01

===============================================================


 INSTANT    0.141500000E+04   TIME STEP NUMBER            1415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28926E-02 0.90140E+00
   Friction velocity        uk    :  0.28926E-02 0.90140E+00
   Dimensionless distance   yplus :  0.23287E-01 0.72569E+01
   Friction thermal sca.    tstar : -0.32067E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17375E-01 0.54144E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87975E-02      33   0.27201E-03   0.33224E+01 0.13238E+03 
c  Velocity[X]                                      0.14887E+01 
c  Velocity[Y]                                      0.18337E+01 
c  Velocity[Z]                                      0.11191E-29 
c  Pressure     0.12530E-06     490   0.96344E-08   0.10842E+00 0.15087E+04 
c  nu_tilda     0.58523E-05      32   0.54525E-05   0.28370E-06 0.14878E+03 
c  TempC        0.35526E+02      26   0.47110E-03   0.49510E+01 0.24691E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3438          10.415          4.5729          4.5729
v  Velocity[Y]            -2.6608          7.3714      -0.0010106      -0.0010106
v  Velocity[Z]       -9.9228e-015      9.284e-015    -6.8642e-018    -6.8642e-018
v  ǁVelocityǁ        0.00051399          10.415          5.2245          5.2245
v  Pressure               -47.248          15.883         -10.959         -10.959
v  nu_tilda           4.3908e-007       0.0042695       0.0013508       0.0013508
v  TempC                       21          73.057          21.846          21.846
v  TurbVisc           3.2692e-014        0.005032       0.0015853       0.0015853
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1415:        0.21120E+01

===============================================================


 INSTANT    0.141600000E+04   TIME STEP NUMBER            1416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65898E-02 0.90284E+00
   Friction velocity        uk    :  0.65898E-02 0.90284E+00
   Dimensionless distance   yplus :  0.53052E-01 0.72685E+01
   Friction thermal sca.    tstar : -0.49897E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39583E-01 0.54231E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.87998E-02      33   0.31257E-03   0.33053E+01 0.13244E+03 
c  Velocity[X]                                      0.14513E+01 
c  Velocity[Y]                                      0.18540E+01 
c  Velocity[Z]                                      0.13391E-29 
c  Pressure     0.10860E-06     456   0.95771E-08   0.93599E-01 0.80058E+03 
c  nu_tilda     0.58543E-05      32   0.16029E-04   0.28410E-06 0.14887E+03 
c  TempC        0.35536E+02      27   0.38792E-03   0.66000E+01 0.29482E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3407          10.415          4.5729          4.5729
v  Velocity[Y]            -2.6593          7.3796     -0.00099097     -0.00099097
v  Velocity[Z]       -8.7607e-015     8.8649e-015     -6.877e-018     -6.877e-018
v  ǁVelocityǁ          0.001126          10.415          5.2242          5.2242
v  Pressure               -47.248          15.772         -11.009         -11.009
v  nu_tilda           4.3907e-007       0.0042695       0.0013513       0.0013513
v  TempC                       21          73.057          21.846          21.846
v  TurbVisc             3.27e-014        0.005032        0.001586        0.001586
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1416:        0.21460E+01

===============================================================


 INSTANT    0.141700000E+04   TIME STEP NUMBER            1417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30453E-02 0.90242E+00
   Friction velocity        uk    :  0.30453E-02 0.90242E+00
   Dimensionless distance   yplus :  0.24517E-01 0.72651E+01
   Friction thermal sca.    tstar : -0.39126E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18292E-01 0.54206E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88020E-02      33   0.31230E-03   0.33402E+01 0.13262E+03 
c  Velocity[X]                                      0.14917E+01 
c  Velocity[Y]                                      0.18485E+01 
c  Velocity[Z]                                      0.12843E-29 
c  Pressure     0.14555E-06     440   0.96804E-08   0.12597E+00 0.49155E+03 
c  nu_tilda     0.58564E-05      32   0.54539E-05   0.28448E-06 0.14895E+03 
c  TempC        0.35545E+02      27   0.37792E-03   0.62453E+01 0.26235E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3376          10.415          4.5729          4.5729
v  Velocity[Y]            -2.6578          7.3483     -0.00097092     -0.00097092
v  Velocity[Z]       -8.3257e-015     9.1921e-015    -6.8961e-018    -6.8961e-018
v  ǁVelocityǁ         0.0019037          10.415          5.2239          5.2239
v  Pressure               -47.205          15.756         -10.987         -10.987
v  nu_tilda           4.3913e-007       0.0042695       0.0013519       0.0013519
v  TempC                       21          73.057          21.846          21.846
v  TurbVisc           3.2695e-014        0.005032       0.0015866       0.0015866
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1417:        0.22620E+01

===============================================================


 INSTANT    0.141800000E+04   TIME STEP NUMBER            1418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57783E-02 0.90112E+00
   Friction velocity        uk    :  0.57783E-02 0.90112E+00
   Dimensionless distance   yplus :  0.46519E-01 0.72546E+01
   Friction thermal sca.    tstar : -0.56665E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34708E-01 0.54128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88043E-02      33   0.31393E-03   0.33373E+01 0.13277E+03 
c  Velocity[X]                                      0.14912E+01 
c  Velocity[Y]                                      0.18461E+01 
c  Velocity[Z]                                      0.10921E-29 
c  Pressure     0.11187E-06     457   0.91897E-08   0.96804E-01 0.49120E+03 
c  nu_tilda     0.58585E-05      32   0.16031E-04   0.28488E-06 0.14904E+03 
c  TempC        0.35555E+02      26   0.30743E-03   0.51369E+01 0.24277E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3344          10.414          4.5729          4.5729
v  Velocity[Y]            -2.6563          7.3692     -0.00095094     -0.00095094
v  Velocity[Z]       -9.1151e-015     9.3021e-015    -6.9117e-018    -6.9117e-018
v  ǁVelocityǁ         0.0015241          10.414          5.2237          5.2237
v  Pressure               -47.209          15.739         -11.023         -11.023
v  nu_tilda           4.3921e-007       0.0042695       0.0013524       0.0013524
v  TempC                       21          73.056          21.847          21.847
v  TurbVisc           3.2714e-014        0.005032       0.0015872       0.0015872
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1418:        0.22140E+01

===============================================================


 INSTANT    0.141900000E+04   TIME STEP NUMBER            1419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68059E-02 0.90222E+00
   Friction velocity        uk    :  0.68059E-02 0.90222E+00
   Dimensionless distance   yplus :  0.54792E-01 0.72635E+01
   Friction thermal sca.    tstar : -0.48365E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40881E-01 0.54194E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88065E-02      33   0.32589E-03   0.33383E+01 0.13294E+03 
c  Velocity[X]                                      0.14713E+01 
c  Velocity[Y]                                      0.18670E+01 
c  Velocity[Z]                                      0.12689E-29 
c  Pressure     0.12551E-06     456   0.96673E-08   0.10963E+00 0.57055E+03 
c  nu_tilda     0.58605E-05      32   0.54403E-05   0.28525E-06 0.14913E+03 
c  TempC        0.35564E+02      26   0.32314E-03   0.38812E+01 0.22203E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3311          10.414          4.5729          4.5729
v  Velocity[Y]            -2.6548          7.3484     -0.00092981     -0.00092981
v  Velocity[Z]       -7.8677e-015     9.3194e-015    -6.9349e-018    -6.9349e-018
v  ǁVelocityǁ        0.00079702          10.414          5.2234          5.2234
v  Pressure               -47.168          15.759         -10.994         -10.994
v  nu_tilda           4.3927e-007       0.0042695       0.0013529       0.0013529
v  TempC                       21          73.056          21.847          21.847
v  TurbVisc           3.2737e-014        0.005032       0.0015879       0.0015879
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1419:        0.22610E+01

===============================================================


 INSTANT    0.142000000E+04   TIME STEP NUMBER            1420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37940E-02 0.90127E+00
   Friction velocity        uk    :  0.37940E-02 0.90127E+00
   Dimensionless distance   yplus :  0.30544E-01 0.72558E+01
   Friction thermal sca.    tstar : -0.86362E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22789E-01 0.54137E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88087E-02      33   0.27447E-03   0.33336E+01 0.13301E+03 
c  Velocity[X]                                      0.14763E+01 
c  Velocity[Y]                                      0.18573E+01 
c  Velocity[Z]                                      0.14375E-29 
c  Pressure     0.12623E-06     458   0.92572E-08   0.10759E+00 0.60142E+03 
c  nu_tilda     0.58626E-05      32   0.16030E-04   0.28565E-06 0.14921E+03 
c  TempC        0.35574E+02      26   0.38791E-03   0.41035E+01 0.22053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3278          10.413          4.5729          4.5729
v  Velocity[Y]            -2.6533          7.3685     -0.00090844     -0.00090844
v  Velocity[Z]       -7.5212e-015      9.307e-015    -6.9498e-018    -6.9498e-018
v  ǁVelocityǁ        0.00052466          10.413          5.2231          5.2231
v  Pressure               -47.172          15.704         -11.036         -11.036
v  nu_tilda           4.3934e-007       0.0042695       0.0013534       0.0013534
v  TempC                       21          73.056          21.847          21.847
v  TurbVisc           3.2755e-014        0.005032       0.0015885       0.0015885
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1420:        0.22370E+01

===============================================================


 INSTANT    0.142100000E+04   TIME STEP NUMBER            1421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45026E-02 0.90298E+00
   Friction velocity        uk    :  0.45026E-02 0.90298E+00
   Dimensionless distance   yplus :  0.36249E-01 0.72696E+01
   Friction thermal sca.    tstar : -0.73006E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27046E-01 0.54239E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88109E-02      33   0.33713E-03   0.33453E+01 0.13321E+03 
c  Velocity[X]                                      0.14852E+01 
c  Velocity[Y]                                      0.18601E+01 
c  Velocity[Z]                                      0.12647E-29 
c  Pressure     0.13273E-06     488   0.92508E-08   0.11489E+00 0.95834E+03 
c  nu_tilda     0.58646E-05      32   0.54441E-05   0.28603E-06 0.14930E+03 
c  TempC        0.35584E+02      27   0.32884E-03   0.41348E+01 0.22492E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3248          10.413          4.5729          4.5729
v  Velocity[Y]            -2.6517          7.3831     -0.00088661     -0.00088661
v  Velocity[Z]        -8.246e-015      9.287e-015     -6.968e-018     -6.968e-018
v  ǁVelocityǁ         0.0011498          10.413          5.2228          5.2228
v  Pressure               -47.132          15.841         -10.985         -10.985
v  nu_tilda           4.3936e-007       0.0042695        0.001354        0.001354
v  TempC                       21          73.056          21.848          21.848
v  TurbVisc           3.2777e-014        0.005032       0.0015891       0.0015891
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1421:        0.23700E+01

===============================================================


 INSTANT    0.142200000E+04   TIME STEP NUMBER            1422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75866E-02 0.90266E+00
   Friction velocity        uk    :  0.75866E-02 0.90266E+00
   Dimensionless distance   yplus :  0.61077E-01 0.72671E+01
   Friction thermal sca.    tstar : -0.41237E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45570E-01 0.54220E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88132E-02      33   0.29618E-03   0.33728E+01 0.13350E+03 
c  Velocity[X]                                      0.14914E+01 
c  Velocity[Y]                                      0.18814E+01 
c  Velocity[Z]                                      0.13405E-29 
c  Pressure     0.12787E-06     505   0.97958E-08   0.11176E+00 0.12997E+04 
c  nu_tilda     0.58667E-05      32   0.16022E-04   0.28644E-06 0.14939E+03 
c  TempC        0.35593E+02      27   0.38963E-03   0.38627E+01 0.21196E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3217          10.412          4.5729          4.5729
v  Velocity[Y]            -2.6502          7.3519     -0.00086469     -0.00086469
v  Velocity[Z]       -7.1281e-015     9.2712e-015     -6.981e-018     -6.981e-018
v  ǁVelocityǁ         0.0019709          10.412          5.2225          5.2225
v  Pressure               -47.129          15.622         -11.059         -11.059
v  nu_tilda           4.3942e-007       0.0042695       0.0013545       0.0013545
v  TempC                       21          73.056          21.848          21.848
v  TurbVisc           3.2783e-014        0.005032       0.0015898       0.0015898
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1422:        0.22410E+01

===============================================================


 INSTANT    0.142300000E+04   TIME STEP NUMBER            1423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18448E-02 0.90113E+00
   Friction velocity        uk    :  0.18448E-02 0.90113E+00
   Dimensionless distance   yplus :  0.14852E-01 0.72547E+01
   Friction thermal sca.    tstar : -0.18215E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11081E-01 0.54128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88154E-02      33   0.31108E-03   0.33525E+01 0.13342E+03 
c  Velocity[X]                                      0.14812E+01 
c  Velocity[Y]                                      0.18713E+01 
c  Velocity[Z]                                      0.13193E-29 
c  Pressure     0.12622E-06     505   0.91597E-08   0.10780E+00 0.10924E+04 
c  nu_tilda     0.58687E-05      32   0.54403E-05   0.28682E-06 0.14947E+03 
c  TempC        0.35603E+02      27   0.37809E-03   0.63035E+01 0.26888E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3185          10.412          4.5729          4.5729
v  Velocity[Y]            -2.6487          7.3702     -0.00084171     -0.00084171
v  Velocity[Z]       -6.9287e-015     9.0383e-015    -7.0063e-018    -7.0063e-018
v  ǁVelocityǁ         0.0014503          10.412          5.2223          5.2223
v  Pressure               -47.094          15.795         -11.002         -11.002
v  nu_tilda           4.3942e-007       0.0042695       0.0013551       0.0013551
v  TempC                       21          73.056          21.848          21.848
v  TurbVisc           3.2801e-014        0.005032       0.0015904       0.0015904
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1423:        0.23780E+01

===============================================================


 INSTANT    0.142400000E+04   TIME STEP NUMBER            1424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71253E-02 0.90235E+00
   Friction velocity        uk    :  0.71253E-02 0.90235E+00
   Dimensionless distance   yplus :  0.57364E-01 0.72645E+01
   Friction thermal sca.    tstar : -0.46292E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42800E-01 0.54202E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88176E-02      33   0.33134E-03   0.33781E+01 0.13371E+03 
c  Velocity[X]                                      0.15092E+01 
c  Velocity[Y]                                      0.18689E+01 
c  Velocity[Z]                                      0.13105E-29 
c  Pressure     0.11326E-06     489   0.90909E-08   0.98615E-01 0.11746E+04 
c  nu_tilda     0.58708E-05      32   0.16026E-04   0.28723E-06 0.14956E+03 
c  TempC        0.35612E+02      26   0.39027E-03   0.59009E+01 0.26373E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3152          10.411          4.5729          4.5729
v  Velocity[Y]            -2.6472           7.348     -0.00081867     -0.00081867
v  Velocity[Z]       -7.5533e-015     9.1721e-015     -7.024e-018     -7.024e-018
v  ǁVelocityǁ        0.00070102          10.412           5.222           5.222
v  Pressure               -47.095          15.599         -11.071         -11.071
v  nu_tilda           4.3949e-007       0.0042695       0.0013556       0.0013556
v  TempC                       21          73.056          21.848          21.848
v  TurbVisc           3.2802e-014        0.005032        0.001591        0.001591
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1424:        0.21080E+01

===============================================================


 INSTANT    0.142500000E+04   TIME STEP NUMBER            1425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63719E-02 0.90161E+00
   Friction velocity        uk    :  0.63719E-02 0.90161E+00
   Dimensionless distance   yplus :  0.51298E-01 0.72586E+01
   Friction thermal sca.    tstar : -0.51677E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38274E-01 0.54157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88198E-02      33   0.24570E-03   0.33767E+01 0.13383E+03 
c  Velocity[X]                                      0.14823E+01 
c  Velocity[Y]                                      0.18944E+01 
c  Velocity[Z]                                      0.11256E-29 
c  Pressure     0.12034E-06     489   0.91375E-08   0.10381E+00 0.14142E+04 
c  nu_tilda     0.58729E-05      32   0.54257E-05   0.28760E-06 0.14965E+03 
c  TempC        0.35621E+02      26   0.31850E-03   0.61244E+01 0.26887E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.312          10.411          4.5729          4.5729
v  Velocity[Y]            -2.6457          7.3745     -0.00079477     -0.00079477
v  Velocity[Z]       -6.9287e-015     9.3581e-015    -7.0398e-018    -7.0398e-018
v  ǁVelocityǁ         0.0006034          10.411          5.2217          5.2217
v  Pressure               -47.053          15.838         -10.995         -10.995
v  nu_tilda           4.3952e-007       0.0042695       0.0013561       0.0013561
v  TempC                       21          73.056          21.849          21.849
v  TurbVisc           3.2822e-014        0.005032       0.0015917       0.0015917
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1425:        0.21260E+01

===============================================================


 INSTANT    0.142600000E+04   TIME STEP NUMBER            1426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90085E-02 0.90280E+00
   Friction velocity        uk    :  0.90085E-02 0.90280E+00
   Dimensionless distance   yplus :  0.72524E-01 0.72682E+01
   Friction thermal sca.    tstar : -0.38882E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54111E-01 0.54229E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88221E-02      33   0.32984E-03   0.33489E+01 0.13379E+03 
c  Velocity[X]                                      0.14647E+01 
c  Velocity[Y]                                      0.18841E+01 
c  Velocity[Z]                                      0.10141E-29 
c  Pressure     0.12557E-06     504   0.93657E-08   0.10731E+00 0.11510E+04 
c  nu_tilda     0.58749E-05      32   0.16018E-04   0.28801E-06 0.14974E+03 
c  TempC        0.35631E+02      27   0.33036E-03   0.47267E+01 0.23104E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3088          10.411          4.5729          4.5729
v  Velocity[Y]            -2.6442           7.378     -0.00077093     -0.00077093
v  Velocity[Z]       -6.9287e-015     9.3826e-015    -7.0588e-018    -7.0588e-018
v  ǁVelocityǁ         0.0013293          10.411          5.2214          5.2214
v  Pressure               -47.057          15.665         -11.065         -11.065
v  nu_tilda            4.395e-007       0.0042695       0.0013566       0.0013566
v  TempC                       21          73.056          21.849          21.849
v  TurbVisc           3.2831e-014        0.005032       0.0015923       0.0015923
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1426:        0.21520E+01

===============================================================


 INSTANT    0.142700000E+04   TIME STEP NUMBER            1427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87049E-02 0.90265E+00
   Friction velocity        uk    :  0.87049E-02 0.90265E+00
   Dimensionless distance   yplus :  0.70081E-01 0.72669E+01
   Friction thermal sca.    tstar : -0.37177E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52288E-01 0.54219E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88243E-02      33   0.32620E-03   0.34057E+01 0.13423E+03 
c  Velocity[X]                                      0.15234E+01 
c  Velocity[Y]                                      0.18823E+01 
c  Velocity[Z]                                      0.11949E-29 
c  Pressure     0.14206E-06     456   0.96407E-08   0.12412E+00 0.64799E+03 
c  nu_tilda     0.58770E-05      32   0.54252E-05   0.28839E-06 0.14982E+03 
c  TempC        0.35640E+02      27   0.41200E-03   0.39933E+01 0.21082E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3057           10.41          4.5729          4.5729
v  Velocity[Y]            -2.6427          7.3546     -0.00074638     -0.00074638
v  Velocity[Z]       -6.9287e-015     9.2818e-015    -7.0869e-018    -7.0869e-018
v  ǁVelocityǁ         0.0020422           10.41          5.2211          5.2211
v  Pressure               -47.015            15.7          -11.03          -11.03
v  nu_tilda           4.3957e-007       0.0042695       0.0013572       0.0013572
v  TempC                       21          73.055          21.849          21.849
v  TurbVisc           3.2826e-014        0.005032       0.0015929       0.0015929
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1427:        0.20410E+01

===============================================================


 INSTANT    0.142800000E+04   TIME STEP NUMBER            1428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36118E-02 0.90137E+00
   Friction velocity        uk    :  0.36118E-02 0.90137E+00
   Dimensionless distance   yplus :  0.29077E-01 0.72567E+01
   Friction thermal sca.    tstar : -0.91289E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21695E-01 0.54143E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88265E-02      33   0.31381E-03   0.33897E+01 0.13429E+03 
c  Velocity[X]                                      0.14869E+01 
c  Velocity[Y]                                      0.19028E+01 
c  Velocity[Z]                                      0.12372E-29 
c  Pressure     0.11517E-06     426   0.99399E-08   0.99064E-01 0.36705E+03 
c  nu_tilda     0.58791E-05      32   0.16018E-04   0.28880E-06 0.14991E+03 
c  TempC        0.35650E+02      27   0.29910E-03   0.52910E+01 0.24115E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3026           10.41          4.5729          4.5729
v  Velocity[Y]            -2.6412          7.3731     -0.00072104     -0.00072104
v  Velocity[Z]       -6.9287e-015     9.3431e-015    -7.1079e-018    -7.1079e-018
v  ǁVelocityǁ         0.0011611           10.41          5.2209          5.2209
v  Pressure               -47.015          15.707         -11.057         -11.057
v  nu_tilda           4.3963e-007       0.0042695       0.0013577       0.0013577
v  TempC                       21          73.056          21.849          21.849
v  TurbVisc           3.2847e-014        0.005032       0.0015936       0.0015936
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1428:        0.19710E+01

===============================================================


 INSTANT    0.142900000E+04   TIME STEP NUMBER            1429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92408E-02 0.90241E+00
   Friction velocity        uk    :  0.92408E-02 0.90241E+00
   Dimensionless distance   yplus :  0.74395E-01 0.72651E+01
   Friction thermal sca.    tstar : -0.35622E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55507E-01 0.54205E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88288E-02      33   0.32391E-03   0.34003E+01 0.13435E+03 
c  Velocity[X]                                      0.15028E+01 
c  Velocity[Y]                                      0.18975E+01 
c  Velocity[Z]                                      0.12413E-29 
c  Pressure     0.13928E-06     442   0.92841E-08   0.12026E+00 0.43951E+03 
c  nu_tilda     0.58811E-05      32   0.54166E-05   0.28919E-06 0.15000E+03 
c  TempC        0.35659E+02      27   0.28821E-03   0.40313E+01 0.20581E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2994          10.409          4.5729          4.5729
v  Velocity[Y]            -2.6397          7.3489     -0.00069537     -0.00069537
v  Velocity[Z]       -6.9287e-015     9.2448e-015    -7.1324e-018    -7.1324e-018
v  ǁVelocityǁ        0.00051626          10.409          5.2206          5.2206
v  Pressure               -46.975          15.678          -11.04          -11.04
v  nu_tilda           4.3969e-007       0.0042695       0.0013583       0.0013583
v  TempC                       21          73.055           21.85           21.85
v  TurbVisc           3.2863e-014        0.005032       0.0015942       0.0015942
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1429:        0.21460E+01

===============================================================


 INSTANT    0.143000000E+04   TIME STEP NUMBER            1430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43666E-02 0.90181E+00
   Friction velocity        uk    :  0.43666E-02 0.90181E+00
   Dimensionless distance   yplus :  0.35154E-01 0.72602E+01
   Friction thermal sca.    tstar : -0.75523E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26229E-01 0.54169E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88310E-02      33   0.25809E-03   0.34119E+01 0.13457E+03 
c  Velocity[X]                                      0.15155E+01 
c  Velocity[Y]                                      0.18964E+01 
c  Velocity[Z]                                      0.13138E-29 
c  Pressure     0.11842E-06     442   0.96185E-08   0.10266E+00 0.44764E+03 
c  nu_tilda     0.58832E-05      32   0.16019E-04   0.28960E-06 0.15009E+03 
c  TempC        0.35669E+02      27   0.38926E-03   0.36511E+01 0.19650E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2961          10.409          4.5729          4.5729
v  Velocity[Y]            -2.6382          7.3758     -0.00066967     -0.00066967
v  Velocity[Z]       -6.9287e-015     9.1191e-015    -7.1463e-018    -7.1463e-018
v  ǁVelocityǁ         0.0008652          10.409          5.2203          5.2203
v  Pressure               -46.977           15.67         -11.072         -11.072
v  nu_tilda           4.3977e-007       0.0042695       0.0013588       0.0013588
v  TempC                       21          73.055           21.85           21.85
v  TurbVisc           3.2882e-014        0.005032       0.0015948       0.0015948
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1430:        0.20410E+01

===============================================================


 INSTANT    0.143100000E+04   TIME STEP NUMBER            1431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77119E-02 0.90342E+00
   Friction velocity        uk    :  0.77119E-02 0.90342E+00
   Dimensionless distance   yplus :  0.62086E-01 0.72732E+01
   Friction thermal sca.    tstar : -0.42574E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46323E-01 0.54266E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88332E-02      33   0.30425E-03   0.33835E+01 0.13459E+03 
c  Velocity[X]                                      0.14665E+01 
c  Velocity[Y]                                      0.19170E+01 
c  Velocity[Z]                                      0.13161E-29 
c  Pressure     0.11237E-06     472   0.99630E-08   0.97309E-01 0.89722E+03 
c  nu_tilda     0.58853E-05      32   0.54122E-05   0.28998E-06 0.15017E+03 
c  TempC        0.35678E+02      27   0.31038E-03   0.64153E+01 0.27233E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2928          10.408          4.5729          4.5729
v  Velocity[Y]            -2.6366          7.3879     -0.00064284     -0.00064284
v  Velocity[Z]       -6.9287e-015     9.1448e-015    -7.1766e-018    -7.1766e-018
v  ǁVelocityǁ         0.0016793          10.408            5.22            5.22
v  Pressure                -46.94          15.797         -11.025         -11.025
v  nu_tilda           4.3974e-007       0.0042695       0.0013594       0.0013594
v  TempC                       21          73.056           21.85           21.85
v  TurbVisc           3.2905e-014        0.005032       0.0015955       0.0015955
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1431:        0.20690E+01

===============================================================


 INSTANT    0.143200000E+04   TIME STEP NUMBER            1432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32397E-02 0.90290E+00
   Friction velocity        uk    :  0.32397E-02 0.90290E+00
   Dimensionless distance   yplus :  0.26082E-01 0.72690E+01
   Friction thermal sca.    tstar : -0.27125E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19460E-01 0.54235E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88354E-02      33   0.31983E-03   0.34116E+01 0.13482E+03 
c  Velocity[X]                                      0.15043E+01 
c  Velocity[Y]                                      0.19073E+01 
c  Velocity[Z]                                      0.15363E-29 
c  Pressure     0.12497E-06     538   0.93036E-08   0.10796E+00 0.14148E+04 
c  nu_tilda     0.58873E-05      32   0.16011E-04   0.29039E-06 0.15026E+03 
c  TempC        0.35688E+02      27   0.34342E-03   0.44512E+01 0.23059E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2897          10.408          4.5729          4.5729
v  Velocity[Y]            -2.6352          7.3541     -0.00061579     -0.00061579
v  Velocity[Z]       -6.9287e-015     9.2505e-015    -7.1932e-018    -7.1932e-018
v  ǁVelocityǁ          0.001627          10.408          5.2197          5.2197
v  Pressure                -46.94           15.54         -11.104         -11.104
v  nu_tilda            4.398e-007       0.0042695       0.0013598       0.0013598
v  TempC                       21          73.055           21.85           21.85
v  TurbVisc           3.2896e-014        0.005032       0.0015961       0.0015961
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1432:        0.22210E+01

===============================================================


 INSTANT    0.143300000E+04   TIME STEP NUMBER            1433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14295E-02 0.90167E+00
   Friction velocity        uk    :  0.14295E-02 0.90167E+00
   Dimensionless distance   yplus :  0.11508E-01 0.72590E+01
   Friction thermal sca.    tstar : -0.69442E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85864E-02 0.54160E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88376E-02      33   0.32907E-03   0.34279E+01 0.13503E+03 
c  Velocity[X]                                      0.15186E+01 
c  Velocity[Y]                                      0.19093E+01 
c  Velocity[Z]                                      0.11837E-29 
c  Pressure     0.13148E-06     522   0.92818E-08   0.11381E+00 0.14455E+04 
c  nu_tilda     0.58894E-05      32   0.54048E-05   0.29078E-06 0.15035E+03 
c  TempC        0.35697E+02      26   0.38160E-03   0.49292E+01 0.23370E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2866          10.407          4.5729          4.5729
v  Velocity[Y]            -2.6337          7.3784      -0.0005881      -0.0005881
v  Velocity[Z]       -6.9287e-015     9.2671e-015    -7.2183e-018    -7.2183e-018
v  ǁVelocityǁ        0.00078837          10.407          5.2194          5.2194
v  Pressure               -46.898          15.791         -11.028         -11.028
v  nu_tilda           4.3984e-007       0.0042695       0.0013604       0.0013604
v  TempC                       21          73.055          21.851          21.851
v  TurbVisc           3.2913e-014        0.005032       0.0015967       0.0015967
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1433:        0.21890E+01

===============================================================


 INSTANT    0.143400000E+04   TIME STEP NUMBER            1434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90805E-02 0.90268E+00
   Friction velocity        uk    :  0.90805E-02 0.90268E+00
   Dimensionless distance   yplus :  0.73104E-01 0.72672E+01
   Friction thermal sca.    tstar : -0.31635E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54544E-01 0.54222E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88399E-02      33   0.32664E-03   0.34353E+01 0.13525E+03 
c  Velocity[X]                                      0.15044E+01 
c  Velocity[Y]                                      0.19309E+01 
c  Velocity[Z]                                      0.11231E-29 
c  Pressure     0.12131E-06     522   0.95894E-08   0.10612E+00 0.14874E+04 
c  nu_tilda     0.58915E-05      32   0.16014E-04   0.29119E-06 0.15044E+03 
c  TempC        0.35707E+02      26   0.37728E-03   0.58058E+01 0.26112E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2834          10.407          4.5729          4.5729
v  Velocity[Y]            -2.6322          7.3542      -0.0005604      -0.0005604
v  Velocity[Z]       -6.9287e-015     9.2534e-015    -7.2349e-018    -7.2349e-018
v  ǁVelocityǁ        0.00054495          10.407          5.2192          5.2192
v  Pressure               -46.902          15.538         -11.115         -11.115
v  nu_tilda           4.3991e-007       0.0042695       0.0013609       0.0013609
v  TempC                       21          73.055          21.851          21.851
v  TurbVisc           3.2928e-014        0.005032       0.0015974       0.0015974
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1434:        0.21840E+01

===============================================================


 INSTANT    0.143500000E+04   TIME STEP NUMBER            1435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56213E-03 0.90186E+00
   Friction velocity        uk    :  0.56213E-03 0.90186E+00
   Dimensionless distance   yplus :  0.45255E-02 0.72606E+01
   Friction thermal sca.    tstar : -0.58612E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33766E-02 0.54172E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88421E-02      33   0.25691E-03   0.34281E+01 0.13522E+03 
c  Velocity[X]                                      0.15068E+01 
c  Velocity[Y]                                      0.19213E+01 
c  Velocity[Z]                                      0.10855E-29 
c  Pressure     0.13090E-06     474   0.96279E-08   0.11282E+00 0.11743E+04 
c  nu_tilda     0.58936E-05      32   0.53909E-05   0.29157E-06 0.15053E+03 
c  TempC        0.35716E+02      27   0.29457E-03   0.46699E+01 0.24811E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2801          10.406          4.5729          4.5729
v  Velocity[Y]            -2.6306          7.3773     -0.00053161     -0.00053161
v  Velocity[Z]       -6.9287e-015     9.2332e-015    -7.2639e-018    -7.2639e-018
v  ǁVelocityǁ         0.0012697          10.406          5.2189          5.2189
v  Pressure               -46.862          15.729         -11.053         -11.053
v  nu_tilda            4.399e-007       0.0042695       0.0013615       0.0013615
v  TempC                       21          73.055          21.851          21.851
v  TurbVisc           3.2948e-014        0.005032        0.001598        0.001598
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1435:        0.21070E+01

===============================================================


 INSTANT    0.143600000E+04   TIME STEP NUMBER            1436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44281E-02 0.90347E+00
   Friction velocity        uk    :  0.44281E-02 0.90347E+00
   Dimensionless distance   yplus :  0.35650E-01 0.72735E+01
   Friction thermal sca.    tstar : -0.36401E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26599E-01 0.54269E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88443E-02      33   0.32622E-03   0.34248E+01 0.13534E+03 
c  Velocity[X]                                      0.15068E+01 
c  Velocity[Y]                                      0.19180E+01 
c  Velocity[Z]                                      0.11307E-29 
c  Pressure     0.11316E-06     441   0.98339E-08   0.98281E-01 0.58744E+03 
c  nu_tilda     0.58956E-05      32   0.16007E-04   0.29199E-06 0.15062E+03 
c  TempC        0.35726E+02      27   0.34049E-03   0.37630E+01 0.22107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2769          10.406          4.5729          4.5729
v  Velocity[Y]            -2.6291           7.388      -0.0005025      -0.0005025
v  Velocity[Z]       -6.9287e-015     9.2173e-015    -7.2762e-018    -7.2762e-018
v  ǁVelocityǁ         0.0019624          10.406          5.2186          5.2186
v  Pressure               -46.863          15.659         -11.091         -11.091
v  nu_tilda           4.3988e-007       0.0042695        0.001362        0.001362
v  TempC                       21          73.055          21.851          21.851
v  TurbVisc           3.2944e-014        0.005032       0.0015986       0.0015986
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1436:        0.20140E+01

===============================================================


 INSTANT    0.143700000E+04   TIME STEP NUMBER            1437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68493E-02 0.90313E+00
   Friction velocity        uk    :  0.68493E-02 0.90313E+00
   Dimensionless distance   yplus :  0.55141E-01 0.72708E+01
   Friction thermal sca.    tstar : -0.31243E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41142E-01 0.54248E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88465E-02      33   0.30462E-03   0.34521E+01 0.13564E+03 
c  Velocity[X]                                      0.15073E+01 
c  Velocity[Y]                                      0.19448E+01 
c  Velocity[Z]                                      0.16537E-29 
c  Pressure     0.13082E-06     456   0.93052E-08   0.11505E+00 0.53654E+03 
c  nu_tilda     0.58977E-05      32   0.53985E-05   0.29238E-06 0.15070E+03 
c  TempC        0.35735E+02      27   0.42415E-03   0.74352E+01 0.27892E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2736          10.405          4.5729          4.5729
v  Velocity[Y]            -2.6276            7.36     -0.00047304     -0.00047304
v  Velocity[Z]       -6.9287e-015     8.7997e-015    -7.3052e-018    -7.3052e-018
v  ǁVelocityǁ         0.0010989          10.405          5.2183          5.2183
v  Pressure               -46.825          15.679         -11.065         -11.065
v  nu_tilda            4.399e-007       0.0042695       0.0013626       0.0013626
v  TempC                       21          73.055          21.852          21.852
v  TurbVisc           3.2937e-014        0.005032       0.0015992       0.0015992
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1437:        0.20500E+01

===============================================================


 INSTANT    0.143800000E+04   TIME STEP NUMBER            1438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77376E-02 0.90148E+00
   Friction velocity        uk    :  0.77376E-02 0.90148E+00
   Dimensionless distance   yplus :  0.62293E-01 0.72575E+01
   Friction thermal sca.    tstar : -0.38414E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46478E-01 0.54149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88487E-02      33   0.32591E-03   0.34346E+01 0.13564E+03 
c  Velocity[X]                                      0.15012E+01 
c  Velocity[Y]                                      0.19334E+01 
c  Velocity[Z]                                      0.13134E-29 
c  Pressure     0.12529E-06     458   0.97709E-08   0.10764E+00 0.71665E+03 
c  nu_tilda     0.58998E-05      32   0.16006E-04   0.29280E-06 0.15079E+03 
c  TempC        0.35745E+02      27   0.31662E-03   0.74010E+01 0.29922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2706          10.405          4.5729          4.5729
v  Velocity[Y]            -2.6262          7.3752     -0.00044318     -0.00044318
v  Velocity[Z]       -6.9287e-015     9.1175e-015    -7.3196e-018    -7.3196e-018
v  ǁVelocityǁ        0.00046706          10.405           5.218           5.218
v  Pressure               -46.825          15.599         -11.111         -11.111
v  nu_tilda           4.3993e-007       0.0042695        0.001363        0.001363
v  TempC                       21          73.055          21.852          21.852
v  TurbVisc           3.2946e-014        0.005032       0.0015999       0.0015999
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1438:        0.20260E+01

===============================================================


 INSTANT    0.143900000E+04   TIME STEP NUMBER            1439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91338E-02 0.90283E+00
   Friction velocity        uk    :  0.91338E-02 0.90283E+00
   Dimensionless distance   yplus :  0.73534E-01 0.72684E+01
   Friction thermal sca.    tstar : -0.36042E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54864E-01 0.54230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88509E-02      33   0.33224E-03   0.34676E+01 0.13594E+03 
c  Velocity[X]                                      0.15365E+01 
c  Velocity[Y]                                      0.19311E+01 
c  Velocity[Z]                                      0.11143E-29 
c  Pressure     0.13888E-06     456   0.94132E-08   0.12185E+00 0.71938E+03 
c  nu_tilda     0.59019E-05      32   0.53838E-05   0.29318E-06 0.15088E+03 
c  TempC        0.35754E+02      27   0.42682E-03   0.38733E+01 0.21864E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2674          10.404          4.5729          4.5729
v  Velocity[Y]            -2.6247          7.3569     -0.00041243     -0.00041243
v  Velocity[Z]       -6.9287e-015     9.2212e-015    -7.3491e-018    -7.3491e-018
v  ǁVelocityǁ         0.0010287          10.404          5.2177          5.2177
v  Pressure               -46.782          15.658         -11.072         -11.072
v  nu_tilda           4.3999e-007       0.0042695       0.0013636       0.0013636
v  TempC                       21          73.054          21.852          21.852
v  TurbVisc           3.2954e-014        0.005032       0.0016005       0.0016005
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1439:        0.20290E+01

===============================================================


 INSTANT    0.144000000E+04   TIME STEP NUMBER            1440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62221E-02 0.90201E+00
   Friction velocity        uk    :  0.62221E-02 0.90201E+00
   Dimensionless distance   yplus :  0.50092E-01 0.72618E+01
   Friction thermal sca.    tstar : -0.55971E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37374E-01 0.54181E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88532E-02      33   0.25400E-03   0.34622E+01 0.13606E+03 
c  Velocity[X]                                      0.15091E+01 
c  Velocity[Y]                                      0.19531E+01 
c  Velocity[Z]                                      0.11505E-29 
c  Pressure     0.11114E-06     440   0.97362E-08   0.96267E-01 0.44881E+03 
c  nu_tilda     0.59040E-05      32   0.16006E-04   0.29360E-06 0.15097E+03 
c  TempC        0.35763E+02      27   0.38202E-03   0.60611E+01 0.27598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2642          10.404          4.5729          4.5729
v  Velocity[Y]            -2.6232          7.3813     -0.00038127     -0.00038127
v  Velocity[Z]       -6.9287e-015     9.2387e-015     -7.372e-018     -7.372e-018
v  ǁVelocityǁ         0.0017831          10.404          5.2174          5.2174
v  Pressure               -46.787          15.642         -11.106         -11.106
v  nu_tilda           4.4004e-007       0.0042695       0.0013641       0.0013641
v  TempC                       21          73.055          21.852          21.852
v  TurbVisc           3.2973e-014        0.005032       0.0016011       0.0016011
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1440:        0.20010E+01

===============================================================


 INSTANT    0.144100000E+04   TIME STEP NUMBER            1441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99864E-02 0.90354E+00
   Friction velocity        uk    :  0.99864E-02 0.90354E+00
   Dimensionless distance   yplus :  0.80397E-01 0.72741E+01
   Friction thermal sca.    tstar : -0.31873E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59985E-01 0.54273E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88554E-02      33   0.31875E-03   0.34444E+01 0.13597E+03 
c  Velocity[X]                                      0.14972E+01 
c  Velocity[Y]                                      0.19472E+01 
c  Velocity[Z]                                      0.10479E-29 
c  Pressure     0.13419E-06     488   0.95720E-08   0.11542E+00 0.81819E+03 
c  nu_tilda     0.59060E-05      32   0.53757E-05   0.29399E-06 0.15106E+03 
c  TempC        0.35773E+02      27   0.34815E-03   0.58353E+01 0.26393E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.261          10.403          4.5729          4.5729
v  Velocity[Y]            -2.6217          7.3888     -0.00034938     -0.00034938
v  Velocity[Z]       -6.9287e-015     9.2245e-015    -7.3945e-018    -7.3945e-018
v  ǁVelocityǁ         0.0012777          10.403          5.2172          5.2172
v  Pressure               -46.745          15.741         -11.061         -11.061
v  nu_tilda           4.4002e-007       0.0042695       0.0013647       0.0013647
v  TempC                       21          73.055          21.853          21.853
v  TurbVisc           3.2985e-014        0.005032       0.0016018       0.0016018
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1441:        0.21050E+01

===============================================================


 INSTANT    0.144200000E+04   TIME STEP NUMBER            1442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11940E-01 0.90327E+00
   Friction velocity        uk    :  0.11940E-01 0.90327E+00
   Dimensionless distance   yplus :  0.96125E-01 0.72719E+01
   Friction thermal sca.    tstar : -0.25765E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71720E-01 0.54257E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88576E-02      33   0.32193E-03   0.34932E+01 0.13641E+03 
c  Velocity[X]                                      0.15474E+01 
c  Velocity[Y]                                      0.19458E+01 
c  Velocity[Z]                                      0.13403E-29 
c  Pressure     0.12218E-06     521   0.98121E-08   0.10773E+00 0.14046E+04 
c  nu_tilda     0.59081E-05      32   0.15999E-04   0.29441E-06 0.15115E+03 
c  TempC        0.35782E+02      26   0.33079E-03   0.44842E+01 0.23854E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2577          10.402          4.5729          4.5729
v  Velocity[Y]            -2.6202          7.3607     -0.00031783     -0.00031783
v  Velocity[Z]       -6.9287e-015     9.2043e-015    -7.4134e-018    -7.4134e-018
v  ǁVelocityǁ         0.0005168          10.402          5.2169          5.2169
v  Pressure                -46.75          15.505         -11.144         -11.144
v  nu_tilda           4.4011e-007       0.0042695       0.0013652       0.0013652
v  TempC                       21          73.054          21.853          21.853
v  TurbVisc           3.2982e-014        0.005032       0.0016024       0.0016024
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1442:        0.21970E+01

===============================================================


 INSTANT    0.144300000E+04   TIME STEP NUMBER            1443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70908E-02 0.90191E+00
   Friction velocity        uk    :  0.70908E-02 0.90191E+00
   Dimensionless distance   yplus :  0.57086E-01 0.72610E+01
   Friction thermal sca.    tstar : -0.46443E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42593E-01 0.54175E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88598E-02      33   0.31262E-03   0.34715E+01 0.13646E+03 
c  Velocity[X]                                      0.15051E+01 
c  Velocity[Y]                                      0.19664E+01 
c  Velocity[Z]                                      0.12998E-29 
c  Pressure     0.11606E-06     504   0.98452E-08   0.10152E+00 0.13775E+04 
c  nu_tilda     0.59102E-05      32   0.53764E-05   0.29480E-06 0.15124E+03 
c  TempC        0.35792E+02      27   0.27916E-03   0.46449E+01 0.22815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2545          10.402          4.5729          4.5729
v  Velocity[Y]            -2.6187          7.3827     -0.00028476     -0.00028476
v  Velocity[Z]       -6.9287e-015     9.1851e-015    -7.4413e-018    -7.4413e-018
v  ǁVelocityǁ        0.00085113          10.402          5.2166          5.2166
v  Pressure               -46.709          15.739         -11.071         -11.071
v  nu_tilda           4.4013e-007       0.0042695       0.0013657       0.0013657
v  TempC                       21          73.054          21.853          21.853
v  TurbVisc           3.3007e-014        0.005032        0.001603        0.001603
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1443:        0.21450E+01

===============================================================


 INSTANT    0.144400000E+04   TIME STEP NUMBER            1444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11616E-01 0.90282E+00
   Friction velocity        uk    :  0.11616E-01 0.90282E+00
   Dimensionless distance   yplus :  0.93513E-01 0.72683E+01
   Friction thermal sca.    tstar : -0.25840E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69771E-01 0.54230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88620E-02      33   0.33856E-03   0.34765E+01 0.13656E+03 
c  Velocity[X]                                      0.15207E+01 
c  Velocity[Y]                                      0.19558E+01 
c  Velocity[Z]                                      0.15103E-29 
c  Pressure     0.12833E-06     520   0.95426E-08   0.11163E+00 0.13489E+04 
c  nu_tilda     0.59123E-05      32   0.15999E-04   0.29522E-06 0.15133E+03 
c  TempC        0.35801E+02      26   0.42697E-03   0.39346E+01 0.21300E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2514          10.401          4.5729          4.5729
v  Velocity[Y]            -2.6172          7.3549     -0.00025154     -0.00025154
v  Velocity[Z]       -6.9287e-015     8.7715e-015    -7.4621e-018    -7.4621e-018
v  ǁVelocityǁ         0.0016753          10.402          5.2163          5.2163
v  Pressure                -46.71          15.493         -11.146         -11.146
v  nu_tilda           4.4021e-007       0.0042695       0.0013662       0.0013662
v  TempC                       21          73.054          21.854          21.854
v  TurbVisc           3.3012e-014        0.005032       0.0016036       0.0016036
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1444:        0.21820E+01

===============================================================


 INSTANT    0.144500000E+04   TIME STEP NUMBER            1445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40493E-02 0.90225E+00
   Friction velocity        uk    :  0.40493E-02 0.90225E+00
   Dimensionless distance   yplus :  0.32600E-01 0.72637E+01
   Friction thermal sca.    tstar : -0.73619E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24323E-01 0.54196E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88642E-02      33   0.26999E-03   0.35027E+01 0.13682E+03 
c  Velocity[X]                                      0.15422E+01 
c  Velocity[Y]                                      0.19605E+01 
c  Velocity[Z]                                      0.12073E-29 
c  Pressure     0.13291E-06     488   0.93216E-08   0.11652E+00 0.13505E+04 
c  nu_tilda     0.59144E-05      32   0.53655E-05   0.29561E-06 0.15141E+03 
c  TempC        0.35811E+02      27   0.32290E-03   0.64854E+01 0.28651E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2482          10.401          4.5729          4.5729
v  Velocity[Y]            -2.6158          7.3843       -0.000218       -0.000218
v  Velocity[Z]       -6.9287e-015      9.085e-015    -7.4921e-018    -7.4921e-018
v  ǁVelocityǁ           0.00138          10.401           5.216           5.216
v  Pressure               -46.671           15.73         -11.077         -11.077
v  nu_tilda           4.4027e-007       0.0042695       0.0013668       0.0013668
v  TempC                       21          73.054          21.854          21.854
v  TurbVisc           3.3038e-014        0.005032       0.0016043       0.0016043
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1445:        0.20970E+01

===============================================================


 INSTANT    0.144600000E+04   TIME STEP NUMBER            1446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84170E-02 0.90370E+00
   Friction velocity        uk    :  0.84170E-02 0.90370E+00
   Dimensionless distance   yplus :  0.67763E-01 0.72754E+01
   Friction thermal sca.    tstar : -0.31335E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50559E-01 0.54282E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88665E-02      33   0.30610E-03   0.34764E+01 0.13684E+03 
c  Velocity[X]                                      0.14986E+01 
c  Velocity[Y]                                      0.19778E+01 
c  Velocity[Z]                                      0.13560E-29 
c  Pressure     0.11464E-06     489   0.97650E-08   0.10026E+00 0.86525E+03 
c  nu_tilda     0.59165E-05      32   0.15993E-04   0.29603E-06 0.15150E+03 
c  TempC        0.35820E+02      27   0.31065E-03   0.56278E+01 0.25765E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.245            10.4          4.5729          4.5729
v  Velocity[Y]            -2.6143          7.3925      -0.0001838      -0.0001838
v  Velocity[Z]       -6.9287e-015     9.1896e-015    -7.5113e-018    -7.5113e-018
v  ǁVelocityǁ        0.00054166          10.401          5.2157          5.2157
v  Pressure               -46.672          15.613         -11.131         -11.131
v  nu_tilda           4.4027e-007       0.0042695       0.0013673       0.0013673
v  TempC                       21          73.054          21.854          21.854
v  TurbVisc           3.3055e-014        0.005032       0.0016049       0.0016049
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1446:        0.24280E+01

===============================================================


 INSTANT    0.144700000E+04   TIME STEP NUMBER            1447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12359E-01 0.90329E+00
   Friction velocity        uk    :  0.12359E-01 0.90329E+00
   Dimensionless distance   yplus :  0.99502E-01 0.72721E+01
   Friction thermal sca.    tstar : -0.24158E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74240E-01 0.54258E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88687E-02      33   0.30881E-03   0.35052E+01 0.13702E+03 
c  Velocity[X]                                      0.15341E+01 
c  Velocity[Y]                                      0.19712E+01 
c  Velocity[Z]                                      0.11889E-29 
c  Pressure     0.13990E-06     424   0.91523E-08   0.12296E+00 0.43769E+03 
c  nu_tilda     0.59186E-05      32   0.53657E-05   0.29643E-06 0.15159E+03 
c  TempC        0.35829E+02      27   0.37084E-03   0.44015E+01 0.22701E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2417            10.4          4.5729          4.5729
v  Velocity[Y]            -2.6128           7.361     -0.00014886     -0.00014886
v  Velocity[Z]       -6.9287e-015      9.205e-015    -7.5379e-018    -7.5379e-018
v  ǁVelocityǁ        0.00078486            10.4          5.2154          5.2154
v  Pressure               -46.633          15.587         -11.114         -11.114
v  nu_tilda           4.4028e-007       0.0042695       0.0013679       0.0013679
v  TempC                       21          73.054          21.854          21.854
v  TurbVisc           3.3055e-014        0.005032       0.0016055       0.0016055
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1447:        0.21590E+01

===============================================================


 INSTANT    0.144800000E+04   TIME STEP NUMBER            1448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95883E-02 0.90190E+00
   Friction velocity        uk    :  0.95883E-02 0.90190E+00
   Dimensionless distance   yplus :  0.77193E-01 0.72609E+01
   Friction thermal sca.    tstar : -0.36577E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57594E-01 0.54174E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88709E-02      33   0.32183E-03   0.35084E+01 0.13718E+03 
c  Velocity[X]                                      0.15405E+01 
c  Velocity[Y]                                      0.19679E+01 
c  Velocity[Z]                                      0.94006E-30 
c  Pressure     0.11129E-06     425   0.95213E-08   0.97264E-01 0.30533E+03 
c  nu_tilda     0.59207E-05      32   0.15993E-04   0.29685E-06 0.15168E+03 
c  TempC        0.35839E+02      27   0.39223E-03   0.47209E+01 0.25371E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2384            10.4          4.5729          4.5729
v  Velocity[Y]            -2.6113          7.3823     -0.00011351     -0.00011351
v  Velocity[Z]       -6.9287e-015     9.1928e-015    -7.5606e-018    -7.5606e-018
v  ǁVelocityǁ          0.001736            10.4          5.2151          5.2151
v  Pressure               -46.636          15.602         -11.137         -11.137
v  nu_tilda           4.4031e-007       0.0042695       0.0013684       0.0013684
v  TempC                       21          73.054          21.855          21.855
v  TurbVisc           3.3057e-014        0.005032       0.0016062       0.0016062
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1448:        0.19660E+01

===============================================================


 INSTANT    0.144900000E+04   TIME STEP NUMBER            1449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62656E-02 0.90305E+00
   Friction velocity        uk    :  0.62656E-02 0.90305E+00
   Dimensionless distance   yplus :  0.50442E-01 0.72701E+01
   Friction thermal sca.    tstar : -0.27866E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37636E-01 0.54243E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88731E-02      33   0.31925E-03   0.35163E+01 0.13737E+03 
c  Velocity[X]                                      0.15237E+01 
c  Velocity[Y]                                      0.19926E+01 
c  Velocity[Z]                                      0.12209E-29 
c  Pressure     0.13272E-06     472   0.96943E-08   0.11743E+00 0.63901E+03 
c  nu_tilda     0.59227E-05      32   0.53557E-05   0.29724E-06 0.15177E+03 
c  TempC        0.35848E+02      26   0.38741E-03   0.71197E+01 0.28752E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2354          10.399          4.5729          4.5729
v  Velocity[Y]            -2.6098          7.3607    -7.7579e-005    -7.7579e-005
v  Velocity[Z]       -6.9287e-015     9.1715e-015    -7.5901e-018    -7.5901e-018
v  ǁVelocityǁ         0.0013548          10.399          5.2148          5.2148
v  Pressure               -46.593          15.639         -11.103         -11.103
v  nu_tilda           4.4036e-007       0.0042695       0.0013689       0.0013689
v  TempC                       21          73.054          21.855          21.855
v  TurbVisc           3.3068e-014        0.005032       0.0016068       0.0016068
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1449:        0.20650E+01

===============================================================


 INSTANT    0.145000000E+04   TIME STEP NUMBER            1450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87650E-02 0.90209E+00
   Friction velocity        uk    :  0.87650E-02 0.90209E+00
   Dimensionless distance   yplus :  0.70564E-01 0.72624E+01
   Friction thermal sca.    tstar : -0.31029E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52649E-01 0.54186E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88753E-02      33   0.27184E-03   0.35072E+01 0.13742E+03 
c  Velocity[X]                                      0.15242E+01 
c  Velocity[Y]                                      0.19830E+01 
c  Velocity[Z]                                      0.12672E-29 
c  Pressure     0.12830E-06     473   0.93639E-08   0.11125E+00 0.79044E+03 
c  nu_tilda     0.59248E-05      32   0.15991E-04   0.29767E-06 0.15186E+03 
c  TempC        0.35858E+02      27   0.31706E-03   0.52785E+01 0.24369E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2322          10.399          4.5729          4.5729
v  Velocity[Y]            -2.6083          7.3815    -4.1332e-005    -4.1332e-005
v  Velocity[Z]       -6.9287e-015     9.1522e-015     -7.606e-018     -7.606e-018
v  ǁVelocityǁ        0.00051979          10.399          5.2145          5.2145
v  Pressure               -46.599          15.551         -11.157         -11.157
v  nu_tilda            4.404e-007       0.0042695       0.0013694       0.0013694
v  TempC                       21          73.054          21.855          21.855
v  TurbVisc           3.3083e-014        0.005032       0.0016074       0.0016074
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1450:        0.20810E+01

===============================================================


 INSTANT    0.145100000E+04   TIME STEP NUMBER            1451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11513E-01 0.90393E+00
   Friction velocity        uk    :  0.11513E-01 0.90393E+00
   Dimensionless distance   yplus :  0.92689E-01 0.72772E+01
   Friction thermal sca.    tstar : -0.28628E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69156E-01 0.54296E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88775E-02      33   0.33042E-03   0.35112E+01 0.13758E+03 
c  Velocity[X]                                      0.15299E+01 
c  Velocity[Y]                                      0.19813E+01 
c  Velocity[Z]                                      0.12781E-29 
c  Pressure     0.12629E-06     457   0.98079E-08   0.11145E+00 0.98835E+03 
c  nu_tilda     0.59269E-05      32   0.53543E-05   0.29806E-06 0.15195E+03 
c  TempC        0.35867E+02      27   0.35705E-03   0.34454E+01 0.20311E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2289          10.398          4.5729          4.5729
v  Velocity[Y]            -2.6069           7.396    -4.2403e-006    -4.2403e-006
v  Velocity[Z]       -6.9287e-015     8.7391e-015    -7.6354e-018    -7.6354e-018
v  ǁVelocityǁ        0.00082389          10.398          5.2143          5.2143
v  Pressure               -46.558          15.697         -11.104         -11.104
v  nu_tilda            4.404e-007       0.0042695         0.00137         0.00137
v  TempC                       21          73.053          21.855          21.855
v  TurbVisc           3.3095e-014        0.005032        0.001608        0.001608
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1451:        0.20280E+01

===============================================================


 INSTANT    0.145200000E+04   TIME STEP NUMBER            1452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80469E-02 0.90354E+00
   Friction velocity        uk    :  0.80469E-02 0.90354E+00
   Dimensionless distance   yplus :  0.64783E-01 0.72741E+01
   Friction thermal sca.    tstar : -0.23902E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48335E-01 0.54273E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88797E-02      33   0.29943E-03   0.35424E+01 0.13788E+03 
c  Velocity[X]                                      0.15403E+01 
c  Velocity[Y]                                      0.20020E+01 
c  Velocity[Z]                                      0.14402E-29 
c  Pressure     0.12263E-06     474   0.91300E-08   0.10884E+00 0.11120E+04 
c  nu_tilda     0.59290E-05      32   0.15984E-04   0.29849E-06 0.15204E+03 
c  TempC        0.35877E+02      27   0.43152E-03   0.51748E+01 0.24238E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2257          10.398          4.5729          4.5729
v  Velocity[Y]            -2.6054          7.3651     3.3203e-005     3.3203e-005
v  Velocity[Z]       -6.9287e-015     9.0537e-015    -7.6594e-018    -7.6594e-018
v  ǁVelocityǁ         0.0017983          10.398           5.214           5.214
v  Pressure               -46.558          15.505         -11.168         -11.168
v  nu_tilda           4.4045e-007       0.0042695       0.0013705       0.0013705
v  TempC                       21          73.053          21.856          21.856
v  TurbVisc           3.3094e-014        0.005032       0.0016087       0.0016087
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1452:        0.20780E+01

===============================================================


 INSTANT    0.145300000E+04   TIME STEP NUMBER            1453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61246E-02 0.90200E+00
   Friction velocity        uk    :  0.61246E-02 0.90200E+00
   Dimensionless distance   yplus :  0.49307E-01 0.72617E+01
   Friction thermal sca.    tstar : -0.29921E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36789E-01 0.54180E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88819E-02      33   0.30915E-03   0.35294E+01 0.13783E+03 
c  Velocity[X]                                      0.15317E+01 
c  Velocity[Y]                                      0.19977E+01 
c  Velocity[Z]                                      0.12881E-29 
c  Pressure     0.13312E-06     474   0.90932E-08   0.11613E+00 0.10540E+04 
c  nu_tilda     0.59311E-05      32   0.53472E-05   0.29889E-06 0.15213E+03 
c  TempC        0.35886E+02      27   0.30016E-03   0.61617E+01 0.27863E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2224          10.397          4.5729          4.5729
v  Velocity[Y]            -2.6039          7.3826     7.1153e-005     7.1153e-005
v  Velocity[Z]       -6.9287e-015      9.156e-015    -7.6889e-018    -7.6889e-018
v  ǁVelocityǁ         0.0012514          10.397          5.2137          5.2137
v  Pressure               -46.519          15.671         -11.113         -11.113
v  nu_tilda           4.4048e-007       0.0042695       0.0013711       0.0013711
v  TempC                       21          73.053          21.856          21.856
v  TurbVisc           3.3108e-014        0.005032       0.0016093       0.0016093
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1453:        0.20780E+01

===============================================================


 INSTANT    0.145400000E+04   TIME STEP NUMBER            1454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39751E-02 0.90317E+00
   Friction velocity        uk    :  0.39751E-02 0.90317E+00
   Dimensionless distance   yplus :  0.32003E-01 0.72711E+01
   Friction thermal sca.    tstar : -0.23588E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23878E-01 0.54251E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88841E-02      33   0.32306E-03   0.35509E+01 0.13809E+03 
c  Velocity[X]                                      0.15585E+01 
c  Velocity[Y]                                      0.19924E+01 
c  Velocity[Z]                                      0.12501E-29 
c  Pressure     0.11894E-06     504   0.95915E-08   0.10617E+00 0.12137E+04 
c  nu_tilda     0.59332E-05      32   0.15987E-04   0.29931E-06 0.15222E+03 
c  TempC        0.35895E+02      26   0.38253E-03   0.41299E+01 0.22184E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2192          10.397          4.5729          4.5729
v  Velocity[Y]            -2.6024          7.3601      0.00010922      0.00010922
v  Velocity[Z]       -6.9287e-015      9.173e-015    -7.7139e-018    -7.7139e-018
v  ǁVelocityǁ        0.00044174          10.397          5.2134          5.2134
v  Pressure               -46.521          15.468         -11.183         -11.183
v  nu_tilda           4.4058e-007       0.0042695       0.0013715       0.0013715
v  TempC                       21          73.053          21.856          21.856
v  TurbVisc           3.3118e-014        0.005032       0.0016099       0.0016099
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1454:        0.21420E+01

===============================================================


 INSTANT    0.145500000E+04   TIME STEP NUMBER            1455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10213E-01 0.90237E+00
   Friction velocity        uk    :  0.10213E-01 0.90237E+00
   Dimensionless distance   yplus :  0.82225E-01 0.72647E+01
   Friction thermal sca.    tstar : -0.32273E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61349E-01 0.54203E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88863E-02      33   0.25445E-03   0.35440E+01 0.13819E+03 
c  Velocity[X]                                      0.15283E+01 
c  Velocity[Y]                                      0.20157E+01 
c  Velocity[Z]                                      0.12461E-29 
c  Pressure     0.12997E-06     505   0.99366E-08   0.11296E+00 0.15066E+04 
c  nu_tilda     0.59353E-05      32   0.53321E-05   0.29971E-06 0.15231E+03 
c  TempC        0.35905E+02      27   0.41233E-03   0.51858E+01 0.23887E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2161          10.396          4.5729          4.5729
v  Velocity[Y]            -2.6009          7.3879      0.00014878      0.00014878
v  Velocity[Z]       -6.9287e-015     9.1585e-015    -7.7519e-018    -7.7519e-018
v  ǁVelocityǁ         0.0010055          10.396          5.2131          5.2131
v  Pressure               -46.479          15.717         -11.103         -11.103
v  nu_tilda            4.406e-007       0.0042695       0.0013721       0.0013721
v  TempC                       21          73.053          21.856          21.856
v  TurbVisc           3.3149e-014        0.005032       0.0016105       0.0016105
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1455:        0.21530E+01

===============================================================


 INSTANT    0.145600000E+04   TIME STEP NUMBER            1456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87973E-02 0.90381E+00
   Friction velocity        uk    :  0.87973E-02 0.90381E+00
   Dimensionless distance   yplus :  0.70824E-01 0.72763E+01
   Friction thermal sca.    tstar : -0.25979E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52843E-01 0.54289E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88886E-02      33   0.33313E-03   0.35203E+01 0.13817E+03 
c  Velocity[X]                                      0.15150E+01 
c  Velocity[Y]                                      0.20052E+01 
c  Velocity[Z]                                      0.14690E-29 
c  Pressure     0.12278E-06     490   0.93174E-08   0.10587E+00 0.10183E+04 
c  nu_tilda     0.59374E-05      32   0.15977E-04   0.30014E-06 0.15240E+03 
c  TempC        0.35914E+02      26   0.39636E-03   0.72580E+01 0.28278E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2129          10.396          4.5729          4.5729
v  Velocity[Y]            -2.5995          7.3923      0.00018882      0.00018882
v  Velocity[Z]       -6.9287e-015     9.1373e-015    -7.7704e-018    -7.7704e-018
v  ǁVelocityǁ         0.0019654          10.396          5.2128          5.2128
v  Pressure               -46.483           15.57         -11.166         -11.166
v  nu_tilda           4.4059e-007       0.0042695       0.0013726       0.0013726
v  TempC                       21          73.053          21.857          21.857
v  TurbVisc           3.3155e-014        0.005032       0.0016112       0.0016112
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1456:        0.21060E+01

===============================================================


 INSTANT    0.145700000E+04   TIME STEP NUMBER            1457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10176E-01 0.90364E+00
   Friction velocity        uk    :  0.10176E-01 0.90364E+00
   Dimensionless distance   yplus :  0.81927E-01 0.72749E+01
   Friction thermal sca.    tstar : -0.22142E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61127E-01 0.54279E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88907E-02      33   0.33219E-03   0.35852E+01 0.13864E+03 
c  Velocity[X]                                      0.15758E+01 
c  Velocity[Y]                                      0.20094E+01 
c  Velocity[Z]                                      0.14831E-29 
c  Pressure     0.14655E-06     440   0.92812E-08   0.13047E+00 0.55076E+03 
c  nu_tilda     0.59395E-05      32   0.53349E-05   0.30054E-06 0.15249E+03 
c  TempC        0.35923E+02      27   0.33846E-03   0.60366E+01 0.27386E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2097          10.395          4.5729          4.5729
v  Velocity[Y]             -2.598           7.368      0.00022882      0.00022882
v  Velocity[Z]       -6.9287e-015     9.1166e-015    -7.8094e-018    -7.8094e-018
v  ǁVelocityǁ        0.00099952          10.395          5.2125          5.2125
v  Pressure               -46.441          15.583         -11.139         -11.139
v  nu_tilda           4.4063e-007       0.0042695       0.0013732       0.0013732
v  TempC                       21          73.053          21.857          21.857
v  TurbVisc           3.3151e-014        0.005032       0.0016118       0.0016118
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1457:        0.19970E+01

===============================================================


 INSTANT    0.145800000E+04   TIME STEP NUMBER            1458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99405E-02 0.90228E+00
   Friction velocity        uk    :  0.99405E-02 0.90228E+00
   Dimensionless distance   yplus :  0.80028E-01 0.72640E+01
   Friction thermal sca.    tstar : -0.27461E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59710E-01 0.54197E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88930E-02      33   0.30883E-03   0.35616E+01 0.13868E+03 
c  Velocity[X]                                      0.15340E+01 
c  Velocity[Y]                                      0.20276E+01 
c  Velocity[Z]                                      0.14842E-29 
c  Pressure     0.11434E-06     441   0.98322E-08   0.10050E+00 0.50835E+03 
c  nu_tilda     0.59416E-05      32   0.15976E-04   0.30097E-06 0.15258E+03 
c  TempC        0.35933E+02      27   0.43263E-03   0.41590E+01 0.23335E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2064          10.395          4.5729          4.5729
v  Velocity[Y]            -2.5965          7.3867      0.00026949      0.00026949
v  Velocity[Z]       -6.9287e-015     8.7076e-015    -7.8263e-018    -7.8263e-018
v  ǁVelocityǁ        0.00042494          10.395          5.2122          5.2122
v  Pressure               -46.446          15.565         -11.177         -11.177
v  nu_tilda           4.4064e-007       0.0042695       0.0013737       0.0013737
v  TempC                       21          73.053          21.857          21.857
v  TurbVisc           3.3163e-014        0.005032       0.0016124       0.0016124
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1458:        0.19980E+01

===============================================================


 INSTANT    0.145900000E+04   TIME STEP NUMBER            1459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83274E-02 0.90330E+00
   Friction velocity        uk    :  0.83274E-02 0.90330E+00
   Dimensionless distance   yplus :  0.67041E-01 0.72722E+01
   Friction thermal sca.    tstar : -0.20942E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50020E-01 0.54259E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88951E-02      33   0.31777E-03   0.35688E+01 0.13873E+03 
c  Velocity[X]                                      0.15500E+01 
c  Velocity[Y]                                      0.20188E+01 
c  Velocity[Z]                                      0.14596E-29 
c  Pressure     0.14449E-06     426   0.98712E-08   0.12519E+00 0.55767E+03 
c  nu_tilda     0.59437E-05      32   0.53289E-05   0.30137E-06 0.15267E+03 
c  TempC        0.35942E+02      27   0.38094E-03   0.82475E+01 0.29675E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.203          10.394          4.5729          4.5729
v  Velocity[Y]             -2.595          7.3617      0.00031099      0.00031099
v  Velocity[Z]       -6.9287e-015     9.0178e-015    -7.8704e-018    -7.8704e-018
v  ǁVelocityǁ        0.00078208          10.394          5.2119          5.2119
v  Pressure               -46.404          15.561         -11.149         -11.149
v  nu_tilda           4.4061e-007       0.0042695       0.0013742       0.0013742
v  TempC                       21          73.053          21.857          21.857
v  TurbVisc           3.3168e-014        0.005032        0.001613        0.001613
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1459:        0.19560E+01

===============================================================


 INSTANT    0.146000000E+04   TIME STEP NUMBER            1460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48033E-02 0.90258E+00
   Friction velocity        uk    :  0.48033E-02 0.90258E+00
   Dimensionless distance   yplus :  0.38670E-01 0.72664E+01
   Friction thermal sca.    tstar : -0.42543E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28852E-01 0.54215E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88974E-02      33   0.26098E-03   0.35813E+01 0.13893E+03 
c  Velocity[X]                                      0.15640E+01 
c  Velocity[Y]                                      0.20173E+01 
c  Velocity[Z]                                      0.12873E-29 
c  Pressure     0.11638E-06     410   0.95089E-08   0.10181E+00 0.33235E+03 
c  nu_tilda     0.59458E-05      32   0.15976E-04   0.30180E-06 0.15276E+03 
c  TempC        0.35952E+02      27   0.36343E-03   0.55508E+01 0.26833E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -6.2          10.393          4.5729          4.5729
v  Velocity[Y]            -2.5935          7.3875      0.00035327      0.00035327
v  Velocity[Z]       -6.9287e-015     9.1215e-015    -7.8888e-018    -7.8888e-018
v  ǁVelocityǁ         0.0013221          10.394          5.2116          5.2116
v  Pressure               -46.406           15.58         -11.173         -11.173
v  nu_tilda            4.406e-007       0.0042695       0.0013747       0.0013747
v  TempC                       21          73.053          21.857          21.857
v  TurbVisc           3.3158e-014        0.005032       0.0016137       0.0016137
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1460:        0.19280E+01

===============================================================


 INSTANT    0.146100000E+04   TIME STEP NUMBER            1461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67681E-02 0.90401E+00
   Friction velocity        uk    :  0.67681E-02 0.90401E+00
   Dimensionless distance   yplus :  0.54488E-01 0.72779E+01
   Friction thermal sca.    tstar : -0.28412E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40654E-01 0.54301E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88996E-02      33   0.30566E-03   0.35593E+01 0.13899E+03 
c  Velocity[X]                                      0.15156E+01 
c  Velocity[Y]                                      0.20437E+01 
c  Velocity[Z]                                      0.11358E-29 
c  Pressure     0.12296E-06     458   0.91950E-08   0.10853E+00 0.72052E+03 
c  nu_tilda     0.59479E-05      32   0.53184E-05   0.30220E-06 0.15285E+03 
c  TempC        0.35961E+02      26   0.31101E-03   0.50263E+01 0.25429E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1968          10.393          4.5729          4.5729
v  Velocity[Y]            -2.5921          7.3988      0.00039562      0.00039562
v  Velocity[Z]       -6.9287e-015     9.1347e-015    -7.9165e-018    -7.9165e-018
v  ǁVelocityǁ         0.0006677          10.393          5.2113          5.2113
v  Pressure               -46.368          15.669         -11.136         -11.136
v  nu_tilda           4.4054e-007       0.0042695       0.0013753       0.0013753
v  TempC                       21          73.053          21.858          21.858
v  TurbVisc           3.3154e-014        0.005032       0.0016143       0.0016143
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1461:        0.20250E+01

===============================================================


 INSTANT    0.146200000E+04   TIME STEP NUMBER            1462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13004E-01 0.90352E+00
   Friction velocity        uk    :  0.13004E-01 0.90352E+00
   Dimensionless distance   yplus :  0.10469E+00 0.72739E+01
   Friction thermal sca.    tstar : -0.19183E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78109E-01 0.54272E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89018E-02      33   0.32235E-03   0.35842E+01 0.13920E+03 
c  Velocity[X]                                      0.15539E+01 
c  Velocity[Y]                                      0.20303E+01 
c  Velocity[Z]                                      0.13893E-29 
c  Pressure     0.13450E-06     504   0.96608E-08   0.11653E+00 0.13259E+04 
c  nu_tilda     0.59500E-05      32   0.15969E-04   0.30264E-06 0.15294E+03 
c  TempC        0.35970E+02      26   0.30886E-03   0.44995E+01 0.23852E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1935          10.392          4.5729          4.5729
v  Velocity[Y]            -2.5906          7.3646      0.00043846      0.00043846
v  Velocity[Z]       -7.2433e-015       9.12e-015    -7.9406e-018    -7.9406e-018
v  ǁVelocityǁ        0.00064696          10.392           5.211           5.211
v  Pressure                -46.37          15.433         -11.212         -11.212
v  nu_tilda            4.406e-007       0.0042695       0.0013758       0.0013758
v  TempC                       21          73.052          21.858          21.858
v  TurbVisc           3.3136e-014        0.005032       0.0016149       0.0016149
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1462:        0.21430E+01

===============================================================


 INSTANT    0.146300000E+04   TIME STEP NUMBER            1463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24540E-02 0.90228E+00
   Friction velocity        uk    :  0.24540E-02 0.90228E+00
   Dimensionless distance   yplus :  0.19756E-01 0.72640E+01
   Friction thermal sca.    tstar : -0.26251E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14740E-01 0.54198E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89040E-02      33   0.32910E-03   0.35971E+01 0.13941E+03 
c  Velocity[X]                                      0.15660E+01 
c  Velocity[Y]                                      0.20311E+01 
c  Velocity[Z]                                      0.12713E-29 
c  Pressure     0.13088E-06     489   0.95227E-08   0.11501E+00 0.13134E+04 
c  nu_tilda     0.59522E-05      32   0.53119E-05   0.30304E-06 0.15303E+03 
c  TempC        0.35980E+02      26   0.44411E-03   0.54852E+01 0.23980E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1903          10.392          4.5729          4.5729
v  Velocity[Y]            -2.5891          7.3897      0.00048255      0.00048255
v  Velocity[Z]       -7.3767e-015     9.0978e-015    -7.9747e-018    -7.9747e-018
v  ǁVelocityǁ         0.0016395          10.392          5.2107          5.2107
v  Pressure               -46.328          15.655         -11.142         -11.142
v  nu_tilda           4.4073e-007       0.0042695       0.0013763       0.0013763
v  TempC                       21           73.05          21.858          21.858
v  TurbVisc           3.3153e-014        0.005032       0.0016155       0.0016155
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1463:        0.21100E+01

===============================================================


 INSTANT    0.146400000E+04   TIME STEP NUMBER            1464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14275E-01 0.90338E+00
   Friction velocity        uk    :  0.14275E-01 0.90338E+00
   Dimensionless distance   yplus :  0.11492E+00 0.72729E+01
   Friction thermal sca.    tstar : -0.22122E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85746E-01 0.54264E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89062E-02      33   0.31815E-03   0.36047E+01 0.13959E+03 
c  Velocity[X]                                      0.15535E+01 
c  Velocity[Y]                                      0.20513E+01 
c  Velocity[Z]                                      0.12835E-29 
c  Pressure     0.12735E-06     505   0.94268E-08   0.11059E+00 0.10471E+04 
c  nu_tilda     0.59543E-05      32   0.15968E-04   0.30347E-06 0.15312E+03 
c  TempC        0.35989E+02      27   0.34043E-03   0.81144E+01 0.31534E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.187          10.391          4.5729          4.5729
v  Velocity[Y]            -2.5876          7.3642      0.00052675      0.00052675
v  Velocity[Z]       -7.0794e-015     9.0792e-015    -7.9948e-018    -7.9948e-018
v  ǁVelocityǁ         0.0011739          10.391          5.2104          5.2104
v  Pressure               -46.332          15.482         -11.205         -11.205
v  nu_tilda           4.4092e-007       0.0042695       0.0013768       0.0013768
v  TempC                       21          73.049          21.858          21.858
v  TurbVisc           3.3195e-014        0.005032       0.0016162       0.0016162
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1464:        0.21600E+01

===============================================================


 INSTANT    0.146500000E+04   TIME STEP NUMBER            1465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14113E-01 0.90244E+00
   Friction velocity        uk    :  0.14113E-01 0.90244E+00
   Dimensionless distance   yplus :  0.11362E+00 0.72652E+01
   Friction thermal sca.    tstar : -0.23803E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84774E-01 0.54207E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89084E-02      33   0.25809E-03   0.36032E+01 0.13958E+03 
c  Velocity[X]                                      0.15569E+01 
c  Velocity[Y]                                      0.20463E+01 
c  Velocity[Z]                                      0.14904E-29 
c  Pressure     0.13940E-06     473   0.94886E-08   0.12099E+00 0.97757E+03 
c  nu_tilda     0.59564E-05      32   0.53048E-05   0.30387E-06 0.15321E+03 
c  TempC        0.35998E+02      27   0.38507E-03   0.47059E+01 0.24433E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1838          10.391          4.5729          4.5729
v  Velocity[Y]            -2.5861          7.3876      0.00057159      0.00057159
v  Velocity[Z]       -8.0444e-015     8.6719e-015    -8.0292e-018    -8.0292e-018
v  ǁVelocityǁ        0.00037125          10.391          5.2101          5.2101
v  Pressure                -46.29          15.626         -11.154         -11.154
v  nu_tilda           4.4117e-007       0.0042695       0.0013774       0.0013774
v  TempC                       21          73.048          21.859          21.859
v  TurbVisc           3.3252e-014        0.005032       0.0016168       0.0016168
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1465:        0.21190E+01

===============================================================


 INSTANT    0.146600000E+04   TIME STEP NUMBER            1466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12920E-01 0.90408E+00
   Friction velocity        uk    :  0.12920E-01 0.90408E+00
   Dimensionless distance   yplus :  0.10401E+00 0.72785E+01
   Friction thermal sca.    tstar : -0.20848E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77604E-01 0.54306E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89106E-02      33   0.32302E-03   0.35963E+01 0.13970E+03 
c  Velocity[X]                                      0.15549E+01 
c  Velocity[Y]                                      0.20413E+01 
c  Velocity[Z]                                      0.13196E-29 
c  Pressure     0.12030E-06     458   0.92704E-08   0.10399E+00 0.60223E+03 
c  nu_tilda     0.59585E-05      32   0.15962E-04   0.30431E-06 0.15331E+03 
c  TempC        0.36008E+02      27   0.30740E-03   0.53096E+01 0.25111E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1807           10.39          4.5729          4.5729
v  Velocity[Y]            -2.5847          7.3979      0.00061681      0.00061681
v  Velocity[Z]       -7.5355e-015     8.9818e-015    -8.0494e-018    -8.0494e-018
v  ǁVelocityǁ         0.0011438           10.39          5.2098          5.2098
v  Pressure               -46.291          15.562         -11.193         -11.193
v  nu_tilda            4.415e-007       0.0042695       0.0013779       0.0013779
v  TempC                       21          73.046          21.859          21.859
v  TurbVisc           3.3326e-014        0.005032       0.0016174       0.0016174
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1466:        0.20440E+01

===============================================================


 INSTANT    0.146700000E+04   TIME STEP NUMBER            1467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72309E-02 0.90378E+00
   Friction velocity        uk    :  0.72309E-02 0.90378E+00
   Dimensionless distance   yplus :  0.58214E-01 0.72760E+01
   Friction thermal sca.    tstar : -0.18960E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43434E-01 0.54287E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89128E-02      33   0.30335E-03   0.36202E+01 0.13999E+03 
c  Velocity[X]                                      0.15552E+01 
c  Velocity[Y]                                      0.20650E+01 
c  Velocity[Z]                                      0.13187E-29 
c  Pressure     0.13425E-06     410   0.91118E-08   0.11955E+00 0.44705E+03 
c  nu_tilda     0.59606E-05      32   0.53018E-05   0.30472E-06 0.15340E+03 
c  TempC        0.36017E+02      26   0.34416E-03   0.45901E+01 0.22761E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1775           10.39          4.5729          4.5729
v  Velocity[Y]            -2.5832          7.3709      0.00066313      0.00066313
v  Velocity[Z]       -7.2395e-015     9.0805e-015    -8.0815e-018    -8.0815e-018
v  ǁVelocityǁ         0.0016472           10.39          5.2095          5.2095
v  Pressure               -46.251          15.546         -11.176         -11.176
v  nu_tilda           4.4185e-007       0.0042695       0.0013784       0.0013784
v  TempC                       21          73.045          21.859          21.859
v  TurbVisc           3.3426e-014        0.005032        0.001618        0.001618
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1467:        0.19280E+01

===============================================================


 INSTANT    0.146800000E+04   TIME STEP NUMBER            1468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11904E-01 0.90221E+00
   Friction velocity        uk    :  0.11904E-01 0.90221E+00
   Dimensionless distance   yplus :  0.95835E-01 0.72634E+01
   Friction thermal sca.    tstar : -0.23515E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71503E-01 0.54193E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89150E-02      33   0.32285E-03   0.36016E+01 0.13997E+03 
c  Velocity[X]                                      0.15485E+01 
c  Velocity[Y]                                      0.20532E+01 
c  Velocity[Z]                                      0.13091E-29 
c  Pressure     0.12830E-06     425   0.96576E-08   0.10922E+00 0.34947E+03 
c  nu_tilda     0.59627E-05      32   0.15960E-04   0.30516E-06 0.15349E+03 
c  TempC        0.36027E+02      27   0.38252E-03   0.40731E+01 0.22125E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1742          10.389          4.5729          4.5729
v  Velocity[Y]            -2.5817          7.3852      0.00070961      0.00070961
v  Velocity[Z]       -7.7434e-015     9.0961e-015    -8.1014e-018    -8.1014e-018
v  ǁVelocityǁ        0.00060162          10.389          5.2092          5.2092
v  Pressure               -46.255          15.542         -11.202         -11.202
v  nu_tilda           4.4222e-007       0.0042695       0.0013789       0.0013789
v  TempC                       21          73.043          21.859          21.859
v  TurbVisc           3.3533e-014        0.005032       0.0016187       0.0016187
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1468:        0.21630E+01

===============================================================


 INSTANT    0.146900000E+04   TIME STEP NUMBER            1469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16588E-01 0.90346E+00
   Friction velocity        uk    :  0.16588E-01 0.90346E+00
   Dimensionless distance   yplus :  0.13355E+00 0.72735E+01
   Friction thermal sca.    tstar : -0.19907E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99640E-01 0.54268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89172E-02      33   0.33603E-03   0.36429E+01 0.14033E+03 
c  Velocity[X]                                      0.15845E+01 
c  Velocity[Y]                                      0.20583E+01 
c  Velocity[Z]                                      0.12535E-29 
c  Pressure     0.14517E-06     421   0.98581E-08   0.12893E+00 0.43837E+03 
c  nu_tilda     0.59648E-05      32   0.52895E-05   0.30556E-06 0.15358E+03 
c  TempC        0.36036E+02      27   0.40272E-03   0.39731E+01 0.22251E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1709          10.388          4.5729          4.5729
v  Velocity[Y]            -2.5802           7.367      0.00075647      0.00075647
v  Velocity[Z]        -7.354e-015     9.0789e-015    -8.1329e-018    -8.1329e-018
v  ǁVelocityǁ        0.00066964          10.389          5.2089          5.2089
v  Pressure               -46.215           15.53         -11.186         -11.186
v  nu_tilda           4.4266e-007       0.0042695       0.0013795       0.0013795
v  TempC                       21          73.042           21.86           21.86
v  TurbVisc           3.3646e-014        0.005032       0.0016193       0.0016193
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1469:        0.20120E+01

===============================================================


 INSTANT    0.147000000E+04   TIME STEP NUMBER            1470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10508E-01 0.90272E+00
   Friction velocity        uk    :  0.10508E-01 0.90272E+00
   Dimensionless distance   yplus :  0.84593E-01 0.72675E+01
   Friction thermal sca.    tstar : -0.23140E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63116E-01 0.54224E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89194E-02      33   0.24675E-03   0.36350E+01 0.14043E+03 
c  Velocity[X]                                      0.15580E+01 
c  Velocity[Y]                                      0.20771E+01 
c  Velocity[Z]                                      0.14035E-29 
c  Pressure     0.11936E-06     426   0.95275E-08   0.10323E+00 0.31486E+03 
c  nu_tilda     0.59669E-05      32   0.15959E-04   0.30600E-06 0.15367E+03 
c  TempC        0.36045E+02      27   0.37888E-03   0.44081E+01 0.22348E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1676          10.388          4.5729          4.5729
v  Velocity[Y]            -2.5787          7.3907      0.00080414      0.00080414
v  Velocity[Z]       -7.4567e-015     9.0589e-015    -8.1545e-018    -8.1545e-018
v  ǁVelocityǁ         0.0017442          10.388          5.2087          5.2087
v  Pressure               -46.218          15.554         -11.209         -11.209
v  nu_tilda           4.4303e-007       0.0042695         0.00138         0.00138
v  TempC                       21          73.041           21.86           21.86
v  TurbVisc           3.3778e-014        0.005032       0.0016199       0.0016199
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1470:        0.19760E+01

===============================================================


 INSTANT    0.147100000E+04   TIME STEP NUMBER            1471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10855E-01 0.90416E+00
   Friction velocity        uk    :  0.10855E-01 0.90416E+00
   Dimensionless distance   yplus :  0.87387E-01 0.72791E+01
   Friction thermal sca.    tstar : -0.18410E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65200E-01 0.54310E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89216E-02      33   0.31611E-03   0.36130E+01 0.14034E+03 
c  Velocity[X]                                      0.15447E+01 
c  Velocity[Y]                                      0.20683E+01 
c  Velocity[Z]                                      0.14695E-29 
c  Pressure     0.14253E-06     490   0.99650E-08   0.12408E+00 0.68648E+03 
c  nu_tilda     0.59691E-05      32   0.52900E-05   0.30640E-06 0.15376E+03 
c  TempC        0.36055E+02      27   0.40425E-03   0.41987E+01 0.21332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1645          10.387          4.5729          4.5729
v  Velocity[Y]            -2.5773          7.3991      0.00085276      0.00085276
v  Velocity[Z]       -8.1197e-015     9.0392e-015    -8.1844e-018    -8.1844e-018
v  ǁVelocityǁ        0.00094369          10.387          5.2084          5.2084
v  Pressure               -46.174          15.612         -11.172         -11.172
v  nu_tilda           4.4331e-007       0.0042695       0.0013805       0.0013805
v  TempC                       21           73.04           21.86           21.86
v  TurbVisc           3.3892e-014        0.005032       0.0016205       0.0016205
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1471:        0.21100E+01

===============================================================


 INSTANT    0.147200000E+04   TIME STEP NUMBER            1472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96201E-02 0.90393E+00
   Friction velocity        uk    :  0.96201E-02 0.90393E+00
   Dimensionless distance   yplus :  0.77449E-01 0.72773E+01
   Friction thermal sca.    tstar : -0.19445E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57785E-01 0.54296E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89238E-02      33   0.31716E-03   0.36591E+01 0.14072E+03 
c  Velocity[X]                                      0.15931E+01 
c  Velocity[Y]                                      0.20661E+01 
c  Velocity[Z]                                      0.14531E-29 
c  Pressure     0.12174E-06     505   0.92564E-08   0.10663E+00 0.98282E+03 
c  nu_tilda     0.59712E-05      32   0.15952E-04   0.30685E-06 0.15385E+03 
c  TempC        0.36064E+02      27   0.35592E-03   0.47506E+01 0.23325E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1613          10.387          4.5729          4.5729
v  Velocity[Y]            -2.5758          7.3707      0.00090151      0.00090151
v  Velocity[Z]       -7.5322e-015     8.6357e-015    -8.2027e-018    -8.2027e-018
v  ǁVelocityǁ         0.0004064          10.387          5.2081          5.2081
v  Pressure               -46.179           15.45         -11.232         -11.232
v  nu_tilda           4.4364e-007       0.0042695        0.001381        0.001381
v  TempC                       21           73.04           21.86           21.86
v  TurbVisc           3.3977e-014        0.005032       0.0016211       0.0016211
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1472:        0.21380E+01

===============================================================


 INSTANT    0.147300000E+04   TIME STEP NUMBER            1473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15568E-01 0.90249E+00
   Friction velocity        uk    :  0.15568E-01 0.90249E+00
   Dimensionless distance   yplus :  0.12533E+00 0.72657E+01
   Friction thermal sca.    tstar : -0.21584E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93514E-01 0.54210E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89260E-02      33   0.30692E-03   0.36467E+01 0.14081E+03 
c  Velocity[X]                                      0.15522E+01 
c  Velocity[Y]                                      0.20946E+01 
c  Velocity[Z]                                      0.13425E-29 
c  Pressure     0.11808E-06     506   0.93064E-08   0.10262E+00 0.12851E+04 
c  nu_tilda     0.59733E-05      32   0.52835E-05   0.30726E-06 0.15394E+03 
c  TempC        0.36073E+02      27   0.41803E-03   0.53781E+01 0.26422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1581          10.386          4.5729          4.5729
v  Velocity[Y]            -2.5743          7.3918      0.00095101      0.00095101
v  Velocity[Z]       -8.0222e-015     8.9404e-015    -8.2318e-018    -8.2318e-018
v  ǁVelocityǁ         0.0013935          10.386          5.2078          5.2078
v  Pressure               -46.139          15.664         -11.165         -11.165
v  nu_tilda           4.4387e-007       0.0042695       0.0013816       0.0013816
v  TempC                       21          73.041          21.861          21.861
v  TurbVisc            3.408e-014        0.005032       0.0016218       0.0016218
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1473:        0.21450E+01

===============================================================


 INSTANT    0.147400000E+04   TIME STEP NUMBER            1474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82305E-02 0.90339E+00
   Friction velocity        uk    :  0.82305E-02 0.90339E+00
   Dimensionless distance   yplus :  0.66261E-01 0.72729E+01
   Friction thermal sca.    tstar : -0.17276E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49438E-01 0.54264E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89282E-02      33   0.33103E-03   0.36437E+01 0.14089E+03 
c  Velocity[X]                                      0.15648E+01 
c  Velocity[Y]                                      0.20789E+01 
c  Velocity[Z]                                      0.15271E-29 
c  Pressure     0.13142E-06     522   0.95478E-08   0.11552E+00 0.16956E+04 
c  nu_tilda     0.59754E-05      32   0.15952E-04   0.30770E-06 0.15403E+03 
c  TempC        0.36083E+02      27   0.33760E-03   0.59610E+01 0.27897E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1548          10.386          4.5729          4.5729
v  Velocity[Y]            -2.5729           7.364        0.001001        0.001001
v  Velocity[Z]       -7.5961e-015      9.039e-015    -8.2528e-018    -8.2528e-018
v  ǁVelocityǁ         0.0012271          10.386          5.2075          5.2075
v  Pressure               -46.143          15.367         -11.261         -11.261
v  nu_tilda           4.4412e-007       0.0042695       0.0013821       0.0013821
v  TempC                       21           73.04          21.861          21.861
v  TurbVisc           3.4151e-014        0.005032       0.0016224       0.0016224
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1474:        0.22060E+01

===============================================================


 INSTANT    0.147500000E+04   TIME STEP NUMBER            1475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13109E-01 0.90286E+00
   Friction velocity        uk    :  0.13109E-01 0.90286E+00
   Dimensionless distance   yplus :  0.10553E+00 0.72687E+01
   Friction thermal sca.    tstar : -0.23079E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78740E-01 0.54232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89304E-02      33   0.27076E-03   0.36649E+01 0.14112E+03 
c  Velocity[X]                                      0.15849E+01 
c  Velocity[Y]                                      0.20800E+01 
c  Velocity[Z]                                      0.12885E-29 
c  Pressure     0.12848E-06     536   0.95312E-08   0.11206E+00 0.16128E+04 
c  nu_tilda     0.59775E-05      32   0.52695E-05   0.30810E-06 0.15412E+03 
c  TempC        0.36092E+02      27   0.41028E-03   0.49397E+01 0.22938E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1515          10.385          4.5729          4.5729
v  Velocity[Y]            -2.5714          7.3935       0.0010517       0.0010517
v  Velocity[Z]        -8.234e-015     9.0528e-015    -8.2832e-018    -8.2832e-018
v  ǁVelocityǁ        0.00031615          10.385          5.2072          5.2072
v  Pressure               -46.103          15.647         -11.177         -11.177
v  nu_tilda           4.4432e-007       0.0042695       0.0013826       0.0013826
v  TempC                       21          73.041          21.861          21.861
v  TurbVisc           3.4228e-014        0.005032        0.001623        0.001623
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1475:        0.22260E+01

===============================================================


 INSTANT    0.147600000E+04   TIME STEP NUMBER            1476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62570E-02 0.90431E+00
   Friction velocity        uk    :  0.62570E-02 0.90431E+00
   Dimensionless distance   yplus :  0.50373E-01 0.72803E+01
   Friction thermal sca.    tstar : -0.18591E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37584E-01 0.54319E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89326E-02      33   0.31349E-03   0.36477E+01 0.14117E+03 
c  Velocity[X]                                      0.15481E+01 
c  Velocity[Y]                                      0.20997E+01 
c  Velocity[Z]                                      0.12762E-29 
c  Pressure     0.11498E-06     488   0.95943E-08   0.10092E+00 0.79068E+03 
c  nu_tilda     0.59797E-05      32   0.15945E-04   0.30854E-06 0.15422E+03 
c  TempC        0.36101E+02      27   0.35373E-03   0.54587E+01 0.25228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1483          10.384          4.5729          4.5729
v  Velocity[Y]            -2.5699          7.4016       0.0011032       0.0011032
v  Velocity[Z]       -7.9731e-015      9.039e-015    -8.2927e-018    -8.2927e-018
v  ǁVelocityǁ          0.001155          10.384          5.2069          5.2069
v  Pressure               -46.103          15.539         -11.225         -11.225
v  nu_tilda            4.444e-007       0.0042695       0.0013831       0.0013831
v  TempC                       21          73.041          21.861          21.861
v  TurbVisc           3.4287e-014        0.005032       0.0016236       0.0016236
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1476:        0.22780E+01

===============================================================


 INSTANT    0.147700000E+04   TIME STEP NUMBER            1477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14890E-01 0.90387E+00
   Friction velocity        uk    :  0.14890E-01 0.90387E+00
   Dimensionless distance   yplus :  0.11987E+00 0.72768E+01
   Friction thermal sca.    tstar : -0.17075E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89439E-01 0.54293E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89348E-02      33   0.30870E-03   0.36813E+01 0.14137E+03 
c  Velocity[X]                                      0.15851E+01 
c  Velocity[Y]                                      0.20962E+01 
c  Velocity[Z]                                      0.12749E-29 
c  Pressure     0.14169E-06     410   0.97466E-08   0.12348E+00 0.43373E+03 
c  nu_tilda     0.59818E-05      32   0.52782E-05   0.30896E-06 0.15431E+03 
c  TempC        0.36110E+02      27   0.38956E-03   0.42551E+01 0.22977E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1451          10.384          4.5729          4.5729
v  Velocity[Y]            -2.5684          7.3701       0.0011546       0.0011546
v  Velocity[Z]       -8.3744e-015     9.0157e-015    -8.3302e-018    -8.3302e-018
v  ǁVelocityǁ         0.0014066          10.384          5.2066          5.2066
v  Pressure               -46.065          15.512          -11.21          -11.21
v  nu_tilda           4.4448e-007       0.0042695       0.0013837       0.0013837
v  TempC                       21          73.041          21.861          21.861
v  TurbVisc           3.4312e-014        0.005032       0.0016242       0.0016242
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1477:        0.21650E+01

===============================================================


 INSTANT    0.147800000E+04   TIME STEP NUMBER            1478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48801E-02 0.90252E+00
   Friction velocity        uk    :  0.48801E-02 0.90252E+00
   Dimensionless distance   yplus :  0.39288E-01 0.72659E+01
   Friction thermal sca.    tstar : -0.19385E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29313E-01 0.54212E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89370E-02      33   0.31715E-03   0.36776E+01 0.14151E+03 
c  Velocity[X]                                      0.15865E+01 
c  Velocity[Y]                                      0.20911E+01 
c  Velocity[Z]                                      0.11905E-29 
c  Pressure     0.11453E-06     440   0.95651E-08   0.99198E-01 0.39365E+03 
c  nu_tilda     0.59839E-05      32   0.15944E-04   0.30941E-06 0.15440E+03 
c  TempC        0.36120E+02      27   0.38441E-03   0.52822E+01 0.26629E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1419          10.383          4.5729          4.5729
v  Velocity[Y]            -2.5669           7.391        0.001207        0.001207
v  Velocity[Z]       -8.3022e-015      8.997e-015    -8.3504e-018    -8.3504e-018
v  ǁVelocityǁ        0.00036752          10.383          5.2063          5.2063
v  Pressure               -46.069          15.512         -11.239         -11.239
v  nu_tilda           4.4455e-007       0.0042695       0.0013842       0.0013842
v  TempC                       21          73.041          21.862          21.862
v  TurbVisc           3.4338e-014        0.005032       0.0016249       0.0016249
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1478:        0.19860E+01

===============================================================


 INSTANT    0.147900000E+04   TIME STEP NUMBER            1479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77889E-02 0.90365E+00
   Friction velocity        uk    :  0.77889E-02 0.90365E+00
   Dimensionless distance   yplus :  0.62706E-01 0.72750E+01
   Friction thermal sca.    tstar : -0.17668E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46786E-01 0.54280E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89392E-02      33   0.32377E-03   0.36825E+01 0.14169E+03 
c  Velocity[X]                                      0.15689E+01 
c  Velocity[Y]                                      0.21137E+01 
c  Velocity[Z]                                      0.15544E-29 
c  Pressure     0.13532E-06     458   0.99559E-08   0.12049E+00 0.53172E+03 
c  nu_tilda     0.59860E-05      32   0.52689E-05   0.30982E-06 0.15449E+03 
c  TempC        0.36129E+02      27   0.35001E-03   0.68434E+01 0.26133E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1386          10.383          4.5729          4.5729
v  Velocity[Y]            -2.5655          7.3698       0.0012605       0.0012605
v  Velocity[Z]       -8.7428e-015     8.5944e-015    -8.3738e-018    -8.3738e-018
v  ǁVelocityǁ        0.00095031          10.383           5.206           5.206
v  Pressure               -46.025           15.52         -11.215         -11.215
v  nu_tilda           4.4459e-007       0.0042695       0.0013847       0.0013847
v  TempC                       21          73.042          21.862          21.862
v  TurbVisc            3.436e-014        0.005032       0.0016255       0.0016255
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1479:        0.20280E+01

===============================================================


 INSTANT    0.148000000E+04   TIME STEP NUMBER            1480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12690E-02 0.90270E+00
   Friction velocity        uk    :  0.12690E-02 0.90270E+00
   Dimensionless distance   yplus :  0.10216E-01 0.72674E+01
   Friction thermal sca.    tstar : -0.19916E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76224E-02 0.54223E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89414E-02      33   0.27158E-03   0.36747E+01 0.14173E+03 
c  Velocity[X]                                      0.15718E+01 
c  Velocity[Y]                                      0.21029E+01 
c  Velocity[Z]                                      0.13248E-29 
c  Pressure     0.12694E-06     442   0.96939E-08   0.10921E+00 0.46879E+03 
c  nu_tilda     0.59882E-05      32   0.15942E-04   0.31026E-06 0.15458E+03 
c  TempC        0.36138E+02      26   0.33099E-03   0.52313E+01 0.23799E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1353          10.382          4.5729          4.5729
v  Velocity[Y]             -2.564          7.3899       0.0013139       0.0013139
v  Velocity[Z]        -8.451e-015     8.8978e-015    -8.3975e-018    -8.3975e-018
v  ǁVelocityǁ         0.0014696          10.382          5.2057          5.2057
v  Pressure               -46.031          15.489         -11.249         -11.249
v  nu_tilda           4.4461e-007       0.0042695       0.0013852       0.0013852
v  TempC                       21          73.041          21.862          21.862
v  TurbVisc           3.4372e-014        0.005032       0.0016261       0.0016261
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1480:        0.20150E+01

===============================================================


 INSTANT    0.148100000E+04   TIME STEP NUMBER            1481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13224E-01 0.90444E+00
   Friction velocity        uk    :  0.13224E-01 0.90444E+00
   Dimensionless distance   yplus :  0.10646E+00 0.72814E+01
   Friction thermal sca.    tstar : -0.17982E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79432E-01 0.54327E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89436E-02      33   0.32985E-03   0.36839E+01 0.14190E+03 
c  Velocity[X]                                      0.15779E+01 
c  Velocity[Y]                                      0.21060E+01 
c  Velocity[Z]                                      0.12788E-29 
c  Pressure     0.12869E-06     504   0.99807E-08   0.11151E+00 0.11495E+04 
c  nu_tilda     0.59903E-05      32   0.52584E-05   0.31067E-06 0.15467E+03 
c  TempC        0.36148E+02      27   0.37106E-03   0.40372E+01 0.23060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.132          10.381          4.5729          4.5729
v  Velocity[Y]            -2.5625          7.4038       0.0013682       0.0013682
v  Velocity[Z]       -8.5141e-015     8.9954e-015    -8.4243e-018    -8.4243e-018
v  ǁVelocityǁ        0.00039291          10.381          5.2054          5.2054
v  Pressure                -45.99          15.659         -11.187         -11.187
v  nu_tilda           4.4456e-007       0.0042695       0.0013858       0.0013858
v  TempC                       21          73.042          21.862          21.862
v  TurbVisc           3.4377e-014        0.005032       0.0016267       0.0016267
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1481:        0.21360E+01

===============================================================


 INSTANT    0.148200000E+04   TIME STEP NUMBER            1482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26220E-02 0.90402E+00
   Friction velocity        uk    :  0.26220E-02 0.90402E+00
   Dimensionless distance   yplus :  0.21109E-01 0.72779E+01
   Friction thermal sca.    tstar : -0.15683E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15750E-01 0.54302E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89458E-02      33   0.29944E-03   0.37138E+01 0.14219E+03 
c  Velocity[X]                                      0.15880E+01 
c  Velocity[Y]                                      0.21258E+01 
c  Velocity[Z]                                      0.10263E-29 
c  Pressure     0.13638E-06     505   0.90267E-08   0.12144E+00 0.14780E+04 
c  nu_tilda     0.59924E-05      32   0.15934E-04   0.31112E-06 0.15477E+03 
c  TempC        0.36157E+02      27   0.32376E-03   0.54239E+01 0.25606E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1289          10.381          4.5729          4.5729
v  Velocity[Y]             -2.561          7.3734       0.0014232       0.0014232
v  Velocity[Z]       -8.3362e-015     9.1186e-015    -8.4486e-018    -8.4486e-018
v  ǁVelocityǁ        0.00091754          10.381          5.2051          5.2051
v  Pressure               -45.988          15.405          -11.27          -11.27
v  nu_tilda           4.4457e-007       0.0042695       0.0013863       0.0013863
v  TempC                       21          73.041          21.863          21.863
v  TurbVisc           3.4364e-014        0.005032       0.0016273       0.0016273
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1482:        0.21570E+01

===============================================================


 INSTANT    0.148300000E+04   TIME STEP NUMBER            1483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14877E-01 0.90258E+00
   Friction velocity        uk    :  0.14877E-01 0.90258E+00
   Dimensionless distance   yplus :  0.11977E+00 0.72664E+01
   Friction thermal sca.    tstar : -0.18382E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89364E-01 0.54216E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89480E-02      33   0.31188E-03   0.36928E+01 0.14212E+03 
c  Velocity[X]                                      0.15768E+01 
c  Velocity[Y]                                      0.21160E+01 
c  Velocity[Z]                                      0.12831E-29 
c  Pressure     0.13068E-06     504   0.93627E-08   0.11254E+00 0.12447E+04 
c  nu_tilda     0.59946E-05      32   0.52575E-05   0.31154E-06 0.15486E+03 
c  TempC        0.36166E+02      26   0.31603E-03   0.49591E+01 0.23943E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1257           10.38          4.5729          4.5729
v  Velocity[Y]            -2.5596          7.3913       0.0014786       0.0014786
v  Velocity[Z]       -8.1607e-015     8.9936e-015    -8.4833e-018    -8.4833e-018
v  ǁVelocityǁ         0.0014514           10.38          5.2048          5.2048
v  Pressure                -45.95          15.607         -11.205         -11.205
v  nu_tilda           4.4451e-007       0.0042695       0.0013868       0.0013868
v  TempC                       21          73.042          21.863          21.863
v  TurbVisc           3.4367e-014        0.005032        0.001628        0.001628
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1483:        0.21340E+01

===============================================================


 INSTANT    0.148400000E+04   TIME STEP NUMBER            1484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49239E-02 0.90376E+00
   Friction velocity        uk    :  0.49239E-02 0.90376E+00
   Dimensionless distance   yplus :  0.39641E-01 0.72759E+01
   Friction thermal sca.    tstar : -0.17180E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29576E-01 0.54286E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89502E-02      33   0.32738E-03   0.37196E+01 0.14241E+03 
c  Velocity[X]                                      0.16056E+01 
c  Velocity[Y]                                      0.21140E+01 
c  Velocity[Z]                                      0.10499E-29 
c  Pressure     0.12049E-06     489   0.97677E-08   0.10583E+00 0.11829E+04 
c  nu_tilda     0.59967E-05      32   0.15934E-04   0.31199E-06 0.15495E+03 
c  TempC        0.36176E+02      27   0.36773E-03   0.45585E+01 0.22374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1225          10.379          4.5729          4.5729
v  Velocity[Y]            -2.5581          7.3688       0.0015345       0.0015345
v  Velocity[Z]       -7.9797e-015     8.9725e-015    -8.5098e-018    -8.5098e-018
v  ǁVelocityǁ        0.00034921          10.379          5.2045          5.2045
v  Pressure               -45.953          15.408         -11.274         -11.274
v  nu_tilda           4.4451e-007       0.0042695       0.0013873       0.0013873
v  TempC                       21          73.041          21.863          21.863
v  TurbVisc           3.4348e-014        0.005032       0.0016286       0.0016286
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1484:        0.21040E+01

===============================================================


 INSTANT    0.148500000E+04   TIME STEP NUMBER            1485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12144E-01 0.90295E+00
   Friction velocity        uk    :  0.12144E-01 0.90295E+00
   Dimensionless distance   yplus :  0.97769E-01 0.72694E+01
   Friction thermal sca.    tstar : -0.18818E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72947E-01 0.54238E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89523E-02      33   0.24222E-03   0.37150E+01 0.14254E+03 
c  Velocity[X]                                      0.15746E+01 
c  Velocity[Y]                                      0.21405E+01 
c  Velocity[Z]                                      0.93681E-30 
c  Pressure     0.11379E-06     506   0.98672E-08   0.98613E-01 0.13876E+04 
c  nu_tilda     0.59988E-05      32   0.52465E-05   0.31240E-06 0.15504E+03 
c  TempC        0.36185E+02      27   0.30830E-03   0.56059E+01 0.26143E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1192          10.379          4.5729          4.5729
v  Velocity[Y]            -2.5566          7.3954       0.0015913       0.0015913
v  Velocity[Z]       -7.8549e-015     8.9515e-015    -8.5434e-018    -8.5434e-018
v  ǁVelocityǁ        0.00094318          10.379          5.2042          5.2042
v  Pressure               -45.916          15.643         -11.202         -11.202
v  nu_tilda           4.4448e-007       0.0042695       0.0013879       0.0013879
v  TempC                       21          73.041          21.863          21.863
v  TurbVisc           3.4346e-014        0.005032       0.0016292       0.0016292
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1485:        0.21380E+01

===============================================================


 INSTANT    0.148600000E+04   TIME STEP NUMBER            1486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61453E-02 0.90425E+00
   Friction velocity        uk    :  0.61453E-02 0.90425E+00
   Dimensionless distance   yplus :  0.49474E-01 0.72798E+01
   Friction thermal sca.    tstar : -0.15489E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36913E-01 0.54316E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89546E-02      33   0.32505E-03   0.36859E+01 0.14246E+03 
c  Velocity[X]                                      0.15581E+01 
c  Velocity[Y]                                      0.21278E+01 
c  Velocity[Z]                                      0.13319E-29 
c  Pressure     0.12457E-06     474   0.91587E-08   0.10665E+00 0.11030E+04 
c  nu_tilda     0.60010E-05      32   0.15926E-04   0.31285E-06 0.15514E+03 
c  TempC        0.36194E+02      27   0.42035E-03   0.44394E+01 0.23288E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1159          10.378          4.5729          4.5729
v  Velocity[Y]            -2.5552          7.4001       0.0016488       0.0016488
v  Velocity[Z]       -9.2251e-015     8.6609e-015    -8.5705e-018    -8.5705e-018
v  ǁVelocityǁ         0.0013153          10.378          5.2039          5.2039
v  Pressure               -45.918          15.472         -11.268         -11.268
v  nu_tilda           4.4447e-007       0.0042695       0.0013884       0.0013884
v  TempC                       21          73.041          21.863          21.863
v  TurbVisc           3.4339e-014        0.005032       0.0016298       0.0016298
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1486:        0.20820E+01

===============================================================


 INSTANT    0.148700000E+04   TIME STEP NUMBER            1487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10355E-01 0.90414E+00
   Friction velocity        uk    :  0.10355E-01 0.90414E+00
   Dimensionless distance   yplus :  0.83367E-01 0.72790E+01
   Friction thermal sca.    tstar : -0.16065E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62201E-01 0.54309E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89567E-02      33   0.32226E-03   0.37448E+01 0.14290E+03 
c  Velocity[X]                                      0.16172E+01 
c  Velocity[Y]                                      0.21276E+01 
c  Velocity[Z]                                      0.12824E-29 
c  Pressure     0.14278E-06     457   0.93185E-08   0.12534E+00 0.67687E+03 
c  nu_tilda     0.60031E-05      32   0.52468E-05   0.31326E-06 0.15523E+03 
c  TempC        0.36203E+02      28   0.36604E-03   0.58920E+01 0.24471E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1127          10.378          4.5729          4.5729
v  Velocity[Y]            -2.5537          7.3756       0.0017069       0.0017069
v  Velocity[Z]       -1.0276e-014     9.5765e-015    -8.6098e-018    -8.6098e-018
v  ǁVelocityǁ        0.00025583          10.378          5.2036          5.2036
v  Pressure               -45.874          15.517         -11.232         -11.232
v  nu_tilda           4.4451e-007       0.0042695       0.0013889       0.0013889
v  TempC                       21          73.041          21.864          21.864
v  TurbVisc           3.4335e-014        0.005032       0.0016304       0.0016304
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1487:        0.20440E+01

===============================================================


 INSTANT    0.148800000E+04   TIME STEP NUMBER            1488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62433E-02 0.90271E+00
   Friction velocity        uk    :  0.62433E-02 0.90271E+00
   Dimensionless distance   yplus :  0.50263E-01 0.72674E+01
   Friction thermal sca.    tstar : -0.18305E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37502E-01 0.54223E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89590E-02      33   0.30889E-03   0.37274E+01 0.14297E+03 
c  Velocity[X]                                      0.15787E+01 
c  Velocity[Y]                                      0.21487E+01 
c  Velocity[Z]                                      0.11193E-29 
c  Pressure     0.11312E-06     458   0.98840E-08   0.97774E-01 0.45970E+03 
c  nu_tilda     0.60052E-05      32   0.15923E-04   0.31371E-06 0.15532E+03 
c  TempC        0.36213E+02      27   0.34046E-03   0.45421E+01 0.22504E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1095          10.377          4.5729          4.5729
v  Velocity[Y]            -2.5522          7.3934       0.0017652       0.0017652
v  Velocity[Z]       -8.1129e-015     8.9496e-015    -8.6433e-018    -8.6433e-018
v  ǁVelocityǁ         0.0010704          10.377          5.2033          5.2033
v  Pressure               -45.881          15.505         -11.268         -11.268
v  nu_tilda           4.4449e-007       0.0042695       0.0013894       0.0013894
v  TempC                       21          73.041          21.864          21.864
v  TurbVisc           3.4347e-014        0.005032       0.0016311       0.0016311
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1488:        0.20470E+01

===============================================================


 INSTANT    0.148900000E+04   TIME STEP NUMBER            1489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75578E-02 0.90367E+00
   Friction velocity        uk    :  0.75578E-02 0.90367E+00
   Dimensionless distance   yplus :  0.60846E-01 0.72752E+01
   Friction thermal sca.    tstar : -0.15646E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45398E-01 0.54281E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89611E-02      33   0.32368E-03   0.37366E+01 0.14302E+03 
c  Velocity[X]                                      0.15939E+01 
c  Velocity[Y]                                      0.21426E+01 
c  Velocity[Z]                                      0.15178E-29 
c  Pressure     0.13896E-06     442   0.94892E-08   0.12010E+00 0.53261E+03 
c  nu_tilda     0.60074E-05      32   0.52411E-05   0.31413E-06 0.15541E+03 
c  TempC        0.36222E+02      27   0.37037E-03   0.41089E+01 0.22580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1063          10.377          4.5729          4.5729
v  Velocity[Y]            -2.5507          7.3679       0.0018246       0.0018246
v  Velocity[Z]       -1.0222e-014     8.9625e-015    -8.6737e-018    -8.6737e-018
v  ǁVelocityǁ         0.0011249          10.377           5.203           5.203
v  Pressure                -45.84          15.499         -11.243         -11.243
v  nu_tilda           4.4453e-007       0.0042695         0.00139         0.00139
v  TempC                       21          73.041          21.864          21.864
v  TurbVisc           3.4341e-014        0.005032       0.0016317       0.0016317
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1489:        0.20020E+01

===============================================================


 INSTANT    0.149000000E+04   TIME STEP NUMBER            1490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80033E-02 0.90294E+00
   Friction velocity        uk    :  0.80033E-02 0.90294E+00
   Dimensionless distance   yplus :  0.64432E-01 0.72693E+01
   Friction thermal sca.    tstar : -0.17014E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48073E-01 0.54237E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89633E-02      33   0.26393E-03   0.37487E+01 0.14322E+03 
c  Velocity[X]                                      0.16087E+01 
c  Velocity[Y]                                      0.21400E+01 
c  Velocity[Z]                                      0.11308E-29 
c  Pressure     0.11608E-06     440   0.99426E-08   0.10065E+00 0.42859E+03 
c  nu_tilda     0.60095E-05      32   0.15923E-04   0.31459E-06 0.15551E+03 
c  TempC        0.36231E+02      26   0.37823E-03   0.63810E+01 0.26318E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.103          10.376          4.5729          4.5729
v  Velocity[Y]            -2.5493          7.3946       0.0018842       0.0018842
v  Velocity[Z]       -1.0901e-014     9.5642e-015    -8.7159e-018    -8.7159e-018
v  ǁVelocityǁ        0.00022071          10.376          5.2027          5.2027
v  Pressure               -45.841          15.491         -11.273         -11.273
v  nu_tilda           4.4459e-007       0.0042695       0.0013905       0.0013905
v  TempC                       21           73.04          21.864          21.864
v  TurbVisc           3.4353e-014        0.005032       0.0016323       0.0016323
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1490:        0.20000E+01

===============================================================


 INSTANT    0.149100000E+04   TIME STEP NUMBER            1491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10083E-01 0.90458E+00
   Friction velocity        uk    :  0.10083E-01 0.90458E+00
   Dimensionless distance   yplus :  0.81177E-01 0.72825E+01
   Friction thermal sca.    tstar : -0.15876E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60567E-01 0.54336E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89655E-02      33   0.30481E-03   0.37231E+01 0.14327E+03 
c  Velocity[X]                                      0.15616E+01 
c  Velocity[Y]                                      0.21615E+01 
c  Velocity[Z]                                      0.10734E-29 
c  Pressure     0.11366E-06     472   0.99227E-08   0.98736E-01 0.92107E+03 
c  nu_tilda     0.60116E-05      32   0.52332E-05   0.31500E-06 0.15560E+03 
c  TempC        0.36241E+02      27   0.34834E-03   0.57703E+01 0.26666E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0997          10.375          4.5729          4.5729
v  Velocity[Y]            -2.5478          7.4063       0.0019449       0.0019449
v  Velocity[Z]       -1.0556e-014     9.4153e-015    -8.7506e-018    -8.7506e-018
v  ǁVelocityǁ         0.0013039          10.375          5.2024          5.2024
v  Pressure               -45.802          15.621         -11.225         -11.225
v  nu_tilda           4.4455e-007       0.0042695        0.001391        0.001391
v  TempC                       21          73.041          21.865          21.865
v  TurbVisc           3.4371e-014        0.005032       0.0016329       0.0016329
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1491:        0.20770E+01

===============================================================


 INSTANT    0.149200000E+04   TIME STEP NUMBER            1492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67457E-02 0.90405E+00
   Friction velocity        uk    :  0.67457E-02 0.90405E+00
   Dimensionless distance   yplus :  0.54308E-01 0.72782E+01
   Friction thermal sca.    tstar : -0.15227E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40520E-01 0.54304E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89677E-02      33   0.31987E-03   0.37499E+01 0.14348E+03 
c  Velocity[X]                                      0.15988E+01 
c  Velocity[Y]                                      0.21510E+01 
c  Velocity[Z]                                      0.11231E-29 
c  Pressure     0.12809E-06     506   0.97154E-08   0.11127E+00 0.14487E+04 
c  nu_tilda     0.60138E-05      32   0.15914E-04   0.31545E-06 0.15569E+03 
c  TempC        0.36250E+02      27   0.28839E-03   0.48207E+01 0.23859E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0963          10.375          4.5729          4.5729
v  Velocity[Y]            -2.5464           7.372       0.0020056       0.0020056
v  Velocity[Z]       -1.2412e-014     9.3032e-015    -8.7931e-018    -8.7931e-018
v  ǁVelocityǁ        0.00078318          10.375          5.2021          5.2021
v  Pressure               -45.804          15.361         -11.306         -11.306
v  nu_tilda           4.4458e-007       0.0042695       0.0013915       0.0013915
v  TempC                       21           73.04          21.865          21.865
v  TurbVisc           3.4359e-014        0.005032       0.0016335       0.0016335
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1492:        0.21490E+01

===============================================================


 INSTANT    0.149300000E+04   TIME STEP NUMBER            1493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11073E-01 0.90280E+00
   Friction velocity        uk    :  0.11073E-01 0.90280E+00
   Dimensionless distance   yplus :  0.89142E-01 0.72681E+01
   Friction thermal sca.    tstar : -0.17314E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66510E-01 0.54228E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89699E-02      33   0.32839E-03   0.37656E+01 0.14367E+03 
c  Velocity[X]                                      0.16117E+01 
c  Velocity[Y]                                      0.21539E+01 
c  Velocity[Z]                                      0.13608E-29 
c  Pressure     0.12887E-06     521   0.93084E-08   0.11166E+00 0.16233E+04 
c  nu_tilda     0.60159E-05      32   0.52254E-05   0.31587E-06 0.15578E+03 
c  TempC        0.36259E+02      27   0.39384E-03   0.41875E+01 0.20481E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0932          10.374          4.5729          4.5729
v  Velocity[Y]            -2.5449          7.3961       0.0020673       0.0020673
v  Velocity[Z]       -1.2443e-014     9.6785e-015    -8.8322e-018    -8.8322e-018
v  ǁVelocityǁ        0.00047226          10.374          5.2018          5.2018
v  Pressure               -45.761          15.637          -11.22          -11.22
v  nu_tilda            4.446e-007       0.0042695       0.0013921       0.0013921
v  TempC                       21          73.041          21.865          21.865
v  TurbVisc           3.4369e-014        0.005032       0.0016341       0.0016341
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1493:        0.21750E+01

===============================================================


 INSTANT    0.149400000E+04   TIME STEP NUMBER            1494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87719E-02 0.90382E+00
   Friction velocity        uk    :  0.87719E-02 0.90382E+00
   Dimensionless distance   yplus :  0.70620E-01 0.72763E+01
   Friction thermal sca.    tstar : -0.14612E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52690E-01 0.54290E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89721E-02      33   0.31065E-03   0.37716E+01 0.14387E+03 
c  Velocity[X]                                      0.15980E+01 
c  Velocity[Y]                                      0.21736E+01 
c  Velocity[Z]                                      0.12062E-29 
c  Pressure     0.12162E-06     506   0.92110E-08   0.10655E+00 0.14749E+04 
c  nu_tilda     0.60181E-05      32   0.15914E-04   0.31633E-06 0.15588E+03 
c  TempC        0.36268E+02      28   0.35478E-03   0.51569E+01 0.24139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0901          10.374          4.5729          4.5729
v  Velocity[Y]            -2.5434          7.3717       0.0021296       0.0021296
v  Velocity[Z]       -1.1423e-014     8.8051e-015    -8.8703e-018    -8.8703e-018
v  ǁVelocityǁ         0.0015351          10.374          5.2015          5.2015
v  Pressure               -45.765          15.387         -11.306         -11.306
v  nu_tilda           4.4465e-007       0.0042695       0.0013925       0.0013925
v  TempC                       21           73.04          21.865          21.865
v  TurbVisc           3.4376e-014        0.005032       0.0016348       0.0016348
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1494:        0.21570E+01

===============================================================


 INSTANT    0.149500000E+04   TIME STEP NUMBER            1495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15747E-01 0.90298E+00
   Friction velocity        uk    :  0.15747E-01 0.90298E+00
   Dimensionless distance   yplus :  0.12677E+00 0.72696E+01
   Friction thermal sca.    tstar : -0.16474E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94586E-01 0.54240E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89743E-02      33   0.24974E-03   0.37608E+01 0.14381E+03 
c  Velocity[X]                                      0.15978E+01 
c  Velocity[Y]                                      0.21630E+01 
c  Velocity[Z]                                      0.11330E-29 
c  Pressure     0.13464E-06     504   0.98614E-08   0.11576E+00 0.12589E+04 
c  nu_tilda     0.60202E-05      32   0.52153E-05   0.31675E-06 0.15597E+03 
c  TempC        0.36278E+02      27   0.33950E-03   0.46504E+01 0.22456E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0868          10.373          4.5729          4.5729
v  Velocity[Y]             -2.542          7.3944       0.0021927       0.0021927
v  Velocity[Z]       -1.3036e-014     8.9014e-015    -8.9112e-018    -8.9112e-018
v  ǁVelocityǁ         0.0003593          10.373          5.2012          5.2012
v  Pressure               -45.724          15.589         -11.239         -11.239
v  nu_tilda           4.4465e-007       0.0042695       0.0013931       0.0013931
v  TempC                       21          73.041          21.865          21.865
v  TurbVisc            3.439e-014        0.005032       0.0016354       0.0016354
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1495:        0.21390E+01

===============================================================


 INSTANT    0.149600000E+04   TIME STEP NUMBER            1496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75082E-02 0.90458E+00
   Friction velocity        uk    :  0.75082E-02 0.90458E+00
   Dimensionless distance   yplus :  0.60446E-01 0.72825E+01
   Friction thermal sca.    tstar : -0.15653E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45099E-01 0.54335E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89765E-02      33   0.31922E-03   0.37604E+01 0.14397E+03 
c  Velocity[X]                                      0.15968E+01 
c  Velocity[Y]                                      0.21636E+01 
c  Velocity[Z]                                      0.98864E-30 
c  Pressure     0.10993E-06     472   0.95866E-08   0.95869E-01 0.78321E+03 
c  nu_tilda     0.60224E-05      32   0.15906E-04   0.31721E-06 0.15606E+03 
c  TempC        0.36287E+02      27   0.33336E-03   0.41263E+01 0.22158E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0835          10.372          4.5729          4.5729
v  Velocity[Y]            -2.5405           7.405       0.0022559       0.0022559
v  Velocity[Z]       -1.1815e-014     8.9149e-015     -8.943e-018     -8.943e-018
v  ǁVelocityǁ        0.00090138          10.372          5.2009          5.2009
v  Pressure                -45.73           15.49         -11.291         -11.291
v  nu_tilda           4.4465e-007       0.0042695       0.0013936       0.0013936
v  TempC                       21           73.04          21.866          21.866
v  TurbVisc            3.439e-014        0.005032        0.001636        0.001636
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1496:        0.20750E+01

===============================================================


 INSTANT    0.149700000E+04   TIME STEP NUMBER            1497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10832E-01 0.90424E+00
   Friction velocity        uk    :  0.10832E-01 0.90424E+00
   Dimensionless distance   yplus :  0.87203E-01 0.72797E+01
   Friction thermal sca.    tstar : -0.14541E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65063E-01 0.54315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89787E-02      33   0.30410E-03   0.37856E+01 0.14425E+03 
c  Velocity[X]                                      0.16000E+01 
c  Velocity[Y]                                      0.21857E+01 
c  Velocity[Z]                                      0.10258E-29 
c  Pressure     0.13432E-06     472   0.97485E-08   0.11791E+00 0.61028E+03 
c  nu_tilda     0.60245E-05      32   0.52223E-05   0.31763E-06 0.15615E+03 
c  TempC        0.36296E+02      27   0.33571E-03   0.41345E+01 0.21534E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0802          10.372          4.5729          4.5729
v  Velocity[Y]            -2.5391          7.3768       0.0023202       0.0023202
v  Velocity[Z]       -1.3532e-014     9.3915e-015    -8.9878e-018    -8.9878e-018
v  ǁVelocityǁ         0.0010352          10.372          5.2006          5.2006
v  Pressure               -45.689          15.517          -11.26          -11.26
v  nu_tilda            4.447e-007       0.0042695       0.0013941       0.0013941
v  TempC                       21          73.041          21.866          21.866
v  TurbVisc           3.4392e-014        0.005032       0.0016366       0.0016366
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1497:        0.20730E+01

===============================================================


 INSTANT    0.149800000E+04   TIME STEP NUMBER            1498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94966E-02 0.90264E+00
   Friction velocity        uk    :  0.94966E-02 0.90264E+00
   Dimensionless distance   yplus :  0.76454E-01 0.72669E+01
   Friction thermal sca.    tstar : -0.14889E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57043E-01 0.54219E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89809E-02      33   0.32221E-03   0.37698E+01 0.14424E+03 
c  Velocity[X]                                      0.15939E+01 
c  Velocity[Y]                                      0.21759E+01 
c  Velocity[Z]                                      0.10138E-29 
c  Pressure     0.13827E-06     473   0.96159E-08   0.11908E+00 0.46561E+03 
c  nu_tilda     0.60267E-05      32   0.15903E-04   0.31808E-06 0.15625E+03 
c  TempC        0.36305E+02      27   0.43354E-03   0.50624E+01 0.23958E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.077          10.371          4.5729          4.5729
v  Velocity[Y]            -2.5376          7.3921       0.0023849       0.0023849
v  Velocity[Z]       -1.2615e-014     9.6365e-015    -9.0217e-018    -9.0217e-018
v  ǁVelocityǁ        0.00024883          10.371          5.2003          5.2003
v  Pressure               -45.689          15.482         -11.292         -11.292
v  nu_tilda           4.4474e-007       0.0042695       0.0013946       0.0013946
v  TempC                       21           73.04          21.866          21.866
v  TurbVisc           3.4405e-014        0.005032       0.0016372       0.0016372
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1498:        0.20860E+01

===============================================================


 INSTANT    0.149900000E+04   TIME STEP NUMBER            1499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14905E-01 0.90398E+00
   Friction velocity        uk    :  0.14905E-01 0.90398E+00
   Dimensionless distance   yplus :  0.12000E+00 0.72776E+01
   Friction thermal sca.    tstar : -0.16189E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89533E-01 0.54299E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89831E-02      33   0.33438E-03   0.38053E+01 0.14458E+03 
c  Velocity[X]                                      0.16297E+01 
c  Velocity[Y]                                      0.21756E+01 
c  Velocity[Z]                                      0.11782E-29 
c  Pressure     0.13242E-06     457   0.93283E-08   0.11730E+00 0.48841E+03 
c  nu_tilda     0.60288E-05      32   0.52082E-05   0.31851E-06 0.15634E+03 
c  TempC        0.36315E+02      26   0.32523E-03   0.71576E+01 0.27472E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0738          10.371          4.5729          4.5729
v  Velocity[Y]            -2.5362          7.3734       0.0024503       0.0024503
v  Velocity[Z]       -1.3098e-014     9.5394e-015    -9.0497e-018    -9.0497e-018
v  ǁVelocityǁ         0.0014145          10.371             5.2             5.2
v  Pressure               -45.649          15.493         -11.271         -11.271
v  nu_tilda           4.4482e-007       0.0042695       0.0013952       0.0013952
v  TempC                       21           73.04          21.866          21.866
v  TurbVisc           3.4418e-014        0.005032       0.0016378       0.0016378
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1499:        0.20490E+01

===============================================================


 INSTANT    0.150000000E+04   TIME STEP NUMBER            1500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77512E-02 0.90311E+00
   Friction velocity        uk    :  0.77512E-02 0.90311E+00
   Dimensionless distance   yplus :  0.62402E-01 0.72706E+01
   Friction thermal sca.    tstar : -0.27266E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46559E-01 0.54247E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200


 Write intermediate restart files
   checkpoint at iteration       1500, Physical time    0.15000E+04


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.62600E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89853E-02      33   0.23826E-03   0.37993E+01 0.14467E+03 
c  Velocity[X]                                      0.16017E+01 
c  Velocity[Y]                                      0.21977E+01 
c  Velocity[Z]                                      0.11889E-29 
c  Pressure     0.11683E-06     425   0.93102E-08   0.10163E+00 0.32273E+03 
c  nu_tilda     0.60310E-05      32   0.15902E-04   0.31897E-06 0.15643E+03 
c  TempC        0.36324E+02      26   0.36373E-03   0.38244E+01 0.21026E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0706           10.37          4.5729          4.5729
v  Velocity[Y]            -2.5347           7.397       0.0025164       0.0025164
v  Velocity[Z]       -1.2137e-014     9.7281e-015    -9.0804e-018    -9.0804e-018
v  ǁVelocityǁ        0.00037232           10.37          5.1997          5.1997
v  Pressure               -45.653          15.505         -11.295         -11.295
v  nu_tilda           4.4487e-007       0.0042695       0.0013957       0.0013957
v  TempC                       21           73.04          21.866          21.866
v  TurbVisc           3.4444e-014        0.005032       0.0016384       0.0016384
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1500:        0.25830E+01

===============================================================


 INSTANT    0.150100000E+04   TIME STEP NUMBER            1501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93989E-02 0.90451E+00
   Friction velocity        uk    :  0.93989E-02 0.90451E+00
   Dimensionless distance   yplus :  0.75667E-01 0.72819E+01
   Friction thermal sca.    tstar : -0.35595E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56456E-01 0.54331E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89875E-02      33   0.31213E-03   0.37766E+01 0.14459E+03 
c  Velocity[X]                                      0.15875E+01 
c  Velocity[Y]                                      0.21891E+01 
c  Velocity[Z]                                      0.12814E-29 
c  Pressure     0.13242E-06     442   0.93601E-08   0.11442E+00 0.65168E+03 
c  nu_tilda     0.60331E-05      32   0.52031E-05   0.31939E-06 0.15653E+03 
c  TempC        0.36333E+02      26   0.38691E-03   0.46573E+01 0.24302E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0673          10.369          4.5729          4.5729
v  Velocity[Y]            -2.5332          7.4044       0.0025832       0.0025832
v  Velocity[Z]       -1.3018e-014     9.9466e-015    -9.1188e-018    -9.1188e-018
v  ǁVelocityǁ         0.0008326          10.369          5.1994          5.1994
v  Pressure               -45.614          15.567         -11.262         -11.262
v  nu_tilda           4.4486e-007       0.0042695       0.0013962       0.0013962
v  TempC                       21          73.041          21.867          21.867
v  TurbVisc           3.4458e-014        0.005032        0.001639        0.001639
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1501:        0.20000E+01

===============================================================


 INSTANT    0.150200000E+04   TIME STEP NUMBER            1502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96644E-02 0.90425E+00
   Friction velocity        uk    :  0.96644E-02 0.90425E+00
   Dimensionless distance   yplus :  0.77805E-01 0.72798E+01
   Friction thermal sca.    tstar : -0.16628E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58051E-01 0.54315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89897E-02      33   0.30959E-03   0.38254E+01 0.14496E+03 
c  Velocity[X]                                      0.16365E+01 
c  Velocity[Y]                                      0.21889E+01 
c  Velocity[Z]                                      0.11393E-29 
c  Pressure     0.12654E-06     505   0.96920E-08   0.11190E+00 0.93738E+03 
c  nu_tilda     0.60353E-05      32   0.15894E-04   0.31985E-06 0.15662E+03 
c  TempC        0.36342E+02      26   0.37653E-03   0.54373E+01 0.25715E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.064          10.369          4.5729          4.5729
v  Velocity[Y]            -2.5318          7.3752       0.0026503       0.0026503
v  Velocity[Z]       -1.2535e-014     1.0565e-014    -9.1469e-018    -9.1469e-018
v  ǁVelocityǁ         0.0008803          10.369          5.1991          5.1991
v  Pressure               -45.617          15.412         -11.318         -11.318
v  nu_tilda            4.449e-007       0.0042695       0.0013967       0.0013967
v  TempC                       21           73.04          21.867          21.867
v  TurbVisc           3.4456e-014        0.005032       0.0016397       0.0016397
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1502:        0.21710E+01

===============================================================


 INSTANT    0.150300000E+04   TIME STEP NUMBER            1503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41458E-02 0.90277E+00
   Friction velocity        uk    :  0.41458E-02 0.90277E+00
   Dimensionless distance   yplus :  0.33376E-01 0.72679E+01
   Friction thermal sca.    tstar : -0.14715E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24903E-01 0.54227E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89918E-02      33   0.30730E-03   0.38035E+01 0.14501E+03 
c  Velocity[X]                                      0.15939E+01 
c  Velocity[Y]                                      0.22096E+01 
c  Velocity[Z]                                      0.11438E-29 
c  Pressure     0.11237E-06     488   0.98421E-08   0.98684E-01 0.11479E+04 
c  nu_tilda     0.60374E-05      32   0.52018E-05   0.32027E-06 0.15671E+03 
c  TempC        0.36352E+02      26   0.32216E-03   0.51124E+01 0.24929E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0607          10.368          4.5729          4.5729
v  Velocity[Y]            -2.5303          7.3971       0.0027185       0.0027185
v  Velocity[Z]       -1.3496e-014     1.1097e-014    -9.1707e-018    -9.1707e-018
v  ǁVelocityǁ        0.00035159          10.368          5.1988          5.1988
v  Pressure               -45.573          15.596         -11.258         -11.258
v  nu_tilda            4.449e-007       0.0042695       0.0013973       0.0013973
v  TempC                       21          73.041          21.867          21.867
v  TurbVisc           3.4468e-014        0.005032       0.0016403       0.0016403
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1503:        0.21120E+01

===============================================================


 INSTANT    0.150400000E+04   TIME STEP NUMBER            1504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68365E-02 0.90371E+00
   Friction velocity        uk    :  0.68365E-02 0.90371E+00
   Dimensionless distance   yplus :  0.55039E-01 0.72755E+01
   Friction thermal sca.    tstar : -0.14316E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41065E-01 0.54283E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89941E-02      33   0.33405E-03   0.38097E+01 0.14513E+03 
c  Velocity[X]                                      0.16106E+01 
c  Velocity[Y]                                      0.21991E+01 
c  Velocity[Z]                                      0.10730E-29 
c  Pressure     0.12768E-06     536   0.94013E-08   0.11127E+00 0.13687E+04 
c  nu_tilda     0.60396E-05      32   0.15892E-04   0.32074E-06 0.15681E+03 
c  TempC        0.36361E+02      26   0.26755E-03   0.44046E+01 0.23229E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0575          10.367          4.5729          4.5729
v  Velocity[Y]            -2.5289          7.3682       0.0027871       0.0027871
v  Velocity[Z]       -1.2394e-014     1.1429e-014    -9.2016e-018    -9.2016e-018
v  ǁVelocityǁ         0.0012967          10.368          5.1985          5.1985
v  Pressure                -45.58          15.359         -11.338         -11.338
v  nu_tilda           4.4496e-007       0.0042695       0.0013977       0.0013977
v  TempC                       21           73.04          21.867          21.867
v  TurbVisc           3.4467e-014        0.005032       0.0016409       0.0016409
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1504:        0.22150E+01

===============================================================


 INSTANT    0.150500000E+04   TIME STEP NUMBER            1505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10694E-01 0.90307E+00
   Friction velocity        uk    :  0.10694E-01 0.90307E+00
   Dimensionless distance   yplus :  0.86092E-01 0.72703E+01
   Friction thermal sca.    tstar : -0.15307E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64234E-01 0.54245E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89962E-02      33   0.27276E-03   0.38298E+01 0.14539E+03 
c  Velocity[X]                                      0.16291E+01 
c  Velocity[Y]                                      0.22007E+01 
c  Velocity[Z]                                      0.10376E-29 
c  Pressure     0.12918E-06     504   0.93057E-08   0.11287E+00 0.11274E+04 
c  nu_tilda     0.60417E-05      32   0.51873E-05   0.32116E-06 0.15690E+03 
c  TempC        0.36370E+02      27   0.39139E-03   0.36394E+01 0.20460E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0543          10.367          4.5729          4.5729
v  Velocity[Y]            -2.5274          7.3985       0.0028563       0.0028563
v  Velocity[Z]       -1.3815e-014     1.2266e-014    -9.2286e-018    -9.2286e-018
v  ǁVelocityǁ       8.6776e-005          10.367          5.1982          5.1982
v  Pressure               -45.539          15.545          -11.28          -11.28
v  nu_tilda           4.4502e-007       0.0042695       0.0013983       0.0013983
v  TempC                       21          73.041          21.867          21.867
v  TurbVisc           3.4486e-014        0.005032       0.0016415       0.0016415
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1505:        0.21460E+01

===============================================================


 INSTANT    0.150600000E+04   TIME STEP NUMBER            1506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96146E-02 0.90463E+00
   Friction velocity        uk    :  0.96146E-02 0.90463E+00
   Dimensionless distance   yplus :  0.77404E-01 0.72829E+01
   Friction thermal sca.    tstar : -0.13887E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57752E-01 0.54338E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.89984E-02      33   0.30440E-03   0.38137E+01 0.14540E+03 
c  Velocity[X]                                      0.15917E+01 
c  Velocity[Y]                                      0.22219E+01 
c  Velocity[Z]                                      0.90200E-30 
c  Pressure     0.11850E-06     425   0.90151E-08   0.10417E+00 0.27315E+03 
c  nu_tilda     0.60439E-05      32   0.15885E-04   0.32162E-06 0.15699E+03 
c  TempC        0.36379E+02      27   0.32064E-03   0.56686E+01 0.24917E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0511          10.366          4.5729          4.5729
v  Velocity[Y]            -2.5259          7.4063       0.0029263       0.0029263
v  Velocity[Z]       -1.3378e-014     1.2837e-014    -9.2531e-018    -9.2531e-018
v  ǁVelocityǁ         0.0012109          10.366          5.1979          5.1979
v  Pressure               -45.542          15.545         -11.298         -11.298
v  nu_tilda           4.4499e-007       0.0042695       0.0013988       0.0013988
v  TempC                       21           73.04          21.868          21.868
v  TurbVisc           3.4505e-014        0.005032       0.0016421       0.0016421
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1506:        0.21890E+01

===============================================================


 INSTANT    0.150700000E+04   TIME STEP NUMBER            1507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13020E-01 0.90420E+00
   Friction velocity        uk    :  0.13020E-01 0.90420E+00
   Dimensionless distance   yplus :  0.10482E+00 0.72795E+01
   Friction thermal sca.    tstar : -0.12974E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78206E-01 0.54313E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90006E-02      33   0.30806E-03   0.38389E+01 0.14557E+03 
c  Velocity[X]                                      0.16254E+01 
c  Velocity[Y]                                      0.22135E+01 
c  Velocity[Z]                                      0.10645E-29 
c  Pressure     0.13375E-06     378   0.94817E-08   0.11751E+00 0.55308E+03 
c  nu_tilda     0.60460E-05      32   0.51928E-05   0.32206E-06 0.15709E+03 
c  TempC        0.36388E+02      27   0.33787E-03   0.40397E+01 0.20115E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0478          10.366          4.5729          4.5729
v  Velocity[Y]            -2.5245          7.3753       0.0029973       0.0029973
v  Velocity[Z]       -1.4061e-014     1.3218e-014    -9.2837e-018    -9.2837e-018
v  ǁVelocityǁ        0.00040891          10.366          5.1976          5.1976
v  Pressure                 -45.5          15.435         -11.306         -11.306
v  nu_tilda           4.4499e-007       0.0042695       0.0013993       0.0013993
v  TempC                       21           73.04          21.868          21.868
v  TurbVisc           3.4495e-014        0.005032       0.0016427       0.0016427
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1507:        0.21010E+01

===============================================================


 INSTANT    0.150800000E+04   TIME STEP NUMBER            1508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54407E-02 0.90288E+00
   Friction velocity        uk    :  0.54407E-02 0.90288E+00
   Dimensionless distance   yplus :  0.43801E-01 0.72688E+01
   Friction thermal sca.    tstar : -0.15351E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32681E-01 0.54233E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90028E-02      33   0.31662E-03   0.38401E+01 0.14571E+03 
c  Velocity[X]                                      0.16299E+01 
c  Velocity[Y]                                      0.22102E+01 
c  Velocity[Z]                                      0.13354E-29 
c  Pressure     0.11931E-06     297   0.98977E-08   0.10507E+00 0.31849E+03 
c  nu_tilda     0.60482E-05      32   0.15882E-04   0.32251E-06 0.15718E+03 
c  TempC        0.36398E+02      27   0.35800E-03   0.38361E+01 0.21505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0444          10.365          4.5729          4.5729
v  Velocity[Y]             -2.523          7.3959       0.0030682       0.0030682
v  Velocity[Z]       -1.4295e-014     1.3404e-014    -9.2979e-018    -9.2979e-018
v  ǁVelocityǁ        0.00088742          10.365          5.1973          5.1973
v  Pressure               -45.504          15.517         -11.311         -11.311
v  nu_tilda           4.4501e-007       0.0042695       0.0013998       0.0013998
v  TempC                       21           73.04          21.868          21.868
v  TurbVisc           3.4495e-014        0.005032       0.0016433       0.0016433
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1508:        0.16780E+01

===============================================================


 INSTANT    0.150900000E+04   TIME STEP NUMBER            1509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12042E-01 0.90394E+00
   Friction velocity        uk    :  0.12042E-01 0.90394E+00
   Dimensionless distance   yplus :  0.96943E-01 0.72773E+01
   Friction thermal sca.    tstar : -0.13398E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72331E-01 0.54297E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90050E-02      33   0.30338E-03   0.38446E+01 0.14589E+03 
c  Velocity[X]                                      0.16117E+01 
c  Velocity[Y]                                      0.22329E+01 
c  Velocity[Z]                                      0.12531E-29 
c  Pressure     0.12901E-06     425   0.94762E-08   0.11397E+00 0.46763E+03 
c  nu_tilda     0.60503E-05      32   0.51846E-05   0.32295E-06 0.15727E+03 
c  TempC        0.36407E+02      27   0.45810E-03   0.57065E+01 0.25655E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0412          10.364          4.5729          4.5729
v  Velocity[Y]            -2.5215          7.3747       0.0031399       0.0031399
v  Velocity[Z]       -1.4386e-014     1.3678e-014     -9.318e-018     -9.318e-018
v  ǁVelocityǁ        0.00060839          10.364           5.197           5.197
v  Pressure                -45.46          15.473         -11.299         -11.299
v  nu_tilda           4.4506e-007       0.0042695       0.0014004       0.0014004
v  TempC                       21           73.04          21.868          21.868
v  TurbVisc           3.4502e-014        0.005032       0.0016439       0.0016439
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1509:        0.19720E+01

===============================================================


 INSTANT    0.151000000E+04   TIME STEP NUMBER            1510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89978E-02 0.90302E+00
   Friction velocity        uk    :  0.89978E-02 0.90302E+00
   Dimensionless distance   yplus :  0.72439E-01 0.72699E+01
   Friction thermal sca.    tstar : -0.14095E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54047E-01 0.54242E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90072E-02      33   0.26511E-03   0.38352E+01 0.14590E+03 
c  Velocity[X]                                      0.16126E+01 
c  Velocity[Y]                                      0.22226E+01 
c  Velocity[Z]                                      0.98719E-30 
c  Pressure     0.13083E-06     425   0.92628E-08   0.11392E+00 0.26754E+03 
c  nu_tilda     0.60525E-05      32   0.15881E-04   0.32341E-06 0.15737E+03 
c  TempC        0.36416E+02      27   0.38531E-03   0.70465E+01 0.29451E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0381          10.364          4.5729          4.5729
v  Velocity[Y]            -2.5201          7.3941       0.0032132       0.0032132
v  Velocity[Z]       -1.3368e-014     1.4053e-014    -9.3468e-018    -9.3468e-018
v  ǁVelocityǁ        0.00068262          10.364          5.1967          5.1967
v  Pressure               -45.467          15.498         -11.319         -11.319
v  nu_tilda            4.451e-007       0.0042695       0.0014008       0.0014008
v  TempC                       21           73.04          21.868          21.868
v  TurbVisc           3.4518e-014        0.005032       0.0016446       0.0016446
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1510:        0.19640E+01

===============================================================


 INSTANT    0.151100000E+04   TIME STEP NUMBER            1511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13232E-01 0.90469E+00
   Friction velocity        uk    :  0.13232E-01 0.90469E+00
   Dimensionless distance   yplus :  0.10653E+00 0.72834E+01
   Friction thermal sca.    tstar : -0.13177E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79482E-01 0.54342E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90094E-02      33   0.32529E-03   0.38443E+01 0.14609E+03 
c  Velocity[X]                                      0.16195E+01 
c  Velocity[Y]                                      0.22247E+01 
c  Velocity[Z]                                      0.85319E-30 
c  Pressure     0.13700E-06     505   0.90531E-08   0.12094E+00 0.76106E+03 
c  nu_tilda     0.60547E-05      32   0.51706E-05   0.32384E-06 0.15746E+03 
c  TempC        0.36425E+02      27   0.38110E-03   0.59785E+01 0.25442E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0348          10.363          4.5729          4.5729
v  Velocity[Y]            -2.5186          7.4088       0.0032858       0.0032858
v  Velocity[Z]       -1.3114e-014     1.3553e-014    -9.3659e-018    -9.3659e-018
v  ǁVelocityǁ          0.000728          10.363          5.1965          5.1965
v  Pressure               -45.425           15.59          -11.28          -11.28
v  nu_tilda            4.451e-007       0.0042695       0.0014014       0.0014014
v  TempC                       21           73.04          21.868          21.868
v  TurbVisc           3.4531e-014        0.005032       0.0016452       0.0016452
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1511:        0.21520E+01

===============================================================


 INSTANT    0.151200000E+04   TIME STEP NUMBER            1512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44209E-02 0.90433E+00
   Friction velocity        uk    :  0.44209E-02 0.90433E+00
   Dimensionless distance   yplus :  0.35591E-01 0.72804E+01
   Friction thermal sca.    tstar : -0.13480E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26555E-01 0.54320E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90116E-02      33   0.29823E-03   0.38725E+01 0.14638E+03 
c  Velocity[X]                                      0.16282E+01 
c  Velocity[Y]                                      0.22443E+01 
c  Velocity[Z]                                      0.95390E-30 
c  Pressure     0.12562E-06     505   0.95926E-08   0.11255E+00 0.11208E+04 
c  nu_tilda     0.60568E-05      32   0.15872E-04   0.32431E-06 0.15755E+03 
c  TempC        0.36435E+02      27   0.36369E-03   0.53891E+01 0.25722E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0316          10.362          4.5729          4.5729
v  Velocity[Y]            -2.5172          7.3777         0.00336         0.00336
v  Velocity[Z]       -1.2747e-014     1.3814e-014    -9.3921e-018    -9.3921e-018
v  ǁVelocityǁ        0.00054053          10.362          5.1962          5.1962
v  Pressure                -45.43          15.402         -11.347         -11.347
v  nu_tilda           4.4514e-007       0.0042695       0.0014019       0.0014019
v  TempC                       21           73.04          21.869          21.869
v  TurbVisc            3.453e-014        0.005032       0.0016458       0.0016458
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1512:        0.21570E+01

===============================================================


 INSTANT    0.151300000E+04   TIME STEP NUMBER            1513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13359E-01 0.90279E+00
   Friction velocity        uk    :  0.13359E-01 0.90279E+00
   Dimensionless distance   yplus :  0.10755E+00 0.72681E+01
   Friction thermal sca.    tstar : -0.13753E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80246E-01 0.54228E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90138E-02      33   0.30740E-03   0.38575E+01 0.14632E+03 
c  Velocity[X]                                      0.16227E+01 
c  Velocity[Y]                                      0.22349E+01 
c  Velocity[Z]                                      0.11777E-29 
c  Pressure     0.12908E-06     506   0.94920E-08   0.11152E+00 0.99115E+03 
c  nu_tilda     0.60590E-05      32   0.51744E-05   0.32474E-06 0.15765E+03 
c  TempC        0.36444E+02      27   0.36114E-03   0.51345E+01 0.24889E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0282          10.362          4.5729          4.5729
v  Velocity[Y]            -2.5157          7.3949       0.0034344       0.0034344
v  Velocity[Z]       -1.2688e-014     1.3707e-014    -9.4109e-018    -9.4109e-018
v  ǁVelocityǁ        0.00080468          10.362          5.1959          5.1959
v  Pressure               -45.389          15.551         -11.295         -11.295
v  nu_tilda           4.4516e-007       0.0042695       0.0014024       0.0014024
v  TempC                       21           73.04          21.869          21.869
v  TurbVisc           3.4542e-014        0.005032       0.0016464       0.0016464
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1513:        0.21560E+01

===============================================================


 INSTANT    0.151400000E+04   TIME STEP NUMBER            1514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83152E-02 0.90395E+00
   Friction velocity        uk    :  0.83152E-02 0.90395E+00
   Dimensionless distance   yplus :  0.66943E-01 0.72774E+01
   Friction thermal sca.    tstar : -0.12856E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49947E-01 0.54298E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90160E-02      33   0.32052E-03   0.38820E+01 0.14658E+03 
c  Velocity[X]                                      0.16481E+01 
c  Velocity[Y]                                      0.22339E+01 
c  Velocity[Z]                                      0.12066E-29 
c  Pressure     0.12315E-06     489   0.96857E-08   0.11026E+00 0.87251E+03 
c  nu_tilda     0.60612E-05      32   0.15871E-04   0.32521E-06 0.15774E+03 
c  TempC        0.36453E+02      27   0.34947E-03   0.41136E+01 0.22773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0249          10.361          4.5729          4.5729
v  Velocity[Y]            -2.5143          7.3721       0.0035097       0.0035097
v  Velocity[Z]       -1.2255e-014     1.4234e-014    -9.4338e-018    -9.4338e-018
v  ǁVelocityǁ        0.00052226          10.361          5.1956          5.1956
v  Pressure                -45.39          15.408         -11.347         -11.347
v  nu_tilda           4.4521e-007       0.0042695       0.0014029       0.0014029
v  TempC                       21           73.04          21.869          21.869
v  TurbVisc            3.455e-014        0.005032        0.001647        0.001647
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1514:        0.21250E+01

===============================================================


 INSTANT    0.151500000E+04   TIME STEP NUMBER            1515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98199E-02 0.90315E+00
   Friction velocity        uk    :  0.98199E-02 0.90315E+00
   Dimensionless distance   yplus :  0.79057E-01 0.72709E+01
   Friction thermal sca.    tstar : -0.13574E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58985E-01 0.54249E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90182E-02      33   0.24770E-03   0.38736E+01 0.14670E+03 
c  Velocity[X]                                      0.16150E+01 
c  Velocity[Y]                                      0.22586E+01 
c  Velocity[Z]                                      0.12094E-29 
c  Pressure     0.11730E-06     489   0.93042E-08   0.10356E+00 0.11499E+04 
c  nu_tilda     0.60633E-05      32   0.51623E-05   0.32564E-06 0.15783E+03 
c  TempC        0.36462E+02      26   0.31351E-03   0.51329E+01 0.24166E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0218           10.36          4.5729          4.5729
v  Velocity[Y]            -2.5128          7.3998       0.0035853       0.0035853
v  Velocity[Z]       -1.1639e-014     1.3769e-014    -9.4576e-018    -9.4576e-018
v  ǁVelocityǁ         0.0007521           10.36          5.1953          5.1953
v  Pressure               -45.352          15.597         -11.288         -11.288
v  nu_tilda           4.4521e-007       0.0042695       0.0014035       0.0014035
v  TempC                       21           73.04          21.869          21.869
v  TurbVisc           3.4565e-014        0.005032       0.0016476       0.0016476
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1515:        0.21130E+01

===============================================================


 INSTANT    0.151600000E+04   TIME STEP NUMBER            1516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75639E-02 0.90458E+00
   Friction velocity        uk    :  0.75639E-02 0.90458E+00
   Dimensionless distance   yplus :  0.60895E-01 0.72825E+01
   Friction thermal sca.    tstar : -0.13281E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45434E-01 0.54335E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90204E-02      33   0.32084E-03   0.38476E+01 0.14663E+03 
c  Velocity[X]                                      0.16013E+01 
c  Velocity[Y]                                      0.22463E+01 
c  Velocity[Z]                                      0.10849E-29 
c  Pressure     0.12841E-06     505   0.92843E-08   0.11257E+00 0.78299E+03 
c  nu_tilda     0.60655E-05      32   0.15863E-04   0.32611E-06 0.15793E+03 
c  TempC        0.36471E+02      26   0.43285E-03   0.45085E+01 0.23018E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0186           10.36          4.5729          4.5729
v  Velocity[Y]            -2.5113          7.4036       0.0036622       0.0036622
v  Velocity[Z]       -1.1212e-014     1.3887e-014     -9.485e-018     -9.485e-018
v  ǁVelocityǁ        0.00058472           10.36           5.195           5.195
v  Pressure               -45.354          15.488         -11.338         -11.338
v  nu_tilda            4.452e-007       0.0042695       0.0014039       0.0014039
v  TempC                       21           73.04          21.869          21.869
v  TurbVisc           3.4563e-014        0.005032       0.0016482       0.0016482
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1516:        0.21470E+01

===============================================================


 INSTANT    0.151700000E+04   TIME STEP NUMBER            1517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12620E-01 0.90435E+00
   Friction velocity        uk    :  0.12620E-01 0.90435E+00
   Dimensionless distance   yplus :  0.10160E+00 0.72806E+01
   Friction thermal sca.    tstar : -0.12550E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75802E-01 0.54322E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90225E-02      33   0.31841E-03   0.39050E+01 0.14706E+03 
c  Velocity[X]                                      0.16572E+01 
c  Velocity[Y]                                      0.22478E+01 
c  Velocity[Z]                                      0.85396E-30 
c  Pressure     0.14239E-06     425   0.99204E-08   0.12648E+00 0.43633E+03 
c  nu_tilda     0.60677E-05      32   0.51612E-05   0.32654E-06 0.15802E+03 
c  TempC        0.36480E+02      27   0.33439E-03   0.56568E+01 0.25128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0153          10.359          4.5729          4.5729
v  Velocity[Y]            -2.5098           7.379       0.0037389       0.0037389
v  Velocity[Z]        -1.089e-014     1.3956e-014     -9.511e-018     -9.511e-018
v  ǁVelocityǁ        0.00065882          10.359          5.1947          5.1947
v  Pressure               -45.314          15.463         -11.324         -11.324
v  nu_tilda           4.4526e-007       0.0042695       0.0014045       0.0014045
v  TempC                       21           73.04           21.87           21.87
v  TurbVisc           3.4561e-014        0.005032       0.0016488       0.0016488
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1517:        0.19540E+01

===============================================================


 INSTANT    0.151800000E+04   TIME STEP NUMBER            1518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69816E-02 0.90293E+00
   Friction velocity        uk    :  0.69816E-02 0.90293E+00
   Dimensionless distance   yplus :  0.56207E-01 0.72692E+01
   Friction thermal sca.    tstar : -0.13238E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41937E-01 0.54236E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90247E-02      33   0.31200E-03   0.38898E+01 0.14713E+03 
c  Velocity[X]                                      0.16216E+01 
c  Velocity[Y]                                      0.22682E+01 
c  Velocity[Z]                                      0.99798E-30 
c  Pressure     0.11526E-06     392   0.91173E-08   0.10205E+00 0.26234E+03 
c  nu_tilda     0.60698E-05      32   0.15859E-04   0.32701E-06 0.15812E+03 
c  TempC        0.36490E+02      27   0.35122E-03   0.37712E+01 0.20833E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.012          10.358          4.5729          4.5729
v  Velocity[Y]            -2.5084          7.3965       0.0038171       0.0038171
v  Velocity[Z]       -1.0292e-014      1.447e-014    -9.5344e-018    -9.5344e-018
v  ǁVelocityǁ        0.00070556          10.358          5.1944          5.1944
v  Pressure               -45.318          15.516         -11.338         -11.338
v  nu_tilda           4.4525e-007       0.0042695        0.001405        0.001405
v  TempC                       21           73.04           21.87           21.87
v  TurbVisc           3.4579e-014        0.005032       0.0016494       0.0016494
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1518:        0.19000E+01

===============================================================


 INSTANT    0.151900000E+04   TIME STEP NUMBER            1519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96495E-02 0.90385E+00
   Friction velocity        uk    :  0.96495E-02 0.90385E+00
   Dimensionless distance   yplus :  0.77685E-01 0.72766E+01
   Friction thermal sca.    tstar : -0.12087E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57962E-01 0.54292E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90269E-02      33   0.31655E-03   0.38975E+01 0.14719E+03 
c  Velocity[X]                                      0.16386E+01 
c  Velocity[Y]                                      0.22589E+01 
c  Velocity[Z]                                      0.10547E-29 
c  Pressure     0.13597E-06     424   0.92803E-08   0.11991E+00 0.48314E+03 
c  nu_tilda     0.60720E-05      32   0.51602E-05   0.32744E-06 0.15821E+03 
c  TempC        0.36499E+02      27   0.30434E-03   0.41376E+01 0.21535E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0087          10.357          4.5729          4.5729
v  Velocity[Y]            -2.5069          7.3716       0.0038954       0.0038954
v  Velocity[Z]       -9.8743e-015     1.4867e-014    -9.5624e-018    -9.5624e-018
v  ǁVelocityǁ        0.00045941          10.358          5.1941          5.1941
v  Pressure               -45.274          15.456         -11.326         -11.326
v  nu_tilda           4.4525e-007       0.0042695       0.0014055       0.0014055
v  TempC                       21           73.04           21.87           21.87
v  TurbVisc           3.4577e-014        0.005032         0.00165         0.00165
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1519:        0.19640E+01

===============================================================


 INSTANT    0.152000000E+04   TIME STEP NUMBER            1520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98488E-02 0.90317E+00
   Friction velocity        uk    :  0.98488E-02 0.90317E+00
   Dimensionless distance   yplus :  0.79289E-01 0.72711E+01
   Friction thermal sca.    tstar : -0.14006E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59159E-01 0.54251E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90291E-02      33   0.26044E-03   0.39120E+01 0.14738E+03 
c  Velocity[X]                                      0.16516E+01 
c  Velocity[Y]                                      0.22604E+01 
c  Velocity[Z]                                      0.10423E-29 
c  Pressure     0.11803E-06     408   0.94948E-08   0.10545E+00 0.27192E+03 
c  nu_tilda     0.60742E-05      32   0.15858E-04   0.32792E-06 0.15831E+03 
c  TempC        0.36508E+02      27   0.29615E-03   0.36719E+01 0.21193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0055          10.357          4.5729          4.5729
v  Velocity[Y]            -2.5055           7.398       0.0039746       0.0039746
v  Velocity[Z]       -9.3127e-015     1.4134e-014     -9.591e-018     -9.591e-018
v  ǁVelocityǁ        0.00093566          10.357          5.1938          5.1938
v  Pressure               -45.281          15.512         -11.341         -11.341
v  nu_tilda            4.453e-007       0.0042695        0.001406        0.001406
v  TempC                       21          73.039           21.87           21.87
v  TurbVisc           3.4578e-014        0.005032       0.0016507       0.0016507
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1520:        0.19270E+01

===============================================================


 INSTANT    0.152100000E+04   TIME STEP NUMBER            1521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13404E-01 0.90476E+00
   Friction velocity        uk    :  0.13404E-01 0.90476E+00
   Dimensionless distance   yplus :  0.10791E+00 0.72839E+01
   Friction thermal sca.    tstar : -0.12616E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80513E-01 0.54346E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90313E-02      33   0.30511E-03   0.38852E+01 0.14742E+03 
c  Velocity[X]                                      0.16043E+01 
c  Velocity[Y]                                      0.22810E+01 
c  Velocity[Z]                                      0.12428E-29 
c  Pressure     0.11774E-06     473   0.99171E-08   0.10397E+00 0.66979E+03 
c  nu_tilda     0.60763E-05      32   0.51499E-05   0.32836E-06 0.15840E+03 
c  TempC        0.36517E+02      27   0.36210E-03   0.36387E+01 0.20124E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0023          10.356          4.5729          4.5729
v  Velocity[Y]             -2.504          7.4088       0.0040541       0.0040541
v  Velocity[Z]       -8.6692e-015      1.443e-014    -9.6184e-018    -9.6184e-018
v  ǁVelocityǁ         0.0002846          10.356          5.1935          5.1935
v  Pressure               -45.239           15.59         -11.308         -11.308
v  nu_tilda            4.453e-007       0.0042695       0.0014066       0.0014066
v  TempC                       21           73.04           21.87           21.87
v  TurbVisc           3.4593e-014        0.005032       0.0016513       0.0016513
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1521:        0.20790E+01

===============================================================


 INSTANT    0.152200000E+04   TIME STEP NUMBER            1522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42297E-02 0.90417E+00
   Friction velocity        uk    :  0.42297E-02 0.90417E+00
   Dimensionless distance   yplus :  0.34052E-01 0.72792E+01
   Friction thermal sca.    tstar : -0.11595E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25407E-01 0.54311E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90335E-02      33   0.32117E-03   0.39131E+01 0.14763E+03 
c  Velocity[X]                                      0.16428E+01 
c  Velocity[Y]                                      0.22703E+01 
c  Velocity[Z]                                      0.84647E-30 
c  Pressure     0.13421E-06     489   0.96939E-08   0.11917E+00 0.11760E+04 
c  nu_tilda     0.60785E-05      32   0.15851E-04   0.32883E-06 0.15849E+03 
c  TempC        0.36526E+02      27   0.39352E-03   0.52904E+01 0.26152E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9991          10.355          4.5729          4.5729
v  Velocity[Y]            -2.5025          7.3745       0.0041351       0.0041351
v  Velocity[Z]       -8.3602e-015     1.4241e-014    -9.6496e-018    -9.6496e-018
v  ǁVelocityǁ         0.0010314          10.355          5.1932          5.1932
v  Pressure               -45.244          15.375         -11.376         -11.376
v  nu_tilda           4.4536e-007       0.0042695        0.001407        0.001407
v  TempC                       21          73.039           21.87           21.87
v  TurbVisc           3.4592e-014        0.005032       0.0016519       0.0016519
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1522:        0.21230E+01

===============================================================


 INSTANT    0.152300000E+04   TIME STEP NUMBER            1523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67077E-02 0.90298E+00
   Friction velocity        uk    :  0.67077E-02 0.90298E+00
   Dimensionless distance   yplus :  0.54001E-01 0.72696E+01
   Friction thermal sca.    tstar : -0.12878E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40291E-01 0.54240E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90357E-02      33   0.32021E-03   0.39223E+01 0.14782E+03 
c  Velocity[X]                                      0.16515E+01 
c  Velocity[Y]                                      0.22709E+01 
c  Velocity[Z]                                      0.94765E-30 
c  Pressure     0.12396E-06     505   0.91483E-08   0.11021E+00 0.11421E+04 
c  nu_tilda     0.60807E-05      32   0.51505E-05   0.32927E-06 0.15859E+03 
c  TempC        0.36536E+02      26   0.37457E-03   0.79938E+01 0.30006E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9958          10.355          4.5729          4.5729
v  Velocity[Y]            -2.5011           7.399       0.0042156       0.0042156
v  Velocity[Z]       -8.1394e-015     1.4922e-014    -9.6714e-018    -9.6714e-018
v  ǁVelocityǁ        0.00040191          10.355          5.1929          5.1929
v  Pressure               -45.202           15.57         -11.318         -11.318
v  nu_tilda           4.4538e-007       0.0042695       0.0014076       0.0014076
v  TempC                       21           73.04          21.871          21.871
v  TurbVisc            3.461e-014        0.005032       0.0016525       0.0016525
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1523:        0.21470E+01

===============================================================


 INSTANT    0.152400000E+04   TIME STEP NUMBER            1524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11269E-01 0.90402E+00
   Friction velocity        uk    :  0.11269E-01 0.90402E+00
   Dimensionless distance   yplus :  0.90726E-01 0.72780E+01
   Friction thermal sca.    tstar : -0.12555E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67692E-01 0.54302E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90379E-02      33   0.30469E-03   0.39309E+01 0.14797E+03 
c  Velocity[X]                                      0.16384E+01 
c  Velocity[Y]                                      0.22925E+01 
c  Velocity[Z]                                      0.10444E-29 
c  Pressure     0.12602E-06     474   0.94513E-08   0.11355E+00 0.78156E+03 
c  nu_tilda     0.60829E-05      32   0.15843E-04   0.32973E-06 0.15868E+03 
c  TempC        0.36545E+02      27   0.31300E-03   0.51881E+01 0.24215E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9925          10.354          4.5729          4.5729
v  Velocity[Y]            -2.4996          7.3743       0.0042981       0.0042981
v  Velocity[Z]       -7.7331e-015     1.4903e-014    -9.7009e-018    -9.7009e-018
v  ǁVelocityǁ        0.00060443          10.354          5.1926          5.1926
v  Pressure               -45.203          15.432         -11.363         -11.363
v  nu_tilda           4.4541e-007       0.0042695       0.0014081       0.0014081
v  TempC                       21          73.039          21.871          21.871
v  TurbVisc           3.4616e-014        0.005032       0.0016531       0.0016531
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1524:        0.20910E+01

===============================================================


 INSTANT    0.152500000E+04   TIME STEP NUMBER            1525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17692E-01 0.90316E+00
   Friction velocity        uk    :  0.17692E-01 0.90316E+00
   Dimensionless distance   yplus :  0.14243E+00 0.72710E+01
   Friction thermal sca.    tstar : -0.12821E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10627E+00 0.54250E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90401E-02      33   0.24865E-03   0.39238E+01 0.14796E+03 
c  Velocity[X]                                      0.16414E+01 
c  Velocity[Y]                                      0.22824E+01 
c  Velocity[Z]                                      0.10953E-29 
c  Pressure     0.13446E-06     488   0.94215E-08   0.11763E+00 0.75106E+03 
c  nu_tilda     0.60850E-05      32   0.51449E-05   0.33018E-06 0.15878E+03 
c  TempC        0.36554E+02      27   0.32913E-03   0.30496E+01 0.20368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9892          10.353          4.5729          4.5729
v  Velocity[Y]            -2.4981          7.3969       0.0043801       0.0043801
v  Velocity[Z]       -7.1466e-015     1.4899e-014    -9.7255e-018    -9.7255e-018
v  ǁVelocityǁ        0.00079561          10.353          5.1923          5.1923
v  Pressure               -45.166          15.547         -11.328         -11.328
v  nu_tilda           4.4546e-007       0.0042695       0.0014086       0.0014086
v  TempC                       21           73.04          21.871          21.871
v  TurbVisc           3.4627e-014        0.005032       0.0016537       0.0016537
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1525:        0.21070E+01

===============================================================


 INSTANT    0.152600000E+04   TIME STEP NUMBER            1526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37587E-02 0.90473E+00
   Friction velocity        uk    :  0.37587E-02 0.90473E+00
   Dimensionless distance   yplus :  0.30260E-01 0.72837E+01
   Friction thermal sca.    tstar : -0.11862E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22577E-01 0.54344E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90423E-02      33   0.31734E-03   0.39175E+01 0.14810E+03 
c  Velocity[X]                                      0.16363E+01 
c  Velocity[Y]                                      0.22812E+01 
c  Velocity[Z]                                      0.92665E-30 
c  Pressure     0.11026E-06     490   0.97535E-08   0.97973E-01 0.57822E+03 
c  nu_tilda     0.60872E-05      32   0.15843E-04   0.33066E-06 0.15887E+03 
c  TempC        0.36563E+02      27   0.40453E-03   0.46222E+01 0.24083E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.986          10.353          4.5729          4.5729
v  Velocity[Y]            -2.4967          7.4068       0.0044638       0.0044638
v  Velocity[Z]       -6.9528e-015     1.5485e-014    -9.7446e-018    -9.7446e-018
v  ǁVelocityǁ        0.00036112          10.353           5.192           5.192
v  Pressure                -45.17          15.484         -11.367         -11.367
v  nu_tilda           4.4548e-007       0.0042695       0.0014091       0.0014091
v  TempC                       21           73.04          21.871          21.871
v  TurbVisc           3.4641e-014        0.005032       0.0016543       0.0016543
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1526:        0.21120E+01

===============================================================


 INSTANT    0.152700000E+04   TIME STEP NUMBER            1527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33435E-02 0.90436E+00
   Friction velocity        uk    :  0.33435E-02 0.90436E+00
   Dimensionless distance   yplus :  0.26918E-01 0.72808E+01
   Friction thermal sca.    tstar : -0.11579E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20084E-01 0.54323E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90445E-02      33   0.29649E-03   0.39461E+01 0.14837E+03 
c  Velocity[X]                                      0.16432E+01 
c  Velocity[Y]                                      0.23029E+01 
c  Velocity[Z]                                      0.94249E-30 
c  Pressure     0.13180E-06     457   0.91391E-08   0.11958E+00 0.58302E+03 
c  nu_tilda     0.60894E-05      32   0.51381E-05   0.33110E-06 0.15897E+03 
c  TempC        0.36572E+02      27   0.33941E-03   0.63882E+01 0.27853E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9828          10.352          4.5729          4.5729
v  Velocity[Y]            -2.4952          7.3791       0.0045476       0.0045476
v  Velocity[Z]       -6.9287e-015     1.6037e-014    -9.7767e-018    -9.7767e-018
v  ǁVelocityǁ        0.00081137          10.352          5.1917          5.1917
v  Pressure               -45.126          15.495         -11.339         -11.339
v  nu_tilda           4.4548e-007       0.0042695       0.0014096       0.0014096
v  TempC                       21           73.04          21.871          21.871
v  TurbVisc           3.4648e-014        0.005032       0.0016549       0.0016549
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1527:        0.20460E+01

===============================================================


 INSTANT    0.152800000E+04   TIME STEP NUMBER            1528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13774E-01 0.90273E+00
   Friction velocity        uk    :  0.13774E-01 0.90273E+00
   Dimensionless distance   yplus :  0.11089E+00 0.72676E+01
   Friction thermal sca.    tstar : -0.12756E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82735E-01 0.54225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90467E-02      33   0.31701E-03   0.39259E+01 0.14834E+03 
c  Velocity[X]                                      0.16328E+01 
c  Velocity[Y]                                      0.22931E+01 
c  Velocity[Z]                                      0.10095E-29 
c  Pressure     0.12888E-06     473   0.95191E-08   0.11342E+00 0.38676E+03 
c  nu_tilda     0.60916E-05      32   0.15837E-04   0.33157E-06 0.15906E+03 
c  TempC        0.36581E+02      27   0.36302E-03   0.49201E+01 0.23447E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9796          10.351          4.5729          4.5729
v  Velocity[Y]            -2.4937          7.3937       0.0046323       0.0046323
v  Velocity[Z]       -6.9287e-015     1.6034e-014    -9.8049e-018    -9.8049e-018
v  ǁVelocityǁ        0.00072223          10.351          5.1914          5.1914
v  Pressure               -45.133          15.478         -11.369         -11.369
v  nu_tilda           4.4549e-007       0.0042695       0.0014101       0.0014101
v  TempC                       21           73.04          21.872          21.872
v  TurbVisc           3.4648e-014        0.005032       0.0016555       0.0016555
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1528:        0.20880E+01

===============================================================


 INSTANT    0.152900000E+04   TIME STEP NUMBER            1529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16462E-01 0.90404E+00
   Friction velocity        uk    :  0.16462E-01 0.90404E+00
   Dimensionless distance   yplus :  0.13253E+00 0.72782E+01
   Friction thermal sca.    tstar : -0.12046E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98885E-01 0.54303E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90488E-02      33   0.32761E-03   0.39609E+01 0.14865E+03 
c  Velocity[X]                                      0.16685E+01 
c  Velocity[Y]                                      0.22924E+01 
c  Velocity[Z]                                      0.10629E-29 
c  Pressure     0.14050E-06     457   0.93634E-08   0.12655E+00 0.53984E+03 
c  nu_tilda     0.60937E-05      32   0.51319E-05   0.33201E-06 0.15915E+03 
c  TempC        0.36590E+02      26   0.31002E-03   0.48753E+01 0.24617E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9762           10.35          4.5729          4.5729
v  Velocity[Y]            -2.4923          7.3747       0.0047175       0.0047175
v  Velocity[Z]       -6.9287e-015     1.6451e-014    -9.8299e-018    -9.8299e-018
v  ǁVelocityǁ        0.00041483          10.351          5.1911          5.1911
v  Pressure               -45.089          15.492         -11.344         -11.344
v  nu_tilda           4.4554e-007       0.0042695       0.0014107       0.0014107
v  TempC                       21           73.04          21.872          21.872
v  TurbVisc            3.465e-014        0.005032       0.0016561       0.0016561
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1529:        0.20570E+01

===============================================================


 INSTANT    0.153000000E+04   TIME STEP NUMBER            1530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64375E-02 0.90323E+00
   Friction velocity        uk    :  0.64375E-02 0.90323E+00
   Dimensionless distance   yplus :  0.51826E-01 0.72716E+01
   Friction thermal sca.    tstar : -0.12160E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38668E-01 0.54254E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90511E-02      33   0.23506E-03   0.39562E+01 0.14876E+03 
c  Velocity[X]                                      0.16420E+01 
c  Velocity[Y]                                      0.23142E+01 
c  Velocity[Z]                                      0.12350E-29 
c  Pressure     0.11738E-06     441   0.91472E-08   0.10453E+00 0.32078E+03 
c  nu_tilda     0.60959E-05      32   0.15833E-04   0.33249E-06 0.15925E+03 
c  TempC        0.36600E+02      26   0.29257E-03   0.37891E+01 0.22138E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9729           10.35          4.5729          4.5729
v  Velocity[Y]            -2.4908          7.3984       0.0048035       0.0048035
v  Velocity[Z]       -6.9287e-015     1.6436e-014    -9.8517e-018    -9.8517e-018
v  ǁVelocityǁ        0.00068762           10.35          5.1908          5.1908
v  Pressure               -45.091          15.509         -11.367         -11.367
v  nu_tilda           4.4556e-007       0.0042695       0.0014111       0.0014111
v  TempC                       21          73.039          21.872          21.872
v  TurbVisc           3.4666e-014        0.005032       0.0016567       0.0016567
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1530:        0.20060E+01

===============================================================


 INSTANT    0.153100000E+04   TIME STEP NUMBER            1531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33570E-02 0.90470E+00
   Friction velocity        uk    :  0.33570E-02 0.90470E+00
   Dimensionless distance   yplus :  0.27026E-01 0.72835E+01
   Friction thermal sca.    tstar : -0.11451E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20164E-01 0.54343E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90532E-02      33   0.31102E-03   0.39325E+01 0.14867E+03 
c  Velocity[X]                                      0.16272E+01 
c  Velocity[Y]                                      0.23053E+01 
c  Velocity[Z]                                      0.12427E-29 
c  Pressure     0.12583E-06     473   0.93436E-08   0.11155E+00 0.68415E+03 
c  nu_tilda     0.60981E-05      32   0.51218E-05   0.33293E-06 0.15934E+03 
c  TempC        0.36609E+02      26   0.42777E-03   0.49829E+01 0.22505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9697          10.349          4.5729          4.5729
v  Velocity[Y]            -2.4894          7.4058       0.0048901       0.0048901
v  Velocity[Z]       -6.9287e-015     1.6927e-014    -9.8883e-018    -9.8883e-018
v  ǁVelocityǁ        0.00084884          10.349          5.1906          5.1906
v  Pressure               -45.052          15.577         -11.332         -11.332
v  nu_tilda           4.4551e-007       0.0042695       0.0014117       0.0014117
v  TempC                       21           73.04          21.872          21.872
v  TurbVisc           3.4674e-014        0.005032       0.0016573       0.0016573
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1531:        0.20820E+01

===============================================================


 INSTANT    0.153200000E+04   TIME STEP NUMBER            1532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16263E-01 0.90437E+00
   Friction velocity        uk    :  0.16263E-01 0.90437E+00
   Dimensionless distance   yplus :  0.13093E+00 0.72808E+01
   Friction thermal sca.    tstar : -0.11867E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97686E-01 0.54323E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90554E-02      33   0.31252E-03   0.39821E+01 0.14905E+03 
c  Velocity[X]                                      0.16788E+01 
c  Velocity[Y]                                      0.23032E+01 
c  Velocity[Z]                                      0.95983E-30 
c  Pressure     0.11876E-06     488   0.90405E-08   0.10763E+00 0.10623E+04 
c  nu_tilda     0.61003E-05      32   0.15829E-04   0.33342E-06 0.15944E+03 
c  TempC        0.36618E+02      26   0.37175E-03   0.81206E+01 0.31538E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9666          10.348          4.5729          4.5729
v  Velocity[Y]            -2.4879          7.3776       0.0049773       0.0049773
v  Velocity[Z]       -6.9287e-015     1.6402e-014    -9.9096e-018    -9.9096e-018
v  ǁVelocityǁ        0.00052451          10.349          5.1903          5.1903
v  Pressure               -45.055          15.394         -11.394         -11.394
v  nu_tilda           4.4556e-007       0.0042695       0.0014122       0.0014122
v  TempC                       21          73.039          21.872          21.872
v  TurbVisc           3.4659e-014        0.005032       0.0016579       0.0016579
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1532:        0.21250E+01

===============================================================


 INSTANT    0.153300000E+04   TIME STEP NUMBER            1533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14175E-01 0.90297E+00
   Friction velocity        uk    :  0.14175E-01 0.90297E+00
   Dimensionless distance   yplus :  0.11412E+00 0.72695E+01
   Friction thermal sca.    tstar : -0.12289E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85148E-01 0.54239E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90576E-02      33   0.29609E-03   0.39660E+01 0.14913E+03 
c  Velocity[X]                                      0.16376E+01 
c  Velocity[Y]                                      0.23284E+01 
c  Velocity[Z]                                      0.10175E-29 
c  Pressure     0.11381E-06     506   0.98316E-08   0.10179E+00 0.13064E+04 
c  nu_tilda     0.61025E-05      32   0.51211E-05   0.33386E-06 0.15953E+03 
c  TempC        0.36627E+02      27   0.35661E-03   0.53185E+01 0.26052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9633          10.348          4.5729          4.5729
v  Velocity[Y]            -2.4864          7.3986       0.0050652       0.0050652
v  Velocity[Z]       -6.9287e-015     1.6395e-014    -9.9408e-018    -9.9408e-018
v  ǁVelocityǁ        0.00050956          10.348            5.19            5.19
v  Pressure               -45.017          15.617         -11.328         -11.328
v  nu_tilda           4.4555e-007       0.0042695       0.0014127       0.0014127
v  TempC                       21           73.04          21.872          21.872
v  TurbVisc           3.4672e-014        0.005032       0.0016585       0.0016585
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1533:        0.21610E+01

===============================================================


 INSTANT    0.153400000E+04   TIME STEP NUMBER            1534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42595E-02 0.90387E+00
   Friction velocity        uk    :  0.42595E-02 0.90387E+00
   Dimensionless distance   yplus :  0.34292E-01 0.72767E+01
   Friction thermal sca.    tstar : -0.11058E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25586E-01 0.54293E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90598E-02      33   0.33040E-03   0.39648E+01 0.14920E+03 
c  Velocity[X]                                      0.16502E+01 
c  Velocity[Y]                                      0.23147E+01 
c  Velocity[Z]                                      0.11673E-29 
c  Pressure     0.12666E-06     520   0.99269E-08   0.11332E+00 0.14763E+04 
c  nu_tilda     0.61046E-05      32   0.15819E-04   0.33433E-06 0.15963E+03 
c  TempC        0.36636E+02      26   0.38660E-03   0.44919E+01 0.24785E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.96          10.347          4.5729          4.5729
v  Velocity[Y]             -2.485          7.3701       0.0051539       0.0051539
v  Velocity[Z]       -6.9287e-015     1.6532e-014    -9.9595e-018    -9.9595e-018
v  ǁVelocityǁ        0.00074404          10.347          5.1897          5.1897
v  Pressure               -45.018          15.357         -11.411         -11.411
v  nu_tilda            4.456e-007       0.0042695       0.0014132       0.0014132
v  TempC                       21          73.039          21.873          21.873
v  TurbVisc            3.467e-014        0.005032       0.0016592       0.0016592
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1534:        0.21890E+01

===============================================================


 INSTANT    0.153500000E+04   TIME STEP NUMBER            1535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11911E-01 0.90325E+00
   Friction velocity        uk    :  0.11911E-01 0.90325E+00
   Dimensionless distance   yplus :  0.95891E-01 0.72718E+01
   Friction thermal sca.    tstar : -0.12040E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71546E-01 0.54256E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90620E-02      33   0.26615E-03   0.39868E+01 0.14942E+03 
c  Velocity[X]                                      0.16713E+01 
c  Velocity[Y]                                      0.23154E+01 
c  Velocity[Z]                                      0.10627E-29 
c  Pressure     0.13044E-06     520   0.94490E-08   0.11691E+00 0.15170E+04 
c  nu_tilda     0.61068E-05      32   0.51118E-05   0.33478E-06 0.15972E+03 
c  TempC        0.36645E+02      26   0.32505E-03   0.72408E+01 0.28527E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9567          10.347          4.5729          4.5729
v  Velocity[Y]            -2.4835          7.3997       0.0052434       0.0052434
v  Velocity[Z]       -6.9287e-015     1.6731e-014    -9.9898e-018    -9.9898e-018
v  ǁVelocityǁ        0.00088481          10.347          5.1894          5.1894
v  Pressure               -44.976          15.613         -11.331         -11.331
v  nu_tilda           4.4565e-007       0.0042695       0.0014137       0.0014137
v  TempC                       21           73.04          21.873          21.873
v  TurbVisc           3.4686e-014        0.005032       0.0016598       0.0016598
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1535:        0.21840E+01

===============================================================


 INSTANT    0.153600000E+04   TIME STEP NUMBER            1536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16585E-01 0.90473E+00
   Friction velocity        uk    :  0.16585E-01 0.90473E+00
   Dimensionless distance   yplus :  0.13352E+00 0.72837E+01
   Friction thermal sca.    tstar : -0.11805E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99624E-01 0.54344E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90642E-02      33   0.30091E-03   0.39659E+01 0.14946E+03 
c  Velocity[X]                                      0.16296E+01 
c  Velocity[Y]                                      0.23362E+01 
c  Velocity[Z]                                      0.88223E-30 
c  Pressure     0.11139E-06     504   0.96126E-08   0.99694E-01 0.81249E+03 
c  nu_tilda     0.61090E-05      32   0.15818E-04   0.33526E-06 0.15982E+03 
c  TempC        0.36654E+02      27   0.35272E-03   0.48905E+01 0.23413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9534          10.346          4.5729          4.5729
v  Velocity[Y]             -2.482          7.4079       0.0053333       0.0053333
v  Velocity[Z]       -6.9287e-015     1.6613e-014    -1.0011e-017    -1.0011e-017
v  ǁVelocityǁ        0.00065544          10.346          5.1891          5.1891
v  Pressure                -44.98          15.505         -11.384         -11.384
v  nu_tilda           4.4565e-007       0.0042695       0.0014142       0.0014142
v  TempC                       21          73.039          21.873          21.873
v  TurbVisc             3.47e-014        0.005032       0.0016604       0.0016604
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1536:        0.21700E+01

===============================================================


 INSTANT    0.153700000E+04   TIME STEP NUMBER            1537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10933E-01 0.90431E+00
   Friction velocity        uk    :  0.10933E-01 0.90431E+00
   Dimensionless distance   yplus :  0.88022E-01 0.72803E+01
   Friction thermal sca.    tstar : -0.11125E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65674E-01 0.54319E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90664E-02      33   0.30468E-03   0.39988E+01 0.14963E+03 
c  Velocity[X]                                      0.16688E+01 
c  Velocity[Y]                                      0.23300E+01 
c  Velocity[Z]                                      0.98770E-30 
c  Pressure     0.14216E-06     458   0.98477E-08   0.12668E+00 0.53585E+03 
c  nu_tilda     0.61112E-05      32   0.51031E-05   0.33571E-06 0.15991E+03 
c  TempC        0.36664E+02      27   0.37576E-03   0.46218E+01 0.24999E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9503          10.345          4.5729          4.5729
v  Velocity[Y]            -2.4805          7.3758       0.0054241       0.0054241
v  Velocity[Z]       -6.9287e-015     1.6018e-014    -1.0041e-017    -1.0041e-017
v  ǁVelocityǁ        0.00051847          10.345          5.1888          5.1888
v  Pressure               -44.939          15.498         -11.359         -11.359
v  nu_tilda           4.4567e-007       0.0042695       0.0014148       0.0014148
v  TempC                       21           73.04          21.873          21.873
v  TurbVisc             3.47e-014        0.005032        0.001661        0.001661
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1537:        0.23540E+01

===============================================================


 INSTANT    0.153800000E+04   TIME STEP NUMBER            1538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78920E-02 0.90295E+00
   Friction velocity        uk    :  0.78920E-02 0.90295E+00
   Dimensionless distance   yplus :  0.63536E-01 0.72693E+01
   Friction thermal sca.    tstar : -0.11420E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47405E-01 0.54237E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90686E-02      33   0.31119E-03   0.39973E+01 0.14978E+03 
c  Velocity[X]                                      0.16704E+01 
c  Velocity[Y]                                      0.23269E+01 
c  Velocity[Z]                                      0.91059E-30 
c  Pressure     0.11153E-06     473   0.92879E-08   0.99970E-01 0.46376E+03 
c  nu_tilda     0.61134E-05      32   0.15814E-04   0.33620E-06 0.16001E+03 
c  TempC        0.36673E+02      27   0.39667E-03   0.59310E+01 0.26403E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9471          10.344          4.5729          4.5729
v  Velocity[Y]            -2.4791          7.3969       0.0055153       0.0055153
v  Velocity[Z]       -6.9287e-015     1.6218e-014    -1.0059e-017    -1.0059e-017
v  ǁVelocityǁ        0.00051629          10.345          5.1885          5.1885
v  Pressure               -44.945          15.486         -11.395         -11.395
v  nu_tilda           4.4567e-007       0.0042695       0.0014152       0.0014152
v  TempC                       21          73.039          21.873          21.873
v  TurbVisc           3.4707e-014        0.005032       0.0016616       0.0016616
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1538:        0.21350E+01

===============================================================


 INSTANT    0.153900000E+04   TIME STEP NUMBER            1539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55415E-02 0.90409E+00
   Friction velocity        uk    :  0.55415E-02 0.90409E+00
   Dimensionless distance   yplus :  0.44613E-01 0.72785E+01
   Friction thermal sca.    tstar : -0.10998E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33286E-01 0.54306E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90708E-02      33   0.30121E-03   0.39981E+01 0.14995E+03 
c  Velocity[X]                                      0.16494E+01 
c  Velocity[Y]                                      0.23487E+01 
c  Velocity[Z]                                      0.11745E-29 
c  Pressure     0.12111E-06     473   0.97155E-08   0.10921E+00 0.50807E+03 
c  nu_tilda     0.61156E-05      32   0.50992E-05   0.33664E-06 0.16010E+03 
c  TempC        0.36682E+02      27   0.32026E-03   0.56808E+01 0.24402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9438          10.344          4.5729          4.5729
v  Velocity[Y]            -2.4776          7.3755       0.0056076       0.0056076
v  Velocity[Z]       -6.9287e-015     1.5485e-014    -1.0082e-017    -1.0082e-017
v  ǁVelocityǁ        0.00060228          10.344          5.1882          5.1882
v  Pressure               -44.903          15.482         -11.373         -11.373
v  nu_tilda           4.4568e-007       0.0042695       0.0014158       0.0014158
v  TempC                       21           73.04          21.873          21.873
v  TurbVisc           3.4709e-014        0.005032       0.0016622       0.0016622
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1539:        0.20780E+01

===============================================================


 INSTANT    0.154000000E+04   TIME STEP NUMBER            1540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14040E-01 0.90310E+00
   Friction velocity        uk    :  0.14040E-01 0.90310E+00
   Dimensionless distance   yplus :  0.11304E+00 0.72705E+01
   Friction thermal sca.    tstar : -0.12011E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84337E-01 0.54246E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90730E-02      33   0.26162E-03   0.39914E+01 0.14995E+03 
c  Velocity[X]                                      0.16535E+01 
c  Velocity[Y]                                      0.23379E+01 
c  Velocity[Z]                                      0.12062E-29 
c  Pressure     0.13157E-06     426   0.98251E-08   0.11669E+00 0.31066E+03 
c  nu_tilda     0.61178E-05      32   0.15809E-04   0.33712E-06 0.16020E+03 
c  TempC        0.36691E+02      27   0.27837E-03   0.36382E+01 0.20804E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9405          10.343          4.5729          4.5729
v  Velocity[Y]            -2.4762          7.3952       0.0057003       0.0057003
v  Velocity[Z]       -6.9287e-015     1.5672e-014    -1.0101e-017    -1.0101e-017
v  ǁVelocityǁ        0.00066975          10.343          5.1879          5.1879
v  Pressure               -44.904          15.484         -11.395         -11.395
v  nu_tilda           4.4573e-007       0.0042695       0.0014162       0.0014162
v  TempC                       21          73.039          21.873          21.873
v  TurbVisc           3.4711e-014        0.005032       0.0016628       0.0016628
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1540:        0.19780E+01

===============================================================


 INSTANT    0.154100000E+04   TIME STEP NUMBER            1541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51085E-02 0.90476E+00
   Friction velocity        uk    :  0.51085E-02 0.90476E+00
   Dimensionless distance   yplus :  0.41127E-01 0.72839E+01
   Friction thermal sca.    tstar : -0.11288E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30685E-01 0.54346E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90752E-02      33   0.32489E-03   0.39968E+01 0.15013E+03 
c  Velocity[X]                                      0.16574E+01 
c  Velocity[Y]                                      0.23394E+01 
c  Velocity[Z]                                      0.94913E-30 
c  Pressure     0.13096E-06     473   0.92564E-08   0.11684E+00 0.88307E+03 
c  nu_tilda     0.61200E-05      32   0.50890E-05   0.33758E-06 0.16029E+03 
c  TempC        0.36700E+02      27   0.42982E-03   0.41671E+01 0.23293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9372          10.342          4.5729          4.5729
v  Velocity[Y]            -2.4747          7.4087       0.0057937       0.0057937
v  Velocity[Z]       -6.9287e-015     1.4624e-014    -1.0127e-017    -1.0127e-017
v  ǁVelocityǁ        0.00077597          10.342          5.1876          5.1876
v  Pressure               -44.864          15.608         -11.349         -11.349
v  nu_tilda           4.4576e-007       0.0042695       0.0014168       0.0014168
v  TempC                       21           73.04          21.874          21.874
v  TurbVisc           3.4727e-014        0.005032       0.0016634       0.0016634
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1541:        0.20640E+01

===============================================================


 INSTANT    0.154200000E+04   TIME STEP NUMBER            1542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12350E-01 0.90432E+00
   Friction velocity        uk    :  0.12350E-01 0.90432E+00
   Dimensionless distance   yplus :  0.99428E-01 0.72804E+01
   Friction thermal sca.    tstar : -0.10546E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74184E-01 0.54320E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90774E-02      33   0.28868E-03   0.40257E+01 0.15040E+03 
c  Velocity[X]                                      0.16657E+01 
c  Velocity[Y]                                      0.23601E+01 
c  Velocity[Z]                                      0.11349E-29 
c  Pressure     0.12197E-06     521   0.91652E-08   0.11091E+00 0.11636E+04 
c  nu_tilda     0.61222E-05      32   0.15808E-04   0.33806E-06 0.16039E+03 
c  TempC        0.36709E+02      27   0.36091E-03   0.67206E+01 0.30065E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.934          10.342          4.5729          4.5729
v  Velocity[Y]            -2.4733          7.3778       0.0058877       0.0058877
v  Velocity[Z]       -6.9287e-015     1.4915e-014    -1.0147e-017    -1.0147e-017
v  ǁVelocityǁ        0.00083929          10.342          5.1873          5.1873
v  Pressure               -44.869          15.407         -11.418         -11.418
v  nu_tilda            4.458e-007       0.0042695       0.0014173       0.0014173
v  TempC                       21          73.039          21.874          21.874
v  TurbVisc           3.4734e-014        0.005032        0.001664        0.001664
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1542:        0.21840E+01

===============================================================


 INSTANT    0.154300000E+04   TIME STEP NUMBER            1543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14384E-01 0.90283E+00
   Friction velocity        uk    :  0.14384E-01 0.90283E+00
   Dimensionless distance   yplus :  0.11580E+00 0.72684E+01
   Friction thermal sca.    tstar : -0.11184E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86398E-01 0.54230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90795E-02      33   0.30058E-03   0.40067E+01 0.15033E+03 
c  Velocity[X]                                      0.16581E+01 
c  Velocity[Y]                                      0.23485E+01 
c  Velocity[Z]                                      0.10886E-29 
c  Pressure     0.12209E-06     488   0.97708E-08   0.10818E+00 0.97004E+03 
c  nu_tilda     0.61244E-05      32   0.50937E-05   0.33852E-06 0.16048E+03 
c  TempC        0.36718E+02      27   0.41150E-03   0.53727E+01 0.25232E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9308          10.341          4.5729          4.5729
v  Velocity[Y]            -2.4718          7.3947       0.0059827       0.0059827
v  Velocity[Z]       -6.9287e-015     1.3904e-014    -1.0173e-017    -1.0173e-017
v  ǁVelocityǁ        0.00080035          10.341          5.1871          5.1871
v  Pressure               -44.827          15.555         -11.368         -11.368
v  nu_tilda           4.4578e-007       0.0042695       0.0014178       0.0014178
v  TempC                       21           73.04          21.874          21.874
v  TurbVisc           3.4748e-014        0.005032       0.0016646       0.0016646
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1543:        0.21120E+01

===============================================================


 INSTANT    0.154400000E+04   TIME STEP NUMBER            1544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92001E-02 0.90394E+00
   Friction velocity        uk    :  0.92001E-02 0.90394E+00
   Dimensionless distance   yplus :  0.74067E-01 0.72774E+01
   Friction thermal sca.    tstar : -0.11363E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55262E-01 0.54297E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90818E-02      33   0.32117E-03   0.40342E+01 0.15061E+03 
c  Velocity[X]                                      0.16858E+01 
c  Velocity[Y]                                      0.23484E+01 
c  Velocity[Z]                                      0.13585E-29 
c  Pressure     0.11803E-06     473   0.97758E-08   0.10726E+00 0.86499E+03 
c  nu_tilda     0.61265E-05      32   0.15802E-04   0.33900E-06 0.16058E+03 
c  TempC        0.36727E+02      26   0.37766E-03   0.81634E+01 0.29803E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9275           10.34          4.5729          4.5729
v  Velocity[Y]            -2.4703          7.3724       0.0060782       0.0060782
v  Velocity[Z]       -6.9287e-015      1.432e-014    -1.0185e-017    -1.0185e-017
v  ǁVelocityǁ         0.0007659           10.34          5.1868          5.1868
v  Pressure               -44.833          15.408         -11.421         -11.421
v  nu_tilda           4.4581e-007       0.0042695       0.0014183       0.0014183
v  TempC                       21          73.039          21.874          21.874
v  TurbVisc            3.474e-014        0.005032       0.0016652       0.0016652
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1544:        0.20660E+01

===============================================================


 INSTANT    0.154500000E+04   TIME STEP NUMBER            1545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76944E-02 0.90320E+00
   Friction velocity        uk    :  0.76944E-02 0.90320E+00
   Dimensionless distance   yplus :  0.61945E-01 0.72714E+01
   Friction thermal sca.    tstar : -0.11535E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46218E-01 0.54252E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90839E-02      33   0.23732E-03   0.40278E+01 0.15073E+03 
c  Velocity[X]                                      0.16556E+01 
c  Velocity[Y]                                      0.23722E+01 
c  Velocity[Z]                                      0.12327E-29 
c  Pressure     0.11080E-06     505   0.95403E-08   0.99175E-01 0.11360E+04 
c  nu_tilda     0.61287E-05      32   0.50846E-05   0.33945E-06 0.16067E+03 
c  TempC        0.36736E+02      27   0.37464E-03   0.60940E+01 0.27144E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9242           10.34          4.5729          4.5729
v  Velocity[Y]            -2.4689          7.3988       0.0061745       0.0061745
v  Velocity[Z]       -6.9287e-015      1.326e-014    -1.0212e-017    -1.0212e-017
v  ǁVelocityǁ        0.00071022           10.34          5.1865          5.1865
v  Pressure               -44.791          15.598         -11.362         -11.362
v  nu_tilda           4.4581e-007       0.0042695       0.0014188       0.0014188
v  TempC                       21           73.04          21.874          21.874
v  TurbVisc           3.4751e-014        0.005032       0.0016658       0.0016658
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1545:        0.21500E+01

===============================================================


 INSTANT    0.154600000E+04   TIME STEP NUMBER            1546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15503E-01 0.90449E+00
   Friction velocity        uk    :  0.15503E-01 0.90449E+00
   Dimensionless distance   yplus :  0.12481E+00 0.72818E+01
   Friction thermal sca.    tstar : -0.10476E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93121E-01 0.54330E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90861E-02      33   0.32372E-03   0.40023E+01 0.15064E+03 
c  Velocity[X]                                      0.16414E+01 
c  Velocity[Y]                                      0.23609E+01 
c  Velocity[Z]                                      0.97334E-30 
c  Pressure     0.12651E-06     456   0.94091E-08   0.11245E+00 0.54604E+03 
c  nu_tilda     0.61309E-05      32   0.15799E-04   0.33994E-06 0.16077E+03 
c  TempC        0.36746E+02      27   0.32331E-03   0.57941E+01 0.26330E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9209          10.339          4.5729          4.5729
v  Velocity[Y]            -2.4674          7.4034       0.0062717       0.0062717
v  Velocity[Z]       -6.9287e-015     1.2676e-014    -1.0232e-017    -1.0232e-017
v  ǁVelocityǁ        0.00074021          10.339          5.1862          5.1862
v  Pressure               -44.793          15.521         -11.397         -11.397
v  nu_tilda           4.4579e-007       0.0042695       0.0014193       0.0014193
v  TempC                       21           73.04          21.874          21.874
v  TurbVisc           3.4751e-014        0.005032       0.0016664       0.0016664
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1546:        0.20210E+01

===============================================================


 INSTANT    0.154700000E+04   TIME STEP NUMBER            1547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13235E-01 0.90437E+00
   Friction velocity        uk    :  0.13235E-01 0.90437E+00
   Dimensionless distance   yplus :  0.10655E+00 0.72808E+01
   Friction thermal sca.    tstar : -0.10539E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79502E-01 0.54323E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90883E-02      33   0.31558E-03   0.40603E+01 0.15109E+03 
c  Velocity[X]                                      0.16980E+01 
c  Velocity[Y]                                      0.23624E+01 
c  Velocity[Z]                                      0.95513E-30 
c  Pressure     0.13275E-06     408   0.99342E-08   0.12119E+00 0.42800E+03 
c  nu_tilda     0.61331E-05      32   0.50766E-05   0.34040E-06 0.16087E+03 
c  TempC        0.36755E+02      27   0.29331E-03   0.64988E+01 0.26346E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9177          10.338          4.5729          4.5729
v  Velocity[Y]             -2.466          7.3788       0.0063692       0.0063692
v  Velocity[Z]       -6.9287e-015     1.3211e-014    -1.0257e-017    -1.0257e-017
v  ǁVelocityǁ        0.00070227          10.338          5.1859          5.1859
v  Pressure               -44.752          15.484          -11.39          -11.39
v  nu_tilda           4.4583e-007       0.0042695       0.0014198       0.0014198
v  TempC                       21          73.042          21.874          21.874
v  TurbVisc           3.4746e-014        0.005032        0.001667        0.001667
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1547:        0.19250E+01

===============================================================


 INSTANT    0.154800000E+04   TIME STEP NUMBER            1548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14149E-02 0.90293E+00
   Friction velocity        uk    :  0.14149E-02 0.90293E+00
   Dimensionless distance   yplus :  0.11391E-01 0.72692E+01
   Friction thermal sca.    tstar : -0.11623E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84988E-02 0.54236E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90905E-02      33   0.29393E-03   0.40419E+01 0.15112E+03 
c  Velocity[X]                                      0.16596E+01 
c  Velocity[Y]                                      0.23822E+01 
c  Velocity[Z]                                      0.11586E-29 
c  Pressure     0.11750E-06     345   0.96965E-08   0.10545E+00 0.27533E+03 
c  nu_tilda     0.61353E-05      32   0.15797E-04   0.34089E-06 0.16096E+03 
c  TempC        0.36764E+02      26   0.45645E-03   0.49074E+01 0.24408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9146          10.338          4.5729          4.5729
v  Velocity[Y]            -2.4645          7.3966       0.0064677       0.0064677
v  Velocity[Z]       -6.9287e-015      1.198e-014    -1.0282e-017    -1.0282e-017
v  ǁVelocityǁ        0.00076018          10.338          5.1856          5.1856
v  Pressure               -44.756          15.544           -11.4           -11.4
v  nu_tilda           4.4582e-007       0.0042695       0.0014203       0.0014203
v  TempC                       21          73.041          21.875          21.875
v  TurbVisc           3.4758e-014        0.005032       0.0016676       0.0016676
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1548:        0.17830E+01

===============================================================


 INSTANT    0.154900000E+04   TIME STEP NUMBER            1549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17244E-02 0.90389E+00
   Friction velocity        uk    :  0.17244E-02 0.90389E+00
   Dimensionless distance   yplus :  0.13882E-01 0.72770E+01
   Friction thermal sca.    tstar : -0.10584E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10358E-01 0.54294E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90927E-02      33   0.30997E-03   0.40482E+01 0.15117E+03 
c  Velocity[X]                                      0.16748E+01 
c  Velocity[Y]                                      0.23733E+01 
c  Velocity[Z]                                      0.11212E-29 
c  Pressure     0.13694E-06     313   0.92271E-08   0.12265E+00 0.48326E+03 
c  nu_tilda     0.61375E-05      32   0.50784E-05   0.34135E-06 0.16106E+03 
c  TempC        0.36773E+02      27   0.35145E-03   0.70741E+01 0.31115E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9113          10.337          4.5729          4.5729
v  Velocity[Y]             -2.463          7.3709       0.0065668       0.0065668
v  Velocity[Z]       -6.9287e-015     1.1468e-014    -1.0306e-017    -1.0306e-017
v  ǁVelocityǁ        0.00074976          10.337          5.1853          5.1853
v  Pressure               -44.717          15.461         -11.401         -11.401
v  nu_tilda           4.4586e-007       0.0042695       0.0014209       0.0014209
v  TempC                       21          73.042          21.875          21.875
v  TurbVisc           3.4755e-014        0.005032       0.0016682       0.0016682
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1549:        0.17090E+01

===============================================================


 INSTANT    0.155000000E+04   TIME STEP NUMBER            1550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15276E-01 0.90315E+00
   Friction velocity        uk    :  0.15276E-01 0.90315E+00
   Dimensionless distance   yplus :  0.12298E+00 0.72710E+01
   Friction thermal sca.    tstar : -0.10877E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91760E-01 0.54250E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90949E-02      33   0.25529E-03   0.40619E+01 0.15135E+03 
c  Velocity[X]                                      0.16893E+01 
c  Velocity[Y]                                      0.23726E+01 
c  Velocity[Z]                                      0.10550E-29 
c  Pressure     0.11192E-06     346   0.97339E-08   0.10093E+00 0.34217E+03 
c  nu_tilda     0.61397E-05      32   0.15790E-04   0.34183E-06 0.16115E+03 
c  TempC        0.36782E+02      26   0.35218E-03   0.56608E+01 0.25497E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9081          10.336          4.5729          4.5729
v  Velocity[Y]            -2.4616          7.3971       0.0066665       0.0066665
v  Velocity[Z]       -6.9287e-015     1.2124e-014    -1.0326e-017    -1.0326e-017
v  ǁVelocityǁ        0.00065099          10.336           5.185           5.185
v  Pressure               -44.721          15.542         -11.405         -11.405
v  nu_tilda           4.4589e-007       0.0042695       0.0014213       0.0014213
v  TempC                       21          73.041          21.875          21.875
v  TurbVisc           3.4767e-014        0.005032       0.0016688       0.0016688
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1550:        0.17760E+01

===============================================================


 INSTANT    0.155100000E+04   TIME STEP NUMBER            1551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84542E-02 0.90473E+00
   Friction velocity        uk    :  0.84542E-02 0.90473E+00
   Dimensionless distance   yplus :  0.68062E-01 0.72837E+01
   Friction thermal sca.    tstar : -0.10400E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50782E-01 0.54345E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90971E-02      33   0.29602E-03   0.40371E+01 0.15140E+03 
c  Velocity[X]                                      0.16429E+01 
c  Velocity[Y]                                      0.23942E+01 
c  Velocity[Z]                                      0.11318E-29 
c  Pressure     0.11125E-06     473   0.92613E-08   0.10043E+00 0.65430E+03 
c  nu_tilda     0.61419E-05      32   0.50703E-05   0.34229E-06 0.16125E+03 
c  TempC        0.36791E+02      26   0.34647E-03   0.56647E+01 0.25420E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9047          10.335          4.5729          4.5729
v  Velocity[Y]            -2.4601           7.409       0.0067671       0.0067671
v  Velocity[Z]       -6.9287e-015     1.1013e-014    -1.0354e-017    -1.0354e-017
v  ǁVelocityǁ        0.00043146          10.335          5.1847          5.1847
v  Pressure               -44.677          15.606         -11.372         -11.372
v  nu_tilda           4.4582e-007       0.0042695       0.0014219       0.0014219
v  TempC                       21          73.042          21.875          21.875
v  TurbVisc           3.4776e-014        0.005032       0.0016694       0.0016694
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1551:        0.20730E+01

===============================================================


 INSTANT    0.155200000E+04   TIME STEP NUMBER            1552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13605E-02 0.90423E+00
   Friction velocity        uk    :  0.13605E-02 0.90423E+00
   Dimensionless distance   yplus :  0.10953E-01 0.72797E+01
   Friction thermal sca.    tstar : -0.10744E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81724E-02 0.54315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90993E-02      33   0.31068E-03   0.40593E+01 0.15157E+03 
c  Velocity[X]                                      0.16767E+01 
c  Velocity[Y]                                      0.23826E+01 
c  Velocity[Z]                                      0.89551E-30 
c  Pressure     0.12856E-06     490   0.92105E-08   0.11607E+00 0.10738E+04 
c  nu_tilda     0.61441E-05      32   0.15790E-04   0.34279E-06 0.16135E+03 
c  TempC        0.36800E+02      27   0.33280E-03   0.55349E+01 0.25026E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9014          10.335          4.5729          4.5729
v  Velocity[Y]            -2.4587          7.3738       0.0068685       0.0068685
v  Velocity[Z]       -6.9287e-015      1.054e-014    -1.0376e-017    -1.0376e-017
v  ǁVelocityǁ        0.00046607          10.335          5.1845          5.1845
v  Pressure               -44.682          15.417         -11.436         -11.436
v  nu_tilda           4.4579e-007       0.0042695       0.0014223       0.0014223
v  TempC                       21           73.04          21.875          21.875
v  TurbVisc           3.4753e-014        0.005032         0.00167         0.00167
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1552:        0.21290E+01

===============================================================


 INSTANT    0.155300000E+04   TIME STEP NUMBER            1553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87680E-02 0.90289E+00
   Friction velocity        uk    :  0.87680E-02 0.90289E+00
   Dimensionless distance   yplus :  0.70589E-01 0.72689E+01
   Friction thermal sca.    tstar : -0.10861E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52667E-01 0.54234E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91015E-02      33   0.31198E-03   0.40723E+01 0.15177E+03 
c  Velocity[X]                                      0.16888E+01 
c  Velocity[Y]                                      0.23836E+01 
c  Velocity[Z]                                      0.12224E-29 
c  Pressure     0.12077E-06     490   0.98041E-08   0.10840E+00 0.10868E+04 
c  nu_tilda     0.61463E-05      32   0.50628E-05   0.34325E-06 0.16144E+03 
c  TempC        0.36809E+02      27   0.42716E-03   0.51660E+01 0.24550E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8983          10.334          4.5729          4.5729
v  Velocity[Y]            -2.4572          7.3982       0.0069702       0.0069702
v  Velocity[Z]       -6.9287e-015     1.1166e-014      -1.04e-017      -1.04e-017
v  ǁVelocityǁ        0.00038401          10.334          5.1842          5.1842
v  Pressure                -44.64          15.593          -11.38          -11.38
v  nu_tilda           4.4579e-007       0.0042695       0.0014229       0.0014229
v  TempC                       21          73.041          21.875          21.875
v  TurbVisc           3.4745e-014        0.005032       0.0016706       0.0016706
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1553:        0.21140E+01

===============================================================


 INSTANT    0.155400000E+04   TIME STEP NUMBER            1554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10848E-01 0.90395E+00
   Friction velocity        uk    :  0.10848E-01 0.90395E+00
   Dimensionless distance   yplus :  0.87330E-01 0.72774E+01
   Friction thermal sca.    tstar : -0.10199E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65158E-01 0.54298E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91037E-02      33   0.30101E-03   0.40788E+01 0.15193E+03 
c  Velocity[X]                                      0.16749E+01 
c  Velocity[Y]                                      0.24039E+01 
c  Velocity[Z]                                      0.13360E-29 
c  Pressure     0.12102E-06     489   0.95707E-08   0.11007E+00 0.90645E+03 
c  nu_tilda     0.61485E-05      32   0.15782E-04   0.34374E-06 0.16154E+03 
c  TempC        0.36818E+02      26   0.29402E-03   0.73469E+01 0.30303E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8951          10.333          4.5729          4.5729
v  Velocity[Y]            -2.4557          7.3731       0.0070731       0.0070731
v  Velocity[Z]       -6.9287e-015      1.008e-014    -1.0432e-017    -1.0432e-017
v  ǁVelocityǁ        0.00027376          10.333          5.1839          5.1839
v  Pressure               -44.646          15.443         -11.436         -11.436
v  nu_tilda           4.4581e-007       0.0042695       0.0014234       0.0014234
v  TempC                       21           73.04          21.876          21.876
v  TurbVisc           3.4745e-014        0.005032       0.0016712       0.0016712
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1554:        0.20940E+01

===============================================================


 INSTANT    0.155500000E+04   TIME STEP NUMBER            1555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65181E-02 0.90306E+00
   Friction velocity        uk    :  0.65181E-02 0.90306E+00
   Dimensionless distance   yplus :  0.52475E-01 0.72702E+01
   Friction thermal sca.    tstar : -0.10537E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39152E-01 0.54244E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91059E-02      33   0.24141E-03   0.40720E+01 0.15191E+03 
c  Velocity[X]                                      0.16768E+01 
c  Velocity[Y]                                      0.23951E+01 
c  Velocity[Z]                                      0.10187E-29 
c  Pressure     0.13192E-06     488   0.91261E-08   0.11781E+00 0.97521E+03 
c  nu_tilda     0.61507E-05      32   0.50610E-05   0.34420E-06 0.16163E+03 
c  TempC        0.36827E+02      26   0.35326E-03   0.47466E+01 0.22920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8918          10.332          4.5729          4.5729
v  Velocity[Y]            -2.4543          7.3962       0.0071763       0.0071763
v  Velocity[Z]       -6.9287e-015     9.6673e-015    -1.0457e-017    -1.0457e-017
v  ǁVelocityǁ        0.00020883          10.332          5.1836          5.1836
v  Pressure               -44.604          15.586         -11.385         -11.385
v  nu_tilda           4.4577e-007       0.0042695       0.0014239       0.0014239
v  TempC                       21           73.04          21.876          21.876
v  TurbVisc           3.4752e-014        0.005032       0.0016718       0.0016718
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1555:        0.21240E+01

===============================================================


 INSTANT    0.155600000E+04   TIME STEP NUMBER            1556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14185E-01 0.90472E+00
   Friction velocity        uk    :  0.14185E-01 0.90472E+00
   Dimensionless distance   yplus :  0.11420E+00 0.72836E+01
   Friction thermal sca.    tstar : -0.10877E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85206E-01 0.54344E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91081E-02      33   0.31590E-03   0.40698E+01 0.15203E+03 
c  Velocity[X]                                      0.16768E+01 
c  Velocity[Y]                                      0.23930E+01 
c  Velocity[Z]                                      0.11273E-29 
c  Pressure     0.10994E-06     442   0.93062E-08   0.99765E-01 0.42871E+03 
c  nu_tilda     0.61529E-05      32   0.15780E-04   0.34469E-06 0.16173E+03 
c  TempC        0.36836E+02      26   0.40732E-03   0.50873E+01 0.25413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8886          10.332          4.5729          4.5729
v  Velocity[Y]            -2.4528          7.4054       0.0072804       0.0072804
v  Velocity[Z]       -6.9287e-015      1.032e-014    -1.0485e-017    -1.0485e-017
v  ǁVelocityǁ         0.0001692          10.332          5.1833          5.1833
v  Pressure               -44.606          15.559         -11.415         -11.415
v  nu_tilda           4.4572e-007       0.0042695       0.0014244       0.0014244
v  TempC                       21          73.039          21.876          21.876
v  TurbVisc           3.4739e-014        0.005032       0.0016724       0.0016724
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1556:        0.20040E+01

===============================================================


 INSTANT    0.155700000E+04   TIME STEP NUMBER            1557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13025E-01 0.90425E+00
   Friction velocity        uk    :  0.13025E-01 0.90425E+00
   Dimensionless distance   yplus :  0.10486E+00 0.72798E+01
   Friction thermal sca.    tstar : -0.10044E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78236E-01 0.54316E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91103E-02      33   0.29108E-03   0.40957E+01 0.15232E+03 
c  Velocity[X]                                      0.16796E+01 
c  Velocity[Y]                                      0.24161E+01 
c  Velocity[Z]                                      0.96446E-30 
c  Pressure     0.12710E-06     409   0.96845E-08   0.11557E+00 0.44347E+03 
c  nu_tilda     0.61552E-05      32   0.50512E-05   0.34516E-06 0.16182E+03 
c  TempC        0.36845E+02      26   0.30586E-03   0.76251E+01 0.29045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8852          10.331          4.5729          4.5729
v  Velocity[Y]            -2.4514          7.3779       0.0073853       0.0073853
v  Velocity[Z]       -6.9287e-015     9.2635e-015     -1.052e-017     -1.052e-017
v  ǁVelocityǁ        0.00016475          10.331           5.183           5.183
v  Pressure               -44.566          15.515         -11.404         -11.404
v  nu_tilda           4.4575e-007       0.0042695       0.0014249       0.0014249
v  TempC                       21           73.04          21.876          21.876
v  TurbVisc           3.4722e-014        0.005032        0.001673        0.001673
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1557:        0.19240E+01

===============================================================


 INSTANT    0.155800000E+04   TIME STEP NUMBER            1558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22330E-02 0.90268E+00
   Friction velocity        uk    :  0.22330E-02 0.90268E+00
   Dimensionless distance   yplus :  0.17977E-01 0.72672E+01
   Friction thermal sca.    tstar : -0.10291E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13413E-01 0.54221E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91125E-02      33   0.31696E-03   0.40756E+01 0.15229E+03 
c  Velocity[X]                                      0.16710E+01 
c  Velocity[Y]                                      0.24046E+01 
c  Velocity[Z]                                      0.96757E-30 
c  Pressure     0.12309E-06     440   0.98286E-08   0.10994E+00 0.34014E+03 
c  nu_tilda     0.61574E-05      32   0.15780E-04   0.34566E-06 0.16192E+03 
c  TempC        0.36854E+02      26   0.40916E-03   0.58818E+01 0.25784E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.882           10.33          4.5729          4.5729
v  Velocity[Y]            -2.4499          7.3921       0.0074907       0.0074907
v  Velocity[Z]        -7.197e-015     8.8598e-015    -1.0553e-017    -1.0553e-017
v  ǁVelocityǁ        0.00026016           10.33          5.1827          5.1827
v  Pressure               -44.569          15.517         -11.429         -11.429
v  nu_tilda           4.4577e-007       0.0042695       0.0014254       0.0014254
v  TempC                       21           73.04          21.876          21.876
v  TurbVisc           3.4732e-014        0.005032       0.0016736       0.0016736
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1558:        0.20040E+01

===============================================================


 INSTANT    0.155900000E+04   TIME STEP NUMBER            1559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12712E-01 0.90395E+00
   Friction velocity        uk    :  0.12712E-01 0.90395E+00
   Dimensionless distance   yplus :  0.10234E+00 0.72774E+01
   Friction thermal sca.    tstar : -0.10037E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76357E-01 0.54298E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91147E-02      33   0.32054E-03   0.41114E+01 0.15259E+03 
c  Velocity[X]                                      0.17052E+01 
c  Velocity[Y]                                      0.24061E+01 
c  Velocity[Z]                                      0.99876E-30 
c  Pressure     0.13254E-06     457   0.93257E-08   0.12117E+00 0.50038E+03 
c  nu_tilda     0.61596E-05      32   0.50518E-05   0.34612E-06 0.16202E+03 
c  TempC        0.36863E+02      26   0.34937E-03   0.74365E+01 0.29567E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8789           10.33          4.5729          4.5729
v  Velocity[Y]            -2.4484          7.3733       0.0075969       0.0075969
v  Velocity[Z]        -7.343e-015     8.6073e-015    -1.0588e-017    -1.0588e-017
v  ǁVelocityǁ        0.00028731           10.33          5.1825          5.1825
v  Pressure               -44.531          15.519         -11.408         -11.408
v  nu_tilda            4.458e-007       0.0042695       0.0014259       0.0014259
v  TempC                       21          73.041          21.876          21.876
v  TurbVisc           3.4738e-014        0.005032       0.0016742       0.0016742
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1559:        0.20430E+01

===============================================================


 INSTANT    0.156000000E+04   TIME STEP NUMBER            1560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10653E-01 0.90311E+00
   Friction velocity        uk    :  0.10653E-01 0.90311E+00
   Dimensionless distance   yplus :  0.85761E-01 0.72706E+01
   Friction thermal sca.    tstar : -0.11050E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63987E-01 0.54247E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91169E-02      33   0.23271E-03   0.41039E+01 0.15268E+03 
c  Velocity[X]                                      0.16776E+01 
c  Velocity[Y]                                      0.24263E+01 
c  Velocity[Z]                                      0.10710E-29 
c  Pressure     0.11386E-06     410   0.93803E-08   0.10313E+00 0.28184E+03 
c  nu_tilda     0.61618E-05      32   0.15770E-04   0.34661E-06 0.16211E+03 
c  TempC        0.36873E+02      27   0.29549E-03   0.52775E+01 0.24781E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8756          10.329          4.5729          4.5729
v  Velocity[Y]            -2.4469          7.3966       0.0077039       0.0077039
v  Velocity[Z]       -7.6307e-015     9.1937e-015    -1.0617e-017    -1.0617e-017
v  ǁVelocityǁ        0.00037112          10.329          5.1822          5.1822
v  Pressure               -44.534          15.559         -11.426         -11.426
v  nu_tilda           4.4581e-007       0.0042695       0.0014264       0.0014264
v  TempC                       21          73.041          21.876          21.876
v  TurbVisc           3.4748e-014        0.005032       0.0016748       0.0016748
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1560:        0.19380E+01

===============================================================


 INSTANT    0.156100000E+04   TIME STEP NUMBER            1561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17215E-02 0.90452E+00
   Friction velocity        uk    :  0.17215E-02 0.90452E+00
   Dimensionless distance   yplus :  0.13859E-01 0.72820E+01
   Friction thermal sca.    tstar : -0.10003E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10340E-01 0.54332E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91191E-02      33   0.30519E-03   0.40834E+01 0.15259E+03 
c  Velocity[X]                                      0.16663E+01 
c  Velocity[Y]                                      0.24171E+01 
c  Velocity[Z]                                      0.10318E-29 
c  Pressure     0.13183E-06     472   0.94956E-08   0.11707E+00 0.66495E+03 
c  nu_tilda     0.61640E-05      32   0.50468E-05   0.34708E-06 0.16221E+03 
c  TempC        0.36882E+02      26   0.38868E-03   0.45766E+01 0.24544E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8724          10.328          4.5729          4.5729
v  Velocity[Y]            -2.4455          7.4039       0.0078118       0.0078118
v  Velocity[Z]       -9.5351e-015     8.3273e-015    -1.0659e-017    -1.0659e-017
v  ǁVelocityǁ        0.00039645          10.328          5.1819          5.1819
v  Pressure                -44.49           15.61         -11.392         -11.392
v  nu_tilda           4.4583e-007       0.0042695       0.0014269       0.0014269
v  TempC                       21          73.041          21.876          21.876
v  TurbVisc           3.4751e-014        0.005032       0.0016754       0.0016754
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1561:        0.21360E+01

===============================================================


 INSTANT    0.156200000E+04   TIME STEP NUMBER            1562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11177E-01 0.90423E+00
   Friction velocity        uk    :  0.11177E-01 0.90423E+00
   Dimensionless distance   yplus :  0.89985E-01 0.72796E+01
   Friction thermal sca.    tstar : -0.97217E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67139E-01 0.54314E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91213E-02      33   0.31237E-03   0.41319E+01 0.15297E+03 
c  Velocity[X]                                      0.17159E+01 
c  Velocity[Y]                                      0.24160E+01 
c  Velocity[Z]                                      0.11955E-29 
c  Pressure     0.12097E-06     505   0.95218E-08   0.11119E+00 0.10500E+04 
c  nu_tilda     0.61662E-05      32   0.15772E-04   0.34758E-06 0.16231E+03 
c  TempC        0.36891E+02      26   0.33040E-03   0.55601E+01 0.27093E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.869          10.327          4.5729          4.5729
v  Velocity[Y]             -2.444          7.3753       0.0079198       0.0079198
v  Velocity[Z]       -8.6972e-015     8.4979e-015    -1.0691e-017    -1.0691e-017
v  ǁVelocityǁ        0.00041484          10.327          5.1816          5.1816
v  Pressure               -44.497          15.437         -11.457         -11.457
v  nu_tilda           4.4592e-007       0.0042695       0.0014274       0.0014274
v  TempC                       21          73.041          21.877          21.877
v  TurbVisc           3.4758e-014        0.005032        0.001676        0.001676
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1562:        0.23850E+01

===============================================================


 INSTANT    0.156300000E+04   TIME STEP NUMBER            1563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16259E-01 0.90287E+00
   Friction velocity        uk    :  0.16259E-01 0.90287E+00
   Dimensionless distance   yplus :  0.13089E+00 0.72687E+01
   Friction thermal sca.    tstar : -0.10188E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97661E-01 0.54233E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91234E-02      33   0.30152E-03   0.41112E+01 0.15303E+03 
c  Velocity[X]                                      0.16729E+01 
c  Velocity[Y]                                      0.24383E+01 
c  Velocity[Z]                                      0.11679E-29 
c  Pressure     0.10386E-06     521   0.99480E-08   0.93818E-01 0.12246E+04 
c  nu_tilda     0.61684E-05      32   0.50404E-05   0.34805E-06 0.16240E+03 
c  TempC        0.36900E+02      27   0.41024E-03   0.62865E+01 0.26611E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8657          10.327          4.5729          4.5729
v  Velocity[Y]            -2.4426          7.3967        0.008029        0.008029
v  Velocity[Z]       -9.0818e-015     8.0775e-015    -1.0722e-017    -1.0722e-017
v  ǁVelocityǁ        0.00037641          10.327          5.1813          5.1813
v  Pressure               -44.456          15.641         -11.393         -11.393
v  nu_tilda           4.4593e-007       0.0042695        0.001428        0.001428
v  TempC                       21          73.041          21.877          21.877
v  TurbVisc           3.4786e-014        0.005032       0.0016766       0.0016766
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1563:        0.23630E+01

===============================================================


 INSTANT    0.156400000E+04   TIME STEP NUMBER            1564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31986E-02 0.90371E+00
   Friction velocity        uk    :  0.31986E-02 0.90371E+00
   Dimensionless distance   yplus :  0.25751E-01 0.72755E+01
   Friction thermal sca.    tstar : -0.10176E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19213E-01 0.54283E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91257E-02      33   0.31847E-03   0.41144E+01 0.15308E+03 
c  Velocity[X]                                      0.16863E+01 
c  Velocity[Y]                                      0.24281E+01 
c  Velocity[Z]                                      0.94813E-30 
c  Pressure     0.13116E-06     490   0.94964E-08   0.11911E+00 0.11236E+04 
c  nu_tilda     0.61706E-05      32   0.15765E-04   0.34855E-06 0.16250E+03 
c  TempC        0.36909E+02      27   0.33706E-03   0.62687E+01 0.26901E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8626          10.326          4.5729          4.5729
v  Velocity[Y]            -2.4411          7.3684       0.0081389       0.0081389
v  Velocity[Z]       -1.0431e-014     8.2075e-015    -1.0765e-017    -1.0765e-017
v  ǁVelocityǁ        0.00037253          10.326           5.181           5.181
v  Pressure               -44.457          15.434         -11.456         -11.456
v  nu_tilda           4.4597e-007       0.0042695       0.0014284       0.0014284
v  TempC                       21          73.041          21.877          21.877
v  TurbVisc           3.4789e-014        0.005032       0.0016772       0.0016772
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1564:        0.21160E+01

===============================================================


 INSTANT    0.156500000E+04   TIME STEP NUMBER            1565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59772E-02 0.90312E+00
   Friction velocity        uk    :  0.59772E-02 0.90312E+00
   Dimensionless distance   yplus :  0.48121E-01 0.72708E+01
   Friction thermal sca.    tstar : -0.10452E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35903E-01 0.54248E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91278E-02      33   0.25947E-03   0.41336E+01 0.15332E+03 
c  Velocity[X]                                      0.17065E+01 
c  Velocity[Y]                                      0.24271E+01 
c  Velocity[Z]                                      0.11009E-29 
c  Pressure     0.12678E-06     520   0.97675E-08   0.11450E+00 0.11229E+04 
c  nu_tilda     0.61728E-05      32   0.50403E-05   0.34901E-06 0.16259E+03 
c  TempC        0.36918E+02      27   0.36047E-03   0.50633E+01 0.23542E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8594          10.325          4.5729          4.5729
v  Velocity[Y]            -2.4396          7.3976       0.0082494       0.0082494
v  Velocity[Z]       -1.0332e-014     8.4485e-015    -1.0794e-017    -1.0794e-017
v  ǁVelocityǁ        0.00031942          10.325          5.1808          5.1808
v  Pressure               -44.418          15.626           -11.4           -11.4
v  nu_tilda             4.46e-007       0.0042695        0.001429        0.001429
v  TempC                       21          73.041          21.877          21.877
v  TurbVisc           3.4802e-014        0.005032       0.0016777       0.0016777
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1565:        0.23700E+01

===============================================================


 INSTANT    0.156600000E+04   TIME STEP NUMBER            1566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13960E-01 0.90457E+00
   Friction velocity        uk    :  0.13960E-01 0.90457E+00
   Dimensionless distance   yplus :  0.11239E+00 0.72824E+01
   Friction thermal sca.    tstar : -0.96873E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83857E-01 0.54335E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91301E-02      33   0.29482E-03   0.41115E+01 0.15334E+03 
c  Velocity[X]                                      0.16643E+01 
c  Velocity[Y]                                      0.24471E+01 
c  Velocity[Z]                                      0.11362E-29 
c  Pressure     0.11319E-06     472   0.98099E-08   0.10239E+00 0.50418E+03 
c  nu_tilda     0.61751E-05      32   0.15757E-04   0.34951E-06 0.16269E+03 
c  TempC        0.36927E+02      27   0.38738E-03   0.56273E+01 0.25650E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8562          10.324          4.5729          4.5729
v  Velocity[Y]            -2.4382          7.4049       0.0083608       0.0083608
v  Velocity[Z]       -1.1372e-014     8.2986e-015    -1.0836e-017    -1.0836e-017
v  ǁVelocityǁ        0.00036633          10.324          5.1805          5.1805
v  Pressure               -44.421          15.574         -11.435         -11.435
v  nu_tilda           4.4595e-007       0.0042695       0.0014294       0.0014294
v  TempC                       21          73.042          21.877          21.877
v  TurbVisc           3.4809e-014        0.005032       0.0016784       0.0016784
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1566:        0.22950E+01

===============================================================


 INSTANT    0.156700000E+04   TIME STEP NUMBER            1567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11473E-01 0.90409E+00
   Friction velocity        uk    :  0.11473E-01 0.90409E+00
   Dimensionless distance   yplus :  0.92363E-01 0.72786E+01
   Friction thermal sca.    tstar : -0.94746E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68913E-01 0.54306E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91322E-02      33   0.29775E-03   0.41408E+01 0.15349E+03 
c  Velocity[X]                                      0.17019E+01 
c  Velocity[Y]                                      0.24389E+01 
c  Velocity[Z]                                      0.86696E-30 
c  Pressure     0.13253E-06     410   0.93910E-08   0.12033E+00 0.49410E+03 
c  nu_tilda     0.61773E-05      32   0.50355E-05   0.34998E-06 0.16279E+03 
c  TempC        0.36936E+02      26   0.35752E-03   0.59692E+01 0.26112E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8529          10.323          4.5729          4.5729
v  Velocity[Y]            -2.4367          7.3732       0.0084728       0.0084728
v  Velocity[Z]       -1.3163e-014     8.2792e-015    -1.0885e-017    -1.0885e-017
v  ǁVelocityǁ        0.00053785          10.323          5.1802          5.1802
v  Pressure               -44.378          15.508         -11.426         -11.426
v  nu_tilda           4.4591e-007       0.0042695         0.00143         0.00143
v  TempC                       21          73.042          21.877          21.877
v  TurbVisc           3.4794e-014        0.005032       0.0016789       0.0016789
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1567:        0.37560E+01

===============================================================


 INSTANT    0.156800000E+04   TIME STEP NUMBER            1568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66479E-02 0.90272E+00
   Friction velocity        uk    :  0.66479E-02 0.90272E+00
   Dimensionless distance   yplus :  0.53520E-01 0.72675E+01
   Friction thermal sca.    tstar : -0.10557E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39932E-01 0.54224E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91344E-02      33   0.31180E-03   0.41439E+01 0.15363E+03 
c  Velocity[X]                                      0.17057E+01 
c  Velocity[Y]                                      0.24382E+01 
c  Velocity[Z]                                      0.92181E-30 
c  Pressure     0.10918E-06     330   0.92952E-08   0.99267E-01 0.31394E+03 
c  nu_tilda     0.61795E-05      32   0.15764E-04   0.35049E-06 0.16288E+03 
c  TempC        0.36945E+02      27   0.32777E-03   0.45420E+01 0.25002E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8496          10.323          4.5729          4.5729
v  Velocity[Y]            -2.4352           7.394       0.0085855       0.0085855
v  Velocity[Z]       -1.2529e-014      8.495e-015    -1.0919e-017    -1.0919e-017
v  ǁVelocityǁ        0.00079503          10.323          5.1799          5.1799
v  Pressure               -44.383           15.58         -11.434         -11.434
v  nu_tilda            4.459e-007       0.0042695       0.0014304       0.0014304
v  TempC                       21          73.042          21.877          21.877
v  TurbVisc           3.4782e-014        0.005032       0.0016795       0.0016795
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1568:        0.17680E+01

===============================================================


 INSTANT    0.156900000E+04   TIME STEP NUMBER            1569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11303E-01 0.90383E+00
   Friction velocity        uk    :  0.11303E-01 0.90383E+00
   Dimensionless distance   yplus :  0.90994E-01 0.72764E+01
   Friction thermal sca.    tstar : -0.98009E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67892E-01 0.54290E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91366E-02      33   0.29994E-03   0.41489E+01 0.15382E+03 
c  Velocity[X]                                      0.16887E+01 
c  Velocity[Y]                                      0.24603E+01 
c  Velocity[Z]                                      0.10217E-29 
c  Pressure     0.12381E-06     410   0.93247E-08   0.11303E+00 0.45970E+03 
c  nu_tilda     0.61817E-05      32   0.50259E-05   0.35096E-06 0.16298E+03 
c  TempC        0.36954E+02      27   0.36690E-03   0.49388E+01 0.24870E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8464          10.322          4.5729          4.5729
v  Velocity[Y]            -2.4337          7.3719        0.008699        0.008699
v  Velocity[Z]       -1.3727e-014     8.2318e-015    -1.0969e-017    -1.0969e-017
v  ǁVelocityǁ         0.0009498          10.322          5.1796          5.1796
v  Pressure               -44.341          15.541         -11.425         -11.425
v  nu_tilda           4.4592e-007       0.0042695        0.001431        0.001431
v  TempC                       21          73.042          21.878          21.878
v  TurbVisc           3.4778e-014        0.005032       0.0016801       0.0016801
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1569:        0.20610E+01

===============================================================


 INSTANT    0.157000000E+04   TIME STEP NUMBER            1570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95936E-02 0.90284E+00
   Friction velocity        uk    :  0.95936E-02 0.90284E+00
   Dimensionless distance   yplus :  0.77235E-01 0.72684E+01
   Friction thermal sca.    tstar : -0.97925E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57626E-01 0.54231E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91388E-02      33   0.26056E-03   0.41376E+01 0.15383E+03 
c  Velocity[X]                                      0.16892E+01 
c  Velocity[Y]                                      0.24484E+01 
c  Velocity[Z]                                      0.12897E-29 
c  Pressure     0.12538E-06     441   0.99600E-08   0.11222E+00 0.33241E+03 
c  nu_tilda     0.61839E-05      32   0.15753E-04   0.35146E-06 0.16308E+03 
c  TempC        0.36963E+02      27   0.38256E-03   0.50561E+01 0.23385E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8433          10.321          4.5729          4.5729
v  Velocity[Y]            -2.4323          7.3921       0.0088132       0.0088132
v  Velocity[Z]       -1.3298e-014     8.5734e-015    -1.1002e-017    -1.1002e-017
v  ǁVelocityǁ        0.00073399          10.321          5.1794          5.1794
v  Pressure               -44.347          15.541         -11.451         -11.451
v  nu_tilda           4.4596e-007       0.0042695       0.0014314       0.0014314
v  TempC                       21          73.041          21.878          21.878
v  TurbVisc           3.4786e-014        0.005032       0.0016807       0.0016807
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1570:        0.20020E+01

===============================================================


 INSTANT    0.157100000E+04   TIME STEP NUMBER            1571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62562E-03 0.90462E+00
   Friction velocity        uk    :  0.62562E-03 0.90462E+00
   Dimensionless distance   yplus :  0.50366E-02 0.72828E+01
   Friction thermal sca.    tstar : -0.96354E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37579E-02 0.54338E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91410E-02      33   0.31677E-03   0.41432E+01 0.15398E+03 
c  Velocity[X]                                      0.16941E+01 
c  Velocity[Y]                                      0.24491E+01 
c  Velocity[Z]                                      0.95782E-30 
c  Pressure     0.11831E-06     474   0.94339E-08   0.10752E+00 0.82110E+03 
c  nu_tilda     0.61861E-05      32   0.50270E-05   0.35193E-06 0.16317E+03 
c  TempC        0.36972E+02      26   0.36814E-03   0.55026E+01 0.24960E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.84           10.32          4.5729          4.5729
v  Velocity[Y]            -2.4308          7.4057        0.008928        0.008928
v  Velocity[Z]       -1.4532e-014     8.1338e-015    -1.1046e-017    -1.1046e-017
v  ǁVelocityǁ        0.00075225           10.32          5.1791          5.1791
v  Pressure               -44.306           15.65         -11.408         -11.408
v  nu_tilda           4.4594e-007       0.0042695        0.001432        0.001432
v  TempC                       21          73.042          21.878          21.878
v  TurbVisc           3.4798e-014        0.005032       0.0016813       0.0016813
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1571:        0.20660E+01

===============================================================


 INSTANT    0.157200000E+04   TIME STEP NUMBER            1572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75424E-02 0.90413E+00
   Friction velocity        uk    :  0.75424E-02 0.90413E+00
   Dimensionless distance   yplus :  0.60721E-01 0.72789E+01
   Friction thermal sca.    tstar : -0.98717E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45305E-01 0.54309E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91432E-02      33   0.28937E-03   0.41713E+01 0.15423E+03 
c  Velocity[X]                                      0.17020E+01 
c  Velocity[Y]                                      0.24694E+01 
c  Velocity[Z]                                      0.98233E-30 
c  Pressure     0.12742E-06     490   0.95557E-08   0.11713E+00 0.92961E+03 
c  nu_tilda     0.61884E-05      32   0.15751E-04   0.35243E-06 0.16327E+03 
c  TempC        0.36981E+02      27   0.33724E-03   0.52784E+01 0.25459E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8368           10.32          4.5729          4.5729
v  Velocity[Y]            -2.4293          7.3748       0.0090439       0.0090439
v  Velocity[Z]       -1.5126e-014     8.6408e-015    -1.1095e-017    -1.1095e-017
v  ǁVelocityǁ         0.0011422           10.32          5.1788          5.1788
v  Pressure               -44.307          15.486         -11.462         -11.462
v  nu_tilda           4.4593e-007       0.0042695       0.0014324       0.0014324
v  TempC                       21           73.04          21.878          21.878
v  TurbVisc            3.479e-014        0.005032       0.0016819       0.0016819
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1572:        0.21190E+01

===============================================================


 INSTANT    0.157300000E+04   TIME STEP NUMBER            1573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74325E-02 0.90262E+00
   Friction velocity        uk    :  0.74325E-02 0.90262E+00
   Dimensionless distance   yplus :  0.59837E-01 0.72667E+01
   Friction thermal sca.    tstar : -0.99086E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44645E-01 0.54218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91454E-02      33   0.29712E-03   0.41556E+01 0.15418E+03 
c  Velocity[X]                                      0.16951E+01 
c  Velocity[Y]                                      0.24605E+01 
c  Velocity[Z]                                      0.97797E-30 
c  Pressure     0.13342E-06     473   0.98661E-08   0.11920E+00 0.97545E+03 
c  nu_tilda     0.61906E-05      32   0.50150E-05   0.35292E-06 0.16337E+03 
c  TempC        0.36990E+02      27   0.35948E-03   0.47987E+01 0.24068E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8334          10.319          4.5729          4.5729
v  Velocity[Y]            -2.4279          7.3915       0.0091602       0.0091602
v  Velocity[Z]       -1.4873e-014     8.2239e-015    -1.1129e-017    -1.1129e-017
v  ǁVelocityǁ         0.0010383          10.319          5.1785          5.1785
v  Pressure               -44.267          15.637         -11.412         -11.412
v  nu_tilda           4.4592e-007       0.0042695        0.001433        0.001433
v  TempC                       21          73.042          21.878          21.878
v  TurbVisc           3.4788e-014        0.005032       0.0016825       0.0016825
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1573:        0.23170E+01

===============================================================


 INSTANT    0.157400000E+04   TIME STEP NUMBER            1574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41542E-02 0.90374E+00
   Friction velocity        uk    :  0.41542E-02 0.90374E+00
   Dimensionless distance   yplus :  0.33444E-01 0.72757E+01
   Friction thermal sca.    tstar : -0.93569E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24953E-01 0.54285E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91476E-02      33   0.31565E-03   0.41809E+01 0.15444E+03 
c  Velocity[X]                                      0.17231E+01 
c  Velocity[Y]                                      0.24578E+01 
c  Velocity[Z]                                      0.91731E-30 
c  Pressure     0.11587E-06     488   0.90269E-08   0.10670E+00 0.99957E+03 
c  nu_tilda     0.61928E-05      32   0.15749E-04   0.35342E-06 0.16346E+03 
c  TempC        0.36999E+02      26   0.34468E-03   0.52990E+01 0.24241E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8302          10.318          4.5729          4.5729
v  Velocity[Y]            -2.4264          7.3691       0.0092773       0.0092773
v  Velocity[Z]       -1.5108e-014     8.5118e-015    -1.1171e-017    -1.1171e-017
v  ǁVelocityǁ        0.00099096          10.318          5.1782          5.1782
v  Pressure                -44.27           15.47         -11.472         -11.472
v  nu_tilda           4.4593e-007       0.0042695       0.0014334       0.0014334
v  TempC                       21          73.041          21.878          21.878
v  TurbVisc           3.4786e-014        0.005032       0.0016831       0.0016831
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1574:        0.21080E+01

===============================================================


 INSTANT    0.157500000E+04   TIME STEP NUMBER            1575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39840E-02 0.90299E+00
   Friction velocity        uk    :  0.39840E-02 0.90299E+00
   Dimensionless distance   yplus :  0.32074E-01 0.72697E+01
   Friction thermal sca.    tstar : -0.97478E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23931E-01 0.54240E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91498E-02      33   0.24391E-03   0.41712E+01 0.15455E+03 
c  Velocity[X]                                      0.16902E+01 
c  Velocity[Y]                                      0.24810E+01 
c  Velocity[Z]                                      0.94207E-30 
c  Pressure     0.10584E-06     504   0.98097E-08   0.96074E-01 0.11412E+04 
c  nu_tilda     0.61950E-05      32   0.50151E-05   0.35389E-06 0.16356E+03 
c  TempC        0.37008E+02      26   0.39460E-03   0.51568E+01 0.24604E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8271          10.317          4.5729          4.5729
v  Velocity[Y]            -2.4249          7.3965       0.0093952       0.0093952
v  Velocity[Z]        -1.529e-014     8.1798e-015    -1.1205e-017    -1.1205e-017
v  ǁVelocityǁ         0.0011781          10.317           5.178           5.178
v  Pressure               -44.231          15.658         -11.414         -11.414
v  nu_tilda           4.4591e-007       0.0042695        0.001434        0.001434
v  TempC                       21          73.042          21.878          21.878
v  TurbVisc            3.479e-014        0.005032       0.0016837       0.0016837
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1575:        0.21400E+01

===============================================================


 INSTANT    0.157600000E+04   TIME STEP NUMBER            1576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26053E-02 0.90441E+00
   Friction velocity        uk    :  0.26053E-02 0.90441E+00
   Dimensionless distance   yplus :  0.20974E-01 0.72811E+01
   Friction thermal sca.    tstar : -0.98828E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15649E-01 0.54325E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91520E-02      33   0.31678E-03   0.41442E+01 0.15447E+03 
c  Velocity[X]                                      0.16745E+01 
c  Velocity[Y]                                      0.24697E+01 
c  Velocity[Z]                                      0.11054E-29 
c  Pressure     0.12281E-06     473   0.95383E-08   0.11049E+00 0.66133E+03 
c  nu_tilda     0.61972E-05      32   0.15738E-04   0.35440E-06 0.16366E+03 
c  TempC        0.37017E+02      26   0.29694E-03   0.59724E+01 0.26420E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8239          10.316          4.5729          4.5729
v  Velocity[Y]            -2.4234             7.4       0.0095138       0.0095138
v  Velocity[Z]       -1.5761e-014      8.158e-015    -1.1249e-017    -1.1249e-017
v  ǁVelocityǁ         0.0011583          10.316          5.1777          5.1777
v  Pressure               -44.233          15.572         -11.457         -11.457
v  nu_tilda           4.4589e-007       0.0042695       0.0014344       0.0014344
v  TempC                       21          73.042          21.878          21.878
v  TurbVisc           3.4781e-014        0.005032       0.0016843       0.0016843
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1576:        0.20860E+01

===============================================================


 INSTANT    0.157700000E+04   TIME STEP NUMBER            1577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48989E-02 0.90415E+00
   Friction velocity        uk    :  0.48989E-02 0.90415E+00
   Dimensionless distance   yplus :  0.39440E-01 0.72790E+01
   Friction thermal sca.    tstar : -0.95773E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29426E-01 0.54310E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91542E-02      33   0.31500E-03   0.42054E+01 0.15488E+03 
c  Velocity[X]                                      0.17337E+01 
c  Velocity[Y]                                      0.24717E+01 
c  Velocity[Z]                                      0.11151E-29 
c  Pressure     0.14595E-06     456   0.92955E-08   0.13374E+00 0.56104E+03 
c  nu_tilda     0.61995E-05      32   0.50097E-05   0.35487E-06 0.16375E+03 
c  TempC        0.37026E+02      27   0.41035E-03   0.45899E+01 0.23479E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8206          10.316          4.5729          4.5729
v  Velocity[Y]             -2.422          7.3751       0.0096331       0.0096331
v  Velocity[Z]       -1.6156e-014     7.8319e-015    -1.1295e-017    -1.1295e-017
v  ǁVelocityǁ        0.00074098          10.316          5.1774          5.1774
v  Pressure               -44.191          15.573         -11.431         -11.431
v  nu_tilda           4.4595e-007       0.0042695        0.001435        0.001435
v  TempC                       21          73.042          21.879          21.879
v  TurbVisc           3.4775e-014        0.005032       0.0016849       0.0016849
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1577:        0.20340E+01

===============================================================


 INSTANT    0.157800000E+04   TIME STEP NUMBER            1578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93687E-03 0.90274E+00
   Friction velocity        uk    :  0.93687E-03 0.90274E+00
   Dimensionless distance   yplus :  0.75425E-02 0.72676E+01
   Friction thermal sca.    tstar : -0.99642E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56275E-02 0.54225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91564E-02      33   0.28892E-03   0.41859E+01 0.15492E+03 
c  Velocity[X]                                      0.16955E+01 
c  Velocity[Y]                                      0.24904E+01 
c  Velocity[Z]                                      0.11144E-29 
c  Pressure     0.10956E-06     442   0.97574E-08   0.99546E-01 0.30543E+03 
c  nu_tilda     0.62017E-05      32   0.15741E-04   0.35539E-06 0.16385E+03 
c  TempC        0.37035E+02      27   0.40334E-03   0.47013E+01 0.23818E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8173          10.315          4.5729          4.5729
v  Velocity[Y]            -2.4205          7.3932       0.0097532       0.0097532
v  Velocity[Z]       -1.5655e-014     8.3645e-015     -1.132e-017     -1.132e-017
v  ǁVelocityǁ         0.0011603          10.315          5.1771          5.1771
v  Pressure               -44.196          15.605         -11.453         -11.453
v  nu_tilda           4.4597e-007       0.0042695       0.0014354       0.0014354
v  TempC                       21          73.041          21.879          21.879
v  TurbVisc           3.4794e-014        0.005032       0.0016855       0.0016855
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1578:        0.19980E+01

===============================================================


 INSTANT    0.157900000E+04   TIME STEP NUMBER            1579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67781E-02 0.90372E+00
   Friction velocity        uk    :  0.67781E-02 0.90372E+00
   Dimensionless distance   yplus :  0.54569E-01 0.72756E+01
   Friction thermal sca.    tstar : -0.10270E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40714E-01 0.54284E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91586E-02      33   0.30617E-03   0.41901E+01 0.15496E+03 
c  Velocity[X]                                      0.17089E+01 
c  Velocity[Y]                                      0.24812E+01 
c  Velocity[Z]                                      0.10252E-29 
c  Pressure     0.12975E-06     378   0.95115E-08   0.11791E+00 0.48974E+03 
c  nu_tilda     0.62039E-05      32   0.49990E-05   0.35586E-06 0.16395E+03 
c  TempC        0.37044E+02      27   0.30238E-03   0.56221E+01 0.24613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.814          10.314          4.5729          4.5729
v  Velocity[Y]             -2.419          7.3677        0.009874        0.009874
v  Velocity[Z]       -1.6018e-014     8.1412e-015    -1.1362e-017    -1.1362e-017
v  ǁVelocityǁ         0.0012197          10.314          5.1769          5.1769
v  Pressure               -44.153           15.53         -11.448         -11.448
v  nu_tilda           4.4596e-007       0.0042695        0.001436        0.001436
v  TempC                       21          73.041          21.879          21.879
v  TurbVisc           3.4802e-014        0.005032       0.0016861       0.0016861
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1579:        0.18500E+01

===============================================================


 INSTANT    0.158000000E+04   TIME STEP NUMBER            1580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68491E-02 0.90297E+00
   Friction velocity        uk    :  0.68491E-02 0.90297E+00
   Dimensionless distance   yplus :  0.55140E-01 0.72695E+01
   Friction thermal sca.    tstar : -0.11084E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41141E-01 0.54239E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91608E-02      33   0.25504E-03   0.42030E+01 0.15515E+03 
c  Velocity[X]                                      0.17231E+01 
c  Velocity[Y]                                      0.24799E+01 
c  Velocity[Z]                                      0.95925E-30 
c  Pressure     0.11143E-06     361   0.97044E-08   0.10166E+00 0.31239E+03 
c  nu_tilda     0.62061E-05      32   0.15736E-04   0.35637E-06 0.16405E+03 
c  TempC        0.37053E+02      26   0.38364E-03   0.38307E+01 0.22016E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8109          10.313          4.5729          4.5729
v  Velocity[Y]            -2.4175          7.3931       0.0099955       0.0099955
v  Velocity[Z]       -1.5888e-014     8.5467e-015    -1.1388e-017    -1.1388e-017
v  ǁVelocityǁ         0.0013722          10.313          5.1766          5.1766
v  Pressure               -44.159          15.604         -11.458         -11.458
v  nu_tilda           4.4595e-007       0.0042695       0.0014365       0.0014365
v  TempC                       21          73.041          21.879          21.879
v  TurbVisc           3.4799e-014        0.005032       0.0016867       0.0016867
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1580:        0.18110E+01

===============================================================


 INSTANT    0.158100000E+04   TIME STEP NUMBER            1581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10610E-01 0.90439E+00
   Friction velocity        uk    :  0.10610E-01 0.90439E+00
   Dimensionless distance   yplus :  0.85416E-01 0.72810E+01
   Friction thermal sca.    tstar : -0.12216E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63730E-01 0.54324E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91630E-02      33   0.29523E-03   0.41795E+01 0.15520E+03 
c  Velocity[X]                                      0.16770E+01 
c  Velocity[Y]                                      0.25025E+01 
c  Velocity[Z]                                      0.11076E-29 
c  Pressure     0.10936E-06     489   0.94291E-08   0.99239E-01 0.66505E+03 
c  nu_tilda     0.62084E-05      32   0.50027E-05   0.35685E-06 0.16414E+03 
c  TempC        0.37062E+02      26   0.33029E-03   0.50121E+01 0.25042E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8077          10.313          4.5729          4.5729
v  Velocity[Y]             -2.416          7.4042        0.010118        0.010118
v  Velocity[Z]       -1.6533e-014     8.1276e-015    -1.1428e-017    -1.1428e-017
v  ǁVelocityǁ         0.0015459          10.313          5.1763          5.1763
v  Pressure               -44.117          15.668         -11.425         -11.425
v  nu_tilda           4.4591e-007       0.0042695        0.001437        0.001437
v  TempC                       21          73.042          21.879          21.879
v  TurbVisc           3.4793e-014        0.005032       0.0016872       0.0016872
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1581:        0.21040E+01

===============================================================


 INSTANT    0.158200000E+04   TIME STEP NUMBER            1582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24032E-02 0.90388E+00
   Friction velocity        uk    :  0.24032E-02 0.90388E+00
   Dimensionless distance   yplus :  0.19347E-01 0.72769E+01
   Friction thermal sca.    tstar : -0.14064E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14435E-01 0.54293E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91653E-02      33   0.30929E-03   0.42069E+01 0.15537E+03 
c  Velocity[X]                                      0.17136E+01 
c  Velocity[Y]                                      0.24933E+01 
c  Velocity[Z]                                      0.93077E-30 
c  Pressure     0.12391E-06     472   0.96379E-08   0.11314E+00 0.99202E+03 
c  nu_tilda     0.62106E-05      32   0.15728E-04   0.35736E-06 0.16424E+03 
c  TempC        0.37071E+02      27   0.41795E-03   0.50527E+01 0.24966E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8045          10.312          4.5729          4.5729
v  Velocity[Y]            -2.4146           7.369        0.010241        0.010241
v  Velocity[Z]       -1.6603e-014     8.5812e-015     -1.146e-017     -1.146e-017
v  ǁVelocityǁ         0.0016883          10.312           5.176           5.176
v  Pressure                -44.12          15.492         -11.483         -11.483
v  nu_tilda           4.4595e-007       0.0042695       0.0014375       0.0014375
v  TempC                       21          73.042          21.879          21.879
v  TurbVisc           3.4782e-014        0.005032       0.0016878       0.0016878
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1582:        0.20690E+01

===============================================================


 INSTANT    0.158300000E+04   TIME STEP NUMBER            1583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78864E-02 0.90257E+00
   Friction velocity        uk    :  0.78864E-02 0.90257E+00
   Dimensionless distance   yplus :  0.63491E-01 0.72663E+01
   Friction thermal sca.    tstar : -0.15831E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47371E-01 0.54215E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91674E-02      33   0.31200E-03   0.42133E+01 0.15553E+03 
c  Velocity[X]                                      0.17224E+01 
c  Velocity[Y]                                      0.24910E+01 
c  Velocity[Z]                                      0.83894E-30 
c  Pressure     0.11990E-06     490   0.93377E-08   0.10921E+00 0.10731E+04 
c  nu_tilda     0.62128E-05      32   0.49930E-05   0.35784E-06 0.16434E+03 
c  TempC        0.37080E+02      27   0.30704E-03   0.67728E+01 0.29199E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8012          10.311          4.5729          4.5729
v  Velocity[Y]            -2.4131          7.3937        0.010365        0.010365
v  Velocity[Z]       -1.6817e-014     8.1401e-015    -1.1494e-017    -1.1494e-017
v  ǁVelocityǁ         0.0020152          10.311          5.1758          5.1758
v  Pressure               -44.078          15.664         -11.428         -11.428
v  nu_tilda           4.4599e-007       0.0042695        0.001438        0.001438
v  TempC                       21          73.042          21.879          21.879
v  TurbVisc           3.4795e-014        0.005032       0.0016884       0.0016884
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1583:        0.21050E+01

===============================================================


 INSTANT    0.158400000E+04   TIME STEP NUMBER            1584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64150E-02 0.90364E+00
   Friction velocity        uk    :  0.64150E-02 0.90364E+00
   Dimensionless distance   yplus :  0.51645E-01 0.72749E+01
   Friction thermal sca.    tstar : -0.22842E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38533E-01 0.54279E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91697E-02      33   0.30230E-03   0.42202E+01 0.15569E+03 
c  Velocity[X]                                      0.17092E+01 
c  Velocity[Y]                                      0.25111E+01 
c  Velocity[Z]                                      0.11636E-29 
c  Pressure     0.11830E-06     506   0.99601E-08   0.10920E+00 0.94195E+03 
c  nu_tilda     0.62151E-05      32   0.15728E-04   0.35836E-06 0.16443E+03 
c  TempC        0.37089E+02      26   0.37554E-03   0.41992E+01 0.22801E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7979           10.31          4.5729          4.5729
v  Velocity[Y]            -2.4116          7.3683        0.010489        0.010489
v  Velocity[Z]       -1.6542e-014     7.7589e-015    -1.1523e-017    -1.1523e-017
v  ǁVelocityǁ         0.0019159           10.31          5.1755          5.1755
v  Pressure               -44.083           15.51         -11.485         -11.485
v  nu_tilda           4.4604e-007       0.0042695       0.0014384       0.0014384
v  TempC                       21          73.041          21.879          21.879
v  TurbVisc           3.4808e-014        0.005032        0.001689        0.001689
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1584:        0.21360E+01

===============================================================


 INSTANT    0.158500000E+04   TIME STEP NUMBER            1585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21459E-02 0.90274E+00
   Friction velocity        uk    :  0.21459E-02 0.90274E+00
   Dimensionless distance   yplus :  0.17276E-01 0.72677E+01
   Friction thermal sca.    tstar : -0.68013E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12890E-01 0.54225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91718E-02      33   0.23819E-03   0.42153E+01 0.15567E+03 
c  Velocity[X]                                      0.17134E+01 
c  Velocity[Y]                                      0.25019E+01 
c  Velocity[Z]                                      0.10940E-29 
c  Pressure     0.12780E-06     506   0.96345E-08   0.11444E+00 0.10098E+04 
c  nu_tilda     0.62173E-05      32   0.49821E-05   0.35883E-06 0.16453E+03 
c  TempC        0.37098E+02      27   0.30279E-03   0.47840E+01 0.25292E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7947           10.31          4.5729          4.5729
v  Velocity[Y]            -2.4101          7.3908        0.010614        0.010614
v  Velocity[Z]        -1.685e-014      7.983e-015    -1.1555e-017    -1.1555e-017
v  ǁVelocityǁ         0.0021957           10.31          5.1752          5.1752
v  Pressure               -44.042          15.658         -11.433         -11.433
v  nu_tilda           4.4609e-007       0.0042695        0.001439        0.001439
v  TempC                       21          73.041           21.88           21.88
v  TurbVisc           3.4824e-014        0.005032       0.0016896       0.0016896
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1585:        0.21500E+01

===============================================================


 INSTANT    0.158600000E+04   TIME STEP NUMBER            1586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55581E-02 0.90432E+00
   Friction velocity        uk    :  0.55581E-02 0.90432E+00
   Dimensionless distance   yplus :  0.44746E-01 0.72804E+01
   Friction thermal sca.    tstar : -0.26157E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33386E-01 0.54320E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91741E-02      33   0.31449E-03   0.42108E+01 0.15579E+03 
c  Velocity[X]                                      0.17101E+01 
c  Velocity[Y]                                      0.25007E+01 
c  Velocity[Z]                                      0.10341E-29 
c  Pressure     0.10579E-06     504   0.91570E-08   0.96767E-01 0.48390E+03 
c  nu_tilda     0.62195E-05      32   0.15721E-04   0.35935E-06 0.16463E+03 
c  TempC        0.37107E+02      27   0.32488E-03   0.37559E+01 0.22365E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7916          10.309          4.5729          4.5729
v  Velocity[Y]            -2.4087          7.4005         0.01074         0.01074
v  Velocity[Z]       -1.6815e-014     8.4085e-015    -1.1579e-017    -1.1579e-017
v  ǁVelocityǁ         0.0022541          10.309           5.175           5.175
v  Pressure               -44.046          15.619         -11.468         -11.468
v  nu_tilda            4.461e-007       0.0042695       0.0014394       0.0014394
v  TempC                       21           73.04           21.88           21.88
v  TurbVisc           3.4838e-014        0.005032       0.0016902       0.0016902
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1586:        0.21480E+01

===============================================================


 INSTANT    0.158700000E+04   TIME STEP NUMBER            1587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75563E-02 0.90395E+00
   Friction velocity        uk    :  0.75563E-02 0.90395E+00
   Dimensionless distance   yplus :  0.60833E-01 0.72774E+01
   Friction thermal sca.    tstar : -0.19162E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45388E-01 0.54298E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91762E-02      33   0.28725E-03   0.42370E+01 0.15606E+03 
c  Velocity[X]                                      0.17130E+01 
c  Velocity[Y]                                      0.25240E+01 
c  Velocity[Z]                                      0.11645E-29 
c  Pressure     0.12559E-06     456   0.94641E-08   0.11621E+00 0.50653E+03 
c  nu_tilda     0.62218E-05      32   0.49865E-05   0.35983E-06 0.16473E+03 
c  TempC        0.37116E+02      26   0.40359E-03   0.45122E+01 0.23086E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7884          10.308          4.5729          4.5729
v  Velocity[Y]            -2.4072          7.3733        0.010867        0.010867
v  Velocity[Z]       -1.7247e-014     8.1111e-015    -1.1614e-017    -1.1614e-017
v  ǁVelocityǁ          0.001115          10.308          5.1747          5.1747
v  Pressure               -44.005            15.6         -11.448         -11.448
v  nu_tilda           4.4609e-007       0.0042695         0.00144         0.00144
v  TempC                       21          73.041           21.88           21.88
v  TurbVisc           3.4841e-014        0.005032       0.0016908       0.0016908
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1587:        0.20450E+01

===============================================================


 INSTANT    0.158800000E+04   TIME STEP NUMBER            1588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91824E-02 0.90239E+00
   Friction velocity        uk    :  0.91824E-02 0.90239E+00
   Dimensionless distance   yplus :  0.73924E-01 0.72648E+01
   Friction thermal sca.    tstar : -0.15702E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55156E-01 0.54204E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91785E-02      33   0.30989E-03   0.42156E+01 0.15601E+03 
c  Velocity[X]                                      0.17045E+01 
c  Velocity[Y]                                      0.25111E+01 
c  Velocity[Z]                                      0.95682E-30 
c  Pressure     0.12532E-06     440   0.99299E-08   0.11299E+00 0.35367E+03 
c  nu_tilda     0.62240E-05      32   0.15718E-04   0.36035E-06 0.16482E+03 
c  TempC        0.37125E+02      27   0.41544E-03   0.61238E+01 0.27028E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7852          10.307          4.5729          4.5729
v  Velocity[Y]            -2.4057          7.3869        0.010995        0.010995
v  Velocity[Z]       -1.7256e-014     8.0503e-015    -1.1644e-017    -1.1644e-017
v  ǁVelocityǁ         0.0025812          10.307          5.1744          5.1744
v  Pressure               -44.005          15.601         -11.472         -11.472
v  nu_tilda           4.4604e-007       0.0042695       0.0014404       0.0014404
v  TempC                       21          73.041           21.88           21.88
v  TurbVisc           3.4839e-014        0.005032       0.0016914       0.0016914
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1588:        0.19920E+01

===============================================================


 INSTANT    0.158900000E+04   TIME STEP NUMBER            1589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69292E-02 0.90360E+00
   Friction velocity        uk    :  0.69292E-02 0.90360E+00
   Dimensionless distance   yplus :  0.55785E-01 0.72746E+01
   Friction thermal sca.    tstar : -0.13690E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41622E-01 0.54276E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91807E-02      33   0.31799E-03   0.42508E+01 0.15631E+03 
c  Velocity[X]                                      0.17389E+01 
c  Velocity[Y]                                      0.25120E+01 
c  Velocity[Z]                                      0.98560E-30 
c  Pressure     0.13469E-06     426   0.99581E-08   0.12382E+00 0.45319E+03 
c  nu_tilda     0.62262E-05      32   0.49728E-05   0.36083E-06 0.16492E+03 
c  TempC        0.37134E+02      27   0.29661E-03   0.56774E+01 0.26969E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7818          10.307          4.5729          4.5729
v  Velocity[Y]            -2.4042          7.3682        0.011123        0.011123
v  Velocity[Z]       -1.7218e-014     8.0235e-015    -1.1668e-017    -1.1668e-017
v  ǁVelocityǁ         0.0027059          10.307          5.1741          5.1741
v  Pressure               -43.966          15.577         -11.458         -11.458
v  nu_tilda           4.4603e-007       0.0042695        0.001441        0.001441
v  TempC                       21          73.042           21.88           21.88
v  TurbVisc           3.4822e-014        0.005032        0.001692        0.001692
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1589:        0.19600E+01

===============================================================


 INSTANT    0.159000000E+04   TIME STEP NUMBER            1590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11062E-01 0.90282E+00
   Friction velocity        uk    :  0.11062E-01 0.90282E+00
   Dimensionless distance   yplus :  0.89054E-01 0.72683E+01
   Friction thermal sca.    tstar : -0.11779E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66444E-01 0.54230E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91829E-02      33   0.22928E-03   0.42441E+01 0.15639E+03 
c  Velocity[X]                                      0.17116E+01 
c  Velocity[Y]                                      0.25325E+01 
c  Velocity[Z]                                      0.10602E-29 
c  Pressure     0.11698E-06     278   0.96472E-08   0.10662E+00 0.31594E+03 
c  nu_tilda     0.62285E-05      32   0.15717E-04   0.36135E-06 0.16502E+03 
c  TempC        0.37143E+02      27   0.32460E-03   0.35929E+01 0.22468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7787          10.306          4.5729          4.5729
v  Velocity[Y]            -2.4027          7.3912        0.011252        0.011252
v  Velocity[Z]       -1.7063e-014     8.4387e-015    -1.1692e-017    -1.1692e-017
v  ǁVelocityǁ         0.0020572          10.306          5.1739          5.1739
v  Pressure               -43.969          15.654         -11.465         -11.465
v  nu_tilda           4.4602e-007       0.0042695       0.0014414       0.0014414
v  TempC                       21          73.041           21.88           21.88
v  TurbVisc           3.4819e-014        0.005032       0.0016926       0.0016926
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1590:        0.16190E+01

===============================================================


 INSTANT    0.159100000E+04   TIME STEP NUMBER            1591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47954E-02 0.90421E+00
   Friction velocity        uk    :  0.47954E-02 0.90421E+00
   Dimensionless distance   yplus :  0.38606E-01 0.72795E+01
   Friction thermal sca.    tstar : -0.11251E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28805E-01 0.54313E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91851E-02      33   0.30245E-03   0.42210E+01 0.15632E+03 
c  Velocity[X]                                      0.16972E+01 
c  Velocity[Y]                                      0.25238E+01 
c  Velocity[Z]                                      0.95148E-30 
c  Pressure     0.11975E-06     456   0.97841E-08   0.10822E+00 0.50367E+03 
c  nu_tilda     0.62307E-05      32   0.49694E-05   0.36184E-06 0.16512E+03 
c  TempC        0.37151E+02      27   0.36158E-03   0.38780E+01 0.21191E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7755          10.305          4.5729          4.5729
v  Velocity[Y]            -2.4012          7.3989        0.011382        0.011382
v  Velocity[Z]       -1.6933e-014     8.0607e-015    -1.1717e-017    -1.1717e-017
v  ǁVelocityǁ         0.0026056          10.305          5.1736          5.1736
v  Pressure               -43.931          15.672         -11.444         -11.444
v  nu_tilda           4.4598e-007       0.0042695        0.001442        0.001442
v  TempC                       21          73.042           21.88           21.88
v  TurbVisc           3.4818e-014        0.005032       0.0016931       0.0016931
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1591:        0.20260E+01

===============================================================


 INSTANT    0.159200000E+04   TIME STEP NUMBER            1592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61254E-02 0.90393E+00
   Friction velocity        uk    :  0.61254E-02 0.90393E+00
   Dimensionless distance   yplus :  0.49314E-01 0.72772E+01
   Friction thermal sca.    tstar : -0.10521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36794E-01 0.54296E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91873E-02      33   0.30475E-03   0.42709E+01 0.15666E+03 
c  Velocity[X]                                      0.17479E+01 
c  Velocity[Y]                                      0.25230E+01 
c  Velocity[Z]                                      0.83678E-30 
c  Pressure     0.11682E-06     472   0.92252E-08   0.10861E+00 0.76922E+03 
c  nu_tilda     0.62329E-05      32   0.15710E-04   0.36236E-06 0.16521E+03 
c  TempC        0.37160E+02      27   0.38049E-03   0.38208E+01 0.23063E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7723          10.304          4.5729          4.5729
v  Velocity[Y]            -2.3998          7.3704        0.011512        0.011512
v  Velocity[Z]       -1.7014e-014      7.904e-015    -1.1749e-017    -1.1749e-017
v  ǁVelocityǁ         0.0026086          10.304          5.1733          5.1733
v  Pressure               -43.933          15.542         -11.491         -11.491
v  nu_tilda           4.4602e-007       0.0042695       0.0014424       0.0014424
v  TempC                       21          73.041          21.881          21.881
v  TurbVisc           3.4804e-014        0.005032       0.0016937       0.0016937
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1592:        0.20700E+01

===============================================================


 INSTANT    0.159300000E+04   TIME STEP NUMBER            1593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39938E-02 0.90251E+00
   Friction velocity        uk    :  0.39938E-02 0.90251E+00
   Dimensionless distance   yplus :  0.32153E-01 0.72658E+01
   Friction thermal sca.    tstar : -0.10048E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23990E-01 0.54211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91895E-02      33   0.28876E-03   0.42508E+01 0.15672E+03 
c  Velocity[X]                                      0.17068E+01 
c  Velocity[Y]                                      0.25440E+01 
c  Velocity[Z]                                      0.89050E-30 
c  Pressure     0.11119E-06     504   0.91848E-08   0.10106E+00 0.10595E+04 
c  nu_tilda     0.62352E-05      32   0.49667E-05   0.36284E-06 0.16531E+03 
c  TempC        0.37169E+02      27   0.32120E-03   0.51922E+01 0.24950E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7691          10.304          4.5729          4.5729
v  Velocity[Y]            -2.3983          7.3908        0.011643        0.011643
v  Velocity[Z]       -1.6674e-014     7.9816e-015    -1.1775e-017    -1.1775e-017
v  ǁVelocityǁ         0.0026518          10.304          5.1731          5.1731
v  Pressure               -43.889          15.716         -11.437         -11.437
v  nu_tilda           4.4602e-007       0.0042695        0.001443        0.001443
v  TempC                       21          73.042          21.881          21.881
v  TurbVisc           3.4818e-014        0.005032       0.0016943       0.0016943
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1593:        0.21340E+01

===============================================================


 INSTANT    0.159400000E+04   TIME STEP NUMBER            1594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13432E-01 0.90333E+00
   Friction velocity        uk    :  0.13432E-01 0.90333E+00
   Dimensionless distance   yplus :  0.10813E+00 0.72724E+01
   Friction thermal sca.    tstar : -0.92713E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80680E-01 0.54261E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91917E-02      33   0.32300E-03   0.42523E+01 0.15679E+03 
c  Velocity[X]                                      0.17201E+01 
c  Velocity[Y]                                      0.25322E+01 
c  Velocity[Z]                                      0.11120E-29 
c  Pressure     0.12370E-06     504   0.93467E-08   0.11308E+00 0.12081E+04 
c  nu_tilda     0.62374E-05      32   0.15708E-04   0.36337E-06 0.16541E+03 
c  TempC        0.37178E+02      27   0.27420E-03   0.51259E+01 0.24424E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7658          10.303          4.5729          4.5729
v  Velocity[Y]            -2.3968          7.3626        0.011775        0.011775
v  Velocity[Z]       -1.6196e-014     8.4013e-015    -1.1795e-017    -1.1795e-017
v  ǁVelocityǁ         0.0019003          10.303          5.1728          5.1728
v  Pressure               -43.893          15.497         -11.506         -11.506
v  nu_tilda           4.4611e-007       0.0042695       0.0014434       0.0014434
v  TempC                       21           73.04          21.881          21.881
v  TurbVisc           3.4818e-014        0.005032       0.0016949       0.0016949
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1594:        0.21360E+01

===============================================================


 INSTANT    0.159500000E+04   TIME STEP NUMBER            1595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38807E-02 0.90278E+00
   Friction velocity        uk    :  0.38807E-02 0.90278E+00
   Dimensionless distance   yplus :  0.31243E-01 0.72680E+01
   Friction thermal sca.    tstar : -0.91387E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23311E-01 0.54227E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91939E-02      33   0.25711E-03   0.42716E+01 0.15700E+03 
c  Velocity[X]                                      0.17392E+01 
c  Velocity[Y]                                      0.25323E+01 
c  Velocity[Z]                                      0.11444E-29 
c  Pressure     0.11883E-06     521   0.96312E-08   0.10889E+00 0.12922E+04 
c  nu_tilda     0.62396E-05      32   0.49533E-05   0.36385E-06 0.16551E+03 
c  TempC        0.37187E+02      26   0.39537E-03   0.61132E+01 0.25652E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7625          10.302          4.5729          4.5729
v  Velocity[Y]            -2.3953          7.3923        0.011908        0.011908
v  Velocity[Z]       -1.6422e-014      7.967e-015    -1.1816e-017    -1.1816e-017
v  ǁVelocityǁ          0.002804          10.302          5.1725          5.1725
v  Pressure               -43.853          15.716          -11.44          -11.44
v  nu_tilda           4.4615e-007       0.0042695        0.001444        0.001444
v  TempC                       21          73.041          21.881          21.881
v  TurbVisc           3.4844e-014        0.005032       0.0016955       0.0016955
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1595:        0.21760E+01

===============================================================


 INSTANT    0.159600000E+04   TIME STEP NUMBER            1596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11969E-01 0.90429E+00
   Friction velocity        uk    :  0.11969E-01 0.90429E+00
   Dimensionless distance   yplus :  0.96356E-01 0.72801E+01
   Friction thermal sca.    tstar : -0.92605E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71892E-01 0.54318E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91961E-02      33   0.29549E-03   0.42499E+01 0.15702E+03 
c  Velocity[X]                                      0.16974E+01 
c  Velocity[Y]                                      0.25525E+01 
c  Velocity[Z]                                      0.10851E-29 
c  Pressure     0.11122E-06     457   0.90982E-08   0.10173E+00 0.51381E+03 
c  nu_tilda     0.62419E-05      32   0.15701E-04   0.36438E-06 0.16561E+03 
c  TempC        0.37196E+02      26   0.32706E-03   0.63263E+01 0.29243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7594          10.301          4.5729          4.5729
v  Velocity[Y]            -2.3939          7.3996        0.012041        0.012041
v  Velocity[Z]       -1.5633e-014     7.9424e-015    -1.1845e-017    -1.1845e-017
v  ǁVelocityǁ         0.0028325          10.301          5.1723          5.1723
v  Pressure               -43.858          15.665         -11.477         -11.477
v  nu_tilda           4.4608e-007       0.0042695       0.0014444       0.0014444
v  TempC                       21          73.041          21.881          21.881
v  TurbVisc           3.4855e-014        0.005032       0.0016961       0.0016961
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1596:        0.20150E+01

===============================================================


 INSTANT    0.159700000E+04   TIME STEP NUMBER            1597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12482E-01 0.90378E+00
   Friction velocity        uk    :  0.12482E-01 0.90378E+00
   Dimensionless distance   yplus :  0.10049E+00 0.72760E+01
   Friction thermal sca.    tstar : -0.86976E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74976E-01 0.54287E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.91983E-02      33   0.29318E-03   0.42809E+01 0.15718E+03 
c  Velocity[X]                                      0.17350E+01 
c  Velocity[Y]                                      0.25460E+01 
c  Velocity[Z]                                      0.10235E-29 
c  Pressure     0.14339E-06     361   0.91249E-08   0.13101E+00 0.49626E+03 
c  nu_tilda     0.62441E-05      32   0.49614E-05   0.36487E-06 0.16570E+03 
c  TempC        0.37205E+02      26   0.37109E-03   0.46847E+01 0.23365E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7563            10.3          4.5729          4.5729
v  Velocity[Y]            -2.3924          7.3676        0.012176        0.012176
v  Velocity[Z]       -1.5233e-014     7.9174e-015    -1.1869e-017    -1.1869e-017
v  ǁVelocityǁ         0.0028881            10.3           5.172           5.172
v  Pressure               -43.817          15.587         -11.473         -11.473
v  nu_tilda           4.4609e-007       0.0042695        0.001445        0.001445
v  TempC                       21          73.042          21.881          21.881
v  TurbVisc           3.4836e-014        0.005032       0.0016967       0.0016967
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1597:        0.19890E+01

===============================================================


 INSTANT    0.159800000E+04   TIME STEP NUMBER            1598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23818E-02 0.90237E+00
   Friction velocity        uk    :  0.23818E-02 0.90237E+00
   Dimensionless distance   yplus :  0.19175E-01 0.72647E+01
   Friction thermal sca.    tstar : -0.88554E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14307E-01 0.54203E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92005E-02      33   0.30714E-03   0.42804E+01 0.15729E+03 
c  Velocity[X]                                      0.17393E+01 
c  Velocity[Y]                                      0.25412E+01 
c  Velocity[Z]                                      0.11207E-29 
c  Pressure     0.11558E-06     392   0.89970E-08   0.10620E+00 0.27806E+03 
c  nu_tilda     0.62464E-05      32   0.15699E-04   0.36539E-06 0.16580E+03 
c  TempC        0.37214E+02      26   0.38201E-03   0.54627E+01 0.26798E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7531            10.3          4.5729          4.5729
v  Velocity[Y]            -2.3909          7.3884         0.01231         0.01231
v  Velocity[Z]       -1.5197e-014     8.4208e-015    -1.1884e-017    -1.1884e-017
v  ǁVelocityǁ         0.0025185            10.3          5.1717          5.1717
v  Pressure               -43.817          15.638         -11.485         -11.485
v  nu_tilda           4.4613e-007       0.0042695       0.0014454       0.0014454
v  TempC                       21          73.041          21.881          21.881
v  TurbVisc           3.4838e-014        0.005032       0.0016972       0.0016972
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1598:        0.21330E+01

===============================================================


 INSTANT    0.159900000E+04   TIME STEP NUMBER            1599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12457E-01 0.90349E+00
   Friction velocity        uk    :  0.12457E-01 0.90349E+00
   Dimensionless distance   yplus :  0.10028E+00 0.72737E+01
   Friction thermal sca.    tstar : -0.86628E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74823E-01 0.54270E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92027E-02      33   0.30475E-03   0.42843E+01 0.15748E+03 
c  Velocity[X]                                      0.17200E+01 
c  Velocity[Y]                                      0.25643E+01 
c  Velocity[Z]                                      0.11458E-29 
c  Pressure     0.12284E-06     424   0.95806E-08   0.11419E+00 0.45095E+03 
c  nu_tilda     0.62486E-05      32   0.49505E-05   0.36588E-06 0.16590E+03 
c  TempC        0.37223E+02      27   0.42566E-03   0.63021E+01 0.27327E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7498          10.299          4.5729          4.5729
v  Velocity[Y]            -2.3894          7.3662        0.012446        0.012446
v  Velocity[Z]       -1.5936e-014     8.2088e-015    -1.1908e-017    -1.1908e-017
v  ǁVelocityǁ         0.0029251          10.299          5.1715          5.1715
v  Pressure               -43.777          15.617         -11.471         -11.471
v  nu_tilda           4.4616e-007       0.0042695        0.001446        0.001446
v  TempC                       21          73.041          21.882          21.882
v  TurbVisc           3.4851e-014        0.005032       0.0016978       0.0016978
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1599:        0.19520E+01

===============================================================


 INSTANT    0.160000000E+04   TIME STEP NUMBER            1600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60815E-02 0.90244E+00
   Friction velocity        uk    :  0.60815E-02 0.90244E+00
   Dimensionless distance   yplus :  0.48960E-01 0.72652E+01
   Friction thermal sca.    tstar : -0.93233E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36530E-01 0.54207E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92049E-02      33   0.25596E-03   0.42734E+01 0.15747E+03 
c  Velocity[X]                                      0.17209E+01 
c  Velocity[Y]                                      0.25525E+01 
c  Velocity[Z]                                      0.10464E-29 
c  Pressure     0.12768E-06     425   0.91416E-08   0.11644E+00 0.33863E+03 
c  nu_tilda     0.62509E-05      32   0.15696E-04   0.36641E-06 0.16600E+03 
c  TempC        0.37232E+02      27   0.34060E-03   0.57807E+01 0.27446E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7466          10.298          4.5729          4.5729
v  Velocity[Y]            -2.3879          7.3862        0.012583        0.012583
v  Velocity[Z]       -1.5507e-014     8.7054e-015    -1.1919e-017    -1.1919e-017
v  ǁVelocityǁ         0.0028955          10.298          5.1712          5.1712
v  Pressure                -43.78          15.613         -11.496         -11.496
v  nu_tilda           4.4618e-007       0.0042695       0.0014464       0.0014464
v  TempC                       21          73.041          21.882          21.882
v  TurbVisc           3.4861e-014        0.005032       0.0016984       0.0016984
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1600:        0.19440E+01

===============================================================


 INSTANT    0.160100000E+04   TIME STEP NUMBER            1601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32842E-02 0.90418E+00
   Friction velocity        uk    :  0.32842E-02 0.90418E+00
   Dimensionless distance   yplus :  0.26440E-01 0.72793E+01
   Friction thermal sca.    tstar : -0.88310E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19728E-01 0.54312E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92071E-02      33   0.31672E-03   0.42796E+01 0.15763E+03 
c  Velocity[X]                                      0.17263E+01 
c  Velocity[Y]                                      0.25533E+01 
c  Velocity[Z]                                      0.80348E-30 
c  Pressure     0.12491E-06     474   0.95846E-08   0.11457E+00 0.82561E+03 
c  nu_tilda     0.62531E-05      32   0.49423E-05   0.36690E-06 0.16610E+03 
c  TempC        0.37241E+02      27   0.33190E-03   0.44009E+01 0.24666E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7433          10.297          4.5729          4.5729
v  Velocity[Y]            -2.3865          7.3998         0.01272         0.01272
v  Velocity[Z]       -1.6083e-014     8.4732e-015    -1.1942e-017    -1.1942e-017
v  ǁVelocityǁ         0.0032221          10.297           5.171           5.171
v  Pressure               -43.742          15.723         -11.454         -11.454
v  nu_tilda           4.4617e-007       0.0042695       0.0014469       0.0014469
v  TempC                       21          73.041          21.882          21.882
v  TurbVisc           3.4868e-014        0.005032        0.001699        0.001699
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1601:        0.20870E+01

===============================================================


 INSTANT    0.160200000E+04   TIME STEP NUMBER            1602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13460E-01 0.90378E+00
   Friction velocity        uk    :  0.13460E-01 0.90378E+00
   Dimensionless distance   yplus :  0.10836E+00 0.72761E+01
   Friction thermal sca.    tstar : -0.84660E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80849E-01 0.54288E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92093E-02      33   0.28743E-03   0.43129E+01 0.15789E+03 
c  Velocity[X]                                      0.17368E+01 
c  Velocity[Y]                                      0.25761E+01 
c  Velocity[Z]                                      0.92484E-30 
c  Pressure     0.12368E-06     488   0.90942E-08   0.11604E+00 0.90658E+03 
c  nu_tilda     0.62553E-05      32   0.15690E-04   0.36743E-06 0.16619E+03 
c  TempC        0.37250E+02      26   0.36008E-03   0.40768E+01 0.23271E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7402          10.296          4.5729          4.5729
v  Velocity[Y]             -2.385          7.3683        0.012858        0.012858
v  Velocity[Z]       -1.5859e-014     8.9567e-015     -1.196e-017     -1.196e-017
v  ǁVelocityǁ          0.003076          10.297          5.1707          5.1707
v  Pressure               -43.745          15.571         -11.508         -11.508
v  nu_tilda           4.4505e-007       0.0042695       0.0014474       0.0014474
v  TempC                       21           73.04          21.882          21.882
v  TurbVisc           3.4863e-014        0.005032       0.0016996       0.0016996
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1602:        0.20950E+01

===============================================================


 INSTANT    0.160300000E+04   TIME STEP NUMBER            1603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62608E-02 0.90225E+00
   Friction velocity        uk    :  0.62608E-02 0.90225E+00
   Dimensionless distance   yplus :  0.50404E-01 0.72637E+01
   Friction thermal sca.    tstar : -0.86764E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37607E-01 0.54195E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92115E-02      33   0.29533E-03   0.42898E+01 0.15781E+03 
c  Velocity[X]                                      0.17267E+01 
c  Velocity[Y]                                      0.25631E+01 
c  Velocity[Z]                                      0.13510E-29 
c  Pressure     0.12304E-06     472   0.90628E-08   0.11226E+00 0.88821E+03 
c  nu_tilda     0.62576E-05      32   0.49457E-05   0.36791E-06 0.16629E+03 
c  TempC        0.37259E+02      26   0.35322E-03   0.48466E+01 0.25135E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.737          10.296          4.5729          4.5729
v  Velocity[Y]            -2.3835          7.3861        0.012997        0.012997
v  Velocity[Z]       -1.6198e-014     1.0667e-014    -1.1968e-017    -1.1968e-017
v  ǁVelocityǁ         0.0027346          10.296          5.1704          5.1704
v  Pressure               -43.701          15.694         -11.462         -11.462
v  nu_tilda           4.4292e-007       0.0042695       0.0014479       0.0014479
v  TempC                       21          73.041          21.882          21.882
v  TurbVisc           3.4514e-014        0.005032       0.0017002       0.0017002
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1603:        0.20750E+01

===============================================================


 INSTANT    0.160400000E+04   TIME STEP NUMBER            1604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66306E-02 0.90344E+00
   Friction velocity        uk    :  0.66306E-02 0.90344E+00
   Dimensionless distance   yplus :  0.53381E-01 0.72733E+01
   Friction thermal sca.    tstar : -0.90668E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39828E-01 0.54267E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92138E-02      33   0.31508E-03   0.43159E+01 0.15806E+03 
c  Velocity[X]                                      0.17535E+01 
c  Velocity[Y]                                      0.25623E+01 
c  Velocity[Z]                                      0.11795E-29 
c  Pressure     0.11456E-06     474   0.97518E-08   0.10781E+00 0.87951E+03 
c  nu_tilda     0.62598E-05      32   0.15682E-04   0.36844E-06 0.16639E+03 
c  TempC        0.37268E+02      27   0.33237E-03   0.51588E+01 0.25689E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7337          10.295          4.5729          4.5729
v  Velocity[Y]             -2.382          7.3627        0.013136        0.013136
v  Velocity[Z]       -1.6109e-014     9.3149e-015    -1.2008e-017    -1.2008e-017
v  ǁVelocityǁ         0.0032804          10.295          5.1702          5.1702
v  Pressure               -43.706          15.554         -11.518         -11.518
v  nu_tilda           4.4077e-007       0.0042695       0.0014484       0.0014484
v  TempC                       21          73.041          21.882          21.882
v  TurbVisc           3.3859e-014        0.005032       0.0017008       0.0017008
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1604:        0.20830E+01

===============================================================


 INSTANT    0.160500000E+04   TIME STEP NUMBER            1605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81110E-02 0.90254E+00
   Friction velocity        uk    :  0.81110E-02 0.90254E+00
   Dimensionless distance   yplus :  0.65299E-01 0.72661E+01
   Friction thermal sca.    tstar : -0.88676E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48720E-01 0.54213E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92159E-02      33   0.23102E-03   0.43072E+01 0.15817E+03 
c  Velocity[X]                                      0.17230E+01 
c  Velocity[Y]                                      0.25841E+01 
c  Velocity[Z]                                      0.10997E-29 
c  Pressure     0.10846E-06     504   0.91537E-08   0.10013E+00 0.11201E+04 
c  nu_tilda     0.62621E-05      32   0.49365E-05   0.36894E-06 0.16649E+03 
c  TempC        0.37277E+02      26   0.33723E-03   0.55180E+01 0.25041E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7304          10.294          4.5729          4.5729
v  Velocity[Y]            -2.3805          7.3896        0.013276        0.013276
v  Velocity[Z]       -1.6282e-014     1.0377e-014    -1.2027e-017    -1.2027e-017
v  ǁVelocityǁ         0.0029926          10.294          5.1699          5.1699
v  Pressure               -43.666           15.73          -11.46          -11.46
v  nu_tilda           4.3855e-007       0.0042695       0.0014489       0.0014489
v  TempC                       21          73.041          21.882          21.882
v  TurbVisc           3.3205e-014        0.005032       0.0017013       0.0017013
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1605:        0.21200E+01

===============================================================


 INSTANT    0.160600000E+04   TIME STEP NUMBER            1606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97268E-02 0.90390E+00
   Friction velocity        uk    :  0.97268E-02 0.90390E+00
   Dimensionless distance   yplus :  0.78307E-01 0.72771E+01
   Friction thermal sca.    tstar : -0.84339E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58426E-01 0.54295E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92182E-02      33   0.31239E-03   0.42806E+01 0.15808E+03 
c  Velocity[X]                                      0.17080E+01 
c  Velocity[Y]                                      0.25726E+01 
c  Velocity[Z]                                      0.11450E-29 
c  Pressure     0.12138E-06     458   0.98469E-08   0.11152E+00 0.66733E+03 
c  nu_tilda     0.62643E-05      32   0.15683E-04   0.36947E-06 0.16659E+03 
c  TempC        0.37285E+02      26   0.37840E-03   0.47746E+01 0.24798E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7273          10.293          4.5729          4.5729
v  Velocity[Y]            -2.3791          7.3933        0.013417        0.013417
v  Velocity[Z]       -1.6057e-014     1.1779e-014    -1.2043e-017    -1.2043e-017
v  ǁVelocityǁ         0.0028693          10.293          5.1697          5.1697
v  Pressure               -43.667          15.641         -11.502         -11.502
v  nu_tilda           4.3635e-007       0.0042695       0.0014494       0.0014494
v  TempC                       21          73.041          21.883          21.883
v  TurbVisc           3.2543e-014        0.005032       0.0017019       0.0017019
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1606:        0.20440E+01

===============================================================


 INSTANT    0.160700000E+04   TIME STEP NUMBER            1607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45738E-02 0.90371E+00
   Friction velocity        uk    :  0.45738E-02 0.90371E+00
   Dimensionless distance   yplus :  0.36822E-01 0.72755E+01
   Friction thermal sca.    tstar : -0.83929E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27473E-01 0.54283E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92204E-02      33   0.30623E-03   0.43378E+01 0.15848E+03 
c  Velocity[X]                                      0.17635E+01 
c  Velocity[Y]                                      0.25743E+01 
c  Velocity[Z]                                      0.10076E-29 
c  Pressure     0.13369E-06     442   0.93094E-08   0.12612E+00 0.48943E+03 
c  nu_tilda     0.62666E-05      32   0.49274E-05   0.36997E-06 0.16668E+03 
c  TempC        0.37294E+02      27   0.35618E-03   0.59382E+01 0.27560E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7241          10.293          4.5729          4.5729
v  Velocity[Y]            -2.3776          7.3688        0.013559        0.013559
v  Velocity[Z]       -1.5791e-014      1.174e-014    -1.2078e-017    -1.2078e-017
v  ǁVelocityǁ          0.002213          10.293          5.1694          5.1694
v  Pressure               -43.628          15.629         -11.483         -11.483
v  nu_tilda           4.3415e-007       0.0042695       0.0014499       0.0014499
v  TempC                       21          73.041          21.883          21.883
v  TurbVisc           3.1893e-014        0.005032       0.0017025       0.0017025
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1607:        0.20150E+01

===============================================================


 INSTANT    0.160800000E+04   TIME STEP NUMBER            1608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11670E-01 0.90230E+00
   Friction velocity        uk    :  0.11670E-01 0.90230E+00
   Dimensionless distance   yplus :  0.93954E-01 0.72642E+01
   Friction thermal sca.    tstar : -0.92252E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70100E-01 0.54199E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92226E-02      33   0.28825E-03   0.43179E+01 0.15851E+03 
c  Velocity[X]                                      0.17255E+01 
c  Velocity[Y]                                      0.25925E+01 
c  Velocity[Z]                                      0.91517E-30 
c  Pressure     0.11153E-06     409   0.99368E-08   0.10363E+00 0.28192E+03 
c  nu_tilda     0.62688E-05      32   0.15677E-04   0.37050E-06 0.16678E+03 
c  TempC        0.37303E+02      26   0.36786E-03   0.53421E+01 0.26030E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.721          10.292          4.5729          4.5729
v  Velocity[Y]            -2.3761          7.3864        0.013702        0.013702
v  Velocity[Z]       -1.5498e-014     1.2532e-014    -1.2103e-017    -1.2103e-017
v  ǁVelocityǁ         0.0025454          10.292          5.1691          5.1691
v  Pressure               -43.629          15.682         -11.497         -11.497
v  nu_tilda           4.3196e-007       0.0042695       0.0014504       0.0014504
v  TempC                       21          73.041          21.883          21.883
v  TurbVisc           3.1256e-014        0.005032       0.0017031       0.0017031
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1608:        0.19140E+01

===============================================================


 INSTANT    0.160900000E+04   TIME STEP NUMBER            1609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80786E-02 0.90327E+00
   Friction velocity        uk    :  0.80786E-02 0.90327E+00
   Dimensionless distance   yplus :  0.65038E-01 0.72720E+01
   Friction thermal sca.    tstar : -0.84952E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48526E-01 0.54257E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92248E-02      33   0.30882E-03   0.43259E+01 0.15855E+03 
c  Velocity[X]                                      0.17422E+01 
c  Velocity[Y]                                      0.25837E+01 
c  Velocity[Z]                                      0.10735E-29 
c  Pressure     0.13664E-06     425   0.97361E-08   0.12619E+00 0.49742E+03 
c  nu_tilda     0.62711E-05      32   0.49243E-05   0.37099E-06 0.16688E+03 
c  TempC        0.37312E+02      27   0.27989E-03   0.53298E+01 0.26645E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7178          10.291          4.5729          4.5729
v  Velocity[Y]            -2.3746          7.3605        0.013845        0.013845
v  Velocity[Z]        -1.517e-014     1.3379e-014    -1.2146e-017    -1.2146e-017
v  ǁVelocityǁ         0.0021721          10.291          5.1689          5.1689
v  Pressure               -43.586          15.625         -11.485         -11.485
v  nu_tilda            4.298e-007       0.0042695       0.0014509       0.0014509
v  TempC                       21           73.04          21.883          21.883
v  TurbVisc           3.0631e-014        0.005032       0.0017037       0.0017037
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1609:        0.19560E+01

===============================================================


 INSTANT    0.161000000E+04   TIME STEP NUMBER            1610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10359E-01 0.90252E+00
   Friction velocity        uk    :  0.10359E-01 0.90252E+00
   Dimensionless distance   yplus :  0.83401E-01 0.72659E+01
   Friction thermal sca.    tstar : -0.86165E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62226E-01 0.54212E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92270E-02      33   0.25132E-03   0.43376E+01 0.15872E+03 
c  Velocity[X]                                      0.17547E+01 
c  Velocity[Y]                                      0.25829E+01 
c  Velocity[Z]                                      0.10263E-29 
c  Pressure     0.11277E-06     393   0.99331E-08   0.10489E+00 0.28960E+03 
c  nu_tilda     0.62733E-05      32   0.15674E-04   0.37153E-06 0.16698E+03 
c  TempC        0.37321E+02      26   0.41749E-03   0.42526E+01 0.24359E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7146           10.29          4.5729          4.5729
v  Velocity[Y]            -2.3731          7.3867        0.013989        0.013989
v  Velocity[Z]        -1.479e-014     1.2457e-014    -1.2178e-017    -1.2178e-017
v  ǁVelocityǁ          0.001929           10.29          5.1686          5.1686
v  Pressure               -43.591          15.679           -11.5           -11.5
v  nu_tilda           4.2767e-007       0.0042695       0.0014513       0.0014513
v  TempC                       21           73.04          21.883          21.883
v  TurbVisc           3.0023e-014        0.005032       0.0017043       0.0017043
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1610:        0.18870E+01

===============================================================


 INSTANT    0.161100000E+04   TIME STEP NUMBER            1611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93469E-02 0.90411E+00
   Friction velocity        uk    :  0.93469E-02 0.90411E+00
   Dimensionless distance   yplus :  0.75249E-01 0.72787E+01
   Friction thermal sca.    tstar : -0.83968E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56144E-01 0.54307E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92292E-02      33   0.29075E-03   0.43130E+01 0.15876E+03 
c  Velocity[X]                                      0.17080E+01 
c  Velocity[Y]                                      0.26050E+01 
c  Velocity[Z]                                      0.96919E-30 
c  Pressure     0.11377E-06     504   0.90038E-08   0.10583E+00 0.85427E+03 
c  nu_tilda     0.62756E-05      32   0.49123E-05   0.37203E-06 0.16708E+03 
c  TempC        0.37330E+02      26   0.35530E-03   0.70962E+01 0.29817E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7113          10.289          4.5729          4.5729
v  Velocity[Y]            -2.3716          7.3974        0.014134        0.014134
v  Velocity[Z]       -1.4508e-014      1.281e-014     -1.222e-017     -1.222e-017
v  ǁVelocityǁ         0.0016906          10.289          5.1684          5.1684
v  Pressure                -43.55          15.789         -11.455         -11.455
v  nu_tilda           4.2556e-007       0.0042695       0.0014519       0.0014519
v  TempC                       21          73.042          21.883          21.883
v  TurbVisc           2.9431e-014        0.005032       0.0017048       0.0017048
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1611:        0.21240E+01

===============================================================


 INSTANT    0.161200000E+04   TIME STEP NUMBER            1612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67038E-03 0.90346E+00
   Friction velocity        uk    :  0.67038E-03 0.90346E+00
   Dimensionless distance   yplus :  0.53970E-02 0.72734E+01
   Friction thermal sca.    tstar : -0.86541E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40267E-02 0.54268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92314E-02      33   0.30608E-03   0.43363E+01 0.15893E+03 
c  Velocity[X]                                      0.17431E+01 
c  Velocity[Y]                                      0.25931E+01 
c  Velocity[Z]                                      0.10589E-29 
c  Pressure     0.12615E-06     522   0.94200E-08   0.11762E+00 0.13384E+04 
c  nu_tilda     0.62778E-05      32   0.15670E-04   0.37257E-06 0.16718E+03 
c  TempC        0.37339E+02      26   0.35374E-03   0.52919E+01 0.25916E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7081          10.288          4.5729          4.5729
v  Velocity[Y]            -2.3701          7.3629         0.01428         0.01428
v  Velocity[Z]       -1.4253e-014     1.2314e-014    -1.2255e-017    -1.2255e-017
v  ǁVelocityǁ         0.0014604          10.288          5.1681          5.1681
v  Pressure               -43.554          15.547         -11.532         -11.532
v  nu_tilda           4.2351e-007       0.0042695       0.0014523       0.0014523
v  TempC                       21          73.041          21.883          21.883
v  TurbVisc           2.8854e-014        0.005032       0.0017054       0.0017054
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1612:        0.21990E+01

===============================================================


 INSTANT    0.161300000E+04   TIME STEP NUMBER            1613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78946E-02 0.90222E+00
   Friction velocity        uk    :  0.78946E-02 0.90222E+00
   Dimensionless distance   yplus :  0.63557E-01 0.72635E+01
   Friction thermal sca.    tstar : -0.87614E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47421E-01 0.54194E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92336E-02      33   0.30701E-03   0.43453E+01 0.15909E+03 
c  Velocity[X]                                      0.17529E+01 
c  Velocity[Y]                                      0.25924E+01 
c  Velocity[Z]                                      0.10280E-29 
c  Pressure     0.12171E-06     504   0.90653E-08   0.11245E+00 0.13140E+04 
c  nu_tilda     0.62801E-05      32   0.49160E-05   0.37306E-06 0.16727E+03 
c  TempC        0.37348E+02      26   0.29668E-03   0.56068E+01 0.26300E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.705          10.288          4.5729          4.5729
v  Velocity[Y]            -2.3686          7.3866        0.014426        0.014426
v  Velocity[Z]       -1.4077e-014     1.3057e-014     -1.229e-017     -1.229e-017
v  ǁVelocityǁ         0.0013556          10.288          5.1679          5.1679
v  Pressure               -43.514           15.77         -11.465         -11.465
v  nu_tilda           4.2147e-007       0.0042695       0.0014529       0.0014529
v  TempC                       21          73.042          21.884          21.884
v  TurbVisc           2.8301e-014        0.005032        0.001706        0.001706
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1613:        0.21320E+01

===============================================================


 INSTANT    0.161400000E+04   TIME STEP NUMBER            1614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39461E-02 0.90321E+00
   Friction velocity        uk    :  0.39461E-02 0.90321E+00
   Dimensionless distance   yplus :  0.31769E-01 0.72714E+01
   Friction thermal sca.    tstar : -0.82360E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23703E-01 0.54253E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92358E-02      33   0.29349E-03   0.43527E+01 0.15923E+03 
c  Velocity[X]                                      0.17405E+01 
c  Velocity[Y]                                      0.26122E+01 
c  Velocity[Z]                                      0.11912E-29 
c  Pressure     0.11983E-06     505   0.98080E-08   0.11264E+00 0.10038E+04 
c  nu_tilda     0.62823E-05      32   0.15661E-04   0.37360E-06 0.16737E+03 
c  TempC        0.37357E+02      27   0.33512E-03   0.44704E+01 0.23217E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7018          10.287          4.5729          4.5729
v  Velocity[Y]            -2.3671          7.3615        0.014573        0.014573
v  Velocity[Z]       -1.3837e-014     1.2998e-014    -1.2343e-017    -1.2343e-017
v  ǁVelocityǁ         0.0012864          10.287          5.1676          5.1676
v  Pressure               -43.513          15.598         -11.522         -11.522
v  nu_tilda           4.1947e-007       0.0042695       0.0014533       0.0014533
v  TempC                       21          73.041          21.884          21.884
v  TurbVisc           2.7762e-014        0.005032       0.0017066       0.0017066
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1614:        0.21490E+01

===============================================================


 INSTANT    0.161500000E+04   TIME STEP NUMBER            1615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45229E-02 0.90234E+00
   Friction velocity        uk    :  0.45229E-02 0.90234E+00
   Dimensionless distance   yplus :  0.36412E-01 0.72644E+01
   Friction thermal sca.    tstar : -0.84838E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27168E-01 0.54201E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92380E-02      33   0.23584E-03   0.43451E+01 0.15921E+03 
c  Velocity[X]                                      0.17417E+01 
c  Velocity[Y]                                      0.26035E+01 
c  Velocity[Z]                                      0.10460E-29 
c  Pressure     0.12394E-06     489   0.97348E-08   0.11396E+00 0.10401E+04 
c  nu_tilda     0.62846E-05      32   0.49080E-05   0.37411E-06 0.16747E+03 
c  TempC        0.37365E+02      27   0.37324E-03   0.50320E+01 0.24874E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6985          10.286          4.5729          4.5729
v  Velocity[Y]            -2.3656          7.3838        0.014721        0.014721
v  Velocity[Z]       -1.3608e-014     1.2526e-014     -1.238e-017     -1.238e-017
v  ǁVelocityǁ         0.0013641          10.286          5.1674          5.1674
v  Pressure               -43.474          15.758         -11.469         -11.469
v  nu_tilda           4.1749e-007       0.0042695       0.0014539       0.0014539
v  TempC                       21          73.042          21.884          21.884
v  TurbVisc           2.7237e-014        0.005032       0.0017072       0.0017072
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1615:        0.21100E+01

===============================================================


 INSTANT    0.161600000E+04   TIME STEP NUMBER            1616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83094E-02 0.90391E+00
   Friction velocity        uk    :  0.83094E-02 0.90391E+00
   Dimensionless distance   yplus :  0.66896E-01 0.72771E+01
   Friction thermal sca.    tstar : -0.87659E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49912E-01 0.54295E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92403E-02      33   0.30930E-03   0.43418E+01 0.15932E+03 
c  Velocity[X]                                      0.17405E+01 
c  Velocity[Y]                                      0.26013E+01 
c  Velocity[Z]                                      0.10625E-29 
c  Pressure     0.10521E-06     488   0.90173E-08   0.98269E-01 0.52675E+03 
c  nu_tilda     0.62868E-05      32   0.15659E-04   0.37464E-06 0.16757E+03 
c  TempC        0.37374E+02      26   0.34918E-03   0.56623E+01 0.27004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6953          10.285          4.5729          4.5729
v  Velocity[Y]            -2.3641          7.3941         0.01487         0.01487
v  Velocity[Z]        -1.448e-014     1.2297e-014     -1.242e-017     -1.242e-017
v  ǁVelocityǁ         0.0014632          10.285          5.1671          5.1671
v  Pressure               -43.475          15.705         -11.505         -11.505
v  nu_tilda           4.1556e-007       0.0042695       0.0014543       0.0014543
v  TempC                       21          73.042          21.884          21.884
v  TurbVisc           2.6726e-014        0.005032       0.0017077       0.0017077
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1616:        0.21080E+01

===============================================================


 INSTANT    0.161700000E+04   TIME STEP NUMBER            1617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82174E-02 0.90357E+00
   Friction velocity        uk    :  0.82174E-02 0.90357E+00
   Dimensionless distance   yplus :  0.66156E-01 0.72744E+01
   Friction thermal sca.    tstar : -0.83277E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49360E-01 0.54275E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92425E-02      33   0.28808E-03   0.43689E+01 0.15960E+03 
c  Velocity[X]                                      0.17451E+01 
c  Velocity[Y]                                      0.26238E+01 
c  Velocity[Z]                                      0.89955E-30 
c  Pressure     0.12525E-06     442   0.99845E-08   0.11743E+00 0.46537E+03 
c  nu_tilda     0.62891E-05      32   0.48985E-05   0.37515E-06 0.16767E+03 
c  TempC        0.37383E+02      27   0.34609E-03   0.43170E+01 0.24850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6922          10.284          4.5729          4.5729
v  Velocity[Y]            -2.3627          7.3654         0.01502         0.01502
v  Velocity[Z]       -1.4619e-014     1.2293e-014    -1.2459e-017    -1.2459e-017
v  ǁVelocityǁ         0.0017039          10.284          5.1669          5.1669
v  Pressure               -43.437          15.691         -11.489         -11.489
v  nu_tilda           4.1369e-007       0.0042695       0.0014548       0.0014548
v  TempC                       21          73.042          21.884          21.884
v  TurbVisc           2.6237e-014        0.005032       0.0017083       0.0017083
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1617:        0.20170E+01

===============================================================


 INSTANT    0.161800000E+04   TIME STEP NUMBER            1618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81534E-02 0.90192E+00
   Friction velocity        uk    :  0.81534E-02 0.90192E+00
   Dimensionless distance   yplus :  0.65641E-01 0.72611E+01
   Friction thermal sca.    tstar : -0.82722E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48975E-01 0.54176E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92447E-02      33   0.30756E-03   0.43460E+01 0.15954E+03 
c  Velocity[X]                                      0.17342E+01 
c  Velocity[Y]                                      0.26118E+01 
c  Velocity[Z]                                      0.98395E-30 
c  Pressure     0.11882E-06     488   0.97412E-08   0.10912E+00 0.36648E+03 
c  nu_tilda     0.62914E-05      32   0.15657E-04   0.37569E-06 0.16777E+03 
c  TempC        0.37392E+02      27   0.32339E-03   0.49077E+01 0.24884E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6891          10.284          4.5729          4.5729
v  Velocity[Y]            -2.3611          7.3803         0.01517         0.01517
v  Velocity[Z]       -1.5494e-014      1.256e-014    -1.2498e-017    -1.2498e-017
v  ǁVelocityǁ         0.0018166          10.284          5.1666          5.1666
v  Pressure               -43.439           15.68         -11.515         -11.515
v  nu_tilda            4.118e-007       0.0042695       0.0014553       0.0014553
v  TempC                       21          73.042          21.884          21.884
v  TurbVisc           2.5768e-014        0.005032       0.0017089       0.0017089
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1618:        0.21090E+01

===============================================================


 INSTANT    0.161900000E+04   TIME STEP NUMBER            1619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12981E-01 0.90323E+00
   Friction velocity        uk    :  0.12981E-01 0.90323E+00
   Dimensionless distance   yplus :  0.10451E+00 0.72716E+01
   Friction thermal sca.    tstar : -0.82115E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77974E-01 0.54255E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92469E-02      33   0.31389E-03   0.43808E+01 0.15982E+03 
c  Velocity[X]                                      0.17687E+01 
c  Velocity[Y]                                      0.26121E+01 
c  Velocity[Z]                                      0.14796E-29 
c  Pressure     0.13115E-06     473   0.94666E-08   0.12376E+00 0.61848E+03 
c  nu_tilda     0.62936E-05      32   0.49002E-05   0.37618E-06 0.16787E+03 
c  TempC        0.37401E+02      26   0.38007E-03   0.44726E+01 0.23285E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6859          10.283          4.5729          4.5729
v  Velocity[Y]            -2.3616          7.3611        0.015321        0.015321
v  Velocity[Z]       -1.6446e-014     1.2867e-014    -1.2533e-017    -1.2533e-017
v  ǁVelocityǁ         0.0020094          10.283          5.1664          5.1664
v  Pressure               -43.396          15.703         -11.485         -11.485
v  nu_tilda           4.0988e-007       0.0042695       0.0014558       0.0014558
v  TempC                       21          73.042          21.885          21.885
v  TurbVisc           2.5299e-014        0.005032       0.0017095       0.0017095
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1619:        0.20660E+01

===============================================================


 INSTANT    0.162000000E+04   TIME STEP NUMBER            1620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65684E-02 0.90234E+00
   Friction velocity        uk    :  0.65684E-02 0.90234E+00
   Dimensionless distance   yplus :  0.52880E-01 0.72645E+01
   Friction thermal sca.    tstar : -0.88660E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39454E-01 0.54201E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92491E-02      33   0.22714E-03   0.43736E+01 0.15990E+03 
c  Velocity[X]                                      0.17415E+01 
c  Velocity[Y]                                      0.26321E+01 
c  Velocity[Z]                                      0.98271E-30 
c  Pressure     0.11033E-06     457   0.98391E-08   0.10298E+00 0.35013E+03 
c  nu_tilda     0.62959E-05      32   0.15646E-04   0.37673E-06 0.16797E+03 
c  TempC        0.37410E+02      27   0.32150E-03   0.52028E+01 0.25230E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6827          10.282          4.5729          4.5729
v  Velocity[Y]            -2.3639          7.3846        0.015473        0.015473
v  Velocity[Z]       -1.5848e-014     1.2482e-014    -1.2561e-017    -1.2561e-017
v  ǁVelocityǁ         0.0021545          10.282          5.1661          5.1661
v  Pressure                 -43.4          15.715         -11.511         -11.511
v  nu_tilda           4.0798e-007       0.0042695       0.0014563       0.0014563
v  TempC                       21          73.041          21.885          21.885
v  TurbVisc            2.483e-014        0.005032       0.0017101       0.0017101
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1620:        0.20460E+01

===============================================================


 INSTANT    0.162100000E+04   TIME STEP NUMBER            1621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94168E-02 0.90375E+00
   Friction velocity        uk    :  0.94168E-02 0.90375E+00
   Dimensionless distance   yplus :  0.75812E-01 0.72758E+01
   Friction thermal sca.    tstar : -0.83022E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56564E-01 0.54286E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92513E-02      33   0.29707E-03   0.43522E+01 0.15982E+03 
c  Velocity[X]                                      0.17288E+01 
c  Velocity[Y]                                      0.26235E+01 
c  Velocity[Z]                                      0.96624E-30 
c  Pressure     0.12604E-06     458   0.99691E-08   0.11557E+00 0.70236E+03 
c  nu_tilda     0.62981E-05      32   0.48926E-05   0.37724E-06 0.16807E+03 
c  TempC        0.37419E+02      27   0.36751E-03   0.51388E+01 0.24481E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6795          10.281          4.5729          4.5729
v  Velocity[Y]            -2.3661          7.3911        0.015626        0.015626
v  Velocity[Z]        -1.637e-014     1.2669e-014    -1.2594e-017    -1.2594e-017
v  ǁVelocityǁ         0.0024177          10.281          5.1659          5.1659
v  Pressure               -43.358          15.782         -11.475         -11.475
v  nu_tilda           4.0614e-007       0.0042695       0.0014568       0.0014568
v  TempC                       21          73.041          21.885          21.885
v  TurbVisc           2.4373e-014        0.005032       0.0017106       0.0017106
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1621:        0.20350E+01

===============================================================


 INSTANT    0.162200000E+04   TIME STEP NUMBER            1622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12411E-01 0.90340E+00
   Friction velocity        uk    :  0.12411E-01 0.90340E+00
   Dimensionless distance   yplus :  0.99917E-01 0.72730E+01
   Friction thermal sca.    tstar : -0.80298E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74549E-01 0.54265E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92535E-02      33   0.30230E-03   0.43974E+01 0.16015E+03 
c  Velocity[X]                                      0.17768E+01 
c  Velocity[Y]                                      0.26206E+01 
c  Velocity[Z]                                      0.98583E-30 
c  Pressure     0.11393E-06     521   0.95410E-08   0.10801E+00 0.96451E+03 
c  nu_tilda     0.63004E-05      32   0.15648E-04   0.37778E-06 0.16816E+03 
c  TempC        0.37428E+02      27   0.35047E-03   0.40387E+01 0.22828E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6762           10.28          4.5729          4.5729
v  Velocity[Y]            -2.3682          7.3625        0.015779        0.015779
v  Velocity[Z]       -1.6111e-014     1.2602e-014    -1.2618e-017    -1.2618e-017
v  ǁVelocityǁ         0.0024686           10.28          5.1656          5.1656
v  Pressure               -43.362          15.619         -11.534         -11.534
v  nu_tilda            4.043e-007       0.0042695       0.0014572       0.0014572
v  TempC                       21          73.041          21.885          21.885
v  TurbVisc           2.3937e-014        0.005032       0.0017112       0.0017112
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1622:        0.21920E+01

===============================================================


 INSTANT    0.162300000E+04   TIME STEP NUMBER            1623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75106E-03 0.90200E+00
   Friction velocity        uk    :  0.75106E-03 0.90200E+00
   Dimensionless distance   yplus :  0.60466E-02 0.72617E+01
   Friction thermal sca.    tstar : -0.82986E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45114E-02 0.54181E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92557E-02      33   0.29564E-03   0.43769E+01 0.16020E+03 
c  Velocity[X]                                      0.17346E+01 
c  Velocity[Y]                                      0.26423E+01 
c  Velocity[Z]                                      0.97140E-30 
c  Pressure     0.10003E-06     522   0.93281E-08   0.93307E-01 0.12218E+04 
c  nu_tilda     0.63027E-05      32   0.48828E-05   0.37828E-06 0.16826E+03 
c  TempC        0.37436E+02      27   0.36076E-03   0.43364E+01 0.21712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6731          10.279          4.5729          4.5729
v  Velocity[Y]            -2.3702          7.3834        0.015933        0.015933
v  Velocity[Z]       -1.6897e-014     1.3157e-014    -1.2652e-017    -1.2652e-017
v  ǁVelocityǁ         0.0022245          10.279          5.1654          5.1654
v  Pressure               -43.321          15.819          -11.47          -11.47
v  nu_tilda           4.0243e-007       0.0042695       0.0014578       0.0014578
v  TempC                       21          73.042          21.885          21.885
v  TurbVisc           2.3507e-014        0.005032       0.0017118       0.0017118
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1623:        0.21790E+01

===============================================================


 INSTANT    0.162400000E+04   TIME STEP NUMBER            1624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68821E-02 0.90286E+00
   Friction velocity        uk    :  0.68821E-02 0.90286E+00
   Dimensionless distance   yplus :  0.55405E-01 0.72686E+01
   Friction thermal sca.    tstar : -0.84993E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41339E-01 0.54232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92580E-02      33   0.31979E-03   0.43815E+01 0.16026E+03 
c  Velocity[X]                                      0.17497E+01 
c  Velocity[Y]                                      0.26318E+01 
c  Velocity[Z]                                      0.10291E-29 
c  Pressure     0.12538E-06     520   0.91432E-08   0.11727E+00 0.11544E+04 
c  nu_tilda     0.63049E-05      32   0.15638E-04   0.37883E-06 0.16836E+03 
c  TempC        0.37445E+02      27   0.30939E-03   0.47730E+01 0.23257E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.67          10.279          4.5729          4.5729
v  Velocity[Y]            -2.3727          7.3548        0.016088        0.016088
v  Velocity[Z]       -1.6974e-014     1.3408e-014    -1.2679e-017    -1.2679e-017
v  ǁVelocityǁ         0.0018586          10.279          5.1651          5.1651
v  Pressure               -43.323          15.613         -11.537         -11.537
v  nu_tilda           4.0057e-007       0.0042695       0.0014582       0.0014582
v  TempC                       21          73.041          21.885          21.885
v  TurbVisc           2.3074e-014        0.005032       0.0017124       0.0017124
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1624:        0.21790E+01

===============================================================


 INSTANT    0.162500000E+04   TIME STEP NUMBER            1625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10414E-01 0.90227E+00
   Friction velocity        uk    :  0.10414E-01 0.90227E+00
   Dimensionless distance   yplus :  0.83839E-01 0.72639E+01
   Friction thermal sca.    tstar : -0.84871E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62553E-01 0.54197E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92602E-02      33   0.25228E-03   0.44000E+01 0.16046E+03 
c  Velocity[X]                                      0.17688E+01 
c  Velocity[Y]                                      0.26311E+01 
c  Velocity[Z]                                      0.10143E-29 
c  Pressure     0.12422E-06     521   0.97215E-08   0.11541E+00 0.12444E+04 
c  nu_tilda     0.63072E-05      32   0.48826E-05   0.37933E-06 0.16846E+03 
c  TempC        0.37454E+02      27   0.41588E-03   0.33765E+01 0.21675E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6667          10.278          4.5729          4.5729
v  Velocity[Y]            -2.3752          7.3839        0.016244        0.016244
v  Velocity[Z]       -1.7166e-014     1.3782e-014    -1.2694e-017    -1.2694e-017
v  ǁVelocityǁ         0.0014412          10.278          5.1649          5.1649
v  Pressure               -43.282          15.818         -11.472         -11.472
v  nu_tilda           3.9877e-007       0.0042695       0.0014588       0.0014588
v  TempC                       21          73.042          21.886          21.886
v  TurbVisc           2.2651e-014        0.005032        0.001713        0.001713
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1625:        0.21860E+01

===============================================================


 INSTANT    0.162600000E+04   TIME STEP NUMBER            1626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80582E-02 0.90372E+00
   Friction velocity        uk    :  0.80582E-02 0.90372E+00
   Dimensionless distance   yplus :  0.64874E-01 0.72756E+01
   Friction thermal sca.    tstar : -0.80538E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48403E-01 0.54284E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92624E-02      33   0.28882E-03   0.43765E+01 0.16048E+03 
c  Velocity[X]                                      0.17262E+01 
c  Velocity[Y]                                      0.26503E+01 
c  Velocity[Z]                                      0.10304E-29 
c  Pressure     0.10748E-06     504   0.91141E-08   0.10034E+00 0.54556E+03 
c  nu_tilda     0.63094E-05      32   0.15631E-04   0.37988E-06 0.16856E+03 
c  TempC        0.37463E+02      27   0.35009E-03   0.56082E+01 0.27756E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6635          10.277          4.5729          4.5729
v  Velocity[Y]            -2.3775          7.3914        0.016401        0.016401
v  Velocity[Z]       -1.6551e-014     1.3784e-014    -1.2715e-017    -1.2715e-017
v  ǁVelocityǁ         0.0010694          10.277          5.1646          5.1646
v  Pressure               -43.285          15.763          -11.51          -11.51
v  nu_tilda           3.9701e-007       0.0042695       0.0014592       0.0014592
v  TempC                       21          73.041          21.886          21.886
v  TurbVisc           2.2246e-014        0.005032       0.0017135       0.0017135
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1626:        0.21450E+01

===============================================================


 INSTANT    0.162700000E+04   TIME STEP NUMBER            1627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13116E-01 0.90328E+00
   Friction velocity        uk    :  0.13116E-01 0.90328E+00
   Dimensionless distance   yplus :  0.10559E+00 0.72721E+01
   Friction thermal sca.    tstar : -0.79141E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78784E-01 0.54258E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92646E-02      33   0.29088E-03   0.44059E+01 0.16063E+03 
c  Velocity[X]                                      0.17628E+01 
c  Velocity[Y]                                      0.26431E+01 
c  Velocity[Z]                                      0.11684E-29 
c  Pressure     0.12628E-06     424   0.94368E-08   0.11821E+00 0.48805E+03 
c  nu_tilda     0.63117E-05      32   0.48718E-05   0.38039E-06 0.16866E+03 
c  TempC        0.37472E+02      27   0.24880E-03   0.49903E+01 0.25251E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6604          10.276          4.5729          4.5729
v  Velocity[Y]            -2.3797          7.3594        0.016558        0.016558
v  Velocity[Z]       -1.6742e-014     1.3353e-014    -1.2734e-017    -1.2734e-017
v  ǁVelocityǁ        0.00059817          10.276          5.1644          5.1644
v  Pressure               -43.243          15.699         -11.501         -11.501
v  nu_tilda           3.9529e-007       0.0042695       0.0014597       0.0014597
v  TempC                       21          73.041          21.886          21.886
v  TurbVisc           2.1855e-014        0.005032       0.0017141       0.0017141
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1627:        0.20260E+01

===============================================================


 INSTANT    0.162800000E+04   TIME STEP NUMBER            1628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64686E-02 0.90186E+00
   Friction velocity        uk    :  0.64686E-02 0.90186E+00
   Dimensionless distance   yplus :  0.52077E-01 0.72606E+01
   Friction thermal sca.    tstar : -0.86762E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38855E-01 0.54172E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92668E-02      33   0.30370E-03   0.44057E+01 0.16074E+03 
c  Velocity[X]                                      0.17662E+01 
c  Velocity[Y]                                      0.26396E+01 
c  Velocity[Z]                                      0.91518E-30 
c  Pressure     0.10475E-06     425   0.92662E-08   0.98064E-01 0.29116E+03 
c  nu_tilda     0.63140E-05      32   0.15636E-04   0.38094E-06 0.16876E+03 
c  TempC        0.37481E+02      27   0.35949E-03   0.28556E+01 0.18812E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6573          10.275          4.5729          4.5729
v  Velocity[Y]            -2.3818          7.3802        0.016716        0.016716
v  Velocity[Z]       -1.6508e-014      1.334e-014    -1.2752e-017    -1.2752e-017
v  ǁVelocityǁ        0.00027268          10.275          5.1642          5.1642
v  Pressure               -43.247          15.751         -11.516         -11.516
v  nu_tilda           3.9358e-007       0.0042695       0.0014602       0.0014602
v  TempC                       21          73.041          21.886          21.886
v  TurbVisc            2.148e-014        0.005032       0.0017147       0.0017147
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1628:        0.22460E+01

===============================================================


 INSTANT    0.162900000E+04   TIME STEP NUMBER            1629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41825E-02 0.90297E+00
   Friction velocity        uk    :  0.41825E-02 0.90297E+00
   Dimensionless distance   yplus :  0.33672E-01 0.72695E+01
   Friction thermal sca.    tstar : -0.87064E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25123E-01 0.54239E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92690E-02      33   0.29302E-03   0.44109E+01 0.16091E+03 
c  Velocity[X]                                      0.17487E+01 
c  Velocity[Y]                                      0.26622E+01 
c  Velocity[Z]                                      0.10425E-29 
c  Pressure     0.12596E-06     458   0.99225E-08   0.11862E+00 0.52949E+03 
c  nu_tilda     0.63162E-05      32   0.48672E-05   0.38144E-06 0.16886E+03 
c  TempC        0.37490E+02      27   0.32255E-03   0.45698E+01 0.23024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6542          10.274          4.5729          4.5729
v  Velocity[Y]            -2.3838          7.3583        0.016875        0.016875
v  Velocity[Z]       -1.7033e-014     1.3803e-014    -1.2775e-017    -1.2775e-017
v  ǁVelocityǁ         0.0002628          10.274          5.1639          5.1639
v  Pressure               -43.207          15.748         -11.494         -11.494
v  nu_tilda           3.9186e-007       0.0042695       0.0014607       0.0014607
v  TempC                       21          73.042          21.886          21.886
v  TurbVisc            2.111e-014        0.005032       0.0017153       0.0017153
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1629:        0.20820E+01

===============================================================


 INSTANT    0.163000000E+04   TIME STEP NUMBER            1630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61838E-02 0.90199E+00
   Friction velocity        uk    :  0.61838E-02 0.90199E+00
   Dimensionless distance   yplus :  0.49784E-01 0.72616E+01
   Friction thermal sca.    tstar : -0.98128E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37144E-01 0.54180E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92713E-02      33   0.25069E-03   0.43988E+01 0.16089E+03 
c  Velocity[X]                                      0.17494E+01 
c  Velocity[Y]                                      0.26494E+01 
c  Velocity[Z]                                      0.10996E-29 
c  Pressure     0.12379E-06     472   0.95295E-08   0.11425E+00 0.38480E+03 
c  nu_tilda     0.63185E-05      32   0.15624E-04   0.38199E-06 0.16896E+03 
c  TempC        0.37498E+02      26   0.40316E-03   0.51043E+01 0.24873E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.651          10.273          4.5729          4.5729
v  Velocity[Y]            -2.3861          7.3782        0.017035        0.017035
v  Velocity[Z]       -1.6357e-014     1.4068e-014    -1.2784e-017    -1.2784e-017
v  ǁVelocityǁ        0.00064262          10.273          5.1637          5.1637
v  Pressure               -43.206          15.736          -11.52          -11.52
v  nu_tilda           3.9016e-007       0.0042695       0.0014612       0.0014612
v  TempC                       21          73.041          21.886          21.886
v  TurbVisc           2.0745e-014        0.005032       0.0017158       0.0017158
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1630:        0.20690E+01

===============================================================


 INSTANT    0.163100000E+04   TIME STEP NUMBER            1631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45464E-02 0.90376E+00
   Friction velocity        uk    :  0.45464E-02 0.90376E+00
   Dimensionless distance   yplus :  0.36602E-01 0.72759E+01
   Friction thermal sca.    tstar : -0.11238E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27309E-01 0.54286E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92735E-02      33   0.31058E-03   0.44041E+01 0.16104E+03 
c  Velocity[X]                                      0.17541E+01 
c  Velocity[Y]                                      0.26500E+01 
c  Velocity[Z]                                      0.11784E-29 
c  Pressure     0.11314E-06     521   0.98763E-08   0.10595E+00 0.86735E+03 
c  nu_tilda     0.63208E-05      32   0.48613E-05   0.38251E-06 0.16906E+03 
c  TempC        0.37507E+02      26   0.31078E-03   0.88832E+01 0.32680E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6479          10.273          4.5729          4.5729
v  Velocity[Y]            -2.3886          7.3917        0.017195        0.017195
v  Velocity[Z]       -1.6034e-014     1.3761e-014    -1.2797e-017    -1.2797e-017
v  ǁVelocityǁ         0.0010624          10.273          5.1634          5.1634
v  Pressure               -43.167          15.857         -11.476         -11.476
v  nu_tilda           3.8844e-007       0.0042695       0.0014617       0.0014617
v  TempC                       21          73.042          21.887          21.887
v  TurbVisc           2.0386e-014        0.005032       0.0017164       0.0017164
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1631:        0.21810E+01

===============================================================


 INSTANT    0.163200000E+04   TIME STEP NUMBER            1632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10191E-01 0.90327E+00
   Friction velocity        uk    :  0.10191E-01 0.90327E+00
   Dimensionless distance   yplus :  0.82048E-01 0.72719E+01
   Friction thermal sca.    tstar : -0.13897E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61217E-01 0.54257E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92757E-02      33   0.28094E-03   0.44314E+01 0.16128E+03 
c  Velocity[X]                                      0.17616E+01 
c  Velocity[Y]                                      0.26699E+01 
c  Velocity[Z]                                      0.76971E-30 
c  Pressure     0.11811E-06     536   0.92764E-08   0.11230E+00 0.10203E+04 
c  nu_tilda     0.63230E-05      32   0.15622E-04   0.38305E-06 0.16916E+03 
c  TempC        0.37516E+02      27   0.36102E-03   0.48674E+01 0.24916E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6446          10.272          4.5729          4.5729
v  Velocity[Y]             -2.391          7.3606        0.017356        0.017356
v  Velocity[Z]       -1.5773e-014     1.3942e-014    -1.2813e-017    -1.2813e-017
v  ǁVelocityǁ         0.0014641          10.272          5.1632          5.1632
v  Pressure               -43.167          15.679         -11.535         -11.535
v  nu_tilda           3.8672e-007       0.0042695       0.0014621       0.0014621
v  TempC                       21          73.041          21.887          21.887
v  TurbVisc           2.0029e-014        0.005032        0.001717        0.001717
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1632:        0.22140E+01

===============================================================


 INSTANT    0.163300000E+04   TIME STEP NUMBER            1633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75202E-02 0.90172E+00
   Friction velocity        uk    :  0.75202E-02 0.90172E+00
   Dimensionless distance   yplus :  0.60543E-01 0.72595E+01
   Friction thermal sca.    tstar : -0.18743E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45172E-01 0.54164E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92779E-02      33   0.29143E-03   0.44141E+01 0.16121E+03 
c  Velocity[X]                                      0.17548E+01 
c  Velocity[Y]                                      0.26593E+01 
c  Velocity[Z]                                      0.95485E-30 
c  Pressure     0.12009E-06     504   0.97193E-08   0.11032E+00 0.98466E+03 
c  nu_tilda     0.63253E-05      32   0.48503E-05   0.38357E-06 0.16925E+03 
c  TempC        0.37525E+02      27   0.37321E-03   0.55978E+01 0.25397E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6413          10.271          4.5729          4.5729
v  Velocity[Y]            -2.3933          7.3773        0.017518        0.017518
v  Velocity[Z]       -1.5841e-014     1.3331e-014     -1.283e-017     -1.283e-017
v  ǁVelocityǁ         0.0019105          10.271           5.163           5.163
v  Pressure                -43.13          15.827         -11.485         -11.485
v  nu_tilda           3.8507e-007       0.0042695       0.0014627       0.0014627
v  TempC                       21          73.042          21.887          21.887
v  TurbVisc           1.9676e-014        0.005032       0.0017176       0.0017176
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1633:        0.21430E+01

===============================================================


 INSTANT    0.163400000E+04   TIME STEP NUMBER            1634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11279E-02 0.90287E+00
   Friction velocity        uk    :  0.11279E-02 0.90287E+00
   Dimensionless distance   yplus :  0.90804E-02 0.72687E+01
   Friction thermal sca.    tstar : -0.12435E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67750E-02 0.54233E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92801E-02      33   0.31135E-03   0.44417E+01 0.16145E+03 
c  Velocity[X]                                      0.17826E+01 
c  Velocity[Y]                                      0.26591E+01 
c  Velocity[Z]                                      0.10723E-29 
c  Pressure     0.11213E-06     522   0.94535E-08   0.10659E+00 0.83880E+03 
c  nu_tilda     0.63276E-05      32   0.15617E-04   0.38412E-06 0.16935E+03 
c  TempC        0.37534E+02      27   0.34811E-03   0.66095E+01 0.28222E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6382           10.27          4.5729          4.5729
v  Velocity[Y]            -2.3954          7.3538        0.017681        0.017681
v  Velocity[Z]       -1.6035e-014     1.3632e-014    -1.2846e-017    -1.2846e-017
v  ǁVelocityǁ         0.0022552           10.27          5.1627          5.1627
v  Pressure               -43.131          15.692         -11.536         -11.536
v  nu_tilda           3.8346e-007       0.0042695       0.0014631       0.0014631
v  TempC                       21          73.042          21.887          21.887
v  TurbVisc           1.9343e-014        0.005032       0.0017181       0.0017181
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1634:        0.21790E+01

===============================================================


 INSTANT    0.163500000E+04   TIME STEP NUMBER            1635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34761E-02 0.90200E+00
   Friction velocity        uk    :  0.34761E-02 0.90200E+00
   Dimensionless distance   yplus :  0.27985E-01 0.72617E+01
   Friction thermal sca.    tstar : -0.20659E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20880E-01 0.54180E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92823E-02      33   0.23850E-03   0.44300E+01 0.16154E+03 
c  Velocity[X]                                      0.17498E+01 
c  Velocity[Y]                                      0.26802E+01 
c  Velocity[Z]                                      0.12276E-29 
c  Pressure     0.10544E-06     522   0.92357E-08   0.98779E-01 0.10918E+04 
c  nu_tilda     0.63298E-05      32   0.48539E-05   0.38463E-06 0.16945E+03 
c  TempC        0.37542E+02      26   0.29391E-03   0.48318E+01 0.24445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6351          10.269          4.5729          4.5729
v  Velocity[Y]            -2.3975          7.3811        0.017845        0.017845
v  Velocity[Z]       -1.6283e-014     1.3876e-014    -1.2859e-017    -1.2859e-017
v  ǁVelocityǁ         0.0019692          10.269          5.1625          5.1625
v  Pressure               -43.089           15.86         -11.479         -11.479
v  nu_tilda           3.8189e-007       0.0042695       0.0014636       0.0014636
v  TempC                       21          73.043          21.887          21.887
v  TurbVisc           1.9022e-014        0.005032       0.0017187       0.0017187
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1635:        0.21590E+01

===============================================================


 INSTANT    0.163600000E+04   TIME STEP NUMBER            1636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92663E-03 0.90342E+00
   Friction velocity        uk    :  0.92663E-03 0.90342E+00
   Dimensionless distance   yplus :  0.74600E-02 0.72732E+01
   Friction thermal sca.    tstar : -0.13417E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55660E-02 0.54266E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92846E-02      33   0.31158E-03   0.44036E+01 0.16147E+03 
c  Velocity[X]                                      0.17352E+01 
c  Velocity[Y]                                      0.26683E+01 
c  Velocity[Z]                                      0.97580E-30 
c  Pressure     0.11678E-06     489   0.98208E-08   0.10822E+00 0.69482E+03 
c  nu_tilda     0.63321E-05      32   0.15606E-04   0.38518E-06 0.16955E+03 
c  TempC        0.37551E+02      27   0.40174E-03   0.42506E+01 0.23120E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.632          10.268          4.5729          4.5729
v  Velocity[Y]            -2.3995           7.385        0.018009        0.018009
v  Velocity[Z]       -1.6083e-014     1.3332e-014    -1.2879e-017    -1.2879e-017
v  ǁVelocityǁ         0.0017734          10.268          5.1623          5.1623
v  Pressure               -43.092           15.77         -11.525         -11.525
v  nu_tilda           3.8034e-007       0.0042695       0.0014641       0.0014641
v  TempC                       21          73.042          21.888          21.888
v  TurbVisc           1.8711e-014        0.005032       0.0017193       0.0017193
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1636:        0.21120E+01

===============================================================


 INSTANT    0.163700000E+04   TIME STEP NUMBER            1637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10653E-01 0.90322E+00
   Friction velocity        uk    :  0.10653E-01 0.90322E+00
   Dimensionless distance   yplus :  0.85761E-01 0.72715E+01
   Friction thermal sca.    tstar : -0.11273E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63988E-01 0.54254E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92868E-02      33   0.30430E-03   0.44592E+01 0.16184E+03 
c  Velocity[X]                                      0.17903E+01 
c  Velocity[Y]                                      0.26689E+01 
c  Velocity[Z]                                      0.87994E-30 
c  Pressure     0.13254E-06     442   0.97804E-08   0.12533E+00 0.52584E+03 
c  nu_tilda     0.63344E-05      32   0.48445E-05   0.38570E-06 0.16965E+03 
c  TempC        0.37560E+02      27   0.37518E-03   0.60284E+01 0.28523E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6287          10.267          4.5729          4.5729
v  Velocity[Y]             -2.402          7.3597        0.018174        0.018174
v  Velocity[Z]       -1.6055e-014     1.3647e-014     -1.289e-017     -1.289e-017
v  ǁVelocityǁ         0.0014901          10.268           5.162           5.162
v  Pressure               -43.051          15.764         -11.503         -11.503
v  nu_tilda           3.7877e-007       0.0042695       0.0014646       0.0014646
v  TempC                       21          73.042          21.888          21.888
v  TurbVisc            1.841e-014        0.005032       0.0017199       0.0017199
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1637:        0.20010E+01

===============================================================


 INSTANT    0.163800000E+04   TIME STEP NUMBER            1638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72828E-02 0.90173E+00
   Friction velocity        uk    :  0.72828E-02 0.90173E+00
   Dimensionless distance   yplus :  0.58632E-01 0.72596E+01
   Friction thermal sca.    tstar : -0.94967E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43746E-01 0.54164E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92890E-02      33   0.28934E-03   0.44374E+01 0.16186E+03 
c  Velocity[X]                                      0.17497E+01 
c  Velocity[Y]                                      0.26877E+01 
c  Velocity[Z]                                      0.95605E-30 
c  Pressure     0.10533E-06     410   0.97671E-08   0.98707E-01 0.30465E+03 
c  nu_tilda     0.63366E-05      32   0.15610E-04   0.38626E-06 0.16975E+03 
c  TempC        0.37569E+02      26   0.33547E-03   0.49262E+01 0.26818E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6256          10.267          4.5729          4.5729
v  Velocity[Y]            -2.4044          7.3765         0.01834         0.01834
v  Velocity[Z]       -1.5876e-014     1.3479e-014     -1.292e-017     -1.292e-017
v  ǁVelocityǁ         0.0013979          10.267          5.1618          5.1618
v  Pressure               -43.054          15.831         -11.516         -11.516
v  nu_tilda            3.772e-007       0.0042695       0.0014651       0.0014651
v  TempC                       21          73.042          21.888          21.888
v  TurbVisc           1.8108e-014        0.005032       0.0017204       0.0017204
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1638:        0.19570E+01

===============================================================


 INSTANT    0.163900000E+04   TIME STEP NUMBER            1639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29408E-02 0.90257E+00
   Friction velocity        uk    :  0.29408E-02 0.90257E+00
   Dimensionless distance   yplus :  0.23675E-01 0.72663E+01
   Friction thermal sca.    tstar : -0.87688E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17664E-01 0.54215E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92912E-02      33   0.29767E-03   0.44390E+01 0.16190E+03 
c  Velocity[X]                                      0.17595E+01 
c  Velocity[Y]                                      0.26795E+01 
c  Velocity[Z]                                      0.10524E-29 
c  Pressure     0.12030E-06     328   0.98980E-08   0.11280E+00 0.56279E+03 
c  nu_tilda     0.63389E-05      32   0.48374E-05   0.38677E-06 0.16985E+03 
c  TempC        0.37578E+02      26   0.36328E-03   0.39556E+01 0.23835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6225          10.266          4.5729          4.5729
v  Velocity[Y]            -2.4067          7.3506        0.018507        0.018507
v  Velocity[Z]       -1.5991e-014     1.4001e-014    -1.2937e-017    -1.2937e-017
v  ǁVelocityǁ         0.0013897          10.266          5.1616          5.1616
v  Pressure               -43.012          15.719         -11.516         -11.516
v  nu_tilda           3.7564e-007       0.0042695       0.0014656       0.0014656
v  TempC                       21          73.043          21.888          21.888
v  TurbVisc            1.781e-014        0.005032        0.001721        0.001721
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1639:        0.17590E+01

===============================================================


 INSTANT    0.164000000E+04   TIME STEP NUMBER            1640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75249E-02 0.90197E+00
   Friction velocity        uk    :  0.75249E-02 0.90197E+00
   Dimensionless distance   yplus :  0.60581E-01 0.72615E+01
   Friction thermal sca.    tstar : -0.85708E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45200E-01 0.54179E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92934E-02      33   0.25807E-03   0.44510E+01 0.16205E+03 
c  Velocity[X]                                      0.17745E+01 
c  Velocity[Y]                                      0.26766E+01 
c  Velocity[Z]                                      0.10318E-29 
c  Pressure     0.10674E-06     442   0.96418E-08   0.10062E+00 0.50954E+03 
c  nu_tilda     0.63412E-05      32   0.15602E-04   0.38732E-06 0.16995E+03 
c  TempC        0.37587E+02      26   0.28422E-03   0.46912E+01 0.25123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6195          10.265          4.5729          4.5729
v  Velocity[Y]            -2.4089          7.3767        0.018674        0.018674
v  Velocity[Z]       -1.5789e-014     1.3812e-014    -1.2953e-017    -1.2953e-017
v  ǁVelocityǁ         0.0015011          10.265          5.1613          5.1613
v  Pressure               -43.013          15.852         -11.511         -11.511
v  nu_tilda           3.7411e-007       0.0042695        0.001466        0.001466
v  TempC                       21          73.043          21.888          21.888
v  TurbVisc           1.7518e-014        0.005032       0.0017216       0.0017216
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1640:        0.19830E+01

===============================================================


 INSTANT    0.164100000E+04   TIME STEP NUMBER            1641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37499E-02 0.90334E+00
   Friction velocity        uk    :  0.37499E-02 0.90334E+00
   Dimensionless distance   yplus :  0.30190E-01 0.72725E+01
   Friction thermal sca.    tstar : -0.78500E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22525E-01 0.54261E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92957E-02      33   0.29314E-03   0.44350E+01 0.16211E+03 
c  Velocity[X]                                      0.17368E+01 
c  Velocity[Y]                                      0.26982E+01 
c  Velocity[Z]                                      0.10860E-29 
c  Pressure     0.10502E-06     457   0.91502E-08   0.98143E-01 0.54947E+03 
c  nu_tilda     0.63435E-05      32   0.48374E-05   0.38784E-06 0.17005E+03 
c  TempC        0.37595E+02      27   0.37450E-03   0.39101E+01 0.21962E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6163          10.264          4.5729          4.5729
v  Velocity[Y]             -2.411          7.3874        0.018843        0.018843
v  Velocity[Z]        -1.554e-014     1.3651e-014    -1.2981e-017    -1.2981e-017
v  ǁVelocityǁ         0.0016491          10.264          5.1611          5.1611
v  Pressure               -42.974          15.875         -11.486         -11.486
v  nu_tilda           3.7258e-007       0.0042695       0.0014666       0.0014666
v  TempC                       21          73.043          21.889          21.889
v  TurbVisc           1.7234e-014        0.005032       0.0017222       0.0017222
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1641:        0.20420E+01

===============================================================


 INSTANT    0.164200000E+04   TIME STEP NUMBER            1642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12237E-01 0.90292E+00
   Friction velocity        uk    :  0.12237E-01 0.90292E+00
   Dimensionless distance   yplus :  0.98518E-01 0.72691E+01
   Friction thermal sca.    tstar : -0.76789E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73506E-01 0.54236E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92979E-02      33   0.30724E-03   0.44668E+01 0.16227E+03 
c  Velocity[X]                                      0.17797E+01 
c  Velocity[Y]                                      0.26871E+01 
c  Velocity[Z]                                      0.95705E-30 
c  Pressure     0.13019E-06     537   0.91723E-08   0.12236E+00 0.94285E+03 
c  nu_tilda     0.63457E-05      32   0.15594E-04   0.38840E-06 0.17015E+03 
c  TempC        0.37604E+02      27   0.33078E-03   0.45185E+01 0.24029E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6131          10.263          4.5729          4.5729
v  Velocity[Y]            -2.4129           7.353        0.019012        0.019012
v  Velocity[Z]       -1.5163e-014     1.3524e-014    -1.2997e-017    -1.2997e-017
v  ǁVelocityǁ         0.0013913          10.263          5.1609          5.1609
v  Pressure               -42.974           15.72         -11.542         -11.542
v  nu_tilda           3.7109e-007       0.0042695        0.001467        0.001467
v  TempC                       21          73.041          21.889          21.889
v  TurbVisc           1.6953e-014        0.005032       0.0017227       0.0017227
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1642:        0.22180E+01

===============================================================


 INSTANT    0.164300000E+04   TIME STEP NUMBER            1643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98573E-02 0.90162E+00
   Friction velocity        uk    :  0.98573E-02 0.90162E+00
   Dimensionless distance   yplus :  0.79358E-01 0.72586E+01
   Friction thermal sca.    tstar : -0.78768E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59210E-01 0.54158E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93001E-02      33   0.30272E-03   0.44725E+01 0.16243E+03 
c  Velocity[X]                                      0.17857E+01 
c  Velocity[Y]                                      0.26867E+01 
c  Velocity[Z]                                      0.94515E-30 
c  Pressure     0.11619E-06     488   0.93292E-08   0.10896E+00 0.10141E+04 
c  nu_tilda     0.63480E-05      32   0.48281E-05   0.38892E-06 0.17025E+03 
c  TempC        0.37613E+02      27   0.32119E-03   0.45172E+01 0.22175E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6098          10.263          4.5729          4.5729
v  Velocity[Y]            -2.4154          7.3766        0.019182        0.019182
v  Velocity[Z]        -1.497e-014     1.3604e-014    -1.3024e-017    -1.3024e-017
v  ǁVelocityǁ         0.0016425          10.263          5.1606          5.1606
v  Pressure               -42.936          15.872         -11.491         -11.491
v  nu_tilda           3.6965e-007       0.0042695       0.0014675       0.0014675
v  TempC                       21          73.042          21.889          21.889
v  TurbVisc           1.6684e-014        0.005032       0.0017233       0.0017233
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1643:        0.21250E+01

===============================================================


 INSTANT    0.164400000E+04   TIME STEP NUMBER            1644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27485E-02 0.90277E+00
   Friction velocity        uk    :  0.27485E-02 0.90277E+00
   Dimensionless distance   yplus :  0.22127E-01 0.72679E+01
   Friction thermal sca.    tstar : -0.82403E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16509E-01 0.54227E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93023E-02      33   0.29050E-03   0.44956E+01 0.16263E+03 
c  Velocity[X]                                      0.17870E+01 
c  Velocity[Y]                                      0.27086E+01 
c  Velocity[Z]                                      0.96797E-30 
c  Pressure     0.13001E-06     506   0.92636E-08   0.12182E+00 0.84237E+03 
c  nu_tilda     0.63503E-05      32   0.15592E-04   0.38948E-06 0.17035E+03 
c  TempC        0.37622E+02      27   0.30125E-03   0.36205E+01 0.21852E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6067          10.262          4.5729          4.5729
v  Velocity[Y]            -2.4178          7.3451        0.019352        0.019352
v  Velocity[Z]       -1.4702e-014     1.3786e-014     -1.305e-017     -1.305e-017
v  ǁVelocityǁ         0.0022074          10.262          5.1604          5.1604
v  Pressure               -42.936          15.739         -11.541         -11.541
v  nu_tilda           3.6821e-007       0.0042695        0.001468        0.001468
v  TempC                       21          73.042          21.889          21.889
v  TurbVisc           1.6425e-014        0.005032       0.0017239       0.0017239
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1644:        0.21460E+01

===============================================================


 INSTANT    0.164500000E+04   TIME STEP NUMBER            1645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88214E-02 0.90196E+00
   Friction velocity        uk    :  0.88214E-02 0.90196E+00
   Dimensionless distance   yplus :  0.71018E-01 0.72614E+01
   Friction thermal sca.    tstar : -0.80121E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52987E-01 0.54178E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93045E-02      33   0.19726E-03   0.44647E+01 0.16254E+03 
c  Velocity[X]                                      0.17657E+01 
c  Velocity[Y]                                      0.26990E+01 
c  Velocity[Z]                                      0.10721E-29 
c  Pressure     0.10424E-06     490   0.97664E-08   0.98342E-01 0.10665E+04 
c  nu_tilda     0.63526E-05      32   0.48193E-05   0.38999E-06 0.17045E+03 
c  TempC        0.37631E+02      27   0.35085E-03   0.37904E+01 0.20704E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6036          10.261          4.5729          4.5729
v  Velocity[Y]            -2.4201          7.3736        0.019524        0.019524
v  Velocity[Z]       -1.4475e-014     1.4172e-014     -1.306e-017     -1.306e-017
v  ǁVelocityǁ         0.0027608          10.261          5.1602          5.1602
v  Pressure               -42.895            15.9         -11.486         -11.486
v  nu_tilda           3.6679e-007       0.0042695       0.0014685       0.0014685
v  TempC                       21          73.043          21.889          21.889
v  TurbVisc           1.6172e-014        0.005032       0.0017244       0.0017244
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1645:        0.21080E+01

===============================================================


 INSTANT    0.164600000E+04   TIME STEP NUMBER            1646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24467E-02 0.90335E+00
   Friction velocity        uk    :  0.24467E-02 0.90335E+00
   Dimensionless distance   yplus :  0.19697E-01 0.72726E+01
   Friction thermal sca.    tstar : -0.76728E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14697E-01 0.54262E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93068E-02      33   0.33581E-03   0.44297E+01 0.16249E+03 
c  Velocity[X]                                      0.17366E+01 
c  Velocity[Y]                                      0.26931E+01 
c  Velocity[Z]                                      0.85602E-30 
c  Pressure     0.10488E-06     505   0.98206E-08   0.98834E-01 0.63630E+03 
c  nu_tilda     0.63548E-05      32   0.15584E-04   0.39056E-06 0.17055E+03 
c  TempC        0.37639E+02      27   0.39560E-03   0.53037E+01 0.24969E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.6005           10.26          4.5729          4.5729
v  Velocity[Y]            -2.4224          7.3838        0.019696        0.019696
v  Velocity[Z]       -1.4158e-014     1.3563e-014      -1.31e-017      -1.31e-017
v  ǁVelocityǁ         0.0026864           10.26            5.16            5.16
v  Pressure               -42.899          15.825          -11.53          -11.53
v  nu_tilda           3.6537e-007       0.0042695       0.0014689       0.0014689
v  TempC                       21          73.042           21.89           21.89
v  TurbVisc           1.5923e-014        0.005032        0.001725        0.001725
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1646:        0.21370E+01

===============================================================


 INSTANT    0.164700000E+04   TIME STEP NUMBER            1647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89092E-02 0.90297E+00
   Friction velocity        uk    :  0.89092E-02 0.90297E+00
   Dimensionless distance   yplus :  0.71726E-01 0.72696E+01
   Friction thermal sca.    tstar : -0.76319E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53515E-01 0.54239E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93090E-02      33   0.30595E-03   0.45275E+01 0.16306E+03 
c  Velocity[X]                                      0.18052E+01 
c  Velocity[Y]                                      0.27223E+01 
c  Velocity[Z]                                      0.11805E-29 
c  Pressure     0.13958E-06     426   0.94215E-08   0.13102E+00 0.48200E+03 
c  nu_tilda     0.63571E-05      32   0.48205E-05   0.39108E-06 0.17065E+03 
c  TempC        0.37648E+02      26   0.30770E-03   0.59659E+01 0.27907E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5972          10.259          4.5729          4.5729
v  Velocity[Y]            -2.4244          7.3511        0.019869        0.019869
v  Velocity[Z]       -1.4731e-014     1.4494e-014    -1.3117e-017    -1.3117e-017
v  ǁVelocityǁ          0.002847          10.259          5.1597          5.1597
v  Pressure               -42.859          15.772         -11.518         -11.518
v  nu_tilda           3.6398e-007       0.0042695       0.0014695       0.0014695
v  TempC                       21          73.042           21.89           21.89
v  TurbVisc           1.5679e-014        0.005032       0.0017256       0.0017256
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1647:        0.19700E+01

===============================================================


 INSTANT    0.164800000E+04   TIME STEP NUMBER            1648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95130E-02 0.90180E+00
   Friction velocity        uk    :  0.95130E-02 0.90180E+00
   Dimensionless distance   yplus :  0.76587E-01 0.72601E+01
   Friction thermal sca.    tstar : -0.83716E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57142E-01 0.54168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93112E-02      33   0.27142E-03   0.44923E+01 0.16298E+03 
c  Velocity[X]                                      0.17846E+01 
c  Velocity[Y]                                      0.27077E+01 
c  Velocity[Z]                                      0.10392E-29 
c  Pressure     0.11025E-06     278   0.88398E-08   0.10324E+00 0.33392E+03 
c  nu_tilda     0.63594E-05      32   0.15582E-04   0.39164E-06 0.17075E+03 
c  TempC        0.37657E+02      26   0.35620E-03   0.52086E+01 0.24688E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.594          10.258          4.5729          4.5729
v  Velocity[Y]            -2.4264           7.372        0.020043        0.020043
v  Velocity[Z]       -1.4891e-014     1.4712e-014    -1.3143e-017    -1.3143e-017
v  ǁVelocityǁ         0.0027132          10.259          5.1595          5.1595
v  Pressure               -42.858          15.849         -11.524         -11.524
v  nu_tilda           3.6256e-007       0.0042695       0.0014699       0.0014699
v  TempC                       21          73.042           21.89           21.89
v  TurbVisc           1.5441e-014        0.005032       0.0017262       0.0017262
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1648:        0.16320E+01

===============================================================


 INSTANT    0.164900000E+04   TIME STEP NUMBER            1649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87295E-02 0.90284E+00
   Friction velocity        uk    :  0.87295E-02 0.90284E+00
   Dimensionless distance   yplus :  0.70278E-01 0.72684E+01
   Friction thermal sca.    tstar : -0.78284E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52435E-01 0.54231E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93134E-02      33   0.32455E-03   0.44653E+01 0.16292E+03 
c  Velocity[X]                                      0.17622E+01 
c  Velocity[Y]                                      0.27031E+01 
c  Velocity[Z]                                      0.10739E-29 
c  Pressure     0.10854E-06     426   0.95093E-08   0.10312E+00 0.46236E+03 
c  nu_tilda     0.63617E-05      32   0.48110E-05   0.39216E-06 0.17085E+03 
c  TempC        0.37666E+02      26   0.37990E-03   0.53663E+01 0.26198E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.591          10.258          4.5729          4.5729
v  Velocity[Y]            -2.4286          7.3532        0.020218        0.020218
v  Velocity[Z]        -1.484e-014     1.4845e-014     -1.317e-017     -1.317e-017
v  ǁVelocityǁ         0.0024814          10.258          5.1593          5.1593
v  Pressure               -42.819          15.818          -11.51          -11.51
v  nu_tilda           3.6112e-007       0.0042695       0.0014704       0.0014704
v  TempC                       21          73.043           21.89           21.89
v  TurbVisc           1.5202e-014        0.005032       0.0017267       0.0017267
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1649:        0.19630E+01

===============================================================


 INSTANT    0.165000000E+04   TIME STEP NUMBER            1650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57956E-02 0.90188E+00
   Friction velocity        uk    :  0.57956E-02 0.90188E+00
   Dimensionless distance   yplus :  0.46658E-01 0.72607E+01
   Friction thermal sca.    tstar : -0.78044E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34812E-01 0.54173E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93157E-02      33   0.22335E-03   0.45022E+01 0.16320E+03 
c  Velocity[X]                                      0.17758E+01 
c  Velocity[Y]                                      0.27264E+01 
c  Velocity[Z]                                      0.12167E-29 
c  Pressure     0.13906E-06     457   0.97734E-08   0.12877E+00 0.31339E+03 
c  nu_tilda     0.63639E-05      32   0.15579E-04   0.39272E-06 0.17095E+03 
c  TempC        0.37674E+02      26   0.30476E-03   0.54719E+01 0.25707E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5879          10.257          4.5729          4.5729
v  Velocity[Y]            -2.4311          7.3712        0.020393        0.020393
v  Velocity[Z]       -1.4693e-014     1.4974e-014    -1.3191e-017    -1.3191e-017
v  ǁVelocityǁ         0.0024549          10.257          5.1591          5.1591
v  Pressure               -42.819          15.826         -11.531         -11.531
v  nu_tilda           3.5966e-007       0.0042695       0.0014709       0.0014709
v  TempC                       21          73.043          21.891          21.891
v  TurbVisc           1.4961e-014        0.005032       0.0017273       0.0017273
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1650:        0.20420E+01

===============================================================


 INSTANT    0.165100000E+04   TIME STEP NUMBER            1651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13074E-02 0.90366E+00
   Friction velocity        uk    :  0.13074E-02 0.90366E+00
   Dimensionless distance   yplus :  0.10525E-01 0.72751E+01
   Friction thermal sca.    tstar : -0.77201E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78529E-02 0.54280E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93179E-02      33   0.29153E-03   0.44633E+01 0.16308E+03 
c  Velocity[X]                                      0.17474E+01 
c  Velocity[Y]                                      0.27158E+01 
c  Velocity[Z]                                      0.13857E-29 
c  Pressure     0.10869E-06     506   0.92663E-08   0.10272E+00 0.96132E+03 
c  nu_tilda     0.63662E-05      32   0.47993E-05   0.39324E-06 0.17105E+03 
c  TempC        0.37683E+02      27   0.34478E-03   0.41899E+01 0.21000E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5848          10.256          4.5729          4.5729
v  Velocity[Y]            -2.4335          7.3839         0.02057         0.02057
v  Velocity[Z]       -1.4504e-014      1.511e-014    -1.3209e-017    -1.3209e-017
v  ǁVelocityǁ         0.0023891          10.256          5.1588          5.1588
v  Pressure               -42.777          15.962         -11.481         -11.481
v  nu_tilda           3.5819e-007       0.0042695       0.0014714       0.0014714
v  TempC                       21          73.043          21.891          21.891
v  TurbVisc           1.4721e-014        0.005032       0.0017279       0.0017279
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1651:        0.21480E+01

===============================================================


 INSTANT    0.165200000E+04   TIME STEP NUMBER            1652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13277E-01 0.90294E+00
   Friction velocity        uk    :  0.13277E-01 0.90294E+00
   Dimensionless distance   yplus :  0.10689E+00 0.72693E+01
   Friction thermal sca.    tstar : -0.79591E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79753E-01 0.54237E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93201E-02      33   0.32645E-03   0.44921E+01 0.16330E+03 
c  Velocity[X]                                      0.17811E+01 
c  Velocity[Y]                                      0.27109E+01 
c  Velocity[Z]                                      0.10869E-29 
c  Pressure     0.11493E-06     536   0.93268E-08   0.10931E+00 0.11585E+04 
c  nu_tilda     0.63685E-05      32   0.15571E-04   0.39381E-06 0.17115E+03 
c  TempC        0.37692E+02      26   0.36186E-03   0.45492E+01 0.24441E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5816          10.255          4.5729          4.5729
v  Velocity[Y]            -2.4357          7.3556        0.020747        0.020747
v  Velocity[Z]       -1.4192e-014     1.4741e-014    -1.3237e-017    -1.3237e-017
v  ǁVelocityǁ         0.0018252          10.255          5.1586          5.1586
v  Pressure               -42.779          15.755         -11.548         -11.548
v  nu_tilda           3.5671e-007       0.0042695       0.0014718       0.0014718
v  TempC                       21          73.042          21.891          21.891
v  TurbVisc           1.4482e-014        0.005032       0.0017285       0.0017285
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1652:        0.22350E+01

===============================================================


 INSTANT    0.165300000E+04   TIME STEP NUMBER            1653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82853E-02 0.90148E+00
   Friction velocity        uk    :  0.82853E-02 0.90148E+00
   Dimensionless distance   yplus :  0.66703E-01 0.72575E+01
   Friction thermal sca.    tstar : -0.79371E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49768E-01 0.54149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93223E-02      33   0.29285E-03   0.45289E+01 0.16359E+03 
c  Velocity[X]                                      0.17929E+01 
c  Velocity[Y]                                      0.27360E+01 
c  Velocity[Z]                                      0.99506E-30 
c  Pressure     0.12421E-06     522   0.93292E-08   0.11554E+00 0.10949E+04 
c  nu_tilda     0.63708E-05      32   0.47971E-05   0.39434E-06 0.17125E+03 
c  TempC        0.37701E+02      27   0.36336E-03   0.45319E+01 0.24168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5784          10.254          4.5729          4.5729
v  Velocity[Y]            -2.4378          7.3708        0.020924        0.020924
v  Velocity[Z]        -1.397e-014     1.4935e-014    -1.3259e-017    -1.3259e-017
v  ǁVelocityǁ         0.0013768          10.254          5.1584          5.1584
v  Pressure               -42.739          15.926         -11.492         -11.492
v  nu_tilda           3.5525e-007       0.0042695       0.0014724       0.0014724
v  TempC                       21          73.043          21.891          21.891
v  TurbVisc           1.4245e-014        0.005032        0.001729        0.001729
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1653:        0.21850E+01

===============================================================


 INSTANT    0.165400000E+04   TIME STEP NUMBER            1654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93783E-02 0.90255E+00
   Friction velocity        uk    :  0.93783E-02 0.90255E+00
   Dimensionless distance   yplus :  0.75502E-01 0.72662E+01
   Friction thermal sca.    tstar : -0.75809E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56333E-01 0.54214E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93246E-02      33   0.26390E-03   0.45010E+01 0.16352E+03 
c  Velocity[X]                                      0.17789E+01 
c  Velocity[Y]                                      0.27221E+01 
c  Velocity[Z]                                      0.11616E-29 
c  Pressure     0.98804E-07     521   0.95215E-08   0.94233E-01 0.95130E+03 
c  nu_tilda     0.63731E-05      32   0.15568E-04   0.39490E-06 0.17135E+03 
c  TempC        0.37710E+02      26   0.30445E-03   0.44286E+01 0.23828E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5753          10.254          4.5729          4.5729
v  Velocity[Y]            -2.4398          7.3464        0.021103        0.021103
v  Velocity[Z]       -1.3775e-014     1.4915e-014    -1.3291e-017    -1.3291e-017
v  ǁVelocityǁ         0.0011173          10.254          5.1582          5.1582
v  Pressure               -42.741          15.771         -11.549         -11.549
v  nu_tilda           3.5379e-007       0.0042695       0.0014728       0.0014728
v  TempC                       21          73.043          21.891          21.891
v  TurbVisc           1.4012e-014        0.005032       0.0017296       0.0017296
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1654:        0.21850E+01

===============================================================


 INSTANT    0.165500000E+04   TIME STEP NUMBER            1655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11715E-01 0.90177E+00
   Friction velocity        uk    :  0.11715E-01 0.90177E+00
   Dimensionless distance   yplus :  0.94312E-01 0.72598E+01
   Friction thermal sca.    tstar : -0.77657E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70368E-01 0.54167E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93268E-02      33   0.26908E-03   0.44838E+01 0.16351E+03 
c  Velocity[X]                                      0.17634E+01 
c  Velocity[Y]                                      0.27204E+01 
c  Velocity[Z]                                      0.10874E-29 
c  Pressure     0.10645E-06     520   0.91975E-08   0.10100E+00 0.11984E+04 
c  nu_tilda     0.63753E-05      32   0.47847E-05   0.39542E-06 0.17145E+03 
c  TempC        0.37718E+02      26   0.27614E-03   0.43497E+01 0.23226E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5722          10.253          4.5729          4.5729
v  Velocity[Y]            -2.4418          7.3765        0.021283        0.021283
v  Velocity[Z]       -1.3631e-014     1.5413e-014    -1.3306e-017    -1.3306e-017
v  ǁVelocityǁ         0.0012723          10.253           5.158           5.158
v  Pressure               -42.701          15.963         -11.487         -11.487
v  nu_tilda           3.5232e-007       0.0042695       0.0014733       0.0014733
v  TempC                       21          73.043          21.892          21.892
v  TurbVisc           1.3783e-014        0.005032       0.0017302       0.0017302
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1655:        0.22230E+01

===============================================================


 INSTANT    0.165600000E+04   TIME STEP NUMBER            1656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56471E-02 0.90309E+00
   Friction velocity        uk    :  0.56471E-02 0.90309E+00
   Dimensionless distance   yplus :  0.45463E-01 0.72705E+01
   Friction thermal sca.    tstar : -0.80120E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33920E-01 0.54246E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93290E-02      33   0.31438E-03   0.45058E+01 0.16374E+03 
c  Velocity[X]                                      0.17628E+01 
c  Velocity[Y]                                      0.27429E+01 
c  Velocity[Z]                                      0.88651E-30 
c  Pressure     0.13337E-06     473   0.99146E-08   0.12371E+00 0.64743E+03 
c  nu_tilda     0.63776E-05      32   0.15561E-04   0.39599E-06 0.17155E+03 
c  TempC        0.37727E+02      27   0.46228E-03   0.45392E+01 0.24344E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5691          10.252          4.5729          4.5729
v  Velocity[Y]            -2.4443          7.3774        0.021463        0.021463
v  Velocity[Z]       -1.3445e-014     1.5513e-014     -1.334e-017     -1.334e-017
v  ǁVelocityǁ         0.0014522          10.252          5.1578          5.1578
v  Pressure               -42.699          15.877         -11.528         -11.528
v  nu_tilda           3.5086e-007       0.0042695       0.0014738       0.0014738
v  TempC                       21          73.042          21.892          21.892
v  TurbVisc           1.3556e-014        0.005032       0.0017307       0.0017307
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1656:        0.20760E+01

===============================================================


 INSTANT    0.165700000E+04   TIME STEP NUMBER            1657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51025E-02 0.90288E+00
   Friction velocity        uk    :  0.51025E-02 0.90288E+00
   Dimensionless distance   yplus :  0.41079E-01 0.72688E+01
   Friction thermal sca.    tstar : -0.76501E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30649E-01 0.54233E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93312E-02      33   0.29570E-03   0.45425E+01 0.16400E+03 
c  Velocity[X]                                      0.18080E+01 
c  Velocity[Y]                                      0.27344E+01 
c  Velocity[Z]                                      0.11104E-29 
c  Pressure     0.12447E-06     440   0.96150E-08   0.11914E+00 0.47219E+03 
c  nu_tilda     0.63799E-05      32   0.47832E-05   0.39652E-06 0.17165E+03 
c  TempC        0.37736E+02      27   0.33707E-03   0.68465E+01 0.30908E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5659          10.251          4.5729          4.5729
v  Velocity[Y]            -2.4467          7.3519        0.021644        0.021644
v  Velocity[Z]       -1.2775e-014     1.5633e-014    -1.3368e-017    -1.3368e-017
v  ǁVelocityǁ         0.0014687          10.251          5.1575          5.1575
v  Pressure               -42.661          15.859         -11.511         -11.511
v  nu_tilda           3.4945e-007       0.0042695       0.0014743       0.0014743
v  TempC                       21          73.042          21.892          21.892
v  TurbVisc           1.3333e-014        0.005032       0.0017313       0.0017313
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1657:        0.20010E+01

===============================================================


 INSTANT    0.165800000E+04   TIME STEP NUMBER            1658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55559E-02 0.90149E+00
   Friction velocity        uk    :  0.55559E-02 0.90149E+00
   Dimensionless distance   yplus :  0.44729E-01 0.72576E+01
   Friction thermal sca.    tstar : -0.76839E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33373E-01 0.54150E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93335E-02      33   0.30535E-03   0.45095E+01 0.16392E+03 
c  Velocity[X]                                      0.17820E+01 
c  Velocity[Y]                                      0.27275E+01 
c  Velocity[Z]                                      0.10912E-29 
c  Pressure     0.96572E-07     394   0.94375E-08   0.90979E-01 0.28945E+03 
c  nu_tilda     0.63822E-05      32   0.15556E-04   0.39709E-06 0.17175E+03 
c  TempC        0.37745E+02      27   0.37179E-03   0.53984E+01 0.25249E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5627           10.25          4.5729          4.5729
v  Velocity[Y]             -2.449          7.3713        0.021826        0.021826
v  Velocity[Z]       -1.2639e-014     1.5495e-014    -1.3407e-017    -1.3407e-017
v  ǁVelocityǁ           0.00164           10.25          5.1573          5.1573
v  Pressure               -42.661          15.914         -11.524         -11.524
v  nu_tilda           3.4804e-007       0.0042695       0.0014747       0.0014747
v  TempC                       21          73.042          21.892          21.892
v  TurbVisc           1.3119e-014        0.005032       0.0017319       0.0017319
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1658:        0.21200E+01

===============================================================


 INSTANT    0.165900000E+04   TIME STEP NUMBER            1659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10009E-01 0.90250E+00
   Friction velocity        uk    :  0.10009E-01 0.90250E+00
   Dimensionless distance   yplus :  0.80580E-01 0.72657E+01
   Friction thermal sca.    tstar : -0.78755E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60122E-01 0.54211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93357E-02      33   0.31068E-03   0.45331E+01 0.16410E+03 
c  Velocity[X]                                      0.17877E+01 
c  Velocity[Y]                                      0.27455E+01 
c  Velocity[Z]                                      0.11437E-29 
c  Pressure     0.11956E-06     313   0.98678E-08   0.11286E+00 0.47687E+03 
c  nu_tilda     0.63845E-05      32   0.47790E-05   0.39762E-06 0.17185E+03 
c  TempC        0.37753E+02      26   0.35249E-03   0.61666E+01 0.27501E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5597          10.249          4.5729          4.5729
v  Velocity[Y]            -2.4511          7.3446        0.022009        0.022009
v  Velocity[Z]         -1.26e-014     1.5533e-014    -1.3434e-017    -1.3434e-017
v  ǁVelocityǁ         0.0020455          10.249          5.1571          5.1571
v  Pressure               -42.623          15.837          -11.52          -11.52
v  nu_tilda           3.4666e-007       0.0042695       0.0014752       0.0014752
v  TempC                       21          73.043          21.893          21.893
v  TurbVisc           1.2909e-014        0.005032       0.0017324       0.0017324
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1659:        0.18550E+01

===============================================================


 INSTANT    0.166000000E+04   TIME STEP NUMBER            1660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42698E-02 0.90179E+00
   Friction velocity        uk    :  0.42698E-02 0.90179E+00
   Dimensionless distance   yplus :  0.34375E-01 0.72600E+01
   Friction thermal sca.    tstar : -0.90351E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25647E-01 0.54168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93379E-02      33   0.20608E-03   0.45419E+01 0.16423E+03 
c  Velocity[X]                                      0.18022E+01 
c  Velocity[Y]                                      0.27396E+01 
c  Velocity[Z]                                      0.10790E-29 
c  Pressure     0.10353E-06     360   0.91468E-08   0.97459E-01 0.31913E+03 
c  nu_tilda     0.63868E-05      32   0.15553E-04   0.39818E-06 0.17195E+03 
c  TempC        0.37762E+02      26   0.35334E-03   0.55153E+01 0.26168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5567          10.248          4.5729          4.5729
v  Velocity[Y]            -2.4531          7.3696        0.022192        0.022192
v  Velocity[Z]       -1.2023e-014       1.55e-014    -1.3469e-017    -1.3469e-017
v  ǁVelocityǁ         0.0023777          10.248          5.1569          5.1569
v  Pressure               -42.623          15.909         -11.528         -11.528
v  nu_tilda           3.4529e-007       0.0042695       0.0014757       0.0014757
v  TempC                       21          73.043          21.893          21.893
v  TurbVisc           1.2705e-014        0.005032        0.001733        0.001733
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1660:        0.18040E+01

===============================================================


 INSTANT    0.166100000E+04   TIME STEP NUMBER            1661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81281E-02 0.90321E+00
   Friction velocity        uk    :  0.81281E-02 0.90321E+00
   Dimensionless distance   yplus :  0.65436E-01 0.72714E+01
   Friction thermal sca.    tstar : -0.10489E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48823E-01 0.54253E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93401E-02      33   0.29853E-03   0.44891E+01 0.16406E+03 
c  Velocity[X]                                      0.17527E+01 
c  Velocity[Y]                                      0.27364E+01 
c  Velocity[Z]                                      0.13635E-29 
c  Pressure     0.94453E-07     504   0.92552E-08   0.89245E-01 0.77247E+03 
c  nu_tilda     0.63891E-05      32   0.47652E-05   0.39871E-06 0.17205E+03 
c  TempC        0.37771E+02      27   0.35914E-03   0.47208E+01 0.24161E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5535          10.248          4.5729          4.5729
v  Velocity[Y]             -2.455           7.383        0.022376        0.022376
v  Velocity[Z]       -1.2368e-014     1.5491e-014    -1.3507e-017    -1.3507e-017
v  ǁVelocityǁ         0.0027998          10.248          5.1567          5.1567
v  Pressure                -42.58          15.989         -11.488         -11.488
v  nu_tilda           3.4394e-007       0.0042695       0.0014762       0.0014762
v  TempC                       21          73.043          21.893          21.893
v  TurbVisc           1.2505e-014        0.005032       0.0017336       0.0017336
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1661:        0.21450E+01

===============================================================


 INSTANT    0.166200000E+04   TIME STEP NUMBER            1662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99988E-02 0.90271E+00
   Friction velocity        uk    :  0.99988E-02 0.90271E+00
   Dimensionless distance   yplus :  0.80497E-01 0.72674E+01
   Friction thermal sca.    tstar : -0.14403E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60060E-01 0.54223E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93424E-02      33   0.29153E-03   0.45366E+01 0.16437E+03 
c  Velocity[X]                                      0.17854E+01 
c  Velocity[Y]                                      0.27512E+01 
c  Velocity[Z]                                      0.11756E-29 
c  Pressure     0.11350E-06     521   0.98277E-08   0.10818E+00 0.11164E+04 
c  nu_tilda     0.63913E-05      32   0.15547E-04   0.39929E-06 0.17215E+03 
c  TempC        0.37780E+02      27   0.26740E-03   0.48152E+01 0.24781E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5504          10.247          4.5729          4.5729
v  Velocity[Y]            -2.4575          7.3471        0.022562        0.022562
v  Velocity[Z]       -1.2009e-014     1.5198e-014    -1.3548e-017    -1.3548e-017
v  ǁVelocityǁ         0.0025962          10.247          5.1565          5.1565
v  Pressure               -42.581          15.798         -11.553         -11.553
v  nu_tilda           3.4261e-007       0.0042695       0.0014766       0.0014766
v  TempC                       21          73.042          21.893          21.893
v  TurbVisc            1.231e-014        0.005032       0.0017341       0.0017341
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1662:        0.21900E+01

===============================================================


 INSTANT    0.166300000E+04   TIME STEP NUMBER            1663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26470E-02 0.90127E+00
   Friction velocity        uk    :  0.26470E-02 0.90127E+00
   Dimensionless distance   yplus :  0.21310E-01 0.72558E+01
   Friction thermal sca.    tstar : -0.32741E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15899E-01 0.54137E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93446E-02      33   0.30384E-03   0.45188E+01 0.16439E+03 
c  Velocity[X]                                      0.17712E+01 
c  Velocity[Y]                                      0.27476E+01 
c  Velocity[Z]                                      0.11187E-29 
c  Pressure     0.97045E-07     521   0.97311E-08   0.91572E-01 0.12089E+04 
c  nu_tilda     0.63936E-05      32   0.47679E-05   0.39981E-06 0.17225E+03 
c  TempC        0.37788E+02      26   0.39722E-03   0.45063E+01 0.22632E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5473          10.246          4.5729          4.5729
v  Velocity[Y]            -2.4599          7.3692        0.022747        0.022747
v  Velocity[Z]       -1.1323e-014     1.5023e-014    -1.3588e-017    -1.3588e-017
v  ǁVelocityǁ         0.0029092          10.246          5.1563          5.1563
v  Pressure               -42.541          15.991         -11.491         -11.491
v  nu_tilda            3.413e-007       0.0042695       0.0014772       0.0014772
v  TempC                       21          73.043          21.894          21.894
v  TurbVisc           1.2122e-014        0.005032       0.0017347       0.0017347
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1663:        0.21890E+01

===============================================================


 INSTANT    0.166400000E+04   TIME STEP NUMBER            1664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88314E-02 0.90230E+00
   Friction velocity        uk    :  0.88314E-02 0.90230E+00
   Dimensionless distance   yplus :  0.71099E-01 0.72642E+01
   Friction thermal sca.    tstar : -0.16141E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53048E-01 0.54199E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93468E-02      33   0.32308E-03   0.45611E+01 0.16468E+03 
c  Velocity[X]                                      0.18133E+01 
c  Velocity[Y]                                      0.27478E+01 
c  Velocity[Z]                                      0.10466E-29 
c  Pressure     0.12654E-06     504   0.97277E-08   0.12044E+00 0.10054E+04 
c  nu_tilda     0.63959E-05      32   0.15538E-04   0.40039E-06 0.17235E+03 
c  TempC        0.37797E+02      26   0.31909E-03   0.53240E+01 0.26730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5441          10.245          4.5729          4.5729
v  Velocity[Y]            -2.4622          7.3466        0.022934        0.022934
v  Velocity[Z]       -1.1696e-014     1.4723e-014     -1.363e-017     -1.363e-017
v  ǁVelocityǁ         0.0026761          10.245          5.1561          5.1561
v  Pressure               -42.543          15.825         -11.551         -11.551
v  nu_tilda           3.3994e-007       0.0042695       0.0014776       0.0014776
v  TempC                       21          73.043          21.894          21.894
v  TurbVisc           1.1937e-014        0.005032       0.0017353       0.0017353
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1664:        0.21500E+01

===============================================================


 INSTANT    0.166500000E+04   TIME STEP NUMBER            1665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72621E-02 0.90144E+00
   Friction velocity        uk    :  0.72621E-02 0.90144E+00
   Dimensionless distance   yplus :  0.58465E-01 0.72572E+01
   Friction thermal sca.    tstar : -0.11231E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43621E-01 0.54147E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93490E-02      33   0.22459E-03   0.45746E+01 0.16481E+03 
c  Velocity[X]                                      0.18055E+01 
c  Velocity[Y]                                      0.27691E+01 
c  Velocity[Z]                                      0.10255E-29 
c  Pressure     0.12097E-06     488   0.96880E-08   0.11282E+00 0.99681E+03 
c  nu_tilda     0.63982E-05      32   0.47594E-05   0.40091E-06 0.17245E+03 
c  TempC        0.37806E+02      26   0.35471E-03   0.44614E+01 0.22764E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5409          10.244          4.5729          4.5729
v  Velocity[Y]            -2.4643          7.3667        0.023121        0.023121
v  Velocity[Z]       -1.1792e-014     1.4484e-014    -1.3659e-017    -1.3659e-017
v  ǁVelocityǁ         0.0027583          10.244          5.1559          5.1559
v  Pressure               -42.503          15.968         -11.499         -11.499
v  nu_tilda           3.3855e-007       0.0042695       0.0014781       0.0014781
v  TempC                       21          73.043          21.894          21.894
v  TurbVisc           1.1749e-014        0.005032       0.0017358       0.0017358
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1665:        0.21170E+01

===============================================================


 INSTANT    0.166600000E+04   TIME STEP NUMBER            1666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10955E-01 0.90306E+00
   Friction velocity        uk    :  0.10955E-01 0.90306E+00
   Dimensionless distance   yplus :  0.88198E-01 0.72702E+01
   Friction thermal sca.    tstar : -0.88983E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65805E-01 0.54244E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93513E-02      33   0.28500E-03   0.45211E+01 0.16462E+03 
c  Velocity[X]                                      0.17641E+01 
c  Velocity[Y]                                      0.27570E+01 
c  Velocity[Z]                                      0.12218E-29 
c  Pressure     0.10030E-06     472   0.95503E-08   0.95362E-01 0.38206E+03 
c  nu_tilda     0.64005E-05      32   0.15536E-04   0.40149E-06 0.17255E+03 
c  TempC        0.37814E+02      27   0.36089E-03   0.62055E+01 0.27292E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5379          10.243          4.5729          4.5729
v  Velocity[Y]            -2.4663          7.3763         0.02331         0.02331
v  Velocity[Z]       -1.2315e-014     1.4088e-014    -1.3711e-017    -1.3711e-017
v  ǁVelocityǁ         0.0026083          10.243          5.1557          5.1557
v  Pressure                 -42.5          15.953         -11.524         -11.524
v  nu_tilda           3.3713e-007       0.0042695       0.0014786       0.0014786
v  TempC                       21          73.043          21.894          21.894
v  TurbVisc           1.1557e-014        0.005032       0.0017364       0.0017364
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1666:        0.20710E+01

===============================================================


 INSTANT    0.166700000E+04   TIME STEP NUMBER            1667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63101E-02 0.90263E+00
   Friction velocity        uk    :  0.63101E-02 0.90263E+00
   Dimensionless distance   yplus :  0.50801E-01 0.72668E+01
   Friction thermal sca.    tstar : -0.77618E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37903E-01 0.54218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93535E-02      33   0.32619E-03   0.45443E+01 0.16485E+03 
c  Velocity[X]                                      0.17900E+01 
c  Velocity[Y]                                      0.27543E+01 
c  Velocity[Z]                                      0.10331E-29 
c  Pressure     0.11525E-06     440   0.90907E-08   0.11074E+00 0.45995E+03 
c  nu_tilda     0.64028E-05      32   0.47456E-05   0.40202E-06 0.17265E+03 
c  TempC        0.37823E+02      27   0.35156E-03   0.56615E+01 0.26744E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5347          10.242          4.5729          4.5729
v  Velocity[Y]            -2.4682          7.3509        0.023499        0.023499
v  Velocity[Z]       -1.2072e-014     1.3652e-014    -1.3748e-017    -1.3748e-017
v  ǁVelocityǁ         0.0026796          10.242          5.1555          5.1555
v  Pressure               -42.461          15.909         -11.513         -11.513
v  nu_tilda           3.3571e-007       0.0042695       0.0014791       0.0014791
v  TempC                       21          73.042          21.894          21.894
v  TurbVisc           1.1364e-014        0.005032        0.001737        0.001737
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1667:        0.20010E+01

===============================================================


 INSTANT    0.166800000E+04   TIME STEP NUMBER            1668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85088E-02 0.90109E+00
   Friction velocity        uk    :  0.85088E-02 0.90109E+00
   Dimensionless distance   yplus :  0.68502E-01 0.72544E+01
   Friction thermal sca.    tstar : -0.80166E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51110E-01 0.54126E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93557E-02      33   0.29507E-03   0.45722E+01 0.16510E+03 
c  Velocity[X]                                      0.17945E+01 
c  Velocity[Y]                                      0.27777E+01 
c  Velocity[Z]                                      0.95650E-30 
c  Pressure     0.12526E-06     442   0.99516E-08   0.11716E+00 0.29749E+03 
c  nu_tilda     0.64051E-05      32   0.15534E-04   0.40260E-06 0.17275E+03 
c  TempC        0.37832E+02      27   0.31715E-03   0.52336E+01 0.25916E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5317          10.242          4.5729          4.5729
v  Velocity[Y]            -2.4705          7.3691        0.023689        0.023689
v  Velocity[Z]       -1.2079e-014     1.3268e-014    -1.3791e-017    -1.3791e-017
v  ǁVelocityǁ         0.0026097          10.242          5.1553          5.1553
v  Pressure               -42.463          15.945         -11.531         -11.531
v  nu_tilda            3.343e-007       0.0042695       0.0014795       0.0014795
v  TempC                       21          73.043          21.895          21.895
v  TurbVisc           1.1175e-014        0.005032       0.0017375       0.0017375
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1668:        0.19890E+01

===============================================================


 INSTANT    0.166900000E+04   TIME STEP NUMBER            1669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12170E-01 0.90223E+00
   Friction velocity        uk    :  0.12170E-01 0.90223E+00
   Dimensionless distance   yplus :  0.97974E-01 0.72636E+01
   Friction thermal sca.    tstar : -0.75336E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73099E-01 0.54194E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93580E-02      33   0.27552E-03   0.45659E+01 0.16507E+03 
c  Velocity[X]                                      0.17992E+01 
c  Velocity[Y]                                      0.27667E+01 
c  Velocity[Z]                                      0.13332E-29 
c  Pressure     0.12102E-06     456   0.93953E-08   0.11438E+00 0.49319E+03 
c  nu_tilda     0.64074E-05      32   0.47492E-05   0.40313E-06 0.17285E+03 
c  TempC        0.37841E+02      26   0.25529E-03   0.51545E+01 0.24436E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5284          10.241          4.5729          4.5729
v  Velocity[Y]             -2.473           7.343         0.02388         0.02388
v  Velocity[Z]       -1.3347e-014     1.2952e-014    -1.3831e-017    -1.3831e-017
v  ǁVelocityǁ         0.0022185          10.241          5.1551          5.1551
v  Pressure               -42.421          15.905         -11.516         -11.516
v  nu_tilda           3.3287e-007       0.0042695         0.00148         0.00148
v  TempC                       21          73.043          21.895          21.895
v  TurbVisc           1.0988e-014        0.005032       0.0017381       0.0017381
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1669:        0.20350E+01

===============================================================


 INSTANT    0.167000000E+04   TIME STEP NUMBER            1670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44731E-02 0.90140E+00
   Friction velocity        uk    :  0.44731E-02 0.90140E+00
   Dimensionless distance   yplus :  0.36011E-01 0.72569E+01
   Friction thermal sca.    tstar : -0.75448E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26868E-01 0.54144E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93602E-02      33   0.27094E-03   0.45490E+01 0.16507E+03 
c  Velocity[X]                                      0.17870E+01 
c  Velocity[Y]                                      0.27620E+01 
c  Velocity[Z]                                      0.10578E-29 
c  Pressure     0.10348E-06     410   0.93312E-08   0.98489E-01 0.31094E+03 
c  nu_tilda     0.64096E-05      32   0.15524E-04   0.40370E-06 0.17295E+03 
c  TempC        0.37849E+02      27   0.37059E-03   0.33377E+01 0.19946E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5255           10.24          4.5729          4.5729
v  Velocity[Y]            -2.4753          7.3685        0.024071        0.024071
v  Velocity[Z]       -1.2869e-014      1.354e-014    -1.3871e-017    -1.3871e-017
v  ǁVelocityǁ         0.0018299           10.24          5.1549          5.1549
v  Pressure               -42.424          15.968         -11.529         -11.529
v  nu_tilda           3.3144e-007       0.0042695       0.0014805       0.0014805
v  TempC                       21          73.043          21.895          21.895
v  TurbVisc           1.0802e-014        0.005032       0.0017387       0.0017387
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1670:        0.19510E+01

===============================================================


 INSTANT    0.167100000E+04   TIME STEP NUMBER            1671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71131E-02 0.90280E+00
   Friction velocity        uk    :  0.71131E-02 0.90280E+00
   Dimensionless distance   yplus :  0.57266E-01 0.72681E+01
   Friction thermal sca.    tstar : -0.73774E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42727E-01 0.54228E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93624E-02      33   0.32405E-03   0.45584E+01 0.16525E+03 
c  Velocity[X]                                      0.17724E+01 
c  Velocity[Y]                                      0.27860E+01 
c  Velocity[Z]                                      0.10808E-29 
c  Pressure     0.11815E-06     489   0.95010E-08   0.11099E+00 0.66496E+03 
c  nu_tilda     0.64119E-05      32   0.47380E-05   0.40424E-06 0.17305E+03 
c  TempC        0.37858E+02      27   0.30100E-03   0.45013E+01 0.23007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5224          10.239          4.5729          4.5729
v  Velocity[Y]            -2.4774          7.3733        0.024263        0.024263
v  Velocity[Z]       -1.4012e-014     1.4392e-014     -1.391e-017     -1.391e-017
v  ǁVelocityǁ         0.0015149          10.239          5.1547          5.1547
v  Pressure               -42.382          16.022         -11.496         -11.496
v  nu_tilda              3.3e-007       0.0042695        0.001481        0.001481
v  TempC                       21          73.043          21.895          21.895
v  TurbVisc           1.0616e-014        0.005032       0.0017392       0.0017392
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1671:        0.21780E+01

===============================================================


 INSTANT    0.167200000E+04   TIME STEP NUMBER            1672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38240E-02 0.90240E+00
   Friction velocity        uk    :  0.38240E-02 0.90240E+00
   Dimensionless distance   yplus :  0.30786E-01 0.72650E+01
   Friction thermal sca.    tstar : -0.77432E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22970E-01 0.54205E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93647E-02      33   0.29209E-03   0.46080E+01 0.16557E+03 
c  Velocity[X]                                      0.18328E+01 
c  Velocity[Y]                                      0.27752E+01 
c  Velocity[Z]                                      0.12142E-29 
c  Pressure     0.12344E-06     505   0.98859E-08   0.11915E+00 0.93812E+03 
c  nu_tilda     0.64142E-05      32   0.15525E-04   0.40481E-06 0.17315E+03 
c  TempC        0.37867E+02      27   0.34587E-03   0.40581E+01 0.21943E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5193          10.238          4.5729          4.5729
v  Velocity[Y]            -2.4795          7.3447        0.024456        0.024456
v  Velocity[Z]       -1.4439e-014     1.4581e-014    -1.3958e-017    -1.3958e-017
v  ǁVelocityǁ         0.0016014          10.238          5.1545          5.1545
v  Pressure               -42.379          15.862         -11.549         -11.549
v  nu_tilda           3.2859e-007       0.0042695       0.0014814       0.0014814
v  TempC                       21          73.042          21.896          21.896
v  TurbVisc           1.0434e-014        0.005032       0.0017398       0.0017398
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1672:        0.21490E+01

===============================================================


 INSTANT    0.167300000E+04   TIME STEP NUMBER            1673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63603E-02 0.90104E+00
   Friction velocity        uk    :  0.63603E-02 0.90104E+00
   Dimensionless distance   yplus :  0.51205E-01 0.72539E+01
   Friction thermal sca.    tstar : -0.76505E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38205E-01 0.54123E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93669E-02      33   0.29640E-03   0.45627E+01 0.16545E+03 
c  Velocity[X]                                      0.17928E+01 
c  Velocity[Y]                                      0.27699E+01 
c  Velocity[Z]                                      0.91542E-30 
c  Pressure     0.97351E-07     489   0.92920E-08   0.91700E-01 0.11998E+04 
c  nu_tilda     0.64165E-05      32   0.47252E-05   0.40535E-06 0.17325E+03 
c  TempC        0.37876E+02      27   0.38652E-03   0.38751E+01 0.22463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5162          10.237          4.5729          4.5729
v  Velocity[Y]            -2.4814          7.3679         0.02465         0.02465
v  Velocity[Z]       -1.4226e-014     1.4021e-014    -1.3998e-017    -1.3998e-017
v  ǁVelocityǁ         0.0018154          10.237          5.1543          5.1543
v  Pressure               -42.341          16.059         -11.488         -11.488
v  nu_tilda           3.2719e-007       0.0042695        0.001482        0.001482
v  TempC                       21          73.043          21.896          21.896
v  TurbVisc           1.0256e-014        0.005032       0.0017403       0.0017403
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1673:        0.21070E+01

===============================================================


 INSTANT    0.167400000E+04   TIME STEP NUMBER            1674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80243E-02 0.90198E+00
   Friction velocity        uk    :  0.80243E-02 0.90198E+00
   Dimensionless distance   yplus :  0.64601E-01 0.72616E+01
   Friction thermal sca.    tstar : -0.72846E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48199E-01 0.54179E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93691E-02      33   0.30284E-03   0.45749E+01 0.16557E+03 
c  Velocity[X]                                      0.17900E+01 
c  Velocity[Y]                                      0.27849E+01 
c  Velocity[Z]                                      0.11623E-29 
c  Pressure     0.10981E-06     505   0.96257E-08   0.10422E+00 0.11140E+04 
c  nu_tilda     0.64188E-05      32   0.15516E-04   0.40593E-06 0.17335E+03 
c  TempC        0.37884E+02      26   0.30441E-03   0.62169E+01 0.26537E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5131          10.236          4.5729          4.5729
v  Velocity[Y]            -2.4835          7.3375        0.024845        0.024845
v  Velocity[Z]       -1.4471e-014     1.4155e-014     -1.405e-017     -1.405e-017
v  ǁVelocityǁ         0.0022152          10.236          5.1541          5.1541
v  Pressure                -42.34          15.866         -11.552         -11.552
v  nu_tilda           3.2582e-007       0.0042695       0.0014824       0.0014824
v  TempC                       21          73.043          21.896          21.896
v  TurbVisc           1.0082e-014        0.005032       0.0017409       0.0017409
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1674:        0.21300E+01

===============================================================


 INSTANT    0.167500000E+04   TIME STEP NUMBER            1675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99428E-02 0.90131E+00
   Friction velocity        uk    :  0.99428E-02 0.90131E+00
   Dimensionless distance   yplus :  0.80046E-01 0.72561E+01
   Friction thermal sca.    tstar : -0.74977E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59724E-01 0.54139E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93713E-02      33   0.19918E-03   0.45868E+01 0.16569E+03 
c  Velocity[X]                                      0.18038E+01 
c  Velocity[Y]                                      0.27830E+01 
c  Velocity[Z]                                      0.11220E-29 
c  Pressure     0.10368E-06     490   0.96677E-08   0.98580E-01 0.10863E+04 
c  nu_tilda     0.64211E-05      32   0.47238E-05   0.40646E-06 0.17345E+03 
c  TempC        0.37893E+02      26   0.38855E-03   0.56806E+01 0.26400E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5098          10.236          4.5729          4.5729
v  Velocity[Y]            -2.4859          7.3654        0.025041        0.025041
v  Velocity[Z]       -1.4654e-014     1.3868e-014    -1.4084e-017    -1.4084e-017
v  ǁVelocityǁ         0.0025325          10.236          5.1539          5.1539
v  Pressure               -42.303          16.039         -11.497         -11.497
v  nu_tilda           3.2446e-007       0.0042695       0.0014829       0.0014829
v  TempC                       21          73.044          21.896          21.896
v  TurbVisc           9.9143e-015        0.005032       0.0017415       0.0017415
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1675:        0.21240E+01

===============================================================


 INSTANT    0.167600000E+04   TIME STEP NUMBER            1676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75804E-02 0.90275E+00
   Friction velocity        uk    :  0.75804E-02 0.90275E+00
   Dimensionless distance   yplus :  0.61027E-01 0.72677E+01
   Friction thermal sca.    tstar : -0.73251E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45533E-01 0.54225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93736E-02      33   0.30783E-03   0.45594E+01 0.16562E+03 
c  Velocity[X]                                      0.17835E+01 
c  Velocity[Y]                                      0.27759E+01 
c  Velocity[Z]                                      0.84952E-30 
c  Pressure     0.10903E-06     472   0.98713E-08   0.10258E+00 0.48895E+03 
c  nu_tilda     0.64234E-05      32   0.15508E-04   0.40704E-06 0.17355E+03 
c  TempC        0.37902E+02      26   0.28905E-03   0.53719E+01 0.27531E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5068          10.235          4.5729          4.5729
v  Velocity[Y]            -2.4883          7.3697        0.025237        0.025237
v  Velocity[Z]       -1.5071e-014     1.4133e-014    -1.4132e-017    -1.4132e-017
v  ǁVelocityǁ         0.0024796          10.235          5.1537          5.1537
v  Pressure               -42.302          15.992         -11.529         -11.529
v  nu_tilda           3.2309e-007       0.0042695       0.0014833       0.0014833
v  TempC                       21          73.043          21.897          21.897
v  TurbVisc           9.7504e-015        0.005032        0.001742        0.001742
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1676:        0.20910E+01

===============================================================


 INSTANT    0.167700000E+04   TIME STEP NUMBER            1677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75971E-02 0.90242E+00
   Friction velocity        uk    :  0.75971E-02 0.90242E+00
   Dimensionless distance   yplus :  0.61162E-01 0.72651E+01
   Friction thermal sca.    tstar : -0.72245E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45633E-01 0.54206E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93758E-02      33   0.31636E-03   0.45871E+01 0.16582E+03 
c  Velocity[X]                                      0.18050E+01 
c  Velocity[Y]                                      0.27821E+01 
c  Velocity[Z]                                      0.12626E-29 
c  Pressure     0.11875E-06     440   0.92992E-08   0.11489E+00 0.50430E+03 
c  nu_tilda     0.64257E-05      32   0.47132E-05   0.40758E-06 0.17365E+03 
c  TempC        0.37910E+02      26   0.36514E-03   0.36480E+01 0.23070E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5037          10.234          4.5729          4.5729
v  Velocity[Y]            -2.4905          7.3442        0.025434        0.025434
v  Velocity[Z]       -1.5386e-014      1.417e-014    -1.4173e-017    -1.4173e-017
v  ǁVelocityǁ         0.0026979          10.234          5.1535          5.1535
v  Pressure               -42.259          15.949         -11.514         -11.514
v  nu_tilda           3.2172e-007       0.0042695       0.0014839       0.0014839
v  TempC                       21          73.043          21.897          21.897
v  TurbVisc           9.5862e-015        0.005032       0.0017426       0.0017426
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1677:        0.20090E+01

===============================================================


 INSTANT    0.167800000E+04   TIME STEP NUMBER            1678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11908E-01 0.90101E+00
   Friction velocity        uk    :  0.11908E-01 0.90101E+00
   Dimensionless distance   yplus :  0.95867E-01 0.72537E+01
   Friction thermal sca.    tstar : -0.73945E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71527E-01 0.54121E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93781E-02      33   0.32130E-03   0.45860E+01 0.16597E+03 
c  Velocity[X]                                      0.17754E+01 
c  Velocity[Y]                                      0.28107E+01 
c  Velocity[Z]                                      0.10565E-29 
c  Pressure     0.10128E-06     297   0.93308E-08   0.96308E-01 0.37259E+03 
c  nu_tilda     0.64280E-05      32   0.15512E-04   0.40816E-06 0.17376E+03 
c  TempC        0.37919E+02      27   0.31124E-03   0.56660E+01 0.26170E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5006          10.233          4.5729          4.5729
v  Velocity[Y]            -2.4925          7.3625        0.025632        0.025632
v  Velocity[Z]       -1.4918e-014     1.3927e-014    -1.4216e-017    -1.4216e-017
v  ǁVelocityǁ         0.0023865          10.233          5.1533          5.1533
v  Pressure                -42.26          16.044          -11.52          -11.52
v  nu_tilda           3.2032e-007       0.0042695       0.0014843       0.0014843
v  TempC                       21          73.043          21.897          21.897
v  TurbVisc           9.4246e-015        0.005032       0.0017432       0.0017432
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1678:        0.16870E+01

===============================================================


 INSTANT    0.167900000E+04   TIME STEP NUMBER            1679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39299E-02 0.90189E+00
   Friction velocity        uk    :  0.39299E-02 0.90189E+00
   Dimensionless distance   yplus :  0.31638E-01 0.72609E+01
   Friction thermal sca.    tstar : -0.71664E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23606E-01 0.54174E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93803E-02      33   0.28102E-03   0.46088E+01 0.16615E+03 
c  Velocity[X]                                      0.18121E+01 
c  Velocity[Y]                                      0.27967E+01 
c  Velocity[Z]                                      0.10109E-29 
c  Pressure     0.12592E-06     344   0.90449E-08   0.11910E+00 0.56778E+03 
c  nu_tilda     0.64303E-05      32   0.47013E-05   0.40869E-06 0.17386E+03 
c  TempC        0.37928E+02      27   0.26637E-03   0.64356E+01 0.27510E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4974          10.232          4.5729          4.5729
v  Velocity[Y]            -2.4944           7.337        0.025831        0.025831
v  Velocity[Z]       -1.5212e-014     1.3711e-014     -1.426e-017     -1.426e-017
v  ǁVelocityǁ         0.0026657          10.232          5.1531          5.1531
v  Pressure                -42.22          15.932          -11.52          -11.52
v  nu_tilda           3.1893e-007       0.0042695       0.0014848       0.0014848
v  TempC                       21          73.043          21.898          21.898
v  TurbVisc           9.2625e-015        0.005032       0.0017437       0.0017437
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1679:        0.17900E+01

===============================================================


 INSTANT    0.168000000E+04   TIME STEP NUMBER            1680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13216E-01 0.90133E+00
   Friction velocity        uk    :  0.13216E-01 0.90133E+00
   Dimensionless distance   yplus :  0.10640E+00 0.72564E+01
   Friction thermal sca.    tstar : -0.79563E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79383E-01 0.54140E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93825E-02      33   0.24202E-03   0.45863E+01 0.16608E+03 
c  Velocity[X]                                      0.17976E+01 
c  Velocity[Y]                                      0.27887E+01 
c  Velocity[Z]                                      0.11409E-29 
c  Pressure     0.10371E-06     297   0.96000E-08   0.99042E-01 0.36493E+03 
c  nu_tilda     0.64326E-05      32   0.15501E-04   0.40928E-06 0.17396E+03 
c  TempC        0.37936E+02      26   0.41647E-03   0.42818E+01 0.23594E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4945          10.231          4.5729          4.5729
v  Velocity[Y]            -2.4964          7.3627         0.02603         0.02603
v  Velocity[Z]       -1.5092e-014     1.3456e-014    -1.4295e-017    -1.4295e-017
v  ǁVelocityǁ         0.0024819          10.231          5.1529          5.1529
v  Pressure               -42.222          16.022         -11.527         -11.527
v  nu_tilda           3.1771e-007       0.0042695       0.0014852       0.0014852
v  TempC                       21          73.043          21.898          21.898
v  TurbVisc           9.1027e-015        0.005032       0.0017443       0.0017443
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1680:        0.16840E+01

===============================================================


 INSTANT    0.168100000E+04   TIME STEP NUMBER            1681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37260E-02 0.90270E+00
   Friction velocity        uk    :  0.37260E-02 0.90270E+00
   Dimensionless distance   yplus :  0.29996E-01 0.72673E+01
   Friction thermal sca.    tstar : -0.74067E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22381E-01 0.54222E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93847E-02      33   0.30460E-03   0.45732E+01 0.16617E+03 
c  Velocity[X]                                      0.17609E+01 
c  Velocity[Y]                                      0.28123E+01 
c  Velocity[Z]                                      0.11498E-29 
c  Pressure     0.98044E-07     488   0.94064E-08   0.93311E-01 0.74427E+03 
c  nu_tilda     0.64349E-05      32   0.46979E-05   0.40982E-06 0.17406E+03 
c  TempC        0.37945E+02      27   0.33838E-03   0.64785E+01 0.30058E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4914           10.23          4.5729          4.5729
v  Velocity[Y]            -2.4989          7.3739        0.026231        0.026231
v  Velocity[Z]       -1.5615e-014     1.3308e-014     -1.434e-017     -1.434e-017
v  ǁVelocityǁ         0.0024981           10.23          5.1527          5.1527
v  Pressure               -42.181            16.1         -11.489         -11.489
v  nu_tilda           3.1666e-007       0.0042695       0.0014858       0.0014858
v  TempC                       21          73.043          21.898          21.898
v  TurbVisc           8.9633e-015        0.005032       0.0017448       0.0017448
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1681:        0.21230E+01

===============================================================


 INSTANT    0.168200000E+04   TIME STEP NUMBER            1682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61353E-02 0.90210E+00
   Friction velocity        uk    :  0.61353E-02 0.90210E+00
   Dimensionless distance   yplus :  0.49393E-01 0.72625E+01
   Friction thermal sca.    tstar : -0.84179E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36853E-01 0.54186E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93870E-02      33   0.28171E-03   0.46183E+01 0.16640E+03 
c  Velocity[X]                                      0.18168E+01 
c  Velocity[Y]                                      0.28015E+01 
c  Velocity[Z]                                      0.10843E-29 
c  Pressure     0.13356E-06     506   0.99512E-08   0.12594E+00 0.11632E+04 
c  nu_tilda     0.64372E-05      32   0.15499E-04   0.41040E-06 0.17416E+03 
c  TempC        0.37954E+02      27   0.32301E-03   0.56837E+01 0.27080E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4884          10.229          4.5729          4.5729
v  Velocity[Y]            -2.5012          7.3389        0.026432        0.026432
v  Velocity[Z]       -1.5528e-014     1.3034e-014    -1.4381e-017    -1.4381e-017
v  ǁVelocityǁ         0.0025127          10.229          5.1525          5.1525
v  Pressure               -42.177          15.892         -11.553         -11.553
v  nu_tilda           3.1573e-007       0.0042695       0.0014862       0.0014862
v  TempC                       21          73.042          21.898          21.898
v  TurbVisc           8.8454e-015        0.005032       0.0017454       0.0017454
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1682:        0.21630E+01

===============================================================


 INSTANT    0.168300000E+04   TIME STEP NUMBER            1683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65558E-02 0.90092E+00
   Friction velocity        uk    :  0.65558E-02 0.90092E+00
   Dimensionless distance   yplus :  0.52779E-01 0.72530E+01
   Friction thermal sca.    tstar : -0.10571E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39379E-01 0.54115E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93892E-02      33   0.30074E-03   0.45974E+01 0.16642E+03 
c  Velocity[X]                                      0.17986E+01 
c  Velocity[Y]                                      0.27988E+01 
c  Velocity[Z]                                      0.96363E-30 
c  Pressure     0.10510E-06     521   0.92496E-08   0.10014E+00 0.12900E+04 
c  nu_tilda     0.64395E-05      32   0.46808E-05   0.41094E-06 0.17426E+03 
c  TempC        0.37962E+02      27   0.26463E-03   0.44484E+01 0.23004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4853          10.229          4.5729          4.5729
v  Velocity[Y]            -2.5034          7.3629        0.026634        0.026634
v  Velocity[Z]       -1.5407e-014     1.2718e-014    -1.4412e-017    -1.4412e-017
v  ǁVelocityǁ         0.0019552          10.229          5.1524          5.1524
v  Pressure               -42.139          16.108         -11.488         -11.488
v  nu_tilda           3.1486e-007       0.0042695       0.0014867       0.0014867
v  TempC                       21          73.043          21.899          21.899
v  TurbVisc           8.7423e-015        0.005032        0.001746        0.001746
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1683:        0.21790E+01

===============================================================


 INSTANT    0.168400000E+04   TIME STEP NUMBER            1684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91152E-02 0.90179E+00
   Friction velocity        uk    :  0.91152E-02 0.90179E+00
   Dimensionless distance   yplus :  0.73383E-01 0.72601E+01
   Friction thermal sca.    tstar : -0.16557E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54752E-01 0.54168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93915E-02      33   0.31006E-03   0.46160E+01 0.16660E+03 
c  Velocity[X]                                      0.17937E+01 
c  Velocity[Y]                                      0.28223E+01 
c  Velocity[Z]                                      0.11129E-29 
c  Pressure     0.10790E-06     504   0.96926E-08   0.10436E+00 0.96689E+03 
c  nu_tilda     0.64418E-05      32   0.15494E-04   0.41152E-06 0.17436E+03 
c  TempC        0.37971E+02      27   0.42207E-03   0.36553E+01 0.21484E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4822          10.228          4.5729          4.5729
v  Velocity[Y]            -2.5055          7.3374        0.026837        0.026837
v  Velocity[Z]       -1.5304e-014     1.2414e-014    -1.4459e-017    -1.4459e-017
v  ǁVelocityǁ          0.001785          10.228          5.1522          5.1522
v  Pressure               -42.138          15.948         -11.544         -11.544
v  nu_tilda           3.1401e-007       0.0042695       0.0014871       0.0014871
v  TempC                       21          73.043          21.899          21.899
v  TurbVisc           8.6467e-015        0.005032       0.0017465       0.0017465
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1684:        0.21570E+01

===============================================================


 INSTANT    0.168500000E+04   TIME STEP NUMBER            1685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59411E-02 0.90086E+00
   Friction velocity        uk    :  0.59411E-02 0.90086E+00
   Dimensionless distance   yplus :  0.47830E-01 0.72525E+01
   Friction thermal sca.    tstar : -0.25273E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35686E-01 0.54112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93937E-02      33   0.20649E-03   0.46186E+01 0.16661E+03 
c  Velocity[X]                                      0.18079E+01 
c  Velocity[Y]                                      0.28107E+01 
c  Velocity[Z]                                      0.10121E-29 
c  Pressure     0.12267E-06     488   0.91725E-08   0.11428E+00 0.90521E+03 
c  nu_tilda     0.64441E-05      32   0.46811E-05   0.41207E-06 0.17446E+03 
c  TempC        0.37980E+02      27   0.37578E-03   0.59892E+01 0.28398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.479          10.227          4.5729          4.5729
v  Velocity[Y]            -2.5074          7.3598        0.027041        0.027041
v  Velocity[Z]       -1.5433e-014     1.2177e-014    -1.4494e-017    -1.4494e-017
v  ǁVelocityǁ         0.0016725          10.227           5.152           5.152
v  Pressure               -42.101          16.075         -11.499         -11.499
v  nu_tilda           3.1317e-007       0.0042695       0.0014877       0.0014877
v  TempC                       21          73.043          21.899          21.899
v  TurbVisc           8.5536e-015        0.005032       0.0017471       0.0017471
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1685:        0.21170E+01

===============================================================


 INSTANT    0.168600000E+04   TIME STEP NUMBER            1686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69640E-02 0.90251E+00
   Friction velocity        uk    :  0.69640E-02 0.90251E+00
   Dimensionless distance   yplus :  0.56065E-01 0.72659E+01
   Friction thermal sca.    tstar : -0.11786E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41831E-01 0.54211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93959E-02      33   0.30936E-03   0.45819E+01 0.16654E+03 
c  Velocity[X]                                      0.17781E+01 
c  Velocity[Y]                                      0.28038E+01 
c  Velocity[Z]                                      0.79613E-30 
c  Pressure     0.96408E-07     442   0.93892E-08   0.92201E-01 0.34315E+03 
c  nu_tilda     0.64464E-05      32   0.15486E-04   0.41265E-06 0.17456E+03 
c  TempC        0.37988E+02      27   0.32835E-03   0.60328E+01 0.27064E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4759          10.226          4.5729          4.5729
v  Velocity[Y]            -2.5092          7.3692        0.027245        0.027245
v  Velocity[Z]       -1.5569e-014     1.1992e-014    -1.4537e-017    -1.4537e-017
v  ǁVelocityǁ         0.0019354          10.226          5.1518          5.1518
v  Pressure               -42.099          16.077         -11.522         -11.522
v  nu_tilda           3.1232e-007       0.0042695       0.0014881       0.0014881
v  TempC                       21          73.043          21.899          21.899
v  TurbVisc            8.462e-015        0.005032       0.0017477       0.0017477
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1686:        0.19920E+01

===============================================================


 INSTANT    0.168700000E+04   TIME STEP NUMBER            1687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97423E-02 0.90198E+00
   Friction velocity        uk    :  0.97423E-02 0.90198E+00
   Dimensionless distance   yplus :  0.78432E-01 0.72616E+01
   Friction thermal sca.    tstar : -0.89456E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58519E-01 0.54179E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93982E-02      33   0.30066E-03   0.46216E+01 0.16685E+03 
c  Velocity[X]                                      0.17951E+01 
c  Velocity[Y]                                      0.28264E+01 
c  Velocity[Z]                                      0.10036E-29 
c  Pressure     0.11918E-06     425   0.97751E-08   0.11499E+00 0.51440E+03 
c  nu_tilda     0.64487E-05      32   0.46734E-05   0.41319E-06 0.17466E+03 
c  TempC        0.37997E+02      26   0.30174E-03   0.47801E+01 0.23973E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4729          10.225          4.5729          4.5729
v  Velocity[Y]            -2.5117          7.3406         0.02745         0.02745
v  Velocity[Z]       -1.5738e-014     1.1776e-014    -1.4574e-017    -1.4574e-017
v  ǁVelocityǁ          0.002439          10.225          5.1516          5.1516
v  Pressure               -42.057          16.008         -11.511         -11.511
v  nu_tilda            3.115e-007       0.0042695       0.0014886       0.0014886
v  TempC                       21          73.042            21.9            21.9
v  TurbVisc            8.371e-015        0.005032       0.0017482       0.0017482
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1687:        0.19580E+01

===============================================================


 INSTANT    0.168800000E+04   TIME STEP NUMBER            1688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45442E-02 0.90046E+00
   Friction velocity        uk    :  0.45442E-02 0.90046E+00
   Dimensionless distance   yplus :  0.36584E-01 0.72493E+01
   Friction thermal sca.    tstar : -0.77445E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27296E-01 0.54088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94004E-02      33   0.29003E-03   0.46297E+01 0.16692E+03 
c  Velocity[X]                                      0.18127E+01 
c  Velocity[Y]                                      0.28170E+01 
c  Velocity[Z]                                      0.10504E-29 
c  Pressure     0.12464E-06     441   0.94984E-08   0.11656E+00 0.30009E+03 
c  nu_tilda     0.64510E-05      32   0.15487E-04   0.41378E-06 0.17476E+03 
c  TempC        0.38006E+02      26   0.33451E-03   0.41643E+01 0.23074E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4698          10.224          4.5729          4.5729
v  Velocity[Y]             -2.514          7.3554        0.027657        0.027657
v  Velocity[Z]       -1.5513e-014     1.1523e-014     -1.461e-017     -1.461e-017
v  ǁVelocityǁ         0.0023834          10.224          5.1514          5.1514
v  Pressure               -42.057          16.044         -11.529         -11.529
v  nu_tilda           3.1068e-007       0.0042695        0.001489        0.001489
v  TempC                       21          73.043            21.9            21.9
v  TurbVisc           8.2831e-015        0.005032       0.0017488       0.0017488
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1688:        0.19960E+01

===============================================================


 INSTANT    0.168900000E+04   TIME STEP NUMBER            1689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10678E-01 0.90175E+00
   Friction velocity        uk    :  0.10678E-01 0.90175E+00
   Dimensionless distance   yplus :  0.85962E-01 0.72597E+01
   Friction thermal sca.    tstar : -0.73367E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64137E-01 0.54166E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94026E-02      33   0.30423E-03   0.46359E+01 0.16706E+03 
c  Velocity[X]                                      0.18214E+01 
c  Velocity[Y]                                      0.28145E+01 
c  Velocity[Z]                                      0.11189E-29 
c  Pressure     0.11594E-06     456   0.92740E-08   0.11135E+00 0.50566E+03 
c  nu_tilda     0.64533E-05      32   0.46563E-05   0.41432E-06 0.17486E+03 
c  TempC        0.38014E+02      27   0.33507E-03   0.48145E+01 0.23990E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4666          10.223          4.5729          4.5729
v  Velocity[Y]            -2.5162          7.3346        0.027863        0.027863
v  Velocity[Z]       -1.5556e-014     1.1262e-014    -1.4647e-017    -1.4647e-017
v  ǁVelocityǁ         0.0024699          10.223          5.1513          5.1513
v  Pressure               -42.016          16.026          -11.51          -11.51
v  nu_tilda           3.0985e-007       0.0042695       0.0014896       0.0014896
v  TempC                       21          73.043            21.9            21.9
v  TurbVisc            8.196e-015        0.005032       0.0017493       0.0017493
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1689:        0.23280E+01

===============================================================


 INSTANT    0.169000000E+04   TIME STEP NUMBER            1690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77165E-02 0.90080E+00
   Friction velocity        uk    :  0.77165E-02 0.90080E+00
   Dimensionless distance   yplus :  0.62123E-01 0.72520E+01
   Friction thermal sca.    tstar : -0.73005E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46351E-01 0.54108E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94049E-02      33   0.24621E-03   0.46295E+01 0.16715E+03 
c  Velocity[X]                                      0.17915E+01 
c  Velocity[Y]                                      0.28381E+01 
c  Velocity[Z]                                      0.10145E-29 
c  Pressure     0.94228E-07     393   0.93401E-08   0.90222E-01 0.31974E+03 
c  nu_tilda     0.64556E-05      32   0.15482E-04   0.41491E-06 0.17496E+03 
c  TempC        0.38023E+02      27   0.44178E-03   0.48326E+01 0.25281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4637          10.222          4.5729          4.5729
v  Velocity[Y]            -2.5183          7.3594        0.028071        0.028071
v  Velocity[Z]       -1.5409e-014     1.1031e-014    -1.4693e-017    -1.4693e-017
v  ǁVelocityǁ         0.0023088          10.222          5.1511          5.1511
v  Pressure               -42.017          16.093         -11.522         -11.522
v  nu_tilda             3.09e-007       0.0042695         0.00149         0.00149
v  TempC                       21          73.043          21.901          21.901
v  TurbVisc           8.1094e-015        0.005032       0.0017499       0.0017499
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1690:        0.19840E+01

===============================================================


 INSTANT    0.169100000E+04   TIME STEP NUMBER            1691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11600E-01 0.90225E+00
   Friction velocity        uk    :  0.11600E-01 0.90225E+00
   Dimensionless distance   yplus :  0.93390E-01 0.72637E+01
   Friction thermal sca.    tstar : -0.71150E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69679E-01 0.54195E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94071E-02      33   0.27288E-03   0.46095E+01 0.16709E+03 
c  Velocity[X]                                      0.17833E+01 
c  Velocity[Y]                                      0.28262E+01 
c  Velocity[Z]                                      0.10586E-29 
c  Pressure     0.12139E-06     473   0.96844E-08   0.11374E+00 0.53355E+03 
c  nu_tilda     0.64579E-05      32   0.46591E-05   0.41545E-06 0.17506E+03 
c  TempC        0.38032E+02      27   0.38509E-03   0.63882E+01 0.29150E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4606          10.222          4.5729          4.5729
v  Velocity[Y]            -2.5203          7.3656        0.028279        0.028279
v  Velocity[Z]       -1.5537e-014     1.0849e-014    -1.4731e-017    -1.4731e-017
v  ǁVelocityǁ         0.0024214          10.222          5.1509          5.1509
v  Pressure               -41.977          16.099         -11.499         -11.499
v  nu_tilda           3.0813e-007       0.0042695       0.0014905       0.0014905
v  TempC                       21          73.043          21.901          21.901
v  TurbVisc           8.0204e-015        0.005032       0.0017504       0.0017504
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1691:        0.20780E+01

===============================================================


 INSTANT    0.169200000E+04   TIME STEP NUMBER            1692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32917E-02 0.90202E+00
   Friction velocity        uk    :  0.32917E-02 0.90202E+00
   Dimensionless distance   yplus :  0.26500E-01 0.72619E+01
   Friction thermal sca.    tstar : -0.75647E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19772E-01 0.54182E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94094E-02      33   0.30624E-03   0.46253E+01 0.16722E+03 
c  Velocity[X]                                      0.18060E+01 
c  Velocity[Y]                                      0.28193E+01 
c  Velocity[Z]                                      0.87487E-30 
c  Pressure     0.12032E-06     521   0.91846E-08   0.11677E+00 0.69740E+03 
c  nu_tilda     0.64602E-05      32   0.15475E-04   0.41604E-06 0.17516E+03 
c  TempC        0.38040E+02      27   0.33933E-03   0.47667E+01 0.25600E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4576          10.221          4.5729          4.5729
v  Velocity[Y]            -2.5221          7.3378        0.028489        0.028489
v  Velocity[Z]       -1.5434e-014     1.0643e-014    -1.4773e-017    -1.4773e-017
v  ǁVelocityǁ         0.0024691          10.221          5.1507          5.1507
v  Pressure               -41.975          15.999         -11.542         -11.542
v  nu_tilda           3.0725e-007       0.0042695       0.0014909       0.0014909
v  TempC                       21          73.042          21.901          21.901
v  TurbVisc            7.931e-015        0.005032        0.001751        0.001751
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1692:        0.21910E+01

===============================================================


 INSTANT    0.169300000E+04   TIME STEP NUMBER            1693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12301E-01 0.90039E+00
   Friction velocity        uk    :  0.12301E-01 0.90039E+00
   Dimensionless distance   yplus :  0.99032E-01 0.72488E+01
   Friction thermal sca.    tstar : -0.73852E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73889E-01 0.54084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94116E-02      33   0.30684E-03   0.46289E+01 0.16736E+03 
c  Velocity[X]                                      0.17872E+01 
c  Velocity[Y]                                      0.28418E+01 
c  Velocity[Z]                                      0.12319E-29 
c  Pressure     0.10419E-06     488   0.99341E-08   0.98533E-01 0.10153E+04 
c  nu_tilda     0.64625E-05      32   0.46466E-05   0.41658E-06 0.17526E+03 
c  TempC        0.38049E+02      27   0.31343E-03   0.43726E+01 0.24712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4546           10.22          4.5729          4.5729
v  Velocity[Y]            -2.5244          7.3578        0.028699        0.028699
v  Velocity[Z]        -1.531e-014     1.0435e-014    -1.4816e-017    -1.4816e-017
v  ǁVelocityǁ         0.0023903           10.22          5.1506          5.1506
v  Pressure               -41.934          16.144         -11.489         -11.489
v  nu_tilda           3.0638e-007       0.0042695       0.0014915       0.0014915
v  TempC                       21          73.043          21.901          21.901
v  TurbVisc           7.8408e-015        0.005032       0.0017516       0.0017516
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1693:        0.21130E+01

===============================================================


 INSTANT    0.169400000E+04   TIME STEP NUMBER            1694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51813E-02 0.90135E+00
   Friction velocity        uk    :  0.51813E-02 0.90135E+00
   Dimensionless distance   yplus :  0.41713E-01 0.72565E+01
   Friction thermal sca.    tstar : -0.71001E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31123E-01 0.54141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94138E-02      33   0.30583E-03   0.46601E+01 0.16754E+03 
c  Velocity[X]                                      0.18266E+01 
c  Velocity[Y]                                      0.28335E+01 
c  Velocity[Z]                                      0.10071E-29 
c  Pressure     0.13440E-06     520   0.92184E-08   0.12804E+00 0.10297E+04 
c  nu_tilda     0.64648E-05      32   0.15472E-04   0.41717E-06 0.17536E+03 
c  TempC        0.38058E+02      27   0.27428E-03   0.43266E+01 0.23858E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4515          10.219          4.5729          4.5729
v  Velocity[Y]            -2.5268          7.3298         0.02891         0.02891
v  Velocity[Z]       -1.5006e-014     1.0236e-014    -1.4858e-017    -1.4858e-017
v  ǁVelocityǁ         0.0024348          10.219          5.1504          5.1504
v  Pressure               -41.933          15.969         -11.549         -11.549
v  nu_tilda           3.0548e-007       0.0042695       0.0014919       0.0014919
v  TempC                       21          73.043          21.902          21.902
v  TurbVisc           7.7514e-015        0.005032       0.0017521       0.0017521
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1694:        0.21800E+01

===============================================================


 INSTANT    0.169500000E+04   TIME STEP NUMBER            1695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71711E-02 0.90079E+00
   Friction velocity        uk    :  0.71711E-02 0.90079E+00
   Dimensionless distance   yplus :  0.57732E-01 0.72520E+01
   Friction thermal sca.    tstar : -0.73000E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43075E-01 0.54108E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94160E-02      33   0.24210E-03   0.46504E+01 0.16759E+03 
c  Velocity[X]                                      0.18197E+01 
c  Velocity[Y]                                      0.28308E+01 
c  Velocity[Z]                                      0.87373E-30 
c  Pressure     0.10819E-06     521   0.94587E-08   0.10357E+00 0.11917E+04 
c  nu_tilda     0.64671E-05      32   0.46310E-05   0.41772E-06 0.17546E+03 
c  TempC        0.38066E+02      27   0.36244E-03   0.40274E+01 0.21395E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4483          10.218          4.5729          4.5729
v  Velocity[Y]             -2.529          7.3579        0.029121        0.029121
v  Velocity[Z]       -1.4754e-014      1.002e-014    -1.4903e-017    -1.4903e-017
v  ǁVelocityǁ         0.0019776          10.218          5.1502          5.1502
v  Pressure               -41.894           16.16         -11.488         -11.488
v  nu_tilda            3.046e-007       0.0042695       0.0014924       0.0014924
v  TempC                       21          73.044          21.902          21.902
v  TurbVisc           7.6616e-015        0.005032       0.0017527       0.0017527
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1695:        0.21660E+01

===============================================================


 INSTANT    0.169600000E+04   TIME STEP NUMBER            1696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39635E-02 0.90219E+00
   Friction velocity        uk    :  0.39635E-02 0.90219E+00
   Dimensionless distance   yplus :  0.31909E-01 0.72632E+01
   Friction thermal sca.    tstar : -0.75590E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23807E-01 0.54192E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94183E-02      33   0.30024E-03   0.46248E+01 0.16760E+03 
c  Velocity[X]                                      0.17740E+01 
c  Velocity[Y]                                      0.28509E+01 
c  Velocity[Z]                                      0.10332E-29 
c  Pressure     0.90154E-07     473   0.98961E-08   0.86014E-01 0.48255E+03 
c  nu_tilda     0.64694E-05      32   0.15467E-04   0.41831E-06 0.17557E+03 
c  TempC        0.38075E+02      27   0.32489E-03   0.44625E+01 0.24290E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4451          10.217          4.5729          4.5729
v  Velocity[Y]            -2.5311          7.3666        0.029334        0.029334
v  Velocity[Z]       -1.4439e-014     9.8311e-015    -1.4942e-017    -1.4942e-017
v  ǁVelocityǁ         0.0018667          10.217            5.15            5.15
v  Pressure               -41.894          16.124         -11.521         -11.521
v  nu_tilda           3.0371e-007       0.0042695       0.0014928       0.0014928
v  TempC                       21          73.043          21.902          21.902
v  TurbVisc           7.5731e-015        0.005032       0.0017532       0.0017532
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1696:        0.20700E+01

===============================================================


 INSTANT    0.169700000E+04   TIME STEP NUMBER            1697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64012E-02 0.90170E+00
   Friction velocity        uk    :  0.64012E-02 0.90170E+00
   Dimensionless distance   yplus :  0.51534E-01 0.72593E+01
   Friction thermal sca.    tstar : -0.71601E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38450E-01 0.54162E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94205E-02      33   0.27082E-03   0.46615E+01 0.16778E+03 
c  Velocity[X]                                      0.18191E+01 
c  Velocity[Y]                                      0.28424E+01 
c  Velocity[Z]                                      0.11040E-29 
c  Pressure     0.13170E-06     377   0.93744E-08   0.12514E+00 0.51817E+03 
c  nu_tilda     0.64717E-05      32   0.46321E-05   0.41886E-06 0.17567E+03 
c  TempC        0.38084E+02      27   0.31666E-03   0.39712E+01 0.21849E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4421          10.216          4.5729          4.5729
v  Velocity[Y]             -2.533          7.3336        0.029547        0.029547
v  Velocity[Z]       -1.4789e-014     9.6499e-015    -1.4986e-017    -1.4986e-017
v  ǁVelocityǁ         0.0019512          10.216          5.1499          5.1499
v  Pressure               -41.853          16.039         -11.515         -11.515
v  nu_tilda           3.0287e-007       0.0042695       0.0014933       0.0014933
v  TempC                       21          73.043          21.903          21.903
v  TurbVisc           7.4855e-015        0.005032       0.0017538       0.0017538
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1697:        0.18640E+01

===============================================================


 INSTANT    0.169800000E+04   TIME STEP NUMBER            1698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21315E-02 0.90044E+00
   Friction velocity        uk    :  0.21315E-02 0.90044E+00
   Dimensionless distance   yplus :  0.17160E-01 0.72491E+01
   Friction thermal sca.    tstar : -0.72392E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12803E-01 0.54087E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94228E-02      33   0.31138E-03   0.46323E+01 0.16772E+03 
c  Velocity[X]                                      0.17977E+01 
c  Velocity[Y]                                      0.28346E+01 
c  Velocity[Z]                                      0.10022E-29 
c  Pressure     0.10326E-06     409   0.97223E-08   0.98920E-01 0.43893E+03 
c  nu_tilda     0.64740E-05      32   0.15463E-04   0.41944E-06 0.17577E+03 
c  TempC        0.38092E+02      27   0.36880E-03   0.46017E+01 0.22878E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4392          10.215          4.5729          4.5729
v  Velocity[Y]            -2.5348          7.3554        0.029762        0.029762
v  Velocity[Z]       -1.4953e-014     9.4304e-015    -1.5039e-017    -1.5039e-017
v  ǁVelocityǁ          0.002173          10.215          5.1497          5.1497
v  Pressure               -41.849          16.149         -11.514         -11.514
v  nu_tilda           3.0204e-007       0.0042695       0.0014938       0.0014938
v  TempC                       21          73.043          21.903          21.903
v  TurbVisc           7.4027e-015        0.005032       0.0017544       0.0017544
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1698:        0.19340E+01

===============================================================


 INSTANT    0.169900000E+04   TIME STEP NUMBER            1699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11928E-01 0.90134E+00
   Friction velocity        uk    :  0.11928E-01 0.90134E+00
   Dimensionless distance   yplus :  0.96031E-01 0.72564E+01
   Friction thermal sca.    tstar : -0.70242E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71650E-01 0.54141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94250E-02      33   0.31979E-03   0.46536E+01 0.16795E+03 
c  Velocity[X]                                      0.17968E+01 
c  Velocity[Y]                                      0.28567E+01 
c  Velocity[Z]                                      0.92593E-30 
c  Pressure     0.10951E-06     360   0.94249E-08   0.10575E+00 0.49228E+03 
c  nu_tilda     0.64763E-05      32   0.46174E-05   0.41999E-06 0.17587E+03 
c  TempC        0.38101E+02      27   0.34547E-03   0.43728E+01 0.22933E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.436          10.214          4.5729          4.5729
v  Velocity[Y]             -2.537           7.333        0.029976        0.029976
v  Velocity[Z]       -1.5068e-014     9.2448e-015    -1.5076e-017    -1.5076e-017
v  ǁVelocityǁ         0.0023131          10.214          5.1495          5.1495
v  Pressure               -41.811          16.068          -11.51          -11.51
v  nu_tilda           3.0125e-007       0.0042695       0.0014943       0.0014943
v  TempC                       21          73.044          21.903          21.903
v  TurbVisc           7.3219e-015        0.005032       0.0017549       0.0017549
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1699:        0.18310E+01

===============================================================


 INSTANT    0.170000000E+04   TIME STEP NUMBER            1700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81432E-03 0.90042E+00
   Friction velocity        uk    :  0.81432E-03 0.90042E+00
   Dimensionless distance   yplus :  0.65558E-02 0.72490E+01
   Friction thermal sca.    tstar : -0.76442E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48914E-02 0.54085E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94272E-02      33   0.23439E-03   0.46735E+01 0.16806E+03 
c  Velocity[X]                                      0.18271E+01 
c  Velocity[Y]                                      0.28464E+01 
c  Velocity[Z]                                      0.10398E-29 
c  Pressure     0.12810E-06     409   0.99089E-08   0.11974E+00 0.29156E+03 
c  nu_tilda     0.64786E-05      32   0.15459E-04   0.42058E-06 0.17597E+03 
c  TempC        0.38110E+02      26   0.31511E-03   0.52011E+01 0.24455E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4328          10.213          4.5729          4.5729
v  Velocity[Y]            -2.5394          7.3524        0.030192        0.030192
v  Velocity[Z]        -1.523e-014     9.0433e-015     -1.512e-017     -1.512e-017
v  ǁVelocityǁ         0.0022664          10.213          5.1494          5.1494
v  Pressure               -41.808          16.114         -11.523         -11.523
v  nu_tilda           3.0047e-007       0.0042695       0.0014947       0.0014947
v  TempC                       21          73.044          21.903          21.903
v  TurbVisc           7.2452e-015        0.005032       0.0017555       0.0017555
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1700:        0.19370E+01

===============================================================


 INSTANT    0.170100000E+04   TIME STEP NUMBER            1701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41975E-02 0.90207E+00
   Friction velocity        uk    :  0.41975E-02 0.90207E+00
   Dimensionless distance   yplus :  0.33793E-01 0.72623E+01
   Friction thermal sca.    tstar : -0.92579E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25213E-01 0.54185E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94295E-02      33   0.29788E-03   0.46461E+01 0.16806E+03 
c  Velocity[X]                                      0.18011E+01 
c  Velocity[Y]                                      0.28449E+01 
c  Velocity[Z]                                      0.96263E-30 
c  Pressure     0.99781E-07     504   0.90352E-08   0.95632E-01 0.77400E+03 
c  nu_tilda     0.64809E-05      32   0.46024E-05   0.42113E-06 0.17607E+03 
c  TempC        0.38118E+02      27   0.37533E-03   0.44623E+01 0.24876E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4299          10.212          4.5729          4.5729
v  Velocity[Y]            -2.5416           7.364        0.030409        0.030409
v  Velocity[Z]       -1.5386e-014     8.8556e-015    -1.5152e-017    -1.5152e-017
v  ǁVelocityǁ         0.0022898          10.213          5.1492          5.1492
v  Pressure               -41.771          16.211         -11.485         -11.485
v  nu_tilda           2.9971e-007       0.0042695       0.0014952       0.0014952
v  TempC                       21          73.044          21.904          21.904
v  TurbVisc           7.1704e-015        0.005032        0.001756        0.001756
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1701:        0.21520E+01

===============================================================


 INSTANT    0.170200000E+04   TIME STEP NUMBER            1702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75808E-03 0.90148E+00
   Friction velocity        uk    :  0.75808E-03 0.90148E+00
   Dimensionless distance   yplus :  0.61030E-02 0.72575E+01
   Friction thermal sca.    tstar : -0.14442E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45535E-02 0.54149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94317E-02      33   0.27199E-03   0.46729E+01 0.16827E+03 
c  Velocity[X]                                      0.18057E+01 
c  Velocity[Y]                                      0.28673E+01 
c  Velocity[Z]                                      0.75784E-30 
c  Pressure     0.11615E-06     504   0.99256E-08   0.11337E+00 0.94468E+03 
c  nu_tilda     0.64832E-05      32   0.15456E-04   0.42172E-06 0.17617E+03 
c  TempC        0.38127E+02      27   0.32295E-03   0.50838E+01 0.27051E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.427          10.212          4.5729          4.5729
v  Velocity[Y]            -2.5437          7.3327        0.030626        0.030626
v  Velocity[Z]       -1.6197e-014     8.6766e-015    -1.5204e-017    -1.5204e-017
v  ǁVelocityǁ         0.0022984          10.212           5.149           5.149
v  Pressure               -41.768          16.051         -11.539         -11.539
v  nu_tilda           2.9895e-007       0.0042695       0.0014957       0.0014957
v  TempC                       21          73.043          21.904          21.904
v  TurbVisc           7.0984e-015        0.005032       0.0017566       0.0017566
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1702:        0.21500E+01

===============================================================


 INSTANT    0.170300000E+04   TIME STEP NUMBER            1703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62095E-02 0.89995E+00
   Friction velocity        uk    :  0.62095E-02 0.89995E+00
   Dimensionless distance   yplus :  0.49991E-01 0.72452E+01
   Friction thermal sca.    tstar : -0.25809E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37299E-01 0.54057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94339E-02      33   0.29857E-03   0.46593E+01 0.16822E+03 
c  Velocity[X]                                      0.18050E+01 
c  Velocity[Y]                                      0.28543E+01 
c  Velocity[Z]                                      0.99021E-30 
c  Pressure     0.11779E-06     506   0.94448E-08   0.11094E+00 0.94955E+03 
c  nu_tilda     0.64856E-05      32   0.46010E-05   0.42227E-06 0.17627E+03 
c  TempC        0.38135E+02      27   0.27471E-03   0.70290E+01 0.28490E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.424          10.211          4.5729          4.5729
v  Velocity[Y]            -2.5457          7.3496        0.030845        0.030845
v  Velocity[Z]       -1.7059e-014     8.4887e-015    -1.5248e-017    -1.5248e-017
v  ǁVelocityǁ         0.0022671          10.211          5.1489          5.1489
v  Pressure               -41.726          16.177         -11.489         -11.489
v  nu_tilda           2.9821e-007       0.0042695       0.0014962       0.0014962
v  TempC                       21          73.043          21.904          21.904
v  TurbVisc           7.0273e-015        0.005032       0.0017571       0.0017571
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1703:        0.21580E+01

===============================================================


 INSTANT    0.170400000E+04   TIME STEP NUMBER            1704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24837E-02 0.90114E+00
   Friction velocity        uk    :  0.24837E-02 0.90114E+00
   Dimensionless distance   yplus :  0.19995E-01 0.72548E+01
   Friction thermal sca.    tstar : -0.10820E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14919E-01 0.54129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94362E-02      33   0.32656E-03   0.46959E+01 0.16851E+03 
c  Velocity[X]                                      0.18468E+01 
c  Velocity[Y]                                      0.28491E+01 
c  Velocity[Z]                                      0.11103E-29 
c  Pressure     0.11689E-06     520   0.92177E-08   0.11323E+00 0.86937E+03 
c  nu_tilda     0.64879E-05      32   0.15448E-04   0.42287E-06 0.17637E+03 
c  TempC        0.38144E+02      27   0.36943E-03   0.41942E+01 0.23075E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4209           10.21          4.5729          4.5729
v  Velocity[Y]            -2.5475          7.3274        0.031064        0.031064
v  Velocity[Z]       -1.6701e-014      8.326e-015     -1.528e-017     -1.528e-017
v  ǁVelocityǁ         0.0022675           10.21          5.1487          5.1487
v  Pressure               -41.725          16.041         -11.541         -11.541
v  nu_tilda           2.9748e-007       0.0042695       0.0014966       0.0014966
v  TempC                       21          73.043          21.905          21.905
v  TurbVisc            6.958e-015        0.005032       0.0017577       0.0017577
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1704:        0.21670E+01

===============================================================


 INSTANT    0.170500000E+04   TIME STEP NUMBER            1705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11956E-01 0.90040E+00
   Friction velocity        uk    :  0.11956E-01 0.90040E+00
   Dimensionless distance   yplus :  0.96254E-01 0.72488E+01
   Friction thermal sca.    tstar : -0.80837E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71816E-01 0.54084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94384E-02      33   0.23169E-03   0.46884E+01 0.16861E+03 
c  Velocity[X]                                      0.18149E+01 
c  Velocity[Y]                                      0.28735E+01 
c  Velocity[Z]                                      0.10102E-29 
c  Pressure     0.10069E-06     538   0.94809E-08   0.95511E-01 0.11488E+04 
c  nu_tilda     0.64902E-05      32   0.45872E-05   0.42341E-06 0.17647E+03 
c  TempC        0.38153E+02      27   0.30757E-03   0.57141E+01 0.27598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4177          10.209          4.5729          4.5729
v  Velocity[Y]            -2.5496          7.3543        0.031284        0.031284
v  Velocity[Z]       -1.7244e-014     8.1675e-015    -1.5313e-017    -1.5313e-017
v  ǁVelocityǁ         0.0022451          10.209          5.1486          5.1486
v  Pressure               -41.685           16.22         -11.482         -11.482
v  nu_tilda           2.9672e-007       0.0042695       0.0014971       0.0014971
v  TempC                       21          73.043          21.905          21.905
v  TurbVisc           6.8893e-015        0.005032       0.0017582       0.0017582
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1705:        0.22540E+01

===============================================================


 INSTANT    0.170600000E+04   TIME STEP NUMBER            1706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34865E-02 0.90184E+00
   Friction velocity        uk    :  0.34865E-02 0.90184E+00
   Dimensionless distance   yplus :  0.28068E-01 0.72605E+01
   Friction thermal sca.    tstar : -0.70423E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20942E-01 0.54171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94407E-02      33   0.28983E-03   0.46481E+01 0.16844E+03 
c  Velocity[X]                                      0.17862E+01 
c  Velocity[Y]                                      0.28620E+01 
c  Velocity[Z]                                      0.97670E-30 
c  Pressure     0.10570E-06     504   0.99217E-08   0.10020E+00 0.59441E+03 
c  nu_tilda     0.64925E-05      32   0.15446E-04   0.42401E-06 0.17657E+03 
c  TempC        0.38161E+02      27   0.34741E-03   0.50899E+01 0.25431E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4145          10.208          4.5729          4.5729
v  Velocity[Y]             -2.552          7.3573        0.031504        0.031504
v  Velocity[Z]       -1.7176e-014     7.9639e-015    -1.5346e-017    -1.5346e-017
v  ǁVelocityǁ         0.0021138          10.208          5.1484          5.1484
v  Pressure               -41.684          16.156         -11.522         -11.522
v  nu_tilda           2.9594e-007       0.0042695       0.0014975       0.0014975
v  TempC                       21          73.043          21.905          21.905
v  TurbVisc           6.8196e-015        0.005032       0.0017588       0.0017588
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1706:        0.21570E+01

===============================================================


 INSTANT    0.170700000E+04   TIME STEP NUMBER            1707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11610E-01 0.90152E+00
   Friction velocity        uk    :  0.11610E-01 0.90152E+00
   Dimensionless distance   yplus :  0.93465E-01 0.72579E+01
   Friction thermal sca.    tstar : -0.69460E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69736E-01 0.54152E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94429E-02      33   0.28980E-03   0.46938E+01 0.16870E+03 
c  Velocity[X]                                      0.18346E+01 
c  Velocity[Y]                                      0.28592E+01 
c  Velocity[Z]                                      0.10189E-29 
c  Pressure     0.11025E-06     426   0.98805E-08   0.10703E+00 0.49316E+03 
c  nu_tilda     0.64948E-05      32   0.45723E-05   0.42456E-06 0.17667E+03 
c  TempC        0.38170E+02      27   0.30665E-03   0.51607E+01 0.24483E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4115          10.207          4.5729          4.5729
v  Velocity[Y]            -2.5542          7.3318        0.031726        0.031726
v  Velocity[Z]       -1.8131e-014     7.8058e-015    -1.5386e-017    -1.5386e-017
v  ǁVelocityǁ         0.0018513          10.207          5.1482          5.1482
v  Pressure               -41.644            16.1         -11.509         -11.509
v  nu_tilda           2.9518e-007       0.0042695       0.0014981       0.0014981
v  TempC                       21          73.042          21.905          21.905
v  TurbVisc           6.7479e-015        0.005032       0.0017593       0.0017593
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1707:        0.19780E+01

===============================================================


 INSTANT    0.170800000E+04   TIME STEP NUMBER            1708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39983E-02 0.90015E+00
   Friction velocity        uk    :  0.39983E-02 0.90015E+00
   Dimensionless distance   yplus :  0.32189E-01 0.72468E+01
   Friction thermal sca.    tstar : -0.76153E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24016E-01 0.54069E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94451E-02      33   0.27644E-03   0.46756E+01 0.16874E+03 
c  Velocity[X]                                      0.17977E+01 
c  Velocity[Y]                                      0.28779E+01 
c  Velocity[Z]                                      0.73813E-30 
c  Pressure     0.96053E-07     377   0.92095E-08   0.91820E-01 0.38558E+03 
c  nu_tilda     0.64971E-05      32   0.15445E-04   0.42516E-06 0.17677E+03 
c  TempC        0.38179E+02      26   0.34500E-03   0.39243E+01 0.23235E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4085          10.206          4.5729          4.5729
v  Velocity[Y]            -2.5563          7.3506        0.031948        0.031948
v  Velocity[Z]       -1.7987e-014     7.6393e-015    -1.5421e-017    -1.5421e-017
v  ǁVelocityǁ         0.0019767          10.206          5.1481          5.1481
v  Pressure                -41.64          16.198         -11.511         -11.511
v  nu_tilda            2.945e-007       0.0042695       0.0014985       0.0014985
v  TempC                       21          73.043          21.906          21.906
v  TurbVisc           6.6794e-015        0.005032       0.0017599       0.0017599
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1708:        0.19060E+01

===============================================================


 INSTANT    0.170900000E+04   TIME STEP NUMBER            1709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70849E-02 0.90102E+00
   Friction velocity        uk    :  0.70849E-02 0.90102E+00
   Dimensionless distance   yplus :  0.57038E-01 0.72538E+01
   Friction thermal sca.    tstar : -0.70799E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42557E-01 0.54122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94474E-02      33   0.30279E-03   0.46795E+01 0.16878E+03 
c  Velocity[X]                                      0.18102E+01 
c  Velocity[Y]                                      0.28693E+01 
c  Velocity[Z]                                      0.12975E-29 
c  Pressure     0.12128E-06     346   0.95787E-08   0.11560E+00 0.53013E+03 
c  nu_tilda     0.64994E-05      32   0.45688E-05   0.42571E-06 0.17687E+03 
c  TempC        0.38187E+02      27   0.31035E-03   0.46475E+01 0.25623E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4055          10.205          4.5729          4.5729
v  Velocity[Y]            -2.5582          7.3245        0.032171        0.032171
v  Velocity[Z]       -1.7679e-014     8.0571e-015    -1.5439e-017    -1.5439e-017
v  ǁVelocityǁ         0.0021833          10.205          5.1479          5.1479
v  Pressure               -41.601          16.093         -11.511         -11.511
v  nu_tilda           2.9392e-007       0.0042695        0.001499        0.001499
v  TempC                       21          73.043          21.906          21.906
v  TurbVisc           6.6176e-015        0.005032       0.0017605       0.0017605
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1709:        0.17930E+01

===============================================================


 INSTANT    0.171000000E+04   TIME STEP NUMBER            1710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54239E-02 0.90039E+00
   Friction velocity        uk    :  0.54239E-02 0.90039E+00
   Dimensionless distance   yplus :  0.43666E-01 0.72488E+01
   Friction thermal sca.    tstar : -0.72059E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32580E-01 0.54084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94496E-02      33   0.25067E-03   0.46951E+01 0.16895E+03 
c  Velocity[X]                                      0.18299E+01 
c  Velocity[Y]                                      0.28652E+01 
c  Velocity[Z]                                      0.10257E-29 
c  Pressure     0.11064E-06     424   0.97766E-08   0.10584E+00 0.45486E+03 
c  nu_tilda     0.65017E-05      32   0.15437E-04   0.42630E-06 0.17697E+03 
c  TempC        0.38196E+02      27   0.34951E-03   0.44028E+01 0.24850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4024          10.204          4.5729          4.5729
v  Velocity[Y]            -2.5601           7.351        0.032395        0.032395
v  Velocity[Z]       -1.7615e-014     7.7159e-015    -1.5467e-017    -1.5467e-017
v  ǁVelocityǁ         0.0020844          10.204          5.1478          5.1478
v  Pressure               -41.598           16.21         -11.509         -11.509
v  nu_tilda           2.9342e-007       0.0042695       0.0014994       0.0014994
v  TempC                       21          73.043          21.906          21.906
v  TurbVisc           6.5655e-015        0.005032        0.001761        0.001761
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1710:        0.19750E+01

===============================================================


 INSTANT    0.171100000E+04   TIME STEP NUMBER            1711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80906E-02 0.90184E+00
   Friction velocity        uk    :  0.80906E-02 0.90184E+00
   Dimensionless distance   yplus :  0.65135E-01 0.72604E+01
   Friction thermal sca.    tstar : -0.69616E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48598E-01 0.54171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94519E-02      33   0.28515E-03   0.46731E+01 0.16897E+03 
c  Velocity[X]                                      0.17876E+01 
c  Velocity[Y]                                      0.28855E+01 
c  Velocity[Z]                                      0.97602E-30 
c  Pressure     0.96464E-07     489   0.93899E-08   0.92262E-01 0.55748E+03 
c  nu_tilda     0.65040E-05      32   0.45559E-05   0.42686E-06 0.17707E+03 
c  TempC        0.38204E+02      27   0.30844E-03   0.51405E+01 0.24274E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3993          10.204          4.5729          4.5729
v  Velocity[Y]             -2.562          7.3618         0.03262         0.03262
v  Velocity[Z]       -1.7956e-014     7.4461e-015    -1.5488e-017    -1.5488e-017
v  ǁVelocityǁ         0.0021582          10.204          5.1476          5.1476
v  Pressure                -41.56          16.239         -11.484         -11.484
v  nu_tilda           2.9302e-007       0.0042695       0.0014999       0.0014999
v  TempC                       21          73.044          21.907          21.907
v  TurbVisc           6.5213e-015        0.005032       0.0017616       0.0017616
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1711:        0.21210E+01

===============================================================


 INSTANT    0.171200000E+04   TIME STEP NUMBER            1712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68221E-02 0.90135E+00
   Friction velocity        uk    :  0.68221E-02 0.90135E+00
   Dimensionless distance   yplus :  0.54922E-01 0.72565E+01
   Friction thermal sca.    tstar : -0.73589E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40978E-01 0.54142E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94541E-02      33   0.28368E-03   0.47007E+01 0.16908E+03 
c  Velocity[X]                                      0.18253E+01 
c  Velocity[Y]                                      0.28754E+01 
c  Velocity[Z]                                      0.94426E-30 
c  Pressure     0.13073E-06     504   0.96064E-08   0.12534E+00 0.89559E+03 
c  nu_tilda     0.65063E-05      32   0.15437E-04   0.42745E-06 0.17718E+03 
c  TempC        0.38213E+02      27   0.32170E-03   0.43068E+01 0.23795E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3964          10.203          4.5729          4.5729
v  Velocity[Y]            -2.5644          7.3268        0.032845        0.032845
v  Velocity[Z]       -1.7651e-014     7.3001e-015     -1.552e-017     -1.552e-017
v  ǁVelocityǁ         0.0021372          10.203          5.1475          5.1475
v  Pressure               -41.556          16.092         -11.536         -11.536
v  nu_tilda           2.9267e-007       0.0042695       0.0015003       0.0015003
v  TempC                       21          73.043          21.907          21.907
v  TurbVisc           6.4858e-015        0.005032       0.0017621       0.0017621
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1712:        0.21410E+01

===============================================================


 INSTANT    0.171300000E+04   TIME STEP NUMBER            1713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27740E-02 0.89992E+00
   Friction velocity        uk    :  0.27740E-02 0.89992E+00
   Dimensionless distance   yplus :  0.22333E-01 0.72450E+01
   Friction thermal sca.    tstar : -0.72101E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16663E-01 0.54055E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94563E-02      33   0.29068E-03   0.46998E+01 0.16917E+03 
c  Velocity[X]                                      0.18258E+01 
c  Velocity[Y]                                      0.28740E+01 
c  Velocity[Z]                                      0.84863E-30 
c  Pressure     0.10067E-06     520   0.97970E-08   0.96454E-01 0.11386E+04 
c  nu_tilda     0.65087E-05      32   0.45387E-05   0.42800E-06 0.17728E+03 
c  TempC        0.38222E+02      27   0.38931E-03   0.37223E+01 0.24284E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3935          10.202          4.5729          4.5729
v  Velocity[Y]            -2.5666          7.3496        0.033072        0.033072
v  Velocity[Z]        -1.763e-014     7.3534e-015    -1.5541e-017    -1.5541e-017
v  ǁVelocityǁ         0.0021269          10.202          5.1473          5.1473
v  Pressure               -41.515          16.263         -11.476         -11.476
v  nu_tilda           2.9237e-007       0.0042695       0.0015009       0.0015009
v  TempC                       21          73.043          21.907          21.907
v  TurbVisc           6.4549e-015        0.005032       0.0017627       0.0017627
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1713:        0.23530E+01

===============================================================


 INSTANT    0.171400000E+04   TIME STEP NUMBER            1714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73639E-02 0.90090E+00
   Friction velocity        uk    :  0.73639E-02 0.90090E+00
   Dimensionless distance   yplus :  0.59285E-01 0.72529E+01
   Friction thermal sca.    tstar : -0.69615E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44233E-01 0.54115E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94586E-02      33   0.29115E-03   0.47001E+01 0.16929E+03 
c  Velocity[X]                                      0.18093E+01 
c  Velocity[Y]                                      0.28909E+01 
c  Velocity[Z]                                      0.79594E-30 
c  Pressure     0.10958E-06     521   0.93765E-08   0.10628E+00 0.97748E+03 
c  nu_tilda     0.65110E-05      32   0.15431E-04   0.42860E-06 0.17738E+03 
c  TempC        0.38230E+02      27   0.38481E-03   0.60367E+01 0.27547E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3904          10.201          4.5729          4.5729
v  Velocity[Y]            -2.5687          7.3235        0.033299        0.033299
v  Velocity[Z]       -1.7232e-014     7.2957e-015    -1.5559e-017    -1.5559e-017
v  ǁVelocityǁ         0.0021045          10.201          5.1472          5.1472
v  Pressure               -41.513          16.107         -11.534         -11.534
v  nu_tilda           2.9211e-007       0.0042695       0.0015013       0.0015013
v  TempC                       21          73.043          21.908          21.908
v  TurbVisc           6.4287e-015        0.005032       0.0017632       0.0017632
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1714:        0.24070E+01

===============================================================


 INSTANT    0.171500000E+04   TIME STEP NUMBER            1715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93860E-02 0.89992E+00
   Friction velocity        uk    :  0.93860E-02 0.89992E+00
   Dimensionless distance   yplus :  0.75564E-01 0.72450E+01
   Friction thermal sca.    tstar : -0.70436E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56379E-01 0.54056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94608E-02      33   0.24552E-03   0.47010E+01 0.16930E+03 
c  Velocity[X]                                      0.18179E+01 
c  Velocity[Y]                                      0.28831E+01 
c  Velocity[Z]                                      0.13440E-29 
c  Pressure     0.11783E-06     505   0.99398E-08   0.11141E+00 0.10448E+04 
c  nu_tilda     0.65133E-05      32   0.45365E-05   0.42915E-06 0.17748E+03 
c  TempC        0.38239E+02      27   0.30317E-03   0.61956E+01 0.26617E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3873            10.2          4.5729          4.5729
v  Velocity[Y]            -2.5707          7.3462        0.033527        0.033527
v  Velocity[Z]        -1.749e-014     7.9468e-015    -1.5574e-017    -1.5574e-017
v  ǁVelocityǁ         0.0020897            10.2           5.147           5.147
v  Pressure               -41.474          16.255          -11.48          -11.48
v  nu_tilda           2.9189e-007       0.0042695       0.0015018       0.0015018
v  TempC                       21          73.043          21.908          21.908
v  TurbVisc           6.4058e-015        0.005032       0.0017638       0.0017638
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1715:        0.23400E+01

===============================================================


 INSTANT    0.171600000E+04   TIME STEP NUMBER            1716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94961E-02 0.90160E+00
   Friction velocity        uk    :  0.94961E-02 0.90160E+00
   Dimensionless distance   yplus :  0.76450E-01 0.72585E+01
   Friction thermal sca.    tstar : -0.74046E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57040E-01 0.54156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94631E-02      33   0.31163E-03   0.47015E+01 0.16943E+03 
c  Velocity[X]                                      0.18208E+01 
c  Velocity[Y]                                      0.28807E+01 
c  Velocity[Z]                                      0.10223E-29 
c  Pressure     0.10814E-06     474   0.96309E-08   0.10370E+00 0.45410E+03 
c  nu_tilda     0.65156E-05      32   0.15425E-04   0.42975E-06 0.17758E+03 
c  TempC        0.38247E+02      26   0.25935E-03   0.47179E+01 0.24415E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3842          10.199          4.5729          4.5729
v  Velocity[Y]            -2.5725          7.3564        0.033756        0.033756
v  Velocity[Z]       -1.7247e-014     7.6007e-015    -1.5593e-017    -1.5593e-017
v  ǁVelocityǁ         0.0019743          10.199          5.1469          5.1469
v  Pressure               -41.472          16.229         -11.511         -11.511
v  nu_tilda           2.9169e-007       0.0042695       0.0015022       0.0015022
v  TempC                       21          73.043          21.908          21.908
v  TurbVisc           6.3865e-015        0.005032       0.0017643       0.0017643
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1716:        0.22210E+01

===============================================================


 INSTANT    0.171700000E+04   TIME STEP NUMBER            1717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78795E-02 0.90125E+00
   Friction velocity        uk    :  0.78795E-02 0.90125E+00
   Dimensionless distance   yplus :  0.63436E-01 0.72557E+01
   Friction thermal sca.    tstar : -0.86710E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47330E-01 0.54135E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94653E-02      33   0.27570E-03   0.47335E+01 0.16968E+03 
c  Velocity[X]                                      0.18326E+01 
c  Velocity[Y]                                      0.29009E+01 
c  Velocity[Z]                                      0.87456E-30 
c  Pressure     0.11750E-06     311   0.99276E-08   0.11279E+00 0.52898E+03 
c  nu_tilda     0.65179E-05      32   0.45242E-05   0.43031E-06 0.17768E+03 
c  TempC        0.38256E+02      27   0.40490E-03   0.38740E+01 0.23644E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.381          10.198          4.5729          4.5729
v  Velocity[Y]            -2.5743          7.3216        0.033985        0.033985
v  Velocity[Z]        -1.749e-014     7.3261e-015    -1.5615e-017    -1.5615e-017
v  ǁVelocityǁ         0.0020603          10.198          5.1467          5.1467
v  Pressure               -41.432          16.137         -11.508         -11.508
v  nu_tilda           2.9154e-007       0.0042695       0.0015027       0.0015027
v  TempC                       21          73.043          21.909          21.909
v  TurbVisc           6.3688e-015        0.005032       0.0017649       0.0017649
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1717:        0.17580E+01

===============================================================


 INSTANT    0.171800000E+04   TIME STEP NUMBER            1718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98312E-02 0.89994E+00
   Friction velocity        uk    :  0.98312E-02 0.89994E+00
   Dimensionless distance   yplus :  0.79148E-01 0.72452E+01
   Friction thermal sca.    tstar : -0.13831E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59053E-01 0.54057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94675E-02      33   0.25997E-03   0.46967E+01 0.16954E+03 
c  Velocity[X]                                      0.18066E+01 
c  Velocity[Y]                                      0.28901E+01 
c  Velocity[Z]                                      0.10822E-29 
c  Pressure     0.10185E-06     424   0.97876E-08   0.98453E-01 0.49916E+03 
c  nu_tilda     0.65202E-05      32   0.15431E-04   0.43091E-06 0.17778E+03 
c  TempC        0.38265E+02      26   0.35401E-03   0.69849E+01 0.31191E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3781          10.197          4.5729          4.5729
v  Velocity[Y]            -2.5767          7.3434        0.034215        0.034215
v  Velocity[Z]       -1.7498e-014     7.3043e-015     -1.564e-017     -1.564e-017
v  ǁVelocityǁ         0.0019985          10.197          5.1466          5.1466
v  Pressure               -41.429          16.261         -11.504         -11.504
v  nu_tilda            2.914e-007       0.0042695       0.0015032       0.0015032
v  TempC                       21          73.043          21.909          21.909
v  TurbVisc           6.3556e-015        0.005032       0.0017654       0.0017654
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1718:        0.20860E+01

===============================================================


 INSTANT    0.171900000E+04   TIME STEP NUMBER            1719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17475E-02 0.90088E+00
   Friction velocity        uk    :  0.17475E-02 0.90088E+00
   Dimensionless distance   yplus :  0.14069E-01 0.72527E+01
   Friction thermal sca.    tstar : -0.25026E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10497E-01 0.54113E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94698E-02      33   0.32694E-03   0.46940E+01 0.16959E+03 
c  Velocity[X]                                      0.18077E+01 
c  Velocity[Y]                                      0.28863E+01 
c  Velocity[Z]                                      0.95606E-30 
c  Pressure     0.10637E-06     378   0.99993E-08   0.10322E+00 0.53502E+03 
c  nu_tilda     0.65225E-05      32   0.45061E-05   0.43146E-06 0.17788E+03 
c  TempC        0.38273E+02      26   0.33983E-03   0.61467E+01 0.25788E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3752          10.197          4.5729          4.5729
v  Velocity[Y]             -2.579          7.3241        0.034447        0.034447
v  Velocity[Z]       -1.7562e-014     7.3656e-015    -1.5656e-017    -1.5656e-017
v  ǁVelocityǁ         0.0020175          10.197          5.1464          5.1464
v  Pressure               -41.387          16.175         -11.498         -11.498
v  nu_tilda            2.913e-007       0.0042695       0.0015037       0.0015037
v  TempC                       21          73.043          21.909          21.909
v  TurbVisc           6.3431e-015        0.005032        0.001766        0.001766
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1719:        0.22020E+01

===============================================================


 INSTANT    0.172000000E+04   TIME STEP NUMBER            1720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12115E-01 0.90005E+00
   Friction velocity        uk    :  0.12115E-01 0.90005E+00
   Dimensionless distance   yplus :  0.97532E-01 0.72460E+01
   Friction thermal sca.    tstar : -0.10135E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72770E-01 0.54063E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94720E-02      33   0.24890E-03   0.47526E+01 0.16994E+03 
c  Velocity[X]                                      0.18428E+01 
c  Velocity[Y]                                      0.29098E+01 
c  Velocity[Z]                                      0.85453E-30 
c  Pressure     0.13517E-06     441   0.99353E-08   0.12681E+00 0.30430E+03 
c  nu_tilda     0.65249E-05      32   0.15421E-04   0.43206E-06 0.17798E+03 
c  TempC        0.38282E+02      26   0.27877E-03   0.43034E+01 0.24332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.372          10.196          4.5729          4.5729
v  Velocity[Y]             -2.581          7.3422        0.034679        0.034679
v  Velocity[Z]       -1.7493e-014     7.2855e-015    -1.5672e-017    -1.5672e-017
v  ǁVelocityǁ         0.0019804          10.196          5.1463          5.1463
v  Pressure               -41.386          16.218         -11.514         -11.514
v  nu_tilda           2.9122e-007       0.0042695       0.0015041       0.0015041
v  TempC                       21          73.043           21.91           21.91
v  TurbVisc           6.3348e-015        0.005032       0.0017665       0.0017665
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1720:        0.23870E+01

===============================================================


 INSTANT    0.172100000E+04   TIME STEP NUMBER            1721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16288E-02 0.90180E+00
   Friction velocity        uk    :  0.16288E-02 0.90180E+00
   Dimensionless distance   yplus :  0.13113E-01 0.72601E+01
   Friction thermal sca.    tstar : -0.76528E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97838E-02 0.54168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94743E-02      33   0.26920E-03   0.47142E+01 0.16986E+03 
c  Velocity[X]                                      0.18149E+01 
c  Velocity[Y]                                      0.28993E+01 
c  Velocity[Z]                                      0.11638E-29 
c  Pressure     0.10464E-06     505   0.93779E-08   0.10086E+00 0.80068E+03 
c  nu_tilda     0.65272E-05      32   0.45057E-05   0.43262E-06 0.17808E+03 
c  TempC        0.38290E+02      26   0.35260E-03   0.37781E+01 0.22956E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3689          10.195          4.5729          4.5729
v  Velocity[Y]             -2.583           7.355        0.034912        0.034912
v  Velocity[Z]        -1.728e-014     7.9228e-015    -1.5685e-017    -1.5685e-017
v  ǁVelocityǁ         0.0019607          10.195          5.1461          5.1461
v  Pressure               -41.346          16.305         -11.472         -11.472
v  nu_tilda           2.9121e-007       0.0042695       0.0015046       0.0015046
v  TempC                       21          73.044           21.91           21.91
v  TurbVisc           6.3281e-015        0.005032       0.0017671       0.0017671
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1721:        0.21420E+01

===============================================================


 INSTANT    0.172200000E+04   TIME STEP NUMBER            1722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11235E-01 0.90134E+00
   Friction velocity        uk    :  0.11235E-01 0.90134E+00
   Dimensionless distance   yplus :  0.90446E-01 0.72564E+01
   Friction thermal sca.    tstar : -0.68349E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67483E-01 0.54141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94765E-02      33   0.31063E-03   0.47085E+01 0.16987E+03 
c  Velocity[X]                                      0.18170E+01 
c  Velocity[Y]                                      0.28915E+01 
c  Velocity[Z]                                      0.97201E-30 
c  Pressure     0.10976E-06     505   0.92637E-08   0.10686E+00 0.94364E+03 
c  nu_tilda     0.65295E-05      32   0.15417E-04   0.43322E-06 0.17818E+03 
c  TempC        0.38299E+02      27   0.38781E-03   0.62154E+01 0.25642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.366          10.194          4.5729          4.5729
v  Velocity[Y]            -2.5848          7.3273        0.035145        0.035145
v  Velocity[Z]       -1.6937e-014     7.6082e-015      -1.57e-017      -1.57e-017
v  ǁVelocityǁ         0.0019356          10.194           5.146           5.146
v  Pressure               -41.343          16.158         -11.528         -11.528
v  nu_tilda           2.9125e-007       0.0042695        0.001505        0.001505
v  TempC                       21          73.043           21.91           21.91
v  TurbVisc            6.327e-015        0.005032       0.0017676       0.0017676
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1722:        0.21490E+01

===============================================================


 INSTANT    0.172300000E+04   TIME STEP NUMBER            1723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61007E-02 0.89978E+00
   Friction velocity        uk    :  0.61007E-02 0.89978E+00
   Dimensionless distance   yplus :  0.49115E-01 0.72438E+01
   Friction thermal sca.    tstar : -0.69297E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36645E-01 0.54047E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94787E-02      33   0.27692E-03   0.47310E+01 0.17009E+03 
c  Velocity[X]                                      0.18168E+01 
c  Velocity[Y]                                      0.29142E+01 
c  Velocity[Z]                                      0.90854E-30 
c  Pressure     0.13119E-06     504   0.97541E-08   0.12337E+00 0.86083E+03 
c  nu_tilda     0.65318E-05      32   0.44888E-05   0.43377E-06 0.17828E+03 
c  TempC        0.38307E+02      27   0.29030E-03   0.64531E+01 0.26932E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3631          10.193          4.5729          4.5729
v  Velocity[Y]            -2.5865          7.3426         0.03538         0.03538
v  Velocity[Z]       -1.6877e-014     8.2016e-015    -1.5712e-017    -1.5712e-017
v  ǁVelocityǁ         0.0019223          10.193          5.1459          5.1459
v  Pressure               -41.304          16.262         -11.484         -11.484
v  nu_tilda           2.9133e-007       0.0042695       0.0015055       0.0015055
v  TempC                       21          73.043          21.911          21.911
v  TurbVisc           6.3304e-015        0.005032       0.0017682       0.0017682
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1723:        0.21530E+01

===============================================================


 INSTANT    0.172400000E+04   TIME STEP NUMBER            1724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94593E-02 0.90111E+00
   Friction velocity        uk    :  0.94593E-02 0.90111E+00
   Dimensionless distance   yplus :  0.76154E-01 0.72546E+01
   Friction thermal sca.    tstar : -0.69797E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56819E-01 0.54127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94810E-02      33   0.28487E-03   0.47216E+01 0.17008E+03 
c  Velocity[X]                                      0.18194E+01 
c  Velocity[Y]                                      0.29021E+01 
c  Velocity[Z]                                      0.10970E-29 
c  Pressure     0.12458E-06     488   0.92957E-08   0.12150E+00 0.51372E+03 
c  nu_tilda     0.65341E-05      32   0.15419E-04   0.43437E-06 0.17838E+03 
c  TempC        0.38316E+02      26   0.35781E-03   0.39058E+01 0.23232E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3601          10.192          4.5729          4.5729
v  Velocity[Y]            -2.5889          7.3194        0.035615        0.035615
v  Velocity[Z]       -1.6377e-014     7.4876e-015    -1.5737e-017    -1.5737e-017
v  ǁVelocityǁ         0.0018941          10.192          5.1457          5.1457
v  Pressure               -41.297          16.206         -11.515         -11.515
v  nu_tilda           2.9141e-007       0.0042695       0.0015059       0.0015059
v  TempC                       21          73.044          21.911          21.911
v  TurbVisc           6.3374e-015        0.005032       0.0017687       0.0017687
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1724:        0.21090E+01

===============================================================


 INSTANT    0.172500000E+04   TIME STEP NUMBER            1725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91341E-02 0.89997E+00
   Friction velocity        uk    :  0.91341E-02 0.89997E+00
   Dimensionless distance   yplus :  0.73536E-01 0.72453E+01
   Friction thermal sca.    tstar : -0.69579E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54866E-01 0.54058E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94832E-02      33   0.26993E-03   0.47101E+01 0.17009E+03 
c  Velocity[X]                                      0.18100E+01 
c  Velocity[Y]                                      0.29001E+01 
c  Velocity[Z]                                      0.88741E-30 
c  Pressure     0.93636E-07     490   0.94739E-08   0.89785E-01 0.79789E+03 
c  nu_tilda     0.65365E-05      32   0.44781E-05   0.43493E-06 0.17848E+03 
c  TempC        0.38325E+02      27   0.29405E-03   0.48375E+01 0.25163E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.357          10.191          4.5729          4.5729
v  Velocity[Y]            -2.5912          7.3479        0.035851        0.035851
v  Velocity[Z]       -1.5901e-014     7.4064e-015    -1.5747e-017    -1.5747e-017
v  ǁVelocityǁ         0.0018839          10.191          5.1456          5.1456
v  Pressure                -41.26          16.303         -11.475         -11.475
v  nu_tilda           2.9149e-007       0.0042695       0.0015065       0.0015065
v  TempC                       21          73.044          21.911          21.911
v  TurbVisc           6.3444e-015        0.005032       0.0017693       0.0017693
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1725:        0.21090E+01

===============================================================


 INSTANT    0.172600000E+04   TIME STEP NUMBER            1726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63827E-02 0.90140E+00
   Friction velocity        uk    :  0.63827E-02 0.90140E+00
   Dimensionless distance   yplus :  0.51385E-01 0.72569E+01
   Friction thermal sca.    tstar : -0.68779E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38339E-01 0.54144E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94855E-02      33   0.30481E-03   0.47372E+01 0.17030E+03 
c  Velocity[X]                                      0.18234E+01 
c  Velocity[Y]                                      0.29138E+01 
c  Velocity[Z]                                      0.87476E-30 
c  Pressure     0.12092E-06     440   0.99616E-08   0.11453E+00 0.47500E+03 
c  nu_tilda     0.65388E-05      32   0.15408E-04   0.43553E-06 0.17858E+03 
c  TempC        0.38333E+02      27   0.39998E-03   0.36647E+01 0.22598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3539           10.19          4.5729          4.5729
v  Velocity[Y]            -2.5933          7.3503        0.036088        0.036088
v  Velocity[Z]       -1.6152e-014     7.2677e-015    -1.5765e-017    -1.5765e-017
v  ǁVelocityǁ         0.0018553           10.19          5.1455          5.1455
v  Pressure               -41.255          16.266         -11.505         -11.505
v  nu_tilda           2.9153e-007       0.0042695       0.0015069       0.0015069
v  TempC                       21          73.043          21.912          21.912
v  TurbVisc           6.3511e-015        0.005032       0.0017698       0.0017698
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1726:        0.19960E+01

===============================================================


 INSTANT    0.172700000E+04   TIME STEP NUMBER            1727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96874E-02 0.90115E+00
   Friction velocity        uk    :  0.96874E-02 0.90115E+00
   Dimensionless distance   yplus :  0.77990E-01 0.72549E+01
   Friction thermal sca.    tstar : -0.67948E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58189E-01 0.54129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94877E-02      33   0.26578E-03   0.47607E+01 0.17050E+03 
c  Velocity[X]                                      0.18490E+01 
c  Velocity[Y]                                      0.29117E+01 
c  Velocity[Z]                                      0.10067E-29 
c  Pressure     0.11552E-06     441   0.98361E-08   0.11375E+00 0.46571E+03 
c  nu_tilda     0.65411E-05      32   0.44716E-05   0.43610E-06 0.17868E+03 
c  TempC        0.38342E+02      27   0.37514E-03   0.61744E+01 0.27287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3507          10.189          4.5729          4.5729
v  Velocity[Y]            -2.5952          7.3245        0.036325        0.036325
v  Velocity[Z]       -1.6064e-014     7.8872e-015    -1.5774e-017    -1.5774e-017
v  ǁVelocityǁ         0.0018483          10.189          5.1453          5.1453
v  Pressure               -41.217          16.223         -11.492         -11.492
v  nu_tilda           2.9159e-007       0.0042695       0.0015074       0.0015074
v  TempC                       21          73.043          21.912          21.912
v  TurbVisc           6.3552e-015        0.005032       0.0017704       0.0017704
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1727:        0.20040E+01

===============================================================


 INSTANT    0.172800000E+04   TIME STEP NUMBER            1728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22065E-02 0.89961E+00
   Friction velocity        uk    :  0.22065E-02 0.89961E+00
   Dimensionless distance   yplus :  0.17764E-01 0.72424E+01
   Friction thermal sca.    tstar : -0.69987E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13254E-01 0.54037E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94900E-02      33   0.30612E-03   0.47111E+01 0.17032E+03 
c  Velocity[X]                                      0.18073E+01 
c  Velocity[Y]                                      0.29038E+01 
c  Velocity[Z]                                      0.11469E-29 
c  Pressure     0.87043E-07     329   0.93732E-08   0.83079E-01 0.36971E+03 
c  nu_tilda     0.65434E-05      32   0.15412E-04   0.43669E-06 0.17878E+03 
c  TempC        0.38350E+02      27   0.32679E-03   0.61326E+01 0.26989E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3478          10.189          4.5729          4.5729
v  Velocity[Y]            -2.5971          7.3439        0.036564        0.036564
v  Velocity[Z]       -1.6481e-014     7.4897e-015    -1.5791e-017    -1.5791e-017
v  ǁVelocityǁ         0.0018195          10.189          5.1452          5.1452
v  Pressure               -41.212          16.315         -11.496         -11.496
v  nu_tilda           2.9164e-007       0.0042695       0.0015078       0.0015078
v  TempC                       21          73.043          21.912          21.912
v  TurbVisc             6.36e-015        0.005032       0.0017709       0.0017709
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1728:        0.17580E+01

===============================================================


 INSTANT    0.172900000E+04   TIME STEP NUMBER            1729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54139E-02 0.90046E+00
   Friction velocity        uk    :  0.54139E-02 0.90046E+00
   Dimensionless distance   yplus :  0.43586E-01 0.72493E+01
   Friction thermal sca.    tstar : -0.68145E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32520E-01 0.54088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94922E-02      33   0.29661E-03   0.47458E+01 0.17056E+03 
c  Velocity[X]                                      0.18284E+01 
c  Velocity[Y]                                      0.29173E+01 
c  Velocity[Z]                                      0.86960E-30 
c  Pressure     0.12269E-06     314   0.95395E-08   0.11752E+00 0.55530E+03 
c  nu_tilda     0.65457E-05      32   0.44572E-05   0.43725E-06 0.17888E+03 
c  TempC        0.38359E+02      27   0.37850E-03   0.38614E+01 0.22277E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3449          10.188          4.5729          4.5729
v  Velocity[Y]            -2.5988          7.3162        0.036803        0.036803
v  Velocity[Z]       -1.6607e-014     7.9938e-015    -1.5804e-017    -1.5804e-017
v  ǁVelocityǁ         0.0018116          10.188           5.145           5.145
v  Pressure               -41.171          16.216         -11.492         -11.492
v  nu_tilda           2.9171e-007       0.0042695       0.0015083       0.0015083
v  TempC                       21          73.044          21.913          21.913
v  TurbVisc           6.3642e-015        0.005032       0.0017715       0.0017715
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1729:        0.17180E+01

===============================================================


 INSTANT    0.173000000E+04   TIME STEP NUMBER            1730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76615E-02 0.89983E+00
   Friction velocity        uk    :  0.76615E-02 0.89983E+00
   Dimensionless distance   yplus :  0.61681E-01 0.72443E+01
   Friction thermal sca.    tstar : -0.74330E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46021E-01 0.54050E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94944E-02      33   0.23497E-03   0.47387E+01 0.17057E+03 
c  Velocity[X]                                      0.18250E+01 
c  Velocity[Y]                                      0.29137E+01 
c  Velocity[Z]                                      0.11204E-29 
c  Pressure     0.99106E-07     377   0.92962E-08   0.96217E-01 0.40826E+03 
c  nu_tilda     0.65480E-05      32   0.15407E-04   0.43786E-06 0.17898E+03 
c  TempC        0.38367E+02      27   0.30334E-03   0.45958E+01 0.23736E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3418          10.187          4.5729          4.5729
v  Velocity[Y]             -2.601          7.3406        0.037043        0.037043
v  Velocity[Z]       -1.6589e-014     8.1757e-015    -1.5818e-017    -1.5818e-017
v  ǁVelocityǁ         0.0017851          10.187          5.1449          5.1449
v  Pressure               -41.169          16.318         -11.495         -11.495
v  nu_tilda           2.9179e-007       0.0042695       0.0015087       0.0015087
v  TempC                       21          73.044          21.913          21.913
v  TurbVisc           6.3706e-015        0.005032        0.001772        0.001772
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1730:        0.18600E+01

===============================================================


 INSTANT    0.173100000E+04   TIME STEP NUMBER            1731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77125E-02 0.90119E+00
   Friction velocity        uk    :  0.77125E-02 0.90119E+00
   Dimensionless distance   yplus :  0.62091E-01 0.72552E+01
   Friction thermal sca.    tstar : -0.69117E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46327E-01 0.54132E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94967E-02      33   0.32684E-03   0.47361E+01 0.17066E+03 
c  Velocity[X]                                      0.18218E+01 
c  Velocity[Y]                                      0.29143E+01 
c  Velocity[Z]                                      0.10357E-29 
c  Pressure     0.11735E-06     458   0.95154E-08   0.11159E+00 0.58429E+03 
c  nu_tilda     0.65504E-05      32   0.44609E-05   0.43841E-06 0.17908E+03 
c  TempC        0.38376E+02      27   0.37453E-03   0.53052E+01 0.25119E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3386          10.186          4.5729          4.5729
v  Velocity[Y]            -2.6033          7.3484        0.037284        0.037284
v  Velocity[Z]       -1.6506e-014     8.8563e-015    -1.5823e-017    -1.5823e-017
v  ǁVelocityǁ         0.0017795          10.186          5.1448          5.1448
v  Pressure               -41.129          16.341         -11.468         -11.468
v  nu_tilda           2.9185e-007       0.0042695       0.0015093       0.0015093
v  TempC                       21          73.044          21.913          21.913
v  TurbVisc           6.3771e-015        0.005032       0.0017726       0.0017726
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1731:        0.20460E+01

===============================================================


 INSTANT    0.173200000E+04   TIME STEP NUMBER            1732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.65806E-02 0.90094E+00
   Friction velocity        uk    :  0.65806E-02 0.90094E+00
   Dimensionless distance   yplus :  0.52978E-01 0.72532E+01
   Friction thermal sca.    tstar : -0.87034E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39528E-01 0.54117E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.94989E-02      33   0.30053E-03   0.47693E+01 0.17088E+03 
c  Velocity[X]                                      0.18603E+01 
c  Velocity[Y]                                      0.29089E+01 
c  Velocity[Z]                                      0.93714E-30 
c  Pressure     0.11623E-06     521   0.95798E-08   0.11377E+00 0.93090E+03 
c  nu_tilda     0.65527E-05      32   0.15400E-04   0.43902E-06 0.17919E+03 
c  TempC        0.38384E+02      27   0.36703E-03   0.59821E+01 0.28488E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3358          10.185          4.5729          4.5729
v  Velocity[Y]            -2.6054          7.3195        0.037526        0.037526
v  Velocity[Z]       -1.6307e-014     8.8357e-015    -1.5836e-017    -1.5836e-017
v  ǁVelocityǁ         0.0017515          10.185          5.1447          5.1447
v  Pressure               -41.125          16.195         -11.523         -11.523
v  nu_tilda           2.9188e-007       0.0042695       0.0015097       0.0015097
v  TempC                       21          73.043          21.914          21.914
v  TurbVisc           6.3829e-015        0.005032       0.0017731       0.0017731
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1732:        0.21910E+01

===============================================================


 INSTANT    0.173300000E+04   TIME STEP NUMBER            1733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15598E-02 0.89952E+00
   Friction velocity        uk    :  0.15598E-02 0.89952E+00
   Dimensionless distance   yplus :  0.12557E-01 0.72418E+01
   Friction thermal sca.    tstar : -0.13831E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93691E-02 0.54032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95011E-02      33   0.27466E-03   0.47468E+01 0.17088E+03 
c  Velocity[X]                                      0.18126E+01 
c  Velocity[Y]                                      0.29342E+01 
c  Velocity[Z]                                      0.10392E-29 
c  Pressure     0.98993E-07     536   0.99706E-08   0.95004E-01 0.12505E+04 
c  nu_tilda     0.65550E-05      32   0.44517E-05   0.43958E-06 0.17928E+03 
c  TempC        0.38393E+02      27   0.35118E-03   0.48622E+01 0.25054E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3329          10.184          4.5729          4.5729
v  Velocity[Y]            -2.6073          7.3403        0.037768        0.037768
v  Velocity[Z]       -1.6255e-014      9.391e-015    -1.5842e-017    -1.5842e-017
v  ǁVelocityǁ         0.0017373          10.184          5.1445          5.1445
v  Pressure               -41.086          16.393         -11.458         -11.458
v  nu_tilda           2.9191e-007       0.0042695       0.0015102       0.0015102
v  TempC                       21          73.044          21.914          21.914
v  TurbVisc           6.3855e-015        0.005032       0.0017737       0.0017737
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1733:        0.22360E+01

===============================================================


 INSTANT    0.173400000E+04   TIME STEP NUMBER            1734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73450E-02 0.90044E+00
   Friction velocity        uk    :  0.73450E-02 0.90044E+00
   Dimensionless distance   yplus :  0.59132E-01 0.72492E+01
   Friction thermal sca.    tstar : -0.19652E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44119E-01 0.54087E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95034E-02      33   0.30300E-03   0.47442E+01 0.17090E+03 
c  Velocity[X]                                      0.18212E+01 
c  Velocity[Y]                                      0.29230E+01 
c  Velocity[Z]                                      0.10945E-29 
c  Pressure     0.10570E-06     538   0.94632E-08   0.10166E+00 0.10815E+04 
c  nu_tilda     0.65573E-05      32   0.15398E-04   0.44018E-06 0.17939E+03 
c  TempC        0.38401E+02      27   0.33469E-03   0.54198E+01 0.25952E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3299          10.183          4.5729          4.5729
v  Velocity[Y]            -2.6092          7.3116        0.038012        0.038012
v  Velocity[Z]       -1.6051e-014     1.0716e-014    -1.5846e-017    -1.5846e-017
v  ǁVelocityǁ         0.0017178          10.183          5.1444          5.1444
v  Pressure               -41.078          16.207         -11.517         -11.517
v  nu_tilda           2.9193e-007       0.0042695       0.0015106       0.0015106
v  TempC                       21          73.044          21.914          21.914
v  TurbVisc           6.3876e-015        0.005032       0.0017742       0.0017742
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1734:        0.22320E+01

===============================================================


 INSTANT    0.173500000E+04   TIME STEP NUMBER            1735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81772E-02 0.89974E+00
   Friction velocity        uk    :  0.81772E-02 0.89974E+00
   Dimensionless distance   yplus :  0.65832E-01 0.72435E+01
   Friction thermal sca.    tstar : -0.96715E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49118E-01 0.54045E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95056E-02      33   0.24258E-03   0.47664E+01 0.17108E+03 
c  Velocity[X]                                      0.18453E+01 
c  Velocity[Y]                                      0.29211E+01 
c  Velocity[Z]                                      0.97709E-30 
c  Pressure     0.10110E-06     506   0.94222E-08   0.97426E-01 0.11242E+04 
c  nu_tilda     0.65597E-05      32   0.44406E-05   0.44075E-06 0.17949E+03 
c  TempC        0.38410E+02      27   0.41531E-03   0.48589E+01 0.25835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3268          10.182          4.5729          4.5729
v  Velocity[Y]            -2.6108          7.3404        0.038255        0.038255
v  Velocity[Z]       -1.5823e-014     1.0932e-014    -1.5849e-017    -1.5849e-017
v  ǁVelocityǁ         0.0016979          10.182          5.1443          5.1443
v  Pressure               -41.042          16.379         -11.459         -11.459
v  nu_tilda           2.9197e-007       0.0042695       0.0015111       0.0015111
v  TempC                       21          73.044          21.915          21.915
v  TurbVisc           6.3897e-015        0.005032       0.0017748       0.0017748
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1735:        0.21510E+01

===============================================================


 INSTANT    0.173600000E+04   TIME STEP NUMBER            1736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33212E-02 0.90133E+00
   Friction velocity        uk    :  0.33212E-02 0.90133E+00
   Dimensionless distance   yplus :  0.26738E-01 0.72563E+01
   Friction thermal sca.    tstar : -0.72259E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19950E-01 0.54140E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95079E-02      33   0.27764E-03   0.47411E+01 0.17106E+03 
c  Velocity[X]                                      0.17996E+01 
c  Velocity[Y]                                      0.29415E+01 
c  Velocity[Z]                                      0.92062E-30 
c  Pressure     0.90686E-07     457   0.98657E-08   0.87667E-01 0.43269E+03 
c  nu_tilda     0.65620E-05      32   0.15394E-04   0.44135E-06 0.17959E+03 
c  TempC        0.38419E+02      27   0.33662E-03   0.60540E+01 0.28552E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3237          10.181          4.5729          4.5729
v  Velocity[Y]             -2.613          7.3489          0.0385          0.0385
v  Velocity[Z]        -1.556e-014     1.1917e-014    -1.5851e-017    -1.5851e-017
v  ǁVelocityǁ          0.001674          10.181          5.1442          5.1442
v  Pressure               -41.036          16.362         -11.487         -11.487
v  nu_tilda           2.9202e-007       0.0042695       0.0015115       0.0015115
v  TempC                       21          73.044          21.915          21.915
v  TurbVisc            6.393e-015        0.005032       0.0017753       0.0017753
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1736:        0.20440E+01

===============================================================


 INSTANT    0.173700000E+04   TIME STEP NUMBER            1737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.68944E-02 0.90075E+00
   Friction velocity        uk    :  0.68944E-02 0.90075E+00
   Dimensionless distance   yplus :  0.55505E-01 0.72517E+01
   Friction thermal sca.    tstar : -0.67225E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41413E-01 0.54106E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95101E-02      33   0.28699E-03   0.47662E+01 0.17120E+03 
c  Velocity[X]                                      0.18337E+01 
c  Velocity[Y]                                      0.29326E+01 
c  Velocity[Z]                                      0.95302E-30 
c  Pressure     0.11989E-06     282   0.99264E-08   0.11477E+00 0.51273E+03 
c  nu_tilda     0.65643E-05      32   0.44448E-05   0.44192E-06 0.17969E+03 
c  TempC        0.38427E+02      27   0.24527E-03   0.54311E+01 0.25992E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3206          10.181          4.5729          4.5729
v  Velocity[Y]            -2.6152          7.3168        0.038746        0.038746
v  Velocity[Z]       -1.5354e-014      1.193e-014    -1.5852e-017    -1.5852e-017
v  ǁVelocityǁ         0.0016612          10.181           5.144           5.144
v  Pressure               -40.998          16.265         -11.485         -11.485
v  nu_tilda           2.9212e-007       0.0042695        0.001512        0.001512
v  TempC                       21          73.043          21.916          21.916
v  TurbVisc            6.398e-015        0.005032       0.0017758       0.0017758
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1737:        0.16340E+01

===============================================================


 INSTANT    0.173800000E+04   TIME STEP NUMBER            1738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43689E-02 0.89948E+00
   Friction velocity        uk    :  0.43689E-02 0.89948E+00
   Dimensionless distance   yplus :  0.35173E-01 0.72415E+01
   Friction thermal sca.    tstar : -0.74069E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26243E-01 0.54029E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95124E-02      33   0.31704E-03   0.47662E+01 0.17129E+03 
c  Velocity[X]                                      0.18398E+01 
c  Velocity[Y]                                      0.29263E+01 
c  Velocity[Z]                                      0.99678E-30 
c  Pressure     0.10114E-06     328   0.92448E-08   0.97690E-01 0.38749E+03 
c  nu_tilda     0.65666E-05      32   0.15390E-04   0.44252E-06 0.17979E+03 
c  TempC        0.38436E+02      27   0.37171E-03   0.32215E+01 0.20883E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3176           10.18          4.5729          4.5729
v  Velocity[Y]            -2.6173          7.3382        0.038992        0.038992
v  Velocity[Z]       -1.5156e-014      1.275e-014    -1.5856e-017    -1.5856e-017
v  ǁVelocityǁ         0.0014391           10.18          5.1439          5.1439
v  Pressure               -40.992          16.361         -11.488         -11.488
v  nu_tilda           2.9223e-007       0.0042695       0.0015124       0.0015124
v  TempC                       21          73.043          21.916          21.916
v  TurbVisc           6.4064e-015        0.005032       0.0017764       0.0017764
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1738:        0.17370E+01

===============================================================


 INSTANT    0.173900000E+04   TIME STEP NUMBER            1739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76865E-02 0.90046E+00
   Friction velocity        uk    :  0.76865E-02 0.90046E+00
   Dimensionless distance   yplus :  0.61881E-01 0.72494E+01
   Friction thermal sca.    tstar : -0.68793E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46170E-01 0.54088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95146E-02      33   0.29325E-03   0.47854E+01 0.17149E+03 
c  Velocity[X]                                      0.18361E+01 
c  Velocity[Y]                                      0.29493E+01 
c  Velocity[Z]                                      0.11073E-29 
c  Pressure     0.11415E-06     425   0.95723E-08   0.11126E+00 0.51548E+03 
c  nu_tilda     0.65689E-05      32   0.44402E-05   0.44308E-06 0.17989E+03 
c  TempC        0.38444E+02      28   0.30488E-03   0.42913E+01 0.23711E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3147          10.179          4.5729          4.5729
v  Velocity[Y]            -2.6193           7.316         0.03924         0.03924
v  Velocity[Z]       -1.4964e-014     1.4314e-014    -1.5843e-017    -1.5843e-017
v  ǁVelocityǁ        0.00086689          10.179          5.1438          5.1438
v  Pressure                -40.95          16.305         -11.474         -11.474
v  nu_tilda           2.9237e-007       0.0042695        0.001513        0.001513
v  TempC                       21          73.044          21.916          21.916
v  TurbVisc           6.4157e-015        0.005032       0.0017769       0.0017769
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1739:        0.19590E+01

===============================================================


 INSTANT    0.174000000E+04   TIME STEP NUMBER            1740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89024E-02 0.89954E+00
   Friction velocity        uk    :  0.89024E-02 0.89954E+00
   Dimensionless distance   yplus :  0.71670E-01 0.72419E+01
   Friction thermal sca.    tstar : -0.69102E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53474E-01 0.54033E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95169E-02      33   0.23087E-03   0.47741E+01 0.17140E+03 
c  Velocity[X]                                      0.18337E+01 
c  Velocity[Y]                                      0.29404E+01 
c  Velocity[Z]                                      0.10267E-29 
c  Pressure     0.12928E-06     441   0.95374E-08   0.12372E+00 0.30743E+03 
c  nu_tilda     0.65713E-05      32   0.15385E-04   0.44369E-06 0.17999E+03 
c  TempC        0.38453E+02      27   0.32356E-03   0.35077E+01 0.20807E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3117          10.178          4.5729          4.5729
v  Velocity[Y]            -2.6211           7.335        0.039487        0.039487
v  Velocity[Z]       -1.4999e-014     1.4177e-014    -1.5848e-017    -1.5848e-017
v  ǁVelocityǁ        0.00053401          10.178          5.1437          5.1437
v  Pressure               -40.947          16.362         -11.485         -11.485
v  nu_tilda           2.9254e-007       0.0042695       0.0015134       0.0015134
v  TempC                       21          73.044          21.917          21.917
v  TurbVisc           6.4287e-015        0.005032       0.0017775       0.0017775
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1740:        0.20140E+01

===============================================================


 INSTANT    0.174100000E+04   TIME STEP NUMBER            1741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62719E-03 0.90102E+00
   Friction velocity        uk    :  0.62719E-03 0.90102E+00
   Dimensionless distance   yplus :  0.50493E-02 0.72538E+01
   Friction thermal sca.    tstar : -0.67544E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37673E-02 0.54122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95191E-02      33   0.29256E-03   0.47618E+01 0.17145E+03 
c  Velocity[X]                                      0.18240E+01 
c  Velocity[Y]                                      0.29378E+01 
c  Velocity[Z]                                      0.10309E-29 
c  Pressure     0.97947E-07     488   0.94268E-08   0.95041E-01 0.71806E+03 
c  nu_tilda     0.65736E-05      32   0.44309E-05   0.44426E-06 0.18009E+03 
c  TempC        0.38461E+02      27   0.33793E-03   0.44183E+01 0.23425E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3085          10.177          4.5729          4.5729
v  Velocity[Y]            -2.6228          7.3476        0.039736        0.039736
v  Velocity[Z]       -1.4866e-014     1.5223e-014    -1.5838e-017    -1.5838e-017
v  ǁVelocityǁ        0.00042882          10.177          5.1435          5.1435
v  Pressure               -40.908           16.43         -11.449         -11.449
v  nu_tilda           2.9276e-007       0.0042695       0.0015139       0.0015139
v  TempC                       21          73.044          21.917          21.917
v  TurbVisc           6.4433e-015        0.005032        0.001778        0.001778
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1741:        0.21140E+01

===============================================================


 INSTANT    0.174200000E+04   TIME STEP NUMBER            1742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42594E-03 0.90060E+00
   Friction velocity        uk    :  0.42594E-03 0.90060E+00
   Dimensionless distance   yplus :  0.34291E-02 0.72504E+01
   Friction thermal sca.    tstar : -0.71127E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25585E-02 0.54096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95214E-02      33   0.27435E-03   0.47793E+01 0.17164E+03 
c  Velocity[X]                                      0.18279E+01 
c  Velocity[Y]                                      0.29514E+01 
c  Velocity[Z]                                      0.89567E-30 
c  Pressure     0.10983E-06     552   0.99779E-08   0.10792E+00 0.10107E+04 
c  nu_tilda     0.65759E-05      32   0.15382E-04   0.44486E-06 0.18019E+03 
c  TempC        0.38470E+02      27   0.33234E-03   0.59801E+01 0.27116E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3057          10.176          4.5729          4.5729
v  Velocity[Y]            -2.6248          7.3161        0.039985        0.039985
v  Velocity[Z]       -1.4689e-014       1.51e-014    -1.5847e-017    -1.5847e-017
v  ǁVelocityǁ         0.0004422          10.176          5.1434          5.1434
v  Pressure               -40.904          16.266         -11.508         -11.508
v  nu_tilda           2.9302e-007       0.0042695       0.0015143       0.0015143
v  TempC                       21          73.043          21.917          21.917
v  TurbVisc            6.463e-015        0.005032       0.0017786       0.0017786
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1742:        0.22840E+01

===============================================================


 INSTANT    0.174300000E+04   TIME STEP NUMBER            1743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47534E-02 0.89904E+00
   Friction velocity        uk    :  0.47534E-02 0.89904E+00
   Dimensionless distance   yplus :  0.38268E-01 0.72379E+01
   Friction thermal sca.    tstar : -0.69201E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28552E-01 0.54003E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95236E-02      33   0.29507E-03   0.47684E+01 0.17160E+03 
c  Velocity[X]                                      0.18265E+01 
c  Velocity[Y]                                      0.29419E+01 
c  Velocity[Z]                                      0.12334E-29 
c  Pressure     0.11029E-06     504   0.98569E-08   0.10574E+00 0.10214E+04 
c  nu_tilda     0.65782E-05      32   0.44371E-05   0.44543E-06 0.18029E+03 
c  TempC        0.38478E+02      27   0.31097E-03   0.45002E+01 0.23679E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3028          10.175          4.5729          4.5729
v  Velocity[Y]            -2.6271          7.3335        0.040236        0.040236
v  Velocity[Z]       -1.4519e-014       1.61e-014    -1.5837e-017    -1.5837e-017
v  ǁVelocityǁ        0.00042983          10.175          5.1433          5.1433
v  Pressure               -40.864          16.412         -11.454         -11.454
v  nu_tilda           2.9334e-007       0.0042695       0.0015148       0.0015148
v  TempC                       21          73.044          21.918          21.918
v  TurbVisc           6.4856e-015       0.0050321       0.0017791       0.0017791
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1743:        0.21480E+01

===============================================================


 INSTANT    0.174400000E+04   TIME STEP NUMBER            1744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28364E-02 0.90021E+00
   Friction velocity        uk    :  0.28364E-02 0.90021E+00
   Dimensionless distance   yplus :  0.22835E-01 0.72473E+01
   Friction thermal sca.    tstar : -0.67128E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17038E-01 0.54073E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95258E-02      33   0.30445E-03   0.47963E+01 0.17182E+03 
c  Velocity[X]                                      0.18581E+01 
c  Velocity[Y]                                      0.29382E+01 
c  Velocity[Z]                                      0.10657E-29 
c  Pressure     0.11625E-06     505   0.91642E-08   0.11401E+00 0.90153E+03 
c  nu_tilda     0.65806E-05      32   0.15374E-04   0.44604E-06 0.18039E+03 
c  TempC        0.38487E+02      27   0.37318E-03   0.57347E+01 0.25756E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2998          10.174          4.5729          4.5729
v  Velocity[Y]            -2.6292          7.3111        0.040487        0.040487
v  Velocity[Z]       -1.4318e-014     1.6672e-014    -1.5831e-017    -1.5831e-017
v  ǁVelocityǁ          0.000409          10.174          5.1432          5.1432
v  Pressure               -40.855          16.266         -11.504         -11.504
v  nu_tilda           2.9369e-007       0.0042695       0.0015152       0.0015152
v  TempC                       21          73.044          21.918          21.918
v  TurbVisc           6.5138e-015       0.0050321       0.0017797       0.0017797
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1744:        0.21580E+01

===============================================================


 INSTANT    0.174500000E+04   TIME STEP NUMBER            1745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52288E-02 0.89945E+00
   Friction velocity        uk    :  0.52288E-02 0.89945E+00
   Dimensionless distance   yplus :  0.42096E-01 0.72412E+01
   Friction thermal sca.    tstar : -0.68436E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31408E-01 0.54027E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95280E-02      33   0.21828E-03   0.47839E+01 0.17188E+03 
c  Velocity[X]                                      0.18243E+01 
c  Velocity[Y]                                      0.29596E+01 
c  Velocity[Z]                                      0.96509E-30 
c  Pressure     0.95926E-07     521   0.92148E-08   0.92773E-01 0.12161E+04 
c  nu_tilda     0.65829E-05      32   0.44335E-05   0.44660E-06 0.18049E+03 
c  TempC        0.38495E+02      27   0.34331E-03   0.69931E+01 0.30577E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2967          10.173          4.5729          4.5729
v  Velocity[Y]            -2.6311          7.3374        0.040739        0.040739
v  Velocity[Z]       -1.4107e-014     1.6575e-014    -1.5833e-017    -1.5833e-017
v  ǁVelocityǁ        0.00021661          10.173          5.1431          5.1431
v  Pressure               -40.818          16.463         -11.443         -11.443
v  nu_tilda           2.9408e-007       0.0042695       0.0015157       0.0015157
v  TempC                       21          73.044          21.918          21.918
v  TurbVisc           6.5448e-015       0.0050321       0.0017802       0.0017802
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1745:        0.21830E+01

===============================================================


 INSTANT    0.174600000E+04   TIME STEP NUMBER            1746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33744E-02 0.90075E+00
   Friction velocity        uk    :  0.33744E-02 0.90075E+00
   Dimensionless distance   yplus :  0.27166E-01 0.72517E+01
   Friction thermal sca.    tstar : -0.76023E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20269E-01 0.54105E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95303E-02      33   0.28715E-03   0.47529E+01 0.17176E+03 
c  Velocity[X]                                      0.18051E+01 
c  Velocity[Y]                                      0.29479E+01 
c  Velocity[Z]                                      0.12092E-29 
c  Pressure     0.11005E-06     473   0.99949E-08   0.10522E+00 0.79464E+03 
c  nu_tilda     0.65852E-05      32   0.15371E-04   0.44721E-06 0.18059E+03 
c  TempC        0.38504E+02      27   0.31059E-03   0.50406E+01 0.25785E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2937          10.172          4.5729          4.5729
v  Velocity[Y]             -2.633          7.3417        0.040992        0.040992
v  Velocity[Z]       -1.3898e-014     1.6742e-014    -1.5836e-017    -1.5836e-017
v  ǁVelocityǁ        0.00033502          10.172           5.143           5.143
v  Pressure               -40.813           16.35          -11.49          -11.49
v  nu_tilda           2.9449e-007       0.0042695       0.0015161       0.0015161
v  TempC                       21          73.044          21.919          21.919
v  TurbVisc           6.5797e-015       0.0050321       0.0017808       0.0017808
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1746:        0.20710E+01

===============================================================


 INSTANT    0.174700000E+04   TIME STEP NUMBER            1747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18699E-02 0.90061E+00
   Friction velocity        uk    :  0.18699E-02 0.90061E+00
   Dimensionless distance   yplus :  0.15054E-01 0.72505E+01
   Friction thermal sca.    tstar : -0.10432E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11232E-01 0.54097E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95325E-02      33   0.28434E-03   0.47964E+01 0.17202E+03 
c  Velocity[X]                                      0.18495E+01 
c  Velocity[Y]                                      0.29468E+01 
c  Velocity[Z]                                      0.91277E-30 
c  Pressure     0.10790E-06     457   0.94662E-08   0.10693E+00 0.60417E+03 
c  nu_tilda     0.65875E-05      32   0.44251E-05   0.44778E-06 0.18069E+03 
c  TempC        0.38512E+02      27   0.32576E-03   0.38738E+01 0.23186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2905          10.171          4.5729          4.5729
v  Velocity[Y]            -2.6346          7.3158        0.041245        0.041245
v  Velocity[Z]       -1.3712e-014     1.7425e-014    -1.5826e-017    -1.5826e-017
v  ǁVelocityǁ        0.00032133          10.171          5.1428          5.1428
v  Pressure               -40.774          16.373         -11.461         -11.461
v  nu_tilda           2.9493e-007       0.0042695       0.0015166       0.0015166
v  TempC                       21          73.044          21.919          21.919
v  TurbVisc           6.6165e-015       0.0050321       0.0017813       0.0017813
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1747:        0.20470E+01

===============================================================


 INSTANT    0.174800000E+04   TIME STEP NUMBER            1748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71157E-03 0.89896E+00
   Friction velocity        uk    :  0.71157E-03 0.89896E+00
   Dimensionless distance   yplus :  0.57287E-02 0.72372E+01
   Friction thermal sca.    tstar : -0.34741E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42742E-02 0.53998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95348E-02      33   0.28650E-03   0.47809E+01 0.17205E+03 
c  Velocity[X]                                      0.18168E+01 
c  Velocity[Y]                                      0.29641E+01 
c  Velocity[Z]                                      0.11011E-29 
c  Pressure     0.93263E-07     425   0.94802E-08   0.90333E-01 0.31654E+03 
c  nu_tilda     0.65899E-05      32   0.15371E-04   0.44839E-06 0.18079E+03 
c  TempC        0.38521E+02      27   0.31152E-03   0.62120E+01 0.26886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2875          10.171          4.5729          4.5729
v  Velocity[Y]            -2.6366          7.3338          0.0415          0.0415
v  Velocity[Z]       -1.3549e-014     1.7309e-014    -1.5837e-017    -1.5837e-017
v  ǁVelocityǁ        0.00032243          10.171          5.1427          5.1427
v  Pressure               -40.768          16.396          -11.48          -11.48
v  nu_tilda           2.9539e-007       0.0042695       0.0015171       0.0015171
v  TempC                       21          73.044           21.92           21.92
v  TurbVisc           6.6569e-015       0.0050321       0.0017818       0.0017818
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1748:        0.19800E+01

===============================================================


 INSTANT    0.174900000E+04   TIME STEP NUMBER            1749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18143E-02 0.89996E+00
   Friction velocity        uk    :  0.18143E-02 0.89996E+00
   Dimensionless distance   yplus :  0.14606E-01 0.72453E+01
   Friction thermal sca.    tstar : -0.11689E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10898E-01 0.54058E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95370E-02      33   0.30592E-03   0.47912E+01 0.17211E+03 
c  Velocity[X]                                      0.18371E+01 
c  Velocity[Y]                                      0.29541E+01 
c  Velocity[Z]                                      0.96461E-30 
c  Pressure     0.12458E-06     441   0.96984E-08   0.12048E+00 0.50167E+03 
c  nu_tilda     0.65922E-05      32   0.44343E-05   0.44896E-06 0.18089E+03 
c  TempC        0.38529E+02      27   0.36771E-03   0.42945E+01 0.23654E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2847           10.17          4.5729          4.5729
v  Velocity[Y]            -2.6388          7.3076        0.041755        0.041755
v  Velocity[Z]        -1.339e-014     1.7931e-014    -1.5837e-017    -1.5837e-017
v  ǁVelocityǁ        0.00029005           10.17          5.1426          5.1426
v  Pressure               -40.728          16.357         -11.464         -11.464
v  nu_tilda           2.9587e-007       0.0042695       0.0015176       0.0015176
v  TempC                       21          73.045           21.92           21.92
v  TurbVisc           6.6983e-015       0.0050321       0.0017824       0.0017824
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1749:        0.20050E+01

===============================================================


 INSTANT    0.175000000E+04   TIME STEP NUMBER            1750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33714E-02 0.89917E+00
   Friction velocity        uk    :  0.33714E-02 0.89917E+00
   Dimensionless distance   yplus :  0.27142E-01 0.72390E+01
   Friction thermal sca.    tstar : -0.78456E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20251E-01 0.54011E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95393E-02      33   0.24350E-03   0.48086E+01 0.17227E+03 
c  Velocity[X]                                      0.18576E+01 
c  Velocity[Y]                                      0.29510E+01 
c  Velocity[Z]                                      0.91487E-30 
c  Pressure     0.11766E-06     425   0.99393E-08   0.11414E+00 0.30308E+03 
c  nu_tilda     0.65945E-05      32   0.15360E-04   0.44956E-06 0.18099E+03 
c  TempC        0.38538E+02      27   0.31474E-03   0.42956E+01 0.24438E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2816          10.169          4.5729          4.5729
v  Velocity[Y]            -2.6409          7.3342        0.042011        0.042011
v  Velocity[Z]       -1.3168e-014     1.7907e-014    -1.5838e-017    -1.5838e-017
v  ǁVelocityǁ        0.00055517          10.169          5.1425          5.1425
v  Pressure               -40.719          16.399         -11.475         -11.475
v  nu_tilda           2.9635e-007       0.0042695        0.001518        0.001518
v  TempC                       21          73.044           21.92           21.92
v  TurbVisc            6.742e-015       0.0050321       0.0017829       0.0017829
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1750:        0.22400E+01

===============================================================


 INSTANT    0.175100000E+04   TIME STEP NUMBER            1751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48575E-02 0.90084E+00
   Friction velocity        uk    :  0.48575E-02 0.90084E+00
   Dimensionless distance   yplus :  0.39106E-01 0.72523E+01
   Friction thermal sca.    tstar : -0.68281E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29177E-01 0.54111E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95415E-02      33   0.27253E-03   0.47741E+01 0.17224E+03 
c  Velocity[X]                                      0.18038E+01 
c  Velocity[Y]                                      0.29704E+01 
c  Velocity[Z]                                      0.10371E-29 
c  Pressure     0.95630E-07     506   0.92857E-08   0.93362E-01 0.94093E+03 
c  nu_tilda     0.65969E-05      32   0.44297E-05   0.45014E-06 0.18109E+03 
c  TempC        0.38546E+02      27   0.32050E-03   0.35911E+01 0.22126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2785          10.168          4.5729          4.5729
v  Velocity[Y]            -2.6429          7.3449        0.042267        0.042267
v  Velocity[Z]       -1.3006e-014     1.7598e-014    -1.5846e-017    -1.5846e-017
v  ǁVelocityǁ       6.1656e-005          10.168          5.1424          5.1424
v  Pressure               -40.682          16.527         -11.427         -11.427
v  nu_tilda           2.9684e-007       0.0042695       0.0015185       0.0015185
v  TempC                       21          73.044          21.921          21.921
v  TurbVisc           6.7859e-015       0.0050321       0.0017835       0.0017835
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1751:        0.23360E+01

===============================================================


 INSTANT    0.175200000E+04   TIME STEP NUMBER            1752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.22350E-02 0.90022E+00
   Friction velocity        uk    :  0.22350E-02 0.90022E+00
   Dimensionless distance   yplus :  0.17994E-01 0.72474E+01
   Friction thermal sca.    tstar : -0.65640E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13425E-01 0.54074E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95438E-02      33   0.27899E-03   0.47937E+01 0.17233E+03 
c  Velocity[X]                                      0.18355E+01 
c  Velocity[Y]                                      0.29582E+01 
c  Velocity[Z]                                      0.10217E-29 
c  Pressure     0.11579E-06     522   0.91358E-08   0.11247E+00 0.13662E+04 
c  nu_tilda     0.65992E-05      32   0.15358E-04   0.45075E-06 0.18119E+03 
c  TempC        0.38555E+02      27   0.32011E-03   0.40172E+01 0.22280E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2756          10.167          4.5729          4.5729
v  Velocity[Y]            -2.6447          7.3106        0.042525        0.042525
v  Velocity[Z]       -1.2801e-014       1.75e-014     -1.585e-017     -1.585e-017
v  ǁVelocityǁ        0.00063199          10.167          5.1423          5.1423
v  Pressure               -40.674          16.286           -11.5           -11.5
v  nu_tilda            2.973e-007       0.0042695       0.0015189       0.0015189
v  TempC                       21          73.043          21.921          21.921
v  TurbVisc           6.8301e-015       0.0050321        0.001784        0.001784
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1752:        0.22010E+01

===============================================================


 INSTANT    0.175300000E+04   TIME STEP NUMBER            1753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58257E-02 0.89894E+00
   Friction velocity        uk    :  0.58257E-02 0.89894E+00
   Dimensionless distance   yplus :  0.46901E-01 0.72371E+01
   Friction thermal sca.    tstar : -0.67800E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34993E-01 0.53997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95460E-02      33   0.29333E-03   0.47951E+01 0.17242E+03 
c  Velocity[X]                                      0.18380E+01 
c  Velocity[Y]                                      0.29571E+01 
c  Velocity[Z]                                      0.83373E-30 
c  Pressure     0.98482E-07     537   0.98705E-08   0.95671E-01 0.13899E+04 
c  nu_tilda     0.66015E-05      32   0.44226E-05   0.45132E-06 0.18129E+03 
c  TempC        0.38563E+02      27   0.38662E-03   0.45493E+01 0.24682E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2728          10.166          4.5729          4.5729
v  Velocity[Y]            -2.6463          7.3335        0.042783        0.042783
v  Velocity[Z]       -1.2584e-014     1.7544e-014    -1.5851e-017    -1.5851e-017
v  ǁVelocityǁ        0.00055786          10.166          5.1422          5.1422
v  Pressure               -40.638          16.516          -11.43          -11.43
v  nu_tilda           2.9778e-007       0.0042695       0.0015194       0.0015194
v  TempC                       21          73.044          21.921          21.921
v  TurbVisc           6.8734e-015       0.0050321       0.0017845       0.0017845
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1753:        0.22660E+01

===============================================================


 INSTANT    0.175400000E+04   TIME STEP NUMBER            1754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26420E-02 0.89984E+00
   Friction velocity        uk    :  0.26420E-02 0.89984E+00
   Dimensionless distance   yplus :  0.21270E-01 0.72443E+01
   Friction thermal sca.    tstar : -0.65810E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15870E-01 0.54051E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95482E-02      33   0.28839E-03   0.48028E+01 0.17255E+03 
c  Velocity[X]                                      0.18271E+01 
c  Velocity[Y]                                      0.29756E+01 
c  Velocity[Z]                                      0.10643E-29 
c  Pressure     0.10921E-06     490   0.93670E-08   0.10721E+00 0.10550E+04 
c  nu_tilda     0.66038E-05      32   0.15353E-04   0.45193E-06 0.18139E+03 
c  TempC        0.38572E+02      27   0.30787E-03   0.56768E+01 0.28440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2698          10.165          4.5729          4.5729
v  Velocity[Y]            -2.6482          7.3082        0.043042        0.043042
v  Velocity[Z]       -1.2378e-014     1.7756e-014    -1.5851e-017    -1.5851e-017
v  ǁVelocityǁ        0.00015512          10.165          5.1421          5.1421
v  Pressure                -40.63          16.345         -11.488         -11.488
v  nu_tilda           2.9825e-007       0.0042695       0.0015198       0.0015198
v  TempC                       21          73.044          21.922          21.922
v  TurbVisc           6.9179e-015       0.0050321       0.0017851       0.0017851
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1754:        0.21090E+01

===============================================================


 INSTANT    0.175500000E+04   TIME STEP NUMBER            1755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23980E-02 0.89889E+00
   Friction velocity        uk    :  0.23980E-02 0.89889E+00
   Dimensionless distance   yplus :  0.19306E-01 0.72367E+01
   Friction thermal sca.    tstar : -0.66600E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14404E-01 0.53994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95505E-02      33   0.24046E-03   0.47916E+01 0.17252E+03 
c  Velocity[X]                                      0.18262E+01 
c  Velocity[Y]                                      0.29654E+01 
c  Velocity[Z]                                      0.13878E-29 
c  Pressure     0.11368E-06     490   0.95841E-08   0.10953E+00 0.10421E+04 
c  nu_tilda     0.66062E-05      32   0.44329E-05   0.45250E-06 0.18149E+03 
c  TempC        0.38580E+02      27   0.25560E-03   0.54833E+01 0.25541E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2668          10.164          4.5729          4.5729
v  Velocity[Y]            -2.6504          7.3297        0.043302        0.043302
v  Velocity[Z]       -1.2214e-014      1.784e-014    -1.5856e-017    -1.5856e-017
v  ǁVelocityǁ        0.00067125          10.164           5.142           5.142
v  Pressure               -40.589          16.484         -11.432         -11.432
v  nu_tilda           2.9866e-007       0.0042695       0.0015203       0.0015203
v  TempC                       21          73.044          21.922          21.922
v  TurbVisc           6.9614e-015       0.0050321       0.0017856       0.0017856
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1755:        0.21290E+01

===============================================================


 INSTANT    0.175600000E+04   TIME STEP NUMBER            1756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74048E-02 0.90059E+00
   Friction velocity        uk    :  0.74048E-02 0.90059E+00
   Dimensionless distance   yplus :  0.59613E-01 0.72504E+01
   Friction thermal sca.    tstar : -0.65934E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44478E-01 0.54096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95527E-02      33   0.30577E-03   0.47940E+01 0.17263E+03 
c  Velocity[X]                                      0.18332E+01 
c  Velocity[Y]                                      0.29608E+01 
c  Velocity[Z]                                      0.91210E-30 
c  Pressure     0.10633E-06     474   0.98047E-08   0.10325E+00 0.43312E+03 
c  nu_tilda     0.66085E-05      32   0.15344E-04   0.45311E-06 0.18159E+03 
c  TempC        0.38589E+02      27   0.38008E-03   0.39061E+01 0.21705E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2637          10.163          4.5729          4.5729
v  Velocity[Y]            -2.6525          7.3408        0.043563        0.043563
v  Velocity[Z]       -1.2013e-014     1.7188e-014    -1.5866e-017    -1.5866e-017
v  ǁVelocityǁ        0.00087318          10.163          5.1419          5.1419
v  Pressure               -40.583           16.47         -11.461         -11.461
v  nu_tilda           2.9906e-007       0.0042695       0.0015207       0.0015207
v  TempC                       21          73.044          21.923          21.923
v  TurbVisc           6.9995e-015       0.0050321       0.0017862       0.0017862
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1756:        0.20750E+01

===============================================================


 INSTANT    0.175700000E+04   TIME STEP NUMBER            1757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35564E-02 0.90021E+00
   Friction velocity        uk    :  0.35564E-02 0.90021E+00
   Dimensionless distance   yplus :  0.28631E-01 0.72473E+01
   Friction thermal sca.    tstar : -0.65541E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21362E-01 0.54073E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95550E-02      33   0.27120E-03   0.48200E+01 0.17282E+03 
c  Velocity[X]                                      0.18377E+01 
c  Velocity[Y]                                      0.29823E+01 
c  Velocity[Z]                                      0.94336E-30 
c  Pressure     0.10888E-06     442   0.96991E-08   0.10717E+00 0.50744E+03 
c  nu_tilda     0.66108E-05      32   0.44297E-05   0.45369E-06 0.18169E+03 
c  TempC        0.38597E+02      27   0.31102E-03   0.63007E+01 0.27468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2606          10.162          4.5729          4.5729
v  Velocity[Y]            -2.6544          7.3118        0.043824        0.043824
v  Velocity[Z]       -1.1781e-014      1.714e-014    -1.5872e-017    -1.5872e-017
v  ǁVelocityǁ        0.00037238          10.162          5.1418          5.1418
v  Pressure               -40.544          16.429         -11.444         -11.444
v  nu_tilda           2.9946e-007       0.0042695       0.0015212       0.0015212
v  TempC                       21          73.044          21.923          21.923
v  TurbVisc           7.0371e-015       0.0050321       0.0017867       0.0017867
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1757:        0.20090E+01

===============================================================


 INSTANT    0.175800000E+04   TIME STEP NUMBER            1758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31072E-02 0.89863E+00
   Friction velocity        uk    :  0.31072E-02 0.89863E+00
   Dimensionless distance   yplus :  0.25015E-01 0.72346E+01
   Friction thermal sca.    tstar : -0.71018E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18664E-01 0.53978E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95572E-02      33   0.28298E-03   0.48014E+01 0.17274E+03 
c  Velocity[X]                                      0.18314E+01 
c  Velocity[Y]                                      0.29700E+01 
c  Velocity[Z]                                      0.94592E-30 
c  Pressure     0.10752E-06     488   0.95558E-08   0.10281E+00 0.36519E+03 
c  nu_tilda     0.66132E-05      32   0.15345E-04   0.45430E-06 0.18179E+03 
c  TempC        0.38606E+02      26   0.36512E-03   0.49847E+01 0.24777E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2576          10.161          4.5729          4.5729
v  Velocity[Y]            -2.6562          7.3263        0.044086        0.044086
v  Velocity[Z]       -1.1567e-014     1.7004e-014    -1.5879e-017    -1.5879e-017
v  ǁVelocityǁ        0.00039862          10.161          5.1417          5.1417
v  Pressure               -40.538          16.443         -11.467         -11.467
v  nu_tilda           2.9987e-007       0.0042695       0.0015217       0.0015217
v  TempC                       21          73.044          21.923          21.923
v  TurbVisc           7.0753e-015       0.0050321       0.0017873       0.0017873
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1758:        0.21090E+01

===============================================================


 INSTANT    0.175900000E+04   TIME STEP NUMBER            1759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28460E-02 0.89978E+00
   Friction velocity        uk    :  0.28460E-02 0.89978E+00
   Dimensionless distance   yplus :  0.22912E-01 0.72439E+01
   Friction thermal sca.    tstar : -0.67297E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17095E-01 0.54047E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95594E-02      33   0.29634E-03   0.48225E+01 0.17292E+03 
c  Velocity[X]                                      0.18542E+01 
c  Velocity[Y]                                      0.29683E+01 
c  Velocity[Z]                                      0.88853E-30 
c  Pressure     0.10412E-06     458   0.92169E-08   0.10311E+00 0.54473E+03 
c  nu_tilda     0.66155E-05      32   0.44245E-05   0.45487E-06 0.18189E+03 
c  TempC        0.38614E+02      27   0.35713E-03   0.55609E+01 0.27543E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2548           10.16          4.5729          4.5729
v  Velocity[Y]            -2.6579          7.3058        0.044349        0.044349
v  Velocity[Z]       -1.1356e-014     1.7269e-014    -1.5882e-017    -1.5882e-017
v  ǁVelocityǁ         0.0009124          10.161          5.1416          5.1416
v  Pressure               -40.499          16.429         -11.444         -11.444
v  nu_tilda           3.0031e-007       0.0042695       0.0015222       0.0015222
v  TempC                       21          73.055          21.924          21.924
v  TurbVisc           7.1137e-015       0.0050321       0.0017878       0.0017878
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1759:        0.20410E+01

===============================================================


 INSTANT    0.176000000E+04   TIME STEP NUMBER            1760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63437E-02 0.89889E+00
   Friction velocity        uk    :  0.63437E-02 0.89889E+00
   Dimensionless distance   yplus :  0.51071E-01 0.72367E+01
   Friction thermal sca.    tstar : -0.70545E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38105E-01 0.53994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95617E-02      33   0.21984E-03   0.48123E+01 0.17298E+03 
c  Velocity[X]                                      0.18262E+01 
c  Velocity[Y]                                      0.29861E+01 
c  Velocity[Z]                                      0.10069E-29 
c  Pressure     0.96874E-07     296   0.96652E-08   0.94178E-01 0.34522E+03 
c  nu_tilda     0.66178E-05      32   0.15338E-04   0.45548E-06 0.18199E+03 
c  TempC        0.38623E+02      27   0.36604E-03   0.74209E+01 0.29112E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2518           10.16          4.5729          4.5729
v  Velocity[Y]            -2.6596            7.33        0.044613        0.044613
v  Velocity[Z]       -1.1194e-014     1.7196e-014    -1.5892e-017    -1.5892e-017
v  ǁVelocityǁ         0.0010514           10.16          5.1415          5.1415
v  Pressure               -40.489          16.505         -11.448         -11.448
v  nu_tilda           3.0076e-007       0.0042695       0.0015226       0.0015226
v  TempC                       21          73.072          21.924          21.924
v  TurbVisc           7.1551e-015       0.0050321       0.0017883       0.0017883
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1760:        0.16600E+01

===============================================================


 INSTANT    0.176100000E+04   TIME STEP NUMBER            1761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43516E-02 0.90030E+00
   Friction velocity        uk    :  0.43516E-02 0.90030E+00
   Dimensionless distance   yplus :  0.35034E-01 0.72480E+01
   Friction thermal sca.    tstar : -0.91364E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26139E-01 0.54078E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95639E-02      33   0.29591E-03   0.47923E+01 0.17290E+03 
c  Velocity[X]                                      0.18106E+01 
c  Velocity[Y]                                      0.29818E+01 
c  Velocity[Z]                                      0.93421E-30 
c  Pressure     0.12566E-06     458   0.98182E-08   0.12120E+00 0.59147E+03 
c  nu_tilda     0.66202E-05      32   0.44332E-05   0.45606E-06 0.18209E+03 
c  TempC        0.38631E+02      27   0.27915E-03   0.61508E+01 0.27643E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2487          10.159          4.5729          4.5729
v  Velocity[Y]            -2.6618          7.3362        0.044876        0.044876
v  Velocity[Z]       -1.0983e-014     1.7061e-014    -1.5904e-017    -1.5904e-017
v  ǁVelocityǁ        0.00058215          10.159          5.1414          5.1414
v  Pressure               -40.452          16.534          -11.42          -11.42
v  nu_tilda           3.0125e-007       0.0042695       0.0015231       0.0015231
v  TempC                       21          73.089          21.925          21.925
v  TurbVisc           7.1983e-015       0.0050321       0.0017889       0.0017889
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1761:        0.20360E+01

===============================================================


 INSTANT    0.176200000E+04   TIME STEP NUMBER            1762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31837E-02 0.90006E+00
   Friction velocity        uk    :  0.31837E-02 0.90006E+00
   Dimensionless distance   yplus :  0.25631E-01 0.72461E+01
   Friction thermal sca.    tstar : -0.16828E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19123E-01 0.54064E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95662E-02      33   0.29678E-03   0.48431E+01 0.17322E+03 
c  Velocity[X]                                      0.18681E+01 
c  Velocity[Y]                                      0.29750E+01 
c  Velocity[Z]                                      0.12612E-29 
c  Pressure     0.12479E-06     506   0.99478E-08   0.12293E+00 0.84678E+03 
c  nu_tilda     0.66225E-05      32   0.15330E-04   0.45667E-06 0.18219E+03 
c  TempC        0.38640E+02      27   0.33864E-03   0.39079E+01 0.23693E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2457          10.158          4.5729          4.5729
v  Velocity[Y]            -2.6639          7.3087        0.045142        0.045142
v  Velocity[Z]       -1.0791e-014     1.6794e-014    -1.5911e-017    -1.5911e-017
v  ǁVelocityǁ        0.00041647          10.158          5.1413          5.1413
v  Pressure               -40.443          16.408         -11.468         -11.468
v  nu_tilda           3.0178e-007       0.0042695       0.0015235       0.0015235
v  TempC                       21          73.105          21.925          21.925
v  TurbVisc           7.2456e-015       0.0050321       0.0017894       0.0017894
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1762:        0.21610E+01

===============================================================


 INSTANT    0.176300000E+04   TIME STEP NUMBER            1763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38163E-02 0.89866E+00
   Friction velocity        uk    :  0.38163E-02 0.89866E+00
   Dimensionless distance   yplus :  0.30724E-01 0.72348E+01
   Friction thermal sca.    tstar : -0.14448E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22923E-01 0.53980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95684E-02      33   0.28028E-03   0.48182E+01 0.17322E+03 
c  Velocity[X]                                      0.18268E+01 
c  Velocity[Y]                                      0.29914E+01 
c  Velocity[Z]                                      0.97827E-30 
c  Pressure     0.10025E-06     538   0.97587E-08   0.97068E-01 0.96003E+03 
c  nu_tilda     0.66248E-05      32   0.44310E-05   0.45725E-06 0.18229E+03 
c  TempC        0.38648E+02      27   0.34432E-03   0.64455E+01 0.28103E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2429          10.157          4.5729          4.5729
v  Velocity[Y]            -2.6659          7.3292        0.045408        0.045408
v  Velocity[Z]       -1.0614e-014       1.67e-014    -1.5911e-017    -1.5911e-017
v  ǁVelocityǁ        0.00078105          10.157          5.1412          5.1412
v  Pressure               -40.407          16.549          -11.42          -11.42
v  nu_tilda           3.0236e-007       0.0042695        0.001524        0.001524
v  TempC                       21          73.121          21.925          21.925
v  TurbVisc           7.2969e-015       0.0050321         0.00179         0.00179
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1763:        0.22350E+01

===============================================================


 INSTANT    0.176400000E+04   TIME STEP NUMBER            1764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18949E-02 0.89961E+00
   Friction velocity        uk    :  0.18949E-02 0.89961E+00
   Dimensionless distance   yplus :  0.15255E-01 0.72424E+01
   Friction thermal sca.    tstar : -0.85705E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11382E-01 0.54037E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95707E-02      33   0.29242E-03   0.48220E+01 0.17321E+03 
c  Velocity[X]                                      0.18422E+01 
c  Velocity[Y]                                      0.29798E+01 
c  Velocity[Z]                                      0.93367E-30 
c  Pressure     0.12312E-06     536   0.98535E-08   0.11946E+00 0.95272E+03 
c  nu_tilda     0.66272E-05      32   0.15326E-04   0.45786E-06 0.18239E+03 
c  TempC        0.38656E+02      27   0.40829E-03   0.54706E+01 0.26870E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.24          10.156          4.5729          4.5729
v  Velocity[Y]            -2.6677          7.3008        0.045675        0.045675
v  Velocity[Z]       -1.0436e-014     1.6595e-014    -1.5922e-017    -1.5922e-017
v  ǁVelocityǁ         0.0010091          10.156          5.1411          5.1411
v  Pressure               -40.397          16.391         -11.472         -11.472
v  nu_tilda           3.0293e-007       0.0042695       0.0015244       0.0015244
v  TempC                       21          73.137          21.926          21.926
v  TurbVisc           7.3525e-015       0.0050321       0.0017905       0.0017905
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1764:        0.22290E+01

===============================================================


 INSTANT    0.176500000E+04   TIME STEP NUMBER            1765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85647E-02 0.89888E+00
   Friction velocity        uk    :  0.85647E-02 0.89888E+00
   Dimensionless distance   yplus :  0.68951E-01 0.72366E+01
   Friction thermal sca.    tstar : -0.67035E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51445E-01 0.53993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95729E-02      33   0.23184E-03   0.48312E+01 0.17333E+03 
c  Velocity[X]                                      0.18512E+01 
c  Velocity[Y]                                      0.29800E+01 
c  Velocity[Z]                                      0.80670E-30 
c  Pressure     0.98773E-07     538   0.93849E-08   0.96269E-01 0.11851E+04 
c  nu_tilda     0.66295E-05      32   0.44262E-05   0.45844E-06 0.18249E+03 
c  TempC        0.38665E+02      27   0.33031E-03   0.61108E+01 0.28334E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2369          10.155          4.5729          4.5729
v  Velocity[Y]            -2.6694           7.328        0.045942        0.045942
v  Velocity[Z]       -1.0252e-014     1.6009e-014    -1.5924e-017    -1.5924e-017
v  ǁVelocityǁ         0.0009863          10.155           5.141           5.141
v  Pressure               -40.357          16.573          -11.41          -11.41
v  nu_tilda           3.0354e-007       0.0042695       0.0015249       0.0015249
v  TempC                       21          73.152          21.926          21.926
v  TurbVisc           7.4086e-015       0.0050321        0.001791        0.001791
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1765:        0.22260E+01

===============================================================


 INSTANT    0.176600000E+04   TIME STEP NUMBER            1766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73277E-02 0.90020E+00
   Friction velocity        uk    :  0.73277E-02 0.90020E+00
   Dimensionless distance   yplus :  0.58993E-01 0.72472E+01
   Friction thermal sca.    tstar : -0.69809E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44015E-01 0.54072E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95751E-02      33   0.28189E-03   0.48029E+01 0.17332E+03 
c  Velocity[X]                                      0.18071E+01 
c  Velocity[Y]                                      0.29958E+01 
c  Velocity[Z]                                      0.11020E-29 
c  Pressure     0.95636E-07     489   0.95635E-08   0.93489E-01 0.52813E+03 
c  nu_tilda     0.66318E-05      32   0.15321E-04   0.45905E-06 0.18259E+03 
c  TempC        0.38673E+02      27   0.31911E-03   0.52512E+01 0.26082E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2339          10.154          4.5729          4.5729
v  Velocity[Y]            -2.6711          7.3355        0.046211        0.046211
v  Velocity[Z]       -1.0075e-014     1.5894e-014    -1.5934e-017    -1.5934e-017
v  ǁVelocityǁ        0.00077642          10.154          5.1409          5.1409
v  Pressure                -40.35          16.521         -11.443         -11.443
v  nu_tilda            3.042e-007       0.0042695       0.0015253       0.0015253
v  TempC                       21          73.166          21.927          21.927
v  TurbVisc           7.4687e-015       0.0050321       0.0017916       0.0017916
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1766:        0.21170E+01

===============================================================


 INSTANT    0.176700000E+04   TIME STEP NUMBER            1767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40341E-02 0.89977E+00
   Friction velocity        uk    :  0.40341E-02 0.89977E+00
   Dimensionless distance   yplus :  0.32477E-01 0.72438E+01
   Friction thermal sca.    tstar : -0.66435E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24232E-01 0.54047E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95774E-02      33   0.29458E-03   0.48362E+01 0.17347E+03 
c  Velocity[X]                                      0.18491E+01 
c  Velocity[Y]                                      0.29871E+01 
c  Velocity[Z]                                      0.93012E-30 
c  Pressure     0.12297E-06     441   0.96137E-08   0.11905E+00 0.49298E+03 
c  nu_tilda     0.66341E-05      32   0.44343E-05   0.45963E-06 0.18269E+03 
c  TempC        0.38682E+02      27   0.33049E-03   0.45684E+01 0.23965E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2308          10.153          4.5729          4.5729
v  Velocity[Y]            -2.6732          7.3041         0.04648         0.04648
v  Velocity[Z]       -9.9055e-015     1.5404e-014    -1.5943e-017    -1.5943e-017
v  ǁVelocityǁ        0.00055356          10.153          5.1408          5.1408
v  Pressure               -40.311          16.469          -11.43          -11.43
v  nu_tilda            3.049e-007       0.0042695       0.0015258       0.0015258
v  TempC                       21           73.18          21.927          21.927
v  TurbVisc           7.5333e-015       0.0050321       0.0017921       0.0017921
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1767:        0.20250E+01

===============================================================


 INSTANT    0.176800000E+04   TIME STEP NUMBER            1768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16668E-02 0.89848E+00
   Friction velocity        uk    :  0.16668E-02 0.89848E+00
   Dimensionless distance   yplus :  0.13419E-01 0.72334E+01
   Friction thermal sca.    tstar : -0.66898E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10012E-01 0.53969E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95796E-02      33   0.29790E-03   0.48491E+01 0.17362E+03 
c  Velocity[X]                                      0.18606E+01 
c  Velocity[Y]                                      0.29885E+01 
c  Velocity[Z]                                      0.96463E-30 
c  Pressure     0.12057E-06     360   0.98450E-08   0.11827E+00 0.35438E+03 
c  nu_tilda     0.66365E-05      32   0.15316E-04   0.46024E-06 0.18279E+03 
c  TempC        0.38690E+02      27   0.34050E-03   0.46845E+01 0.24656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2278          10.152          4.5729          4.5729
v  Velocity[Y]            -2.6752          7.3239        0.046749        0.046749
v  Velocity[Z]       -9.7455e-015     1.5502e-014    -1.5954e-017    -1.5954e-017
v  ǁVelocityǁ        0.00075842          10.152          5.1407          5.1407
v  Pressure               -40.304          16.549         -11.435         -11.435
v  nu_tilda           3.0559e-007       0.0042695       0.0015262       0.0015262
v  TempC                       21          73.194          21.927          21.927
v  TurbVisc           7.6028e-015       0.0050321       0.0017927       0.0017927
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1768:        0.18140E+01

===============================================================


 INSTANT    0.176900000E+04   TIME STEP NUMBER            1769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37159E-02 0.89953E+00
   Friction velocity        uk    :  0.37159E-02 0.89953E+00
   Dimensionless distance   yplus :  0.29916E-01 0.72418E+01
   Friction thermal sca.    tstar : -0.65579E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22321E-01 0.54032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95818E-02      33   0.27589E-03   0.48549E+01 0.17374E+03 
c  Velocity[X]                                      0.18480E+01 
c  Velocity[Y]                                      0.30069E+01 
c  Velocity[Z]                                      0.11715E-29 
c  Pressure     0.11687E-06     392   0.96928E-08   0.11373E+00 0.52807E+03 
c  nu_tilda     0.66388E-05      32   0.44355E-05   0.46081E-06 0.18289E+03 
c  TempC        0.38699E+02      27   0.33362E-03   0.52477E+01 0.26745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.225          10.151          4.5729          4.5729
v  Velocity[Y]            -2.6772          7.2952         0.04702         0.04702
v  Velocity[Z]       -9.5783e-015     1.5824e-014    -1.5959e-017    -1.5959e-017
v  ǁVelocityǁ        0.00086835          10.151          5.1406          5.1406
v  Pressure               -40.265          16.463         -11.431         -11.431
v  nu_tilda           3.0633e-007       0.0042695       0.0015267       0.0015267
v  TempC                       21          73.207          21.928          21.928
v  TurbVisc           7.6718e-015       0.0050321       0.0017932       0.0017932
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1769:        0.18940E+01

===============================================================


 INSTANT    0.177000000E+04   TIME STEP NUMBER            1770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86157E-02 0.89884E+00
   Friction velocity        uk    :  0.86157E-02 0.89884E+00
   Dimensionless distance   yplus :  0.69362E-01 0.72363E+01
   Friction thermal sca.    tstar : -0.66726E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51752E-01 0.53991E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95841E-02      33   0.18986E-03   0.48218E+01 0.17362E+03 
c  Velocity[X]                                      0.18315E+01 
c  Velocity[Y]                                      0.29902E+01 
c  Velocity[Z]                                      0.86442E-30 
c  Pressure     0.10289E-06     393   0.92926E-08   0.10039E+00 0.39520E+03 
c  nu_tilda     0.66411E-05      32   0.15312E-04   0.46143E-06 0.18299E+03 
c  TempC        0.38707E+02      27   0.31623E-03   0.49057E+01 0.26305E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.222           10.15          4.5729          4.5729
v  Velocity[Y]             -2.679          7.3228        0.047291        0.047291
v  Velocity[Z]       -9.4006e-015     1.6085e-014    -1.5962e-017    -1.5962e-017
v  ǁVelocityǁ        0.00083106           10.15          5.1406          5.1406
v  Pressure               -40.254          16.556         -11.432         -11.432
v  nu_tilda           3.0711e-007       0.0042695       0.0015271       0.0015271
v  TempC                       21           73.22          21.928          21.928
v  TurbVisc           7.7465e-015       0.0050321       0.0017937       0.0017937
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1770:        0.18890E+01

===============================================================


 INSTANT    0.177100000E+04   TIME STEP NUMBER            1771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48089E-02 0.90031E+00
   Friction velocity        uk    :  0.48089E-02 0.90031E+00
   Dimensionless distance   yplus :  0.38715E-01 0.72481E+01
   Friction thermal sca.    tstar : -0.65083E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28885E-01 0.54079E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95863E-02      33   0.31970E-03   0.47939E+01 0.17356E+03 
c  Velocity[X]                                      0.18055E+01 
c  Velocity[Y]                                      0.29884E+01 
c  Velocity[Z]                                      0.99583E-30 
c  Pressure     0.90252E-07     504   0.92982E-08   0.88396E-01 0.63291E+03 
c  nu_tilda     0.66435E-05      32   0.44282E-05   0.46201E-06 0.18309E+03 
c  TempC        0.38716E+02      27   0.36452E-03   0.42698E+01 0.23770E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2189          10.149          4.5729          4.5729
v  Velocity[Y]            -2.6808          7.3356        0.047563        0.047563
v  Velocity[Z]       -9.2415e-015     1.6132e-014    -1.5965e-017    -1.5965e-017
v  ǁVelocityǁ        0.00080501          10.149          5.1405          5.1405
v  Pressure               -40.217          16.601         -11.401         -11.401
v  nu_tilda           3.0793e-007       0.0042695       0.0015276       0.0015276
v  TempC                       21          73.232          21.929          21.929
v  TurbVisc           7.8259e-015       0.0050321       0.0017943       0.0017943
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1771:        0.21730E+01

===============================================================


 INSTANT    0.177200000E+04   TIME STEP NUMBER            1772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50318E-02 0.89984E+00
   Friction velocity        uk    :  0.50318E-02 0.89984E+00
   Dimensionless distance   yplus :  0.40510E-01 0.72443E+01
   Friction thermal sca.    tstar : -0.64499E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30225E-01 0.54051E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95886E-02      33   0.29273E-03   0.48871E+01 0.17403E+03 
c  Velocity[X]                                      0.18735E+01 
c  Velocity[Y]                                      0.30136E+01 
c  Velocity[Z]                                      0.87575E-30 
c  Pressure     0.13846E-06     521   0.98730E-08   0.13358E+00 0.10850E+04 
c  nu_tilda     0.66458E-05      32   0.15307E-04   0.46262E-06 0.18319E+03 
c  TempC        0.38724E+02      27   0.27690E-03   0.70708E+01 0.29228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2159          10.148          4.5729          4.5729
v  Velocity[Y]            -2.6825          7.3003        0.047836        0.047836
v  Velocity[Z]       -9.0768e-015     1.5976e-014    -1.5974e-017    -1.5974e-017
v  ǁVelocityǁ        0.00077177          10.148          5.1404          5.1404
v  Pressure               -40.206          16.418         -11.459         -11.459
v  nu_tilda           3.0879e-007       0.0042695       0.0015281       0.0015281
v  TempC                       21          73.244          21.929          21.929
v  TurbVisc           7.9102e-015       0.0050321       0.0017948       0.0017948
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1772:        0.21900E+01

===============================================================


 INSTANT    0.177300000E+04   TIME STEP NUMBER            1773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.80405E-02 0.89866E+00
   Friction velocity        uk    :  0.80405E-02 0.89866E+00
   Dimensionless distance   yplus :  0.64732E-01 0.72349E+01
   Friction thermal sca.    tstar : -0.66791E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48297E-01 0.53980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95908E-02      33   0.25934E-03   0.48489E+01 0.17395E+03 
c  Velocity[X]                                      0.18490E+01 
c  Velocity[Y]                                      0.29999E+01 
c  Velocity[Z]                                      0.99497E-30 
c  Pressure     0.10073E-06     522   0.99258E-08   0.98364E-01 0.12339E+04 
c  nu_tilda     0.66482E-05      32   0.44373E-05   0.46320E-06 0.18328E+03 
c  TempC        0.38733E+02      27   0.37211E-03   0.50587E+01 0.25375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2131          10.148          4.5729          4.5729
v  Velocity[Y]            -2.6843          7.3235         0.04811         0.04811
v  Velocity[Z]       -8.9158e-015     1.6018e-014     -1.598e-017     -1.598e-017
v  ǁVelocityǁ         0.0007504          10.148          5.1403          5.1403
v  Pressure               -40.171          16.613         -11.397         -11.397
v  nu_tilda           3.0968e-007       0.0042695       0.0015286       0.0015286
v  TempC                       21          73.255          21.929          21.929
v  TurbVisc           7.9991e-015       0.0050321       0.0017953       0.0017953
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1773:        0.21790E+01

===============================================================


 INSTANT    0.177400000E+04   TIME STEP NUMBER            1774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55025E-02 0.89965E+00
   Friction velocity        uk    :  0.55025E-02 0.89965E+00
   Dimensionless distance   yplus :  0.44299E-01 0.72428E+01
   Friction thermal sca.    tstar : -0.69799E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33052E-01 0.54040E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95930E-02      33   0.31546E-03   0.48213E+01 0.17386E+03 
c  Velocity[X]                                      0.18308E+01 
c  Velocity[Y]                                      0.29904E+01 
c  Velocity[Z]                                      0.12634E-29 
c  Pressure     0.99907E-07     521   0.93490E-08   0.98363E-01 0.87652E+03 
c  nu_tilda     0.66505E-05      32   0.15298E-04   0.46382E-06 0.18338E+03 
c  TempC        0.38741E+02      27   0.35829E-03   0.63410E+01 0.28834E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2102          10.147          4.5729          4.5729
v  Velocity[Y]            -2.6864           7.302        0.048384        0.048384
v  Velocity[Z]       -8.7546e-015       1.58e-014     -1.599e-017     -1.599e-017
v  ǁVelocityǁ        0.00072166          10.147          5.1402          5.1402
v  Pressure                -40.16          16.477         -11.445         -11.445
v  nu_tilda           3.1062e-007       0.0042695        0.001529        0.001529
v  TempC                       21          73.266           21.93           21.93
v  TurbVisc           8.0913e-015       0.0050321       0.0017959       0.0017959
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1774:        0.21740E+01

===============================================================


 INSTANT    0.177500000E+04   TIME STEP NUMBER            1775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36728E-02 0.89868E+00
   Friction velocity        uk    :  0.36728E-02 0.89868E+00
   Dimensionless distance   yplus :  0.29568E-01 0.72350E+01
   Friction thermal sca.    tstar : -0.76391E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22061E-01 0.53981E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95953E-02      33   0.21416E-03   0.48644E+01 0.17411E+03 
c  Velocity[X]                                      0.18441E+01 
c  Velocity[Y]                                      0.30203E+01 
c  Velocity[Z]                                      0.10163E-29 
c  Pressure     0.13662E-06     520   0.97003E-08   0.13277E+00 0.10183E+04 
c  nu_tilda     0.66528E-05      32   0.44382E-05   0.46440E-06 0.18348E+03 
c  TempC        0.38749E+02      27   0.35115E-03   0.63006E+01 0.27077E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2072          10.146          4.5729          4.5729
v  Velocity[Y]            -2.6884          7.3227        0.048658        0.048658
v  Velocity[Z]       -8.5867e-015     1.5583e-014    -1.5994e-017    -1.5994e-017
v  ǁVelocityǁ        0.00068739          10.146          5.1401          5.1401
v  Pressure                -40.12           16.61         -11.391         -11.391
v  nu_tilda           3.1159e-007       0.0042695       0.0015295       0.0015295
v  TempC                       21          73.276           21.93           21.93
v  TurbVisc           8.1895e-015       0.0050321       0.0017964       0.0017964
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1775:        0.21810E+01

===============================================================


 INSTANT    0.177600000E+04   TIME STEP NUMBER            1776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.66386E-02 0.90035E+00
   Friction velocity        uk    :  0.66386E-02 0.90035E+00
   Dimensionless distance   yplus :  0.53445E-01 0.72484E+01
   Friction thermal sca.    tstar : -0.10606E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39876E-01 0.54081E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95975E-02      33   0.25589E-03   0.48161E+01 0.17396E+03 
c  Velocity[X]                                      0.18129E+01 
c  Velocity[Y]                                      0.30032E+01 
c  Velocity[Z]                                      0.10866E-29 
c  Pressure     0.90109E-07     473   0.93449E-08   0.87357E-01 0.40600E+03 
c  nu_tilda     0.66552E-05      32   0.15296E-04   0.46501E-06 0.18358E+03 
c  TempC        0.38758E+02      27   0.28823E-03   0.48972E+01 0.25773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2042          10.145          4.5729          4.5729
v  Velocity[Y]            -2.6902          7.3309        0.048935        0.048935
v  Velocity[Z]       -8.4316e-015      1.548e-014       -1.6e-017       -1.6e-017
v  ǁVelocityǁ        0.00065767          10.145            5.14            5.14
v  Pressure               -40.112          16.612         -11.416         -11.416
v  nu_tilda           3.1261e-007       0.0042695       0.0015299       0.0015299
v  TempC                       21          73.286          21.931          21.931
v  TurbVisc           8.2931e-015       0.0050321        0.001797        0.001797
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1776:        0.20630E+01

===============================================================


 INSTANT    0.177700000E+04   TIME STEP NUMBER            1777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41885E-02 0.89980E+00
   Friction velocity        uk    :  0.41885E-02 0.89980E+00
   Dimensionless distance   yplus :  0.33720E-01 0.72440E+01
   Friction thermal sca.    tstar : -0.30054E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25159E-01 0.54048E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.95997E-02      33   0.32813E-03   0.48331E+01 0.17409E+03 
c  Velocity[X]                                      0.18375E+01 
c  Velocity[Y]                                      0.29956E+01 
c  Velocity[Z]                                      0.84040E-30 
c  Pressure     0.11266E-06     378   0.94590E-08   0.11096E+00 0.52814E+03 
c  nu_tilda     0.66575E-05      32   0.44312E-05   0.46559E-06 0.18368E+03 
c  TempC        0.38766E+02      27   0.26945E-03   0.42342E+01 0.23937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2011          10.144          4.5729          4.5729
v  Velocity[Y]             -2.692           7.306        0.049211        0.049211
v  Velocity[Z]       -8.2745e-015     1.5139e-014       -1.6e-017       -1.6e-017
v  ǁVelocityǁ        0.00064804          10.144            5.14            5.14
v  Pressure               -40.072          16.521         -11.411         -11.411
v  nu_tilda           3.1369e-007       0.0042695       0.0015304       0.0015304
v  TempC                       21          73.296          21.931          21.931
v  TurbVisc           8.4021e-015       0.0050321       0.0017975       0.0017975
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1777:        0.18620E+01

===============================================================


 INSTANT    0.177800000E+04   TIME STEP NUMBER            1778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74482E-02 0.89842E+00
   Friction velocity        uk    :  0.74482E-02 0.89842E+00
   Dimensionless distance   yplus :  0.59963E-01 0.72329E+01
   Friction thermal sca.    tstar : -0.11347E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44739E-01 0.53965E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96020E-02      33   0.31097E-03   0.48516E+01 0.17425E+03 
c  Velocity[X]                                      0.18336E+01 
c  Velocity[Y]                                      0.30180E+01 
c  Velocity[Z]                                      0.99399E-30 
c  Pressure     0.97270E-07     328   0.96530E-08   0.94432E-01 0.34641E+03 
c  nu_tilda     0.66598E-05      32   0.15294E-04   0.46621E-06 0.18378E+03 
c  TempC        0.38775E+02      27   0.39138E-03   0.38267E+01 0.22460E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.198          10.143          4.5729          4.5729
v  Velocity[Y]            -2.6937          7.3191        0.049488        0.049488
v  Velocity[Z]       -8.1194e-015       1.48e-014    -1.6016e-017    -1.6016e-017
v  ǁVelocityǁ        0.00060513          10.143          5.1399          5.1399
v  Pressure               -40.064          16.598         -11.417         -11.417
v  nu_tilda           3.1476e-007       0.0042695       0.0015308       0.0015308
v  TempC                       21          73.304          21.931          21.931
v  TurbVisc            8.519e-015       0.0050321        0.001798        0.001798
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1778:        0.17340E+01

===============================================================


 INSTANT    0.177900000E+04   TIME STEP NUMBER            1779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.47819E-02 0.89938E+00
   Friction velocity        uk    :  0.47819E-02 0.89938E+00
   Dimensionless distance   yplus :  0.38498E-01 0.72406E+01
   Friction thermal sca.    tstar : -0.78674E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28724E-01 0.54023E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96042E-02      33   0.26783E-03   0.48630E+01 0.17438E+03 
c  Velocity[X]                                      0.18535E+01 
c  Velocity[Y]                                      0.30094E+01 
c  Velocity[Z]                                      0.98320E-30 
c  Pressure     0.10488E-06     393   0.95318E-08   0.10301E+00 0.51446E+03 
c  nu_tilda     0.66622E-05      32   0.44438E-05   0.46679E-06 0.18388E+03 
c  TempC        0.38783E+02      27   0.31673E-03   0.57818E+01 0.26718E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1953          10.142          4.5729          4.5729
v  Velocity[Y]            -2.6953          7.2987        0.049766        0.049766
v  Velocity[Z]       -7.9596e-015     1.5117e-014    -1.6016e-017    -1.6016e-017
v  ǁVelocityǁ        0.00058649          10.142          5.1398          5.1398
v  Pressure               -40.025          16.517         -11.411         -11.411
v  nu_tilda           3.1584e-007       0.0042695       0.0015313       0.0015313
v  TempC                       21          73.313          21.932          21.932
v  TurbVisc           8.6358e-015       0.0050321       0.0017986       0.0017986
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1779:        0.18940E+01

===============================================================


 INSTANT    0.178000000E+04   TIME STEP NUMBER            1780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70988E-02 0.89874E+00
   Friction velocity        uk    :  0.70988E-02 0.89874E+00
   Dimensionless distance   yplus :  0.57150E-01 0.72355E+01
   Friction thermal sca.    tstar : -0.66385E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42640E-01 0.53985E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96065E-02      33   0.24872E-03   0.48347E+01 0.17428E+03 
c  Velocity[X]                                      0.18341E+01 
c  Velocity[Y]                                      0.30006E+01 
c  Velocity[Z]                                      0.99054E-30 
c  Pressure     0.10567E-06     440   0.99761E-08   0.10332E+00 0.51939E+03 
c  nu_tilda     0.66645E-05      32   0.15283E-04   0.46740E-06 0.18398E+03 
c  TempC        0.38792E+02      27   0.31439E-03   0.47753E+01 0.23130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1923          10.141          4.5729          4.5729
v  Velocity[Y]            -2.6974          7.3248        0.050045        0.050045
v  Velocity[Z]       -7.7952e-015     1.4536e-014    -1.6021e-017    -1.6021e-017
v  ǁVelocityǁ        0.00053558          10.141          5.1397          5.1397
v  Pressure               -40.013          16.646         -11.402         -11.402
v  nu_tilda           3.1688e-007       0.0042695       0.0015317       0.0015317
v  TempC                       21          73.321          21.932          21.932
v  TurbVisc           8.7541e-015       0.0050321       0.0017991       0.0017991
v  total_pressure     1.0128e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1780:        0.21610E+01

===============================================================


 INSTANT    0.178100000E+04   TIME STEP NUMBER            1781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11030E-02 0.89990E+00
   Friction velocity        uk    :  0.11030E-02 0.89990E+00
   Dimensionless distance   yplus :  0.88799E-02 0.72448E+01
   Friction thermal sca.    tstar : -0.64844E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66254E-02 0.54054E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96087E-02      33   0.30246E-03   0.48487E+01 0.17447E+03 
c  Velocity[X]                                      0.18247E+01 
c  Velocity[Y]                                      0.30241E+01 
c  Velocity[Z]                                      0.93455E-30 
c  Pressure     0.10868E-06     472   0.98938E-08   0.10467E+00 0.54488E+03 
c  nu_tilda     0.66668E-05      32   0.44410E-05   0.46799E-06 0.18408E+03 
c  TempC        0.38800E+02      27   0.31189E-03   0.35785E+01 0.21739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1892           10.14          4.5729          4.5729
v  Velocity[Y]            -2.6994          7.3282        0.050325        0.050325
v  Velocity[Z]       -7.6425e-015     1.4461e-014    -1.6035e-017    -1.6035e-017
v  ǁVelocityǁ         0.0005106           10.14          5.1396          5.1396
v  Pressure               -39.976           16.66         -11.378         -11.378
v  nu_tilda           3.1796e-007       0.0042695       0.0015322       0.0015322
v  TempC                       21          73.329          21.933          21.933
v  TurbVisc           8.8709e-015       0.0050321       0.0017996       0.0017996
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1781:        0.24030E+01

===============================================================


 INSTANT    0.178200000E+04   TIME STEP NUMBER            1782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44683E-02 0.89958E+00
   Friction velocity        uk    :  0.44683E-02 0.89958E+00
   Dimensionless distance   yplus :  0.35973E-01 0.72423E+01
   Friction thermal sca.    tstar : -0.68941E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26840E-01 0.54035E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96109E-02      33   0.27695E-03   0.48890E+01 0.17464E+03 
c  Velocity[X]                                      0.18714E+01 
c  Velocity[Y]                                      0.30176E+01 
c  Velocity[Z]                                      0.11983E-29 
c  Pressure     0.12000E-06     520   0.93372E-08   0.12012E+00 0.88460E+03 
c  nu_tilda     0.66692E-05      32   0.15282E-04   0.46861E-06 0.18418E+03 
c  TempC        0.38808E+02      27   0.25411E-03   0.44991E+01 0.23321E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1862          10.139          4.5729          4.5729
v  Velocity[Y]            -2.7013          7.2987        0.050604        0.050604
v  Velocity[Z]       -7.4891e-015     1.4553e-014    -1.6051e-017    -1.6051e-017
v  ǁVelocityǁ        0.00047121          10.139          5.1396          5.1396
v  Pressure               -39.966          16.519         -11.427         -11.427
v  nu_tilda            3.191e-007       0.0042695       0.0015326       0.0015326
v  TempC                       21          73.336          21.933          21.933
v  TurbVisc           8.9926e-015       0.0050321       0.0018002       0.0018002
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1782:        0.21730E+01

===============================================================


 INSTANT    0.178300000E+04   TIME STEP NUMBER            1783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53993E-02 0.89817E+00
   Friction velocity        uk    :  0.53993E-02 0.89817E+00
   Dimensionless distance   yplus :  0.43468E-01 0.72309E+01
   Friction thermal sca.    tstar : -0.67442E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32432E-01 0.53950E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96132E-02      33   0.28744E-03   0.48486E+01 0.17455E+03 
c  Velocity[X]                                      0.18399E+01 
c  Velocity[Y]                                      0.30086E+01 
c  Velocity[Z]                                      0.11374E-29 
c  Pressure     0.86310E-07     536   0.96689E-08   0.84100E-01 0.11383E+04 
c  nu_tilda     0.66715E-05      32   0.44376E-05   0.46919E-06 0.18428E+03 
c  TempC        0.38817E+02      27   0.34790E-03   0.28494E+01 0.20198E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1834          10.138          4.5729          4.5729
v  Velocity[Y]            -2.7031          7.3216        0.050886        0.050886
v  Velocity[Z]       -7.3958e-015     1.4189e-014    -1.6056e-017    -1.6056e-017
v  ǁVelocityǁ        0.00044979          10.138          5.1395          5.1395
v  Pressure               -39.927          16.694         -11.368         -11.368
v  nu_tilda           3.2031e-007       0.0042695       0.0015331       0.0015331
v  TempC                       21          73.343          21.934          21.934
v  TurbVisc           9.1212e-015       0.0050321       0.0018007       0.0018007
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1783:        0.22170E+01

===============================================================


 INSTANT    0.178400000E+04   TIME STEP NUMBER            1784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32070E-02 0.89916E+00
   Friction velocity        uk    :  0.32070E-02 0.89916E+00
   Dimensionless distance   yplus :  0.25818E-01 0.72388E+01
   Friction thermal sca.    tstar : -0.65099E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19263E-01 0.54010E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96154E-02      33   0.29023E-03   0.48627E+01 0.17467E+03 
c  Velocity[X]                                      0.18443E+01 
c  Velocity[Y]                                      0.30184E+01 
c  Velocity[Z]                                      0.90243E-30 
c  Pressure     0.11612E-06     537   0.99587E-08   0.11217E+00 0.12314E+04 
c  nu_tilda     0.66738E-05      32   0.15276E-04   0.46981E-06 0.18438E+03 
c  TempC        0.38825E+02      27   0.35133E-03   0.57359E+01 0.27217E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1805          10.137          4.5729          4.5729
v  Velocity[Y]            -2.7048          7.2914        0.051167        0.051167
v  Velocity[Z]       -7.3972e-015     1.3949e-014    -1.6066e-017    -1.6066e-017
v  ǁVelocityǁ        0.00041044          10.137          5.1394          5.1394
v  Pressure               -39.917          16.484         -11.434         -11.434
v  nu_tilda           3.2159e-007       0.0042695       0.0015335       0.0015335
v  TempC                       21          73.349          21.934          21.934
v  TurbVisc           9.2606e-015       0.0050321       0.0018012       0.0018012
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1784:        0.22190E+01

===============================================================


 INSTANT    0.178500000E+04   TIME STEP NUMBER            1785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59689E-02 0.89858E+00
   Friction velocity        uk    :  0.59689E-02 0.89858E+00
   Dimensionless distance   yplus :  0.48054E-01 0.72342E+01
   Friction thermal sca.    tstar : -0.66894E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35853E-01 0.53975E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96176E-02      33   0.19920E-03   0.48648E+01 0.17473E+03 
c  Velocity[X]                                      0.18493E+01 
c  Velocity[Y]                                      0.30155E+01 
c  Velocity[Z]                                      0.91320E-30 
c  Pressure     0.91084E-07     568   0.97308E-08   0.89356E-01 0.14264E+04 
c  nu_tilda     0.66762E-05      32   0.44471E-05   0.47039E-06 0.18448E+03 
c  TempC        0.38834E+02      27   0.32610E-03   0.55112E+01 0.26909E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1775          10.136          4.5729          4.5729
v  Velocity[Y]            -2.7063          7.3201        0.051449        0.051449
v  Velocity[Z]       -7.4025e-015     1.3771e-014    -1.6078e-017    -1.6078e-017
v  ǁVelocityǁ        0.00037276          10.136          5.1393          5.1393
v  Pressure               -39.879          16.718         -11.361         -11.361
v  nu_tilda           3.2292e-007       0.0042695        0.001534        0.001534
v  TempC                       21          73.355          21.934          21.934
v  TurbVisc           9.4097e-015       0.0050321       0.0018018       0.0018018
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1785:        0.22940E+01

===============================================================


 INSTANT    0.178600000E+04   TIME STEP NUMBER            1786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42294E-02 0.89990E+00
   Friction velocity        uk    :  0.42294E-02 0.89990E+00
   Dimensionless distance   yplus :  0.34049E-01 0.72448E+01
   Friction thermal sca.    tstar : -0.64721E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25405E-01 0.54055E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96199E-02      33   0.29755E-03   0.48253E+01 0.17459E+03 
c  Velocity[X]                                      0.18154E+01 
c  Velocity[Y]                                      0.30099E+01 
c  Velocity[Z]                                      0.97161E-30 
c  Pressure     0.85132E-07     474   0.97045E-08   0.82942E-01 0.66485E+03 
c  nu_tilda     0.66785E-05      32   0.15267E-04   0.47101E-06 0.18458E+03 
c  TempC        0.38842E+02      27   0.34058E-03   0.53955E+01 0.25340E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1745          10.135          4.5729          4.5729
v  Velocity[Y]            -2.7084          7.3299        0.051732        0.051732
v  Velocity[Z]       -8.4309e-015     1.3754e-014    -1.6096e-017    -1.6096e-017
v  ǁVelocityǁ        0.00033629          10.135          5.1393          5.1393
v  Pressure               -39.865          16.636         -11.397         -11.397
v  nu_tilda            3.243e-007       0.0042695       0.0015344       0.0015344
v  TempC                       21           73.36          21.935          21.935
v  TurbVisc           9.5666e-015       0.0050321       0.0018023       0.0018023
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1786:        0.20890E+01

===============================================================


 INSTANT    0.178700000E+04   TIME STEP NUMBER            1787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34246E-02 0.89949E+00
   Friction velocity        uk    :  0.34246E-02 0.89949E+00
   Dimensionless distance   yplus :  0.27571E-01 0.72415E+01
   Friction thermal sca.    tstar : -0.64220E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20571E-01 0.54030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96221E-02      33   0.30845E-03   0.48822E+01 0.17491E+03 
c  Velocity[X]                                      0.18553E+01 
c  Velocity[Y]                                      0.30268E+01 
c  Velocity[Z]                                      0.98674E-30 
c  Pressure     0.11386E-06     456   0.95030E-08   0.11191E+00 0.49202E+03 
c  nu_tilda     0.66809E-05      32   0.44453E-05   0.47160E-06 0.18468E+03 
c  TempC        0.38850E+02      27   0.30765E-03   0.48919E+01 0.24444E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1714          10.134          4.5729          4.5729
v  Velocity[Y]            -2.7104          7.2969        0.052016        0.052016
v  Velocity[Z]       -8.4177e-015     1.3344e-014    -1.6117e-017    -1.6117e-017
v  ǁVelocityǁ        0.00030291          10.134          5.1392          5.1392
v  Pressure               -39.828          16.605          -11.38          -11.38
v  nu_tilda           3.2574e-007       0.0042695       0.0015349       0.0015349
v  TempC                       21          73.365          21.935          21.935
v  TurbVisc           9.7314e-015       0.0050321       0.0018028       0.0018028
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1787:        0.20400E+01

===============================================================


 INSTANT    0.178800000E+04   TIME STEP NUMBER            1788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26983E-02 0.89810E+00
   Friction velocity        uk    :  0.26983E-02 0.89810E+00
   Dimensionless distance   yplus :  0.21723E-01 0.72303E+01
   Friction thermal sca.    tstar : -0.65487E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16208E-01 0.53946E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96244E-02      33   0.26742E-03   0.48847E+01 0.17501E+03 
c  Velocity[X]                                      0.18665E+01 
c  Velocity[Y]                                      0.30182E+01 
c  Velocity[Z]                                      0.90444E-30 
c  Pressure     0.10887E-06     424   0.98237E-08   0.10531E+00 0.31530E+03 
c  nu_tilda     0.66832E-05      32   0.15270E-04   0.47222E-06 0.18478E+03 
c  TempC        0.38859E+02      27   0.32543E-03   0.36838E+01 0.21943E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1684          10.133          4.5729          4.5729
v  Velocity[Y]            -2.7123          7.3172        0.052301        0.052301
v  Velocity[Z]       -9.2316e-015      1.304e-014    -1.6141e-017    -1.6141e-017
v  ǁVelocityǁ        0.00025495          10.133          5.1391          5.1391
v  Pressure               -39.816          16.659         -11.389         -11.389
v  nu_tilda            3.272e-007       0.0042695       0.0015353       0.0015353
v  TempC                       21           73.37          21.936          21.936
v  TurbVisc            9.905e-015       0.0050321       0.0018034       0.0018034
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1788:        0.19790E+01

===============================================================


 INSTANT    0.178900000E+04   TIME STEP NUMBER            1789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28756E-02 0.89919E+00
   Friction velocity        uk    :  0.28756E-02 0.89919E+00
   Dimensionless distance   yplus :  0.23151E-01 0.72391E+01
   Friction thermal sca.    tstar : -0.64891E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17273E-01 0.54012E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96266E-02      33   0.28831E-03   0.48654E+01 0.17495E+03 
c  Velocity[X]                                      0.18441E+01 
c  Velocity[Y]                                      0.30213E+01 
c  Velocity[Z]                                      0.83421E-30 
c  Pressure     0.11411E-06     472   0.94594E-08   0.11364E+00 0.51211E+03 
c  nu_tilda     0.66855E-05      32   0.44420E-05   0.47280E-06 0.18487E+03 
c  TempC        0.38867E+02      27   0.37440E-03   0.39925E+01 0.23356E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1655          10.132          4.5729          4.5729
v  Velocity[Y]            -2.7141          7.2977        0.052585        0.052585
v  Velocity[Z]       -9.0298e-015     1.3048e-014    -1.6165e-017    -1.6165e-017
v  ǁVelocityǁ        0.00021095          10.133          5.1391          5.1391
v  Pressure               -39.779          16.647         -11.368         -11.368
v  nu_tilda           3.2864e-007       0.0042695       0.0015358       0.0015358
v  TempC                       21          73.374          21.936          21.936
v  TurbVisc           1.0084e-014       0.0050321       0.0018039       0.0018039
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1789:        0.20700E+01

===============================================================


 INSTANT    0.179000000E+04   TIME STEP NUMBER            1790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40823E-02 0.89824E+00
   Friction velocity        uk    :  0.40823E-02 0.89824E+00
   Dimensionless distance   yplus :  0.32865E-01 0.72315E+01
   Friction thermal sca.    tstar : -0.71284E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24521E-01 0.53955E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96288E-02      33   0.21732E-03   0.48659E+01 0.17500E+03 
c  Velocity[X]                                      0.18355E+01 
c  Velocity[Y]                                      0.30304E+01 
c  Velocity[Z]                                      0.15212E-29 
c  Pressure     0.10709E-06     456   0.93093E-08   0.10384E+00 0.36395E+03 
c  nu_tilda     0.66879E-05      32   0.15262E-04   0.47342E-06 0.18497E+03 
c  TempC        0.38876E+02      27   0.30492E-03   0.46651E+01 0.25190E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1626          10.131          4.5729          4.5729
v  Velocity[Y]            -2.7158          7.3153        0.052872        0.052872
v  Velocity[Z]       -9.7414e-015     1.2615e-014    -1.6183e-017    -1.6183e-017
v  ǁVelocityǁ        0.00017999          10.132           5.139           5.139
v  Pressure               -39.767          16.659         -11.388         -11.388
v  nu_tilda            3.301e-007       0.0042695       0.0015362       0.0015362
v  TempC                       21          73.377          21.936          21.936
v  TurbVisc           1.0263e-014       0.0050321       0.0018045       0.0018045
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1790:        0.20360E+01

===============================================================


 INSTANT    0.179100000E+04   TIME STEP NUMBER            1791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94936E-03 0.89970E+00
   Friction velocity        uk    :  0.94936E-03 0.89970E+00
   Dimensionless distance   yplus :  0.76430E-02 0.72432E+01
   Friction thermal sca.    tstar : -0.91293E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57025E-02 0.54043E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96311E-02      33   0.29155E-03   0.48341E+01 0.17494E+03 
c  Velocity[X]                                      0.18101E+01 
c  Velocity[Y]                                      0.30240E+01 
c  Velocity[Z]                                      0.10850E-29 
c  Pressure     0.84776E-07     521   0.92423E-08   0.83094E-01 0.87944E+03 
c  nu_tilda     0.66902E-05      32   0.44521E-05   0.47400E-06 0.18507E+03 
c  TempC        0.38884E+02      27   0.33584E-03   0.40733E+01 0.24327E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1596          10.131          4.5729          4.5729
v  Velocity[Y]            -2.7173          7.3269        0.053158        0.053158
v  Velocity[Z]       -1.1075e-014     1.2289e-014    -1.6207e-017    -1.6207e-017
v  ǁVelocityǁ        0.00014448          10.131          5.1389          5.1389
v  Pressure               -39.727          16.761         -11.341         -11.341
v  nu_tilda           3.3159e-007       0.0042695       0.0015367       0.0015367
v  TempC                       21          73.381          21.937          21.937
v  TurbVisc           1.0446e-014       0.0050321        0.001805        0.001805
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1791:        0.21780E+01

===============================================================


 INSTANT    0.179200000E+04   TIME STEP NUMBER            1792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32124E-02 0.89926E+00
   Friction velocity        uk    :  0.32124E-02 0.89926E+00
   Dimensionless distance   yplus :  0.25862E-01 0.72396E+01
   Friction thermal sca.    tstar : -0.15789E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19296E-01 0.54016E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96333E-02      33   0.31850E-03   0.48984E+01 0.17529E+03 
c  Velocity[X]                                      0.18743E+01 
c  Velocity[Y]                                      0.30241E+01 
c  Velocity[Z]                                      0.85565E-30 
c  Pressure     0.12173E-06     522   0.92540E-08   0.12095E+00 0.11564E+04 
c  nu_tilda     0.66926E-05      32   0.15255E-04   0.47463E-06 0.18517E+03 
c  TempC        0.38892E+02      27   0.37961E-03   0.49047E+01 0.25871E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1567           10.13          4.5729          4.5729
v  Velocity[Y]            -2.7192          7.2994        0.053446        0.053446
v  Velocity[Z]       -1.0491e-014     1.2088e-014    -1.6231e-017    -1.6231e-017
v  ǁVelocityǁ        0.00010296           10.13          5.1388          5.1388
v  Pressure               -39.716          16.565         -11.404         -11.404
v  nu_tilda           3.3309e-007       0.0042695       0.0015371       0.0015371
v  TempC                       21          73.384          21.937          21.937
v  TurbVisc           1.0636e-014       0.0050321       0.0018055       0.0018055
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1792:        0.21910E+01

===============================================================


 INSTANT    0.179300000E+04   TIME STEP NUMBER            1793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.24880E-02 0.89783E+00
   Friction velocity        uk    :  0.24880E-02 0.89783E+00
   Dimensionless distance   yplus :  0.20030E-01 0.72281E+01
   Friction thermal sca.    tstar : -0.17612E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14945E-01 0.53930E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96355E-02      33   0.28237E-03   0.49152E+01 0.17544E+03 
c  Velocity[X]                                      0.18738E+01 
c  Velocity[Y]                                      0.30414E+01 
c  Velocity[Z]                                      0.93764E-30 
c  Pressure     0.12026E-06     553   0.93177E-08   0.11541E+00 0.12494E+04 
c  nu_tilda     0.66949E-05      32   0.44525E-05   0.47522E-06 0.18527E+03 
c  TempC        0.38901E+02      27   0.35659E-03   0.46643E+01 0.25579E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1538          10.129          4.5729          4.5729
v  Velocity[Y]            -2.7212          7.3128        0.053734        0.053734
v  Velocity[Z]       -1.1357e-014     1.2099e-014    -1.6257e-017    -1.6257e-017
v  ǁVelocityǁ       6.8734e-005          10.129          5.1388          5.1388
v  Pressure               -39.677          16.755         -11.338         -11.338
v  nu_tilda           3.3462e-007       0.0042695       0.0015376       0.0015376
v  TempC                       21          73.387          21.938          21.938
v  TurbVisc            1.083e-014       0.0050321       0.0018061       0.0018061
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1793:        0.22570E+01

===============================================================


 INSTANT    0.179400000E+04   TIME STEP NUMBER            1794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16453E-02 0.89896E+00
   Friction velocity        uk    :  0.16453E-02 0.89896E+00
   Dimensionless distance   yplus :  0.13246E-01 0.72372E+01
   Friction thermal sca.    tstar : -0.95071E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98831E-02 0.53998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96378E-02      33   0.26010E-03   0.48796E+01 0.17530E+03 
c  Velocity[X]                                      0.18475E+01 
c  Velocity[Y]                                      0.30321E+01 
c  Velocity[Z]                                      0.92868E-30 
c  Pressure     0.10194E-06     504   0.91324E-08   0.10176E+00 0.92385E+03 
c  nu_tilda     0.66972E-05      32   0.15254E-04   0.47584E-06 0.18537E+03 
c  TempC        0.38909E+02      27   0.30673E-03   0.47002E+01 0.25845E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1509          10.128          4.5729          4.5729
v  Velocity[Y]            -2.7231          7.2896        0.054022        0.054022
v  Velocity[Z]        -1.093e-014     1.1686e-014    -1.6283e-017    -1.6283e-017
v  ǁVelocityǁ       3.7372e-005          10.128          5.1387          5.1387
v  Pressure               -39.666          16.614          -11.39          -11.39
v  nu_tilda           3.3615e-007       0.0042695        0.001538        0.001538
v  TempC                       21          73.389          21.938          21.938
v  TurbVisc            1.103e-014       0.0050321       0.0018066       0.0018066
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1794:        0.21460E+01

===============================================================


 INSTANT    0.179500000E+04   TIME STEP NUMBER            1795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13880E-02 0.89808E+00
   Friction velocity        uk    :  0.13880E-02 0.89808E+00
   Dimensionless distance   yplus :  0.11175E-01 0.72301E+01
   Friction thermal sca.    tstar : -0.13052E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83375E-02 0.53945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96400E-02      33   0.27086E-03   0.48565E+01 0.17526E+03 
c  Velocity[X]                                      0.18298E+01 
c  Velocity[Y]                                      0.30267E+01 
c  Velocity[Z]                                      0.80650E-30 
c  Pressure     0.92984E-07     552   0.93221E-08   0.91450E-01 0.10483E+04 
c  nu_tilda     0.66996E-05      32   0.44480E-05   0.47642E-06 0.18547E+03 
c  TempC        0.38918E+02      27   0.22378E-03   0.53547E+01 0.26606E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.148          10.127          4.5729          4.5729
v  Velocity[Y]            -2.7249          7.3173        0.054311        0.054311
v  Velocity[Z]       -1.1854e-014     1.1412e-014    -1.6312e-017    -1.6312e-017
v  ǁVelocityǁ       4.2204e-005          10.127          5.1386          5.1386
v  Pressure               -39.628          16.763         -11.335         -11.335
v  nu_tilda           3.3771e-007       0.0042695       0.0015385       0.0015385
v  TempC                       21          73.391          21.939          21.939
v  TurbVisc           1.1233e-014       0.0050321       0.0018071       0.0018071
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1795:        0.22690E+01

===============================================================


 INSTANT    0.179600000E+04   TIME STEP NUMBER            1796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12498E-02 0.89956E+00
   Friction velocity        uk    :  0.12498E-02 0.89956E+00
   Dimensionless distance   yplus :  0.10062E-01 0.72421E+01
   Friction thermal sca.    tstar : -0.21434E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75073E-02 0.54034E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96422E-02      33   0.29417E-03   0.49012E+01 0.17552E+03 
c  Velocity[X]                                      0.18516E+01 
c  Velocity[Y]                                      0.30496E+01 
c  Velocity[Z]                                      0.10131E-29 
c  Pressure     0.13559E-06     473   0.92407E-08   0.12916E+00 0.61344E+03 
c  nu_tilda     0.67019E-05      32   0.15247E-04   0.47704E-06 0.18557E+03 
c  TempC        0.38926E+02      27   0.41218E-03   0.30926E+01 0.20434E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.145          10.126          4.5729          4.5729
v  Velocity[Y]            -2.7265          7.3202        0.054602        0.054602
v  Velocity[Z]       -1.2154e-014     1.1447e-014    -1.6334e-017    -1.6334e-017
v  ǁVelocityǁ       8.2295e-005          10.126          5.1386          5.1386
v  Pressure               -39.613          16.694         -11.369         -11.369
v  nu_tilda           3.3929e-007       0.0042695       0.0015389       0.0015389
v  TempC                       21          73.392          21.939          21.939
v  TurbVisc           1.1443e-014       0.0050321       0.0018077       0.0018077
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1796:        0.20860E+01

===============================================================


 INSTANT    0.179700000E+04   TIME STEP NUMBER            1797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15994E-02 0.89948E+00
   Friction velocity        uk    :  0.15994E-02 0.89948E+00
   Dimensionless distance   yplus :  0.12876E-01 0.72414E+01
   Friction thermal sca.    tstar : -0.16733E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96069E-02 0.54029E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96445E-02      33   0.25590E-03   0.49022E+01 0.17560E+03 
c  Velocity[X]                                      0.18653E+01 
c  Velocity[Y]                                      0.30369E+01 
c  Velocity[Z]                                      0.11214E-29 
c  Pressure     0.10942E-06     488   0.97600E-08   0.10913E+00 0.55265E+03 
c  nu_tilda     0.67043E-05      32   0.44584E-05   0.47764E-06 0.18567E+03 
c  TempC        0.38934E+02      28   0.36617E-03   0.51041E+01 0.24755E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1418          10.125          4.5729          4.5729
v  Velocity[Y]            -2.7281          7.2938        0.054892        0.054892
v  Velocity[Z]       -1.1833e-014     1.1128e-014    -1.6359e-017    -1.6359e-017
v  ǁVelocityǁ        0.00011781          10.125          5.1385          5.1385
v  Pressure               -39.577          16.703         -11.344         -11.344
v  nu_tilda           3.4089e-007       0.0042695       0.0015394       0.0015394
v  TempC                       21          73.394          21.939          21.939
v  TurbVisc           1.1659e-014       0.0050321       0.0018082       0.0018082
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1797:        0.21030E+01

===============================================================


 INSTANT    0.179800000E+04   TIME STEP NUMBER            1798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23805E-02 0.89781E+00
   Friction velocity        uk    :  0.23805E-02 0.89781E+00
   Dimensionless distance   yplus :  0.19165E-01 0.72280E+01
   Friction thermal sca.    tstar : -0.11233E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14299E-01 0.53929E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96467E-02      33   0.31333E-03   0.48567E+01 0.17542E+03 
c  Velocity[X]                                      0.18288E+01 
c  Velocity[Y]                                      0.30279E+01 
c  Velocity[Z]                                      0.10642E-29 
c  Pressure     0.91885E-07     457   0.91535E-08   0.89343E-01 0.36437E+03 
c  nu_tilda     0.67066E-05      32   0.15242E-04   0.47826E-06 0.18577E+03 
c  TempC        0.38943E+02      27   0.30394E-03   0.51206E+01 0.24252E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1388          10.124          4.5729          4.5729
v  Velocity[Y]            -2.7299          7.3146        0.055184        0.055184
v  Velocity[Z]        -1.193e-014     1.1058e-014    -1.6381e-017    -1.6381e-017
v  ǁVelocityǁ        0.00016105          10.124          5.1385          5.1385
v  Pressure               -39.563          16.706         -11.363         -11.363
v  nu_tilda           3.4254e-007       0.0042695       0.0015398       0.0015398
v  TempC                       21          73.395           21.94           21.94
v  TurbVisc           1.1881e-014       0.0050321       0.0018087       0.0018087
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1798:        0.20390E+01

===============================================================


 INSTANT    0.179900000E+04   TIME STEP NUMBER            1799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18774E-02 0.89890E+00
   Friction velocity        uk    :  0.18774E-02 0.89890E+00
   Dimensionless distance   yplus :  0.15114E-01 0.72367E+01
   Friction thermal sca.    tstar : -0.87214E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11277E-01 0.53994E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96489E-02      33   0.31591E-03   0.49030E+01 0.17571E+03 
c  Velocity[X]                                      0.18511E+01 
c  Velocity[Y]                                      0.30519E+01 
c  Velocity[Z]                                      0.10278E-29 
c  Pressure     0.12015E-06     473   0.94452E-08   0.11778E+00 0.50164E+03 
c  nu_tilda     0.67089E-05      32   0.44577E-05   0.47885E-06 0.18586E+03 
c  TempC        0.38951E+02      27   0.29066E-03   0.48916E+01 0.24702E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1359          10.123          4.5729          4.5729
v  Velocity[Y]            -2.7319          7.2873        0.055476        0.055476
v  Velocity[Z]       -1.1971e-014      1.124e-014    -1.6407e-017    -1.6407e-017
v  ǁVelocityǁ        0.00021138          10.123          5.1384          5.1384
v  Pressure               -39.526          16.689         -11.344         -11.344
v  nu_tilda            3.442e-007       0.0042695       0.0015403       0.0015403
v  TempC                       21          73.396           21.94           21.94
v  TurbVisc           1.2112e-014       0.0050321       0.0018092       0.0018092
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1799:        0.20760E+01

===============================================================


 INSTANT    0.180000000E+04   TIME STEP NUMBER            1800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36577E-02 0.89811E+00
   Friction velocity        uk    :  0.36577E-02 0.89811E+00
   Dimensionless distance   yplus :  0.29447E-01 0.72304E+01
   Friction thermal sca.    tstar : -0.73026E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21971E-01 0.53947E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96512E-02      33   0.22461E-03   0.49147E+01 0.17583E+03 
c  Velocity[X]                                      0.18759E+01 
c  Velocity[Y]                                      0.30388E+01 
c  Velocity[Z]                                      0.77345E-30 
c  Pressure     0.10357E-06     426   0.96735E-08   0.10038E+00 0.31297E+03 
c  nu_tilda     0.67113E-05      32   0.15240E-04   0.47947E-06 0.18596E+03 
c  TempC        0.38960E+02      27   0.33785E-03   0.41772E+01 0.24321E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.133          10.122          4.5729          4.5729
v  Velocity[Y]            -2.7338          7.3131        0.055769        0.055769
v  Velocity[Z]       -1.2276e-014     1.1473e-014    -1.6432e-017    -1.6432e-017
v  ǁVelocityǁ        0.00025447          10.122          5.1383          5.1383
v  Pressure               -39.513          16.736         -11.353         -11.353
v  nu_tilda           3.4589e-007       0.0042695       0.0015407       0.0015407
v  TempC                       21          73.396          21.941          21.941
v  TurbVisc           1.2349e-014       0.0050321       0.0018098       0.0018098
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1800:        0.19680E+01

===============================================================


 INSTANT    0.180100000E+04   TIME STEP NUMBER            1801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32908E-02 0.89969E+00
   Friction velocity        uk    :  0.32908E-02 0.89969E+00
   Dimensionless distance   yplus :  0.26493E-01 0.72431E+01
   Friction thermal sca.    tstar : -0.65000E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19767E-01 0.54042E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96534E-02      33   0.29319E-03   0.48663E+01 0.17565E+03 
c  Velocity[X]                                      0.18284E+01 
c  Velocity[Y]                                      0.30378E+01 
c  Velocity[Z]                                      0.75424E-30 
c  Pressure     0.99439E-07     537   0.98412E-08   0.97887E-01 0.94277E+03 
c  nu_tilda     0.67136E-05      32   0.44542E-05   0.48006E-06 0.18606E+03 
c  TempC        0.38968E+02      27   0.31624E-03   0.43071E+01 0.23606E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.13          10.121          4.5729          4.5729
v  Velocity[Y]            -2.7355          7.3261        0.056062        0.056062
v  Velocity[Z]       -1.2482e-014     1.1762e-014    -1.6463e-017    -1.6463e-017
v  ǁVelocityǁ        0.00030297          10.121          5.1383          5.1383
v  Pressure               -39.473           16.85         -11.302         -11.302
v  nu_tilda           3.4759e-007       0.0042695       0.0015412       0.0015412
v  TempC                       21          73.396          21.941          21.941
v  TurbVisc           1.2593e-014       0.0050321       0.0018103       0.0018103
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1801:        0.22310E+01

===============================================================


 INSTANT    0.180200000E+04   TIME STEP NUMBER            1802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45706E-02 0.89913E+00
   Friction velocity        uk    :  0.45706E-02 0.89913E+00
   Dimensionless distance   yplus :  0.36796E-01 0.72386E+01
   Friction thermal sca.    tstar : -0.63770E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27454E-01 0.54008E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96557E-02      33   0.28350E-03   0.49029E+01 0.17586E+03 
c  Velocity[X]                                      0.18539E+01 
c  Velocity[Y]                                      0.30490E+01 
c  Velocity[Z]                                      0.95839E-30 
c  Pressure     0.11283E-06     552   0.97710E-08   0.11038E+00 0.13006E+04 
c  nu_tilda     0.67160E-05      32   0.15235E-04   0.48068E-06 0.18616E+03 
c  TempC        0.38976E+02      27   0.26254E-03   0.50331E+01 0.25296E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1271           10.12          4.5729          4.5729
v  Velocity[Y]            -2.7372          7.2903        0.056356        0.056356
v  Velocity[Z]       -1.1918e-014     1.1141e-014    -1.6487e-017    -1.6487e-017
v  ǁVelocityǁ        0.00035024           10.12          5.1382          5.1382
v  Pressure               -39.461          16.629         -11.372         -11.372
v  nu_tilda           3.4933e-007       0.0042695       0.0015416       0.0015416
v  TempC                       21          73.396          21.941          21.941
v  TurbVisc           1.2842e-014       0.0050321       0.0018109       0.0018109
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1802:        0.22650E+01

===============================================================


 INSTANT    0.180300000E+04   TIME STEP NUMBER            1803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45821E-02 0.89786E+00
   Friction velocity        uk    :  0.45821E-02 0.89786E+00
   Dimensionless distance   yplus :  0.36889E-01 0.72284E+01
   Friction thermal sca.    tstar : -0.65241E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27523E-01 0.53932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96579E-02      33   0.25817E-03   0.48897E+01 0.17587E+03 
c  Velocity[X]                                      0.18482E+01 
c  Velocity[Y]                                      0.30415E+01 
c  Velocity[Z]                                      0.98206E-30 
c  Pressure     0.94150E-07     568   0.98400E-08   0.92318E-01 0.13657E+04 
c  nu_tilda     0.67183E-05      32   0.44649E-05   0.48127E-06 0.18626E+03 
c  TempC        0.38985E+02      27   0.44016E-03   0.48818E+01 0.25450E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1243          10.119          4.5729          4.5729
v  Velocity[Y]            -2.7387          7.3138        0.056651        0.056651
v  Velocity[Z]       -1.2098e-014     1.1092e-014    -1.6514e-017    -1.6514e-017
v  ǁVelocityǁ         0.0004016          10.119          5.1382          5.1382
v  Pressure               -39.423          16.851         -11.301         -11.301
v  nu_tilda           3.5108e-007       0.0042695       0.0015421       0.0015421
v  TempC                       21          73.395          21.942          21.942
v  TurbVisc           1.3101e-014       0.0050321       0.0018114       0.0018114
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1803:        0.23050E+01

===============================================================


 INSTANT    0.180400000E+04   TIME STEP NUMBER            1804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49803E-02 0.89872E+00
   Friction velocity        uk    :  0.49803E-02 0.89872E+00
   Dimensionless distance   yplus :  0.40095E-01 0.72353E+01
   Friction thermal sca.    tstar : -0.63541E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29915E-01 0.53983E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96601E-02      33   0.29745E-03   0.48780E+01 0.17585E+03 
c  Velocity[X]                                      0.18409E+01 
c  Velocity[Y]                                      0.30370E+01 
c  Velocity[Z]                                      0.10353E-29 
c  Pressure     0.98555E-07     520   0.96265E-08   0.97042E-01 0.11920E+04 
c  nu_tilda     0.67206E-05      32   0.15226E-04   0.48190E-06 0.18636E+03 
c  TempC        0.38993E+02      27   0.33558E-03   0.81905E+01 0.31467E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1214          10.118          4.5729          4.5729
v  Velocity[Y]            -2.7404          7.2909        0.056947        0.056947
v  Velocity[Z]       -1.1945e-014      1.101e-014    -1.6537e-017    -1.6537e-017
v  ǁVelocityǁ        0.00044746          10.118          5.1381          5.1381
v  Pressure               -39.411          16.651         -11.365         -11.365
v  nu_tilda           3.5288e-007       0.0042695       0.0015425       0.0015425
v  TempC                       21          73.394          21.942          21.942
v  TurbVisc           1.3366e-014       0.0050321       0.0018119       0.0018119
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1804:        0.21680E+01

===============================================================


 INSTANT    0.180500000E+04   TIME STEP NUMBER            1805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33935E-02 0.89781E+00
   Friction velocity        uk    :  0.33935E-02 0.89781E+00
   Dimensionless distance   yplus :  0.27320E-01 0.72280E+01
   Friction thermal sca.    tstar : -0.65445E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20384E-01 0.53929E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96623E-02      33   0.24145E-03   0.48951E+01 0.17599E+03 
c  Velocity[X]                                      0.18436E+01 
c  Velocity[Y]                                      0.30515E+01 
c  Velocity[Z]                                      0.86930E-30 
c  Pressure     0.10106E-06     538   0.93723E-08   0.98556E-01 0.12608E+04 
c  nu_tilda     0.67230E-05      32   0.44633E-05   0.48249E-06 0.18646E+03 
c  TempC        0.39001E+02      27   0.31941E-03   0.49309E+01 0.25260E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1184          10.117          4.5729          4.5729
v  Velocity[Y]            -2.7424           7.312        0.057243        0.057243
v  Velocity[Z]       -1.2564e-014     1.1268e-014    -1.6565e-017    -1.6565e-017
v  ǁVelocityǁ        0.00049548          10.118           5.138           5.138
v  Pressure               -39.372           16.84         -11.299         -11.299
v  nu_tilda           3.5474e-007       0.0042695       0.0015431       0.0015431
v  TempC                       21          73.393          21.943          21.943
v  TurbVisc           1.3642e-014       0.0050321       0.0018124       0.0018124
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1805:        0.22340E+01

===============================================================


 INSTANT    0.180600000E+04   TIME STEP NUMBER            1806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23370E-02 0.89924E+00
   Friction velocity        uk    :  0.23370E-02 0.89924E+00
   Dimensionless distance   yplus :  0.18814E-01 0.72395E+01
   Friction thermal sca.    tstar : -0.68743E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14038E-01 0.54015E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96646E-02      33   0.28792E-03   0.48706E+01 0.17594E+03 
c  Velocity[X]                                      0.18254E+01 
c  Velocity[Y]                                      0.30453E+01 
c  Velocity[Z]                                      0.11927E-29 
c  Pressure     0.95673E-07     472   0.99340E-08   0.94053E-01 0.50254E+03 
c  nu_tilda     0.67253E-05      32   0.15225E-04   0.48311E-06 0.18656E+03 
c  TempC        0.39010E+02      27   0.32331E-03   0.46143E+01 0.24983E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1155          10.117          4.5729          4.5729
v  Velocity[Y]            -2.7443          7.3194        0.057539        0.057539
v  Velocity[Z]       -1.4881e-014     1.1291e-014    -1.6602e-017    -1.6602e-017
v  ǁVelocityǁ        0.00055228          10.117           5.138           5.138
v  Pressure               -39.357            16.8         -11.326         -11.326
v  nu_tilda           3.5663e-007       0.0042695       0.0015434       0.0015434
v  TempC                       21          73.391          21.943          21.943
v  TurbVisc           1.3933e-014       0.0050321        0.001813        0.001813
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1806:        0.20630E+01

===============================================================


 INSTANT    0.180700000E+04   TIME STEP NUMBER            1807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.56351E-02 0.89887E+00
   Friction velocity        uk    :  0.56351E-02 0.89887E+00
   Dimensionless distance   yplus :  0.45366E-01 0.72365E+01
   Friction thermal sca.    tstar : -0.75701E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33848E-01 0.53993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96668E-02      33   0.29276E-03   0.49208E+01 0.17625E+03 
c  Velocity[X]                                      0.18740E+01 
c  Velocity[Y]                                      0.30469E+01 
c  Velocity[Z]                                      0.73439E-30 
c  Pressure     0.11970E-06     472   0.97970E-08   0.11993E+00 0.48045E+03 
c  nu_tilda     0.67277E-05      32   0.44576E-05   0.48371E-06 0.18665E+03 
c  TempC        0.39018E+02      27   0.37341E-03   0.42496E+01 0.24053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1123          10.116          4.5729          4.5729
v  Velocity[Y]             -2.746          7.2951        0.057837        0.057837
v  Velocity[Z]        -1.482e-014     1.1253e-014    -1.6635e-017    -1.6635e-017
v  ǁVelocityǁ        0.00059293          10.116          5.1379          5.1379
v  Pressure                -39.32          16.764          -11.31          -11.31
v  nu_tilda            3.586e-007       0.0042695        0.001544        0.001544
v  TempC                       21          73.389          21.944          21.944
v  TurbVisc           1.4232e-014       0.0050321       0.0018135       0.0018135
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1807:        0.20830E+01

===============================================================


 INSTANT    0.180800000E+04   TIME STEP NUMBER            1808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52675E-02 0.89736E+00
   Friction velocity        uk    :  0.52675E-02 0.89736E+00
   Dimensionless distance   yplus :  0.42407E-01 0.72244E+01
   Friction thermal sca.    tstar : -0.99014E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31640E-01 0.53902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96690E-02      33   0.26462E-03   0.49162E+01 0.17626E+03 
c  Velocity[X]                                      0.18550E+01 
c  Velocity[Y]                                      0.30612E+01 
c  Velocity[Z]                                      0.89061E-30 
c  Pressure     0.11601E-06     457   0.98019E-08   0.11080E+00 0.37885E+03 
c  nu_tilda     0.67300E-05      32   0.15222E-04   0.48434E-06 0.18675E+03 
c  TempC        0.39027E+02      27   0.36454E-03   0.46438E+01 0.23975E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1093          10.115          4.5729          4.5729
v  Velocity[Y]            -2.7476          7.3051        0.058135        0.058135
v  Velocity[Z]       -1.6414e-014     1.0996e-014    -1.6669e-017    -1.6669e-017
v  ǁVelocityǁ        0.00064312          10.115          5.1379          5.1379
v  Pressure               -39.305          16.768          -11.33          -11.33
v  nu_tilda           3.6064e-007       0.0042695       0.0015443       0.0015443
v  TempC                       21          73.387          21.944          21.944
v  TurbVisc           1.4548e-014       0.0050321        0.001814        0.001814
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1808:        0.20230E+01

===============================================================


 INSTANT    0.180900000E+04   TIME STEP NUMBER            1809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25579E-02 0.89857E+00
   Friction velocity        uk    :  0.25579E-02 0.89857E+00
   Dimensionless distance   yplus :  0.20593E-01 0.72341E+01
   Friction thermal sca.    tstar : -0.17996E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15365E-01 0.53974E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96713E-02      33   0.27251E-03   0.48906E+01 0.17620E+03 
c  Velocity[X]                                      0.18390E+01 
c  Velocity[Y]                                      0.30516E+01 
c  Velocity[Z]                                      0.86924E-30 
c  Pressure     0.10112E-06     488   0.92732E-08   0.10095E+00 0.57700E+03 
c  nu_tilda     0.67324E-05      32   0.44691E-05   0.48492E-06 0.18685E+03 
c  TempC        0.39035E+02      27   0.31521E-03   0.48847E+01 0.25510E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1064          10.114          4.5729          4.5729
v  Velocity[Y]            -2.7491          7.2857        0.058434        0.058434
v  Velocity[Z]       -1.6059e-014     1.0841e-014    -1.6695e-017    -1.6695e-017
v  ǁVelocityǁ         0.0006948          10.114          5.1378          5.1378
v  Pressure               -39.269          16.784         -11.303         -11.303
v  nu_tilda           3.6275e-007       0.0042695       0.0015449       0.0015449
v  TempC                       21          73.385          21.944          21.944
v  TurbVisc           1.4881e-014       0.0050321       0.0018146       0.0018146
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1809:        0.21100E+01

===============================================================


 INSTANT    0.181000000E+04   TIME STEP NUMBER            1810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49158E-02 0.89764E+00
   Friction velocity        uk    :  0.49158E-02 0.89764E+00
   Dimensionless distance   yplus :  0.39575E-01 0.72266E+01
   Friction thermal sca.    tstar : -0.16549E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29528E-01 0.53919E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96735E-02      33   0.27753E-03   0.48886E+01 0.17624E+03 
c  Velocity[X]                                      0.18429E+01 
c  Velocity[Y]                                      0.30457E+01 
c  Velocity[Z]                                      0.84533E-30 
c  Pressure     0.95634E-07     457   0.91475E-08   0.93438E-01 0.37872E+03 
c  nu_tilda     0.67347E-05      32   0.15212E-04   0.48555E-06 0.18695E+03 
c  TempC        0.39043E+02      27   0.42223E-03   0.41455E+01 0.23918E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1035          10.113          4.5729          4.5729
v  Velocity[Y]            -2.7507          7.3119        0.058734        0.058734
v  Velocity[Z]       -1.7516e-014     1.0657e-014    -1.6726e-017    -1.6726e-017
v  ǁVelocityǁ        0.00075146          10.113          5.1378          5.1378
v  Pressure               -39.254          16.785         -11.323         -11.323
v  nu_tilda           3.6494e-007       0.0042695       0.0015452       0.0015452
v  TempC                       21          73.383          21.945          21.945
v  TurbVisc           1.5233e-014       0.0050321       0.0018151       0.0018151
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1810:        0.24020E+01

===============================================================


 INSTANT    0.181100000E+04   TIME STEP NUMBER            1811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52101E-02 0.89928E+00
   Friction velocity        uk    :  0.52101E-02 0.89928E+00
   Dimensionless distance   yplus :  0.41945E-01 0.72398E+01
   Friction thermal sca.    tstar : -0.96164E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31295E-01 0.54017E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96757E-02      33   0.28197E-03   0.49275E+01 0.17647E+03 
c  Velocity[X]                                      0.18529E+01 
c  Velocity[Y]                                      0.30745E+01 
c  Velocity[Z]                                      0.13320E-29 
c  Pressure     0.14109E-06     537   0.98680E-08   0.13718E+00 0.98379E+03 
c  nu_tilda     0.67370E-05      32   0.44644E-05   0.48614E-06 0.18705E+03 
c  TempC        0.39052E+02      27   0.36805E-03   0.56846E+01 0.26635E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1006          10.112          4.5729          4.5729
v  Velocity[Y]            -2.7528          7.3168        0.059033        0.059033
v  Velocity[Z]       -2.0172e-014     1.0461e-014    -1.6767e-017    -1.6767e-017
v  ǁVelocityǁ        0.00080636          10.112          5.1377          5.1377
v  Pressure               -39.214          16.901          -11.27          -11.27
v  nu_tilda           3.6721e-007       0.0042695       0.0015457       0.0015457
v  TempC                       21           73.38          21.945          21.945
v  TurbVisc           1.5605e-014       0.0050321       0.0018156       0.0018156
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1811:        0.25560E+01

===============================================================


 INSTANT    0.181200000E+04   TIME STEP NUMBER            1812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58700E-02 0.89906E+00
   Friction velocity        uk    :  0.58700E-02 0.89906E+00
   Dimensionless distance   yplus :  0.47257E-01 0.72380E+01
   Friction thermal sca.    tstar : -0.74114E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35259E-01 0.54004E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96780E-02      33   0.24736E-03   0.49198E+01 0.17646E+03 
c  Velocity[X]                                      0.18608E+01 
c  Velocity[Y]                                      0.30590E+01 
c  Velocity[Z]                                      0.90657E-30 
c  Pressure     0.10558E-06     538   0.97859E-08   0.10461E+00 0.10773E+04 
c  nu_tilda     0.67394E-05      32   0.15216E-04   0.48677E-06 0.18715E+03 
c  TempC        0.39060E+02      27   0.35631E-03   0.62053E+01 0.26084E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0976          10.111          4.5729          4.5729
v  Velocity[Y]            -2.7546          7.2881        0.059335        0.059335
v  Velocity[Z]       -1.9094e-014     1.0153e-014    -1.6792e-017    -1.6792e-017
v  ǁVelocityǁ        0.00085707          10.111          5.1377          5.1377
v  Pressure               -39.201          16.731         -11.328         -11.328
v  nu_tilda           3.6955e-007       0.0042695       0.0015461       0.0015461
v  TempC                       21          73.377          21.946          21.946
v  TurbVisc           1.5996e-014       0.0050321       0.0018162       0.0018162
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1812:        0.23540E+01

===============================================================


 INSTANT    0.181300000E+04   TIME STEP NUMBER            1813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21839E-02 0.89752E+00
   Friction velocity        uk    :  0.21839E-02 0.89752E+00
   Dimensionless distance   yplus :  0.17582E-01 0.72257E+01
   Friction thermal sca.    tstar : -0.65368E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13118E-01 0.53911E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96802E-02      33   0.31618E-03   0.48748E+01 0.17633E+03 
c  Velocity[X]                                      0.18260E+01 
c  Velocity[Y]                                      0.30487E+01 
c  Velocity[Z]                                      0.77267E-30 
c  Pressure     0.84820E-07     521   0.97366E-08   0.83050E-01 0.11407E+04 
c  nu_tilda     0.67417E-05      32   0.44578E-05   0.48736E-06 0.18725E+03 
c  TempC        0.39068E+02      27   0.36812E-03   0.53458E+01 0.24064E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0947           10.11          4.5729          4.5729
v  Velocity[Y]            -2.7563          7.3119        0.059636        0.059636
v  Velocity[Z]       -2.0825e-014     9.9137e-015    -1.6829e-017    -1.6829e-017
v  ǁVelocityǁ        0.00091096           10.11          5.1376          5.1376
v  Pressure               -39.162          16.902         -11.269         -11.269
v  nu_tilda           3.7197e-007       0.0042695       0.0015466       0.0015466
v  TempC                       21          73.375          21.946          21.946
v  TurbVisc           1.6409e-014       0.0050321       0.0018167       0.0018167
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1813:        0.21850E+01

===============================================================


 INSTANT    0.181400000E+04   TIME STEP NUMBER            1814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34161E-02 0.89847E+00
   Friction velocity        uk    :  0.34161E-02 0.89847E+00
   Dimensionless distance   yplus :  0.27502E-01 0.72333E+01
   Friction thermal sca.    tstar : -0.68316E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20520E-01 0.53969E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96824E-02      33   0.27778E-03   0.49239E+01 0.17662E+03 
c  Velocity[X]                                      0.18522E+01 
c  Velocity[Y]                                      0.30717E+01 
c  Velocity[Z]                                      0.10426E-29 
c  Pressure     0.12629E-06     521   0.91128E-08   0.12292E+00 0.11785E+04 
c  nu_tilda     0.67441E-05      32   0.15207E-04   0.48799E-06 0.18735E+03 
c  TempC        0.39077E+02      27   0.27126E-03   0.43984E+01 0.23126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0918          10.109          4.5729          4.5729
v  Velocity[Y]            -2.7579          7.2814        0.059938        0.059938
v  Velocity[Z]       -2.0041e-014     9.6609e-015    -1.6852e-017    -1.6852e-017
v  ǁVelocityǁ        0.00097058          10.109          5.1376          5.1376
v  Pressure               -39.149          16.702         -11.331         -11.331
v  nu_tilda           3.7443e-007       0.0042695        0.001547        0.001547
v  TempC                       21          73.372          21.946          21.946
v  TurbVisc           1.6842e-014       0.0050321       0.0018172       0.0018172
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1814:        0.21860E+01

===============================================================


 INSTANT    0.181500000E+04   TIME STEP NUMBER            1815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58270E-02 0.89787E+00
   Friction velocity        uk    :  0.58270E-02 0.89787E+00
   Dimensionless distance   yplus :  0.46911E-01 0.72285E+01
   Friction thermal sca.    tstar : -0.67113E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35001E-01 0.53933E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96846E-02      33   0.19145E-03   0.49082E+01 0.17659E+03 
c  Velocity[X]                                      0.18435E+01 
c  Velocity[Y]                                      0.30647E+01 
c  Velocity[Z]                                      0.10283E-29 
c  Pressure     0.10847E-06     552   0.95827E-08   0.10755E+00 0.15136E+04 
c  nu_tilda     0.67464E-05      32   0.44674E-05   0.48858E-06 0.18744E+03 
c  TempC        0.39085E+02      27   0.38306E-03   0.39640E+01 0.23297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0888          10.108          4.5729          4.5729
v  Velocity[Y]            -2.7594            7.31         0.06024         0.06024
v  Velocity[Z]       -2.1925e-014     9.5023e-015    -1.6885e-017    -1.6885e-017
v  ǁVelocityǁ         0.0010227          10.108          5.1375          5.1375
v  Pressure                -39.11           16.95         -11.253         -11.253
v  nu_tilda           3.7697e-007       0.0042695       0.0015475       0.0015475
v  TempC                       21          73.369          21.947          21.947
v  TurbVisc           1.7293e-014       0.0050321       0.0018177       0.0018177
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1815:        0.22430E+01

===============================================================


 INSTANT    0.181600000E+04   TIME STEP NUMBER            1816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48623E-02 0.89918E+00
   Friction velocity        uk    :  0.48623E-02 0.89918E+00
   Dimensionless distance   yplus :  0.39145E-01 0.72390E+01
   Friction thermal sca.    tstar : -0.64241E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29207E-01 0.54011E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96869E-02      33   0.31605E-03   0.48717E+01 0.17646E+03 
c  Velocity[X]                                      0.18176E+01 
c  Velocity[Y]                                      0.30541E+01 
c  Velocity[Z]                                      0.78654E-30 
c  Pressure     0.93423E-07     520   0.93465E-08   0.91014E-01 0.70435E+03 
c  nu_tilda     0.67488E-05      32   0.15200E-04   0.48921E-06 0.18754E+03 
c  TempC        0.39093E+02      27   0.33193E-03   0.63590E+01 0.29505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0859          10.107          4.5729          4.5729
v  Velocity[Y]            -2.7609          7.3196        0.060544        0.060544
v  Velocity[Z]       -2.2589e-014     9.2222e-015    -1.6912e-017    -1.6912e-017
v  ǁVelocityǁ         0.0010812          10.107          5.1375          5.1375
v  Pressure               -39.093          16.865          -11.29          -11.29
v  nu_tilda           3.7953e-007       0.0042695       0.0015479       0.0015479
v  TempC                       21          73.365          21.947          21.947
v  TurbVisc           1.7765e-014       0.0050321       0.0018183       0.0018183
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1816:        0.21830E+01

===============================================================


 INSTANT    0.181700000E+04   TIME STEP NUMBER            1817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63918E-02 0.89870E+00
   Friction velocity        uk    :  0.63918E-02 0.89870E+00
   Dimensionless distance   yplus :  0.51458E-01 0.72352E+01
   Friction thermal sca.    tstar : -0.63848E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38394E-01 0.53982E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96891E-02      33   0.27775E-03   0.49556E+01 0.17693E+03 
c  Velocity[X]                                      0.18768E+01 
c  Velocity[Y]                                      0.30788E+01 
c  Velocity[Z]                                      0.84638E-30 
c  Pressure     0.13164E-06     473   0.92211E-08   0.12891E+00 0.48944E+03 
c  nu_tilda     0.67511E-05      32   0.44569E-05   0.48981E-06 0.18764E+03 
c  TempC        0.39102E+02      27   0.33452E-03   0.51402E+01 0.24807E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0829          10.106          4.5729          4.5729
v  Velocity[Y]            -2.7629          7.2862        0.060848        0.060848
v  Velocity[Z]       -2.2027e-014     9.0059e-015    -1.6932e-017    -1.6932e-017
v  ǁVelocityǁ          0.001152          10.106          5.1374          5.1374
v  Pressure               -39.056          16.825         -11.274         -11.274
v  nu_tilda           3.8218e-007       0.0042695       0.0015484       0.0015484
v  TempC                       21          73.362          21.948          21.948
v  TurbVisc           1.8253e-014       0.0050321       0.0018188       0.0018188
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1817:        0.20770E+01

===============================================================


 INSTANT    0.181800000E+04   TIME STEP NUMBER            1818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44048E-02 0.89744E+00
   Friction velocity        uk    :  0.44048E-02 0.89744E+00
   Dimensionless distance   yplus :  0.35462E-01 0.72250E+01
   Friction thermal sca.    tstar : -0.69300E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26458E-01 0.53907E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96913E-02      33   0.25072E-03   0.49148E+01 0.17675E+03 
c  Velocity[X]                                      0.18497E+01 
c  Velocity[Y]                                      0.30651E+01 
c  Velocity[Z]                                      0.11158E-29 
c  Pressure     0.98153E-07     362   0.93073E-08   0.96956E-01 0.33784E+03 
c  nu_tilda     0.67534E-05      32   0.15206E-04   0.49044E-06 0.18774E+03 
c  TempC        0.39110E+02      27   0.30081E-03   0.48367E+01 0.25501E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0799          10.105          4.5729          4.5729
v  Velocity[Y]            -2.7648          7.3064        0.061152        0.061152
v  Velocity[Z]       -2.2272e-014     8.7745e-015    -1.6957e-017    -1.6957e-017
v  ǁVelocityǁ          0.001227          10.106          5.1374          5.1374
v  Pressure               -39.041          16.893         -11.279         -11.279
v  nu_tilda           3.8503e-007       0.0042695       0.0015488       0.0015488
v  TempC                       21          73.357          21.948          21.948
v  TurbVisc           1.8768e-014       0.0050321       0.0018193       0.0018193
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1818:        0.18200E+01

===============================================================


 INSTANT    0.181900000E+04   TIME STEP NUMBER            1819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74462E-02 0.89832E+00
   Friction velocity        uk    :  0.74462E-02 0.89832E+00
   Dimensionless distance   yplus :  0.59947E-01 0.72321E+01
   Friction thermal sca.    tstar : -0.65123E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44727E-01 0.53959E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96936E-02      33   0.32121E-03   0.48891E+01 0.17671E+03 
c  Velocity[X]                                      0.18318E+01 
c  Velocity[Y]                                      0.30573E+01 
c  Velocity[Z]                                      0.78713E-30 
c  Pressure     0.10202E-06     458   0.94626E-08   0.10190E+00 0.47575E+03 
c  nu_tilda     0.67558E-05      32   0.44530E-05   0.49103E-06 0.18784E+03 
c  TempC        0.39118E+02      27   0.29360E-03   0.39408E+01 0.24370E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0769          10.104          4.5729          4.5729
v  Velocity[Y]            -2.7665          7.2868        0.061458        0.061458
v  Velocity[Z]       -2.2425e-014     8.5952e-015    -1.6982e-017    -1.6982e-017
v  ǁVelocityǁ         0.0012474          10.105          5.1373          5.1373
v  Pressure               -39.004          16.856         -11.264         -11.264
v  nu_tilda           3.8794e-007       0.0042695       0.0015493       0.0015493
v  TempC                       21          73.353          21.948          21.948
v  TurbVisc           1.9336e-014       0.0050321       0.0018199       0.0018199
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1819:        0.20550E+01

===============================================================


 INSTANT    0.182000000E+04   TIME STEP NUMBER            1820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17132E-02 0.89728E+00
   Friction velocity        uk    :  0.17132E-02 0.89728E+00
   Dimensionless distance   yplus :  0.13792E-01 0.72237E+01
   Friction thermal sca.    tstar : -0.64936E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10291E-01 0.53897E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96958E-02      33   0.24055E-03   0.49173E+01 0.17690E+03 
c  Velocity[X]                                      0.18396E+01 
c  Velocity[Y]                                      0.30777E+01 
c  Velocity[Z]                                      0.86026E-30 
c  Pressure     0.11685E-06     456   0.97911E-08   0.11292E+00 0.37760E+03 
c  nu_tilda     0.67581E-05      32   0.15194E-04   0.49165E-06 0.18793E+03 
c  TempC        0.39127E+02      27   0.37970E-03   0.53785E+01 0.24419E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.074          10.104          4.5729          4.5729
v  Velocity[Y]             -2.768           7.304        0.061764        0.061764
v  Velocity[Z]        -2.311e-014     8.4046e-015    -1.7005e-017    -1.7005e-017
v  ǁVelocityǁ         0.0013051          10.104          5.1373          5.1373
v  Pressure               -38.988          16.856         -11.283         -11.283
v  nu_tilda           3.9101e-007       0.0042695       0.0015497       0.0015497
v  TempC                       21          73.349          21.949          21.949
v  TurbVisc           1.9926e-014       0.0050321       0.0018204       0.0018204
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1820:        0.20400E+01

===============================================================


 INSTANT    0.182100000E+04   TIME STEP NUMBER            1821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63895E-02 0.89878E+00
   Friction velocity        uk    :  0.63895E-02 0.89878E+00
   Dimensionless distance   yplus :  0.51440E-01 0.72358E+01
   Friction thermal sca.    tstar : -0.64572E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38380E-01 0.53987E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96980E-02      33   0.27447E-03   0.48987E+01 0.17688E+03 
c  Velocity[X]                                      0.18308E+01 
c  Velocity[Y]                                      0.30679E+01 
c  Velocity[Z]                                      0.93233E-30 
c  Pressure     0.94555E-07     520   0.94997E-08   0.92700E-01 0.96545E+03 
c  nu_tilda     0.67605E-05      32   0.44497E-05   0.49225E-06 0.18803E+03 
c  TempC        0.39135E+02      27   0.26808E-03   0.66853E+01 0.27699E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0711          10.103          4.5729          4.5729
v  Velocity[Y]            -2.7695          7.3151        0.062071        0.062071
v  Velocity[Z]       -2.3641e-014     8.1719e-015    -1.7029e-017    -1.7029e-017
v  ǁVelocityǁ         0.0013857          10.103          5.1372          5.1372
v  Pressure               -38.947          16.977         -11.231         -11.231
v  nu_tilda            3.941e-007       0.0042695       0.0015502       0.0015502
v  TempC                       21          73.344          21.949          21.949
v  TurbVisc           2.0565e-014       0.0050321       0.0018209       0.0018209
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1821:        0.21760E+01

===============================================================


 INSTANT    0.182200000E+04   TIME STEP NUMBER            1822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60652E-02 0.89843E+00
   Friction velocity        uk    :  0.60652E-02 0.89843E+00
   Dimensionless distance   yplus :  0.48829E-01 0.72330E+01
   Friction thermal sca.    tstar : -0.67638E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36432E-01 0.53966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97002E-02      33   0.29665E-03   0.49218E+01 0.17702E+03 
c  Velocity[X]                                      0.18602E+01 
c  Velocity[Y]                                      0.30616E+01 
c  Velocity[Z]                                      0.95787E-30 
c  Pressure     0.10258E-06     536   0.94308E-08   0.10188E+00 0.11698E+04 
c  nu_tilda     0.67628E-05      32   0.15195E-04   0.49288E-06 0.18813E+03 
c  TempC        0.39143E+02      27   0.32243E-03   0.40649E+01 0.24007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0681          10.102          4.5729          4.5729
v  Velocity[Y]             -2.771           7.287        0.062378        0.062378
v  Velocity[Z]       -2.2715e-014      8.028e-015     -1.704e-017     -1.704e-017
v  ǁVelocityǁ         0.0014402          10.102          5.1372          5.1372
v  Pressure               -38.933          16.781         -11.293         -11.293
v  nu_tilda           3.9717e-007       0.0042695       0.0015506       0.0015506
v  TempC                       21          73.339           21.95           21.95
v  TurbVisc           2.1223e-014       0.0050321       0.0018215       0.0018215
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1822:        0.22070E+01

===============================================================


 INSTANT    0.182300000E+04   TIME STEP NUMBER            1823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28728E-02 0.89705E+00
   Friction velocity        uk    :  0.28728E-02 0.89705E+00
   Dimensionless distance   yplus :  0.23128E-01 0.72219E+01
   Friction thermal sca.    tstar : -0.66507E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17256E-01 0.53883E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97024E-02      33   0.26977E-03   0.49297E+01 0.17711E+03 
c  Velocity[X]                                      0.18420E+01 
c  Velocity[Y]                                      0.30877E+01 
c  Velocity[Z]                                      0.10657E-29 
c  Pressure     0.10754E-06     520   0.92228E-08   0.10562E+00 0.14091E+04 
c  nu_tilda     0.67652E-05      32   0.44372E-05   0.49347E-06 0.18823E+03 
c  TempC        0.39152E+02      27   0.30459E-03   0.44903E+01 0.24434E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0653          10.101          4.5729          4.5729
v  Velocity[Y]            -2.7729          7.3022        0.062685        0.062685
v  Velocity[Z]       -2.3189e-014     7.8434e-015    -1.7065e-017    -1.7065e-017
v  ǁVelocityǁ         0.0014876          10.101          5.1372          5.1372
v  Pressure               -38.895              17         -11.219         -11.219
v  nu_tilda           4.0029e-007       0.0042695       0.0015511       0.0015511
v  TempC                       21          73.333           21.95           21.95
v  TurbVisc           2.1892e-014       0.0050321        0.001822        0.001822
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1823:        0.21820E+01

===============================================================


 INSTANT    0.182400000E+04   TIME STEP NUMBER            1824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50109E-02 0.89804E+00
   Friction velocity        uk    :  0.50109E-02 0.89804E+00
   Dimensionless distance   yplus :  0.40341E-01 0.72298E+01
   Friction thermal sca.    tstar : -0.63916E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30099E-01 0.53943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97047E-02      33   0.29565E-03   0.49127E+01 0.17707E+03 
c  Velocity[X]                                      0.18410E+01 
c  Velocity[Y]                                      0.30717E+01 
c  Velocity[Z]                                      0.89119E-30 
c  Pressure     0.89509E-07     522   0.93022E-08   0.88197E-01 0.11896E+04 
c  nu_tilda     0.67675E-05      32   0.15190E-04   0.49411E-06 0.18833E+03 
c  TempC        0.39160E+02      27   0.34708E-03   0.46066E+01 0.24569E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0624            10.1          4.5729          4.5729
v  Velocity[Y]            -2.7748          7.2785        0.062994        0.062994
v  Velocity[Z]       -2.2973e-014     7.6747e-015    -1.7079e-017    -1.7079e-017
v  ǁVelocityǁ         0.0014081            10.1          5.1371          5.1371
v  Pressure                -38.88          16.804         -11.282         -11.282
v  nu_tilda           4.0353e-007       0.0042695       0.0015515       0.0015515
v  TempC                       21          73.328           21.95           21.95
v  TurbVisc           2.2588e-014       0.0050321       0.0018225       0.0018225
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1824:        0.21810E+01

===============================================================


 INSTANT    0.182500000E+04   TIME STEP NUMBER            1825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15155E-02 0.89735E+00
   Friction velocity        uk    :  0.15155E-02 0.89735E+00
   Dimensionless distance   yplus :  0.12201E-01 0.72243E+01
   Friction thermal sca.    tstar : -0.68578E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91032E-02 0.53901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97069E-02      33   0.26891E-03   0.49283E+01 0.17721E+03 
c  Velocity[X]                                      0.18624E+01 
c  Velocity[Y]                                      0.30659E+01 
c  Velocity[Z]                                      0.85060E-30 
c  Pressure     0.10761E-06     554   0.99710E-08   0.10573E+00 0.12209E+04 
c  nu_tilda     0.67699E-05      32   0.44411E-05   0.49469E-06 0.18842E+03 
c  TempC        0.39168E+02      27   0.31659E-03   0.59117E+01 0.27428E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0593          10.099          4.5729          4.5729
v  Velocity[Y]            -2.7764          7.3081        0.063303        0.063303
v  Velocity[Z]       -2.3989e-014     7.5012e-015    -1.7104e-017    -1.7104e-017
v  ǁVelocityǁ        0.00028548          10.099          5.1371          5.1371
v  Pressure               -38.841          16.995         -11.219         -11.219
v  nu_tilda           4.0682e-007       0.0042695        0.001552        0.001552
v  TempC                       21          73.323          21.951          21.951
v  TurbVisc           2.3328e-014       0.0050321        0.001823        0.001823
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1825:        0.22770E+01

===============================================================


 INSTANT    0.182600000E+04   TIME STEP NUMBER            1826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39847E-02 0.89874E+00
   Friction velocity        uk    :  0.39847E-02 0.89874E+00
   Dimensionless distance   yplus :  0.32080E-01 0.72354E+01
   Friction thermal sca.    tstar : -0.83222E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23935E-01 0.53985E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97091E-02      33   0.27263E-03   0.49370E+01 0.17734E+03 
c  Velocity[X]                                      0.18497E+01 
c  Velocity[Y]                                      0.30873E+01 
c  Velocity[Z]                                      0.88595E-30 
c  Pressure     0.11865E-06     520   0.97890E-08   0.11446E+00 0.68074E+03 
c  nu_tilda     0.67722E-05      32   0.15180E-04   0.49532E-06 0.18852E+03 
c  TempC        0.39177E+02      27   0.37439E-03   0.51413E+01 0.26132E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0563          10.098          4.5729          4.5729
v  Velocity[Y]             -2.778          7.3096        0.063613        0.063613
v  Velocity[Z]       -2.3954e-014     7.3112e-015    -1.7125e-017    -1.7125e-017
v  ǁVelocityǁ         0.0013664          10.098           5.137           5.137
v  Pressure               -38.823          16.907         -11.253         -11.253
v  nu_tilda           4.1009e-007       0.0042695       0.0015524       0.0015524
v  TempC                       21          73.317          21.951          21.951
v  TurbVisc           2.4097e-014       0.0050321       0.0018236       0.0018236
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1826:        0.21870E+01

===============================================================


 INSTANT    0.182700000E+04   TIME STEP NUMBER            1827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67637E-02 0.89861E+00
   Friction velocity        uk    :  0.67637E-02 0.89861E+00
   Dimensionless distance   yplus :  0.54452E-01 0.72344E+01
   Friction thermal sca.    tstar : -0.11040E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40627E-01 0.53977E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97114E-02      33   0.24610E-03   0.49262E+01 0.17728E+03 
c  Velocity[X]                                      0.18470E+01 
c  Velocity[Y]                                      0.30792E+01 
c  Velocity[Z]                                      0.96630E-30 
c  Pressure     0.11378E-06     505   0.98486E-08   0.11460E+00 0.63626E+03 
c  nu_tilda     0.67746E-05      32   0.44277E-05   0.49592E-06 0.18862E+03 
c  TempC        0.39185E+02      27   0.34797E-03   0.63258E+01 0.27649E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0533          10.097          4.5729          4.5729
v  Velocity[Y]            -2.7795          7.2833        0.063922        0.063922
v  Velocity[Z]       -2.3919e-014     7.3669e-015    -1.7136e-017    -1.7136e-017
v  ǁVelocityǁ         0.0013035          10.097           5.137           5.137
v  Pressure               -38.786          16.941         -11.222         -11.222
v  nu_tilda           4.1337e-007       0.0042695       0.0015529       0.0015529
v  TempC                       21          73.312          21.952          21.952
v  TurbVisc           2.4883e-014       0.0050321       0.0018241       0.0018241
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1827:        0.21630E+01

===============================================================


 INSTANT    0.182800000E+04   TIME STEP NUMBER            1828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31489E-02 0.89695E+00
   Friction velocity        uk    :  0.31489E-02 0.89695E+00
   Dimensionless distance   yplus :  0.25350E-01 0.72211E+01
   Friction thermal sca.    tstar : -0.23979E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18914E-01 0.53877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97136E-02      33   0.31134E-03   0.48986E+01 0.17720E+03 
c  Velocity[X]                                      0.18295E+01 
c  Velocity[Y]                                      0.30691E+01 
c  Velocity[Z]                                      0.77899E-30 
c  Pressure     0.90011E-07     506   0.97679E-08   0.88157E-01 0.40846E+03 
c  nu_tilda     0.67769E-05      32   0.15184E-04   0.49655E-06 0.18872E+03 
c  TempC        0.39193E+02      27   0.26475E-03   0.61525E+01 0.26115E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0504          10.096          4.5729          4.5729
v  Velocity[Y]            -2.7808          7.3037        0.064233        0.064233
v  Velocity[Z]       -2.3852e-014     7.0373e-015     -1.715e-017     -1.715e-017
v  ǁVelocityǁ         0.0011191          10.096          5.1369          5.1369
v  Pressure               -38.769          16.932         -11.243         -11.243
v  nu_tilda           4.1681e-007       0.0042695       0.0015533       0.0015533
v  TempC                       21          73.306          21.952          21.952
v  TurbVisc           2.5688e-014       0.0050321       0.0018246       0.0018246
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1828:        0.21530E+01

===============================================================


 INSTANT    0.182900000E+04   TIME STEP NUMBER            1829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54992E-02 0.89804E+00
   Friction velocity        uk    :  0.54992E-02 0.89804E+00
   Dimensionless distance   yplus :  0.44273E-01 0.72298E+01
   Friction thermal sca.    tstar : -0.14775E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33032E-01 0.53943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97158E-02      33   0.29685E-03   0.49656E+01 0.17758E+03 
c  Velocity[X]                                      0.18718E+01 
c  Velocity[Y]                                      0.30938E+01 
c  Velocity[Z]                                      0.91258E-30 
c  Pressure     0.14054E-06     457   0.97910E-08   0.13662E+00 0.49387E+03 
c  nu_tilda     0.67792E-05      32   0.44111E-05   0.49715E-06 0.18881E+03 
c  TempC        0.39202E+02      27   0.38850E-03   0.48459E+01 0.23454E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0476          10.095          4.5729          4.5729
v  Velocity[Y]            -2.7828           7.276        0.064545        0.064545
v  Velocity[Z]       -2.4217e-014     7.3091e-015    -1.7164e-017    -1.7164e-017
v  ǁVelocityǁ        0.00096388          10.095          5.1369          5.1369
v  Pressure               -38.733          16.905         -11.225         -11.225
v  nu_tilda           4.2017e-007       0.0042695       0.0015538       0.0015538
v  TempC                       21            73.3          21.952          21.952
v  TurbVisc           2.6554e-014       0.0050321       0.0018251       0.0018251
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1829:        0.20320E+01

===============================================================


 INSTANT    0.183000000E+04   TIME STEP NUMBER            1830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52644E-02 0.89743E+00
   Friction velocity        uk    :  0.52644E-02 0.89743E+00
   Dimensionless distance   yplus :  0.42382E-01 0.72249E+01
   Friction thermal sca.    tstar : -0.96688E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31622E-01 0.53906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97180E-02      33   0.20001E-03   0.49366E+01 0.17749E+03 
c  Velocity[X]                                      0.18577E+01 
c  Velocity[Y]                                      0.30790E+01 
c  Velocity[Z]                                      0.88193E-30 
c  Pressure     0.99448E-07     277   0.93620E-08   0.98263E-01 0.37725E+03 
c  nu_tilda     0.67816E-05      32   0.15179E-04   0.49778E-06 0.18891E+03 
c  TempC        0.39210E+02      27   0.28300E-03   0.70003E+01 0.30334E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0447          10.094          4.5729          4.5729
v  Velocity[Y]            -2.7846          7.3015        0.064856        0.064856
v  Velocity[Z]       -2.4635e-014     6.8696e-015    -1.7182e-017    -1.7182e-017
v  ǁVelocityǁ        0.00084635          10.094          5.1369          5.1369
v  Pressure               -38.715          16.989         -11.225         -11.225
v  nu_tilda            4.236e-007       0.0042695       0.0015542       0.0015542
v  TempC                       21          73.294          21.953          21.953
v  TurbVisc           2.7421e-014       0.0050321       0.0018257       0.0018257
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1830:        0.16180E+01

===============================================================


 INSTANT    0.183100000E+04   TIME STEP NUMBER            1831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69803E-02 0.89883E+00
   Friction velocity        uk    :  0.69803E-02 0.89883E+00
   Dimensionless distance   yplus :  0.56196E-01 0.72362E+01
   Friction thermal sca.    tstar : -0.77094E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41928E-01 0.53990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97202E-02      33   0.31051E-03   0.48848E+01 0.17731E+03 
c  Velocity[X]                                      0.18131E+01 
c  Velocity[Y]                                      0.30717E+01 
c  Velocity[Z]                                      0.70924E-30 
c  Pressure     0.90487E-07     506   0.96965E-08   0.89124E-01 0.68482E+03 
c  nu_tilda     0.67839E-05      32   0.44046E-05   0.49837E-06 0.18901E+03 
c  TempC        0.39218E+02      27   0.41156E-03   0.40210E+01 0.23417E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0416          10.093          4.5729          4.5729
v  Velocity[Y]            -2.7862          7.3145        0.065169        0.065169
v  Velocity[Z]       -2.5168e-014     6.6394e-015    -1.7199e-017    -1.7199e-017
v  ǁVelocityǁ        0.00071881          10.093          5.1368          5.1368
v  Pressure               -38.675          17.036          -11.19          -11.19
v  nu_tilda           4.2713e-007       0.0042695       0.0015547       0.0015547
v  TempC                       21          73.288          21.953          21.953
v  TurbVisc           2.8327e-014       0.0050321       0.0018262       0.0018262
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1831:        0.21470E+01

===============================================================


 INSTANT    0.183200000E+04   TIME STEP NUMBER            1832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54915E-02 0.89842E+00
   Friction velocity        uk    :  0.54915E-02 0.89842E+00
   Dimensionless distance   yplus :  0.44211E-01 0.72329E+01
   Friction thermal sca.    tstar : -0.64784E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32986E-01 0.53965E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97225E-02      33   0.30063E-03   0.49499E+01 0.17764E+03 
c  Velocity[X]                                      0.18569E+01 
c  Velocity[Y]                                      0.30930E+01 
c  Velocity[Z]                                      0.11368E-29 
c  Pressure     0.12114E-06     536   0.91057E-08   0.11887E+00 0.10711E+04 
c  nu_tilda     0.67863E-05      32   0.15172E-04   0.49901E-06 0.18911E+03 
c  TempC        0.39227E+02      27   0.34137E-03   0.66100E+01 0.28483E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0387          10.092          4.5729          4.5729
v  Velocity[Y]            -2.7878          7.2793        0.065483        0.065483
v  Velocity[Z]       -2.4977e-014     6.5968e-015    -1.7202e-017    -1.7202e-017
v  ǁVelocityǁ        0.00058062          10.092          5.1368          5.1368
v  Pressure               -38.658          16.863         -11.246         -11.246
v  nu_tilda           4.3066e-007       0.0042695       0.0015551       0.0015551
v  TempC                       21          73.282          21.953          21.953
v  TurbVisc           2.9281e-014       0.0050321       0.0018267       0.0018267
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1832:        0.22170E+01

===============================================================


 INSTANT    0.183300000E+04   TIME STEP NUMBER            1833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17940E-02 0.89705E+00
   Friction velocity        uk    :  0.17940E-02 0.89705E+00
   Dimensionless distance   yplus :  0.14443E-01 0.72218E+01
   Friction thermal sca.    tstar : -0.17582E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10776E-01 0.53883E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97247E-02      33   0.27515E-03   0.49573E+01 0.17774E+03 
c  Velocity[X]                                      0.18710E+01 
c  Velocity[Y]                                      0.30863E+01 
c  Velocity[Z]                                      0.86769E-30 
c  Pressure     0.11279E-06     553   0.98421E-08   0.11081E+00 0.13118E+04 
c  nu_tilda     0.67886E-05      32   0.43768E-05   0.49961E-06 0.18920E+03 
c  TempC        0.39235E+02      27   0.32439E-03   0.52730E+01 0.25496E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.036          10.091          4.5729          4.5729
v  Velocity[Y]            -2.7892          7.3018        0.065796        0.065796
v  Velocity[Z]       -2.5087e-014      7.326e-015    -1.7209e-017    -1.7209e-017
v  ǁVelocityǁ        0.00051058          10.091          5.1368          5.1368
v  Pressure                -38.62          17.061         -11.177         -11.177
v  nu_tilda           4.3413e-007       0.0042695       0.0015556       0.0015556
v  TempC                       21          73.276          21.954          21.954
v  TurbVisc           3.0262e-014       0.0050321       0.0018272       0.0018272
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1833:        0.22480E+01

===============================================================


 INSTANT    0.183400000E+04   TIME STEP NUMBER            1834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32377E-02 0.89808E+00
   Friction velocity        uk    :  0.32377E-02 0.89808E+00
   Dimensionless distance   yplus :  0.26066E-01 0.72301E+01
   Friction thermal sca.    tstar : -0.97718E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19448E-01 0.53945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97269E-02      33   0.29065E-03   0.49274E+01 0.17765E+03 
c  Velocity[X]                                      0.18518E+01 
c  Velocity[Y]                                      0.30756E+01 
c  Velocity[Z]                                      0.88384E-30 
c  Pressure     0.99731E-07     536   0.94565E-08   0.98746E-01 0.96851E+03 
c  nu_tilda     0.67910E-05      32   0.15184E-04   0.50025E-06 0.18930E+03 
c  TempC        0.39243E+02      27   0.37283E-03   0.46410E+01 0.26013E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.033           10.09          4.5729          4.5729
v  Velocity[Y]            -2.7905          7.2797        0.066111        0.066111
v  Velocity[Z]       -2.4818e-014     6.7342e-015    -1.7218e-017    -1.7218e-017
v  ǁVelocityǁ        0.00046112           10.09          5.1367          5.1367
v  Pressure               -38.604          16.914         -11.229         -11.229
v  nu_tilda           4.3769e-007       0.0042695        0.001556        0.001556
v  TempC                       21           73.27          21.954          21.954
v  TurbVisc           3.1251e-014       0.0050321       0.0018278       0.0018278
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1834:        0.22260E+01

===============================================================


 INSTANT    0.183500000E+04   TIME STEP NUMBER            1835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.19782E-02 0.89714E+00
   Friction velocity        uk    :  0.19782E-02 0.89714E+00
   Dimensionless distance   yplus :  0.15926E-01 0.72226E+01
   Friction thermal sca.    tstar : -0.66145E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11882E-01 0.53889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97291E-02      33   0.23928E-03   0.49283E+01 0.17771E+03 
c  Velocity[X]                                      0.18398E+01 
c  Velocity[Y]                                      0.30885E+01 
c  Velocity[Z]                                      0.78783E-30 
c  Pressure     0.11040E-06     522   0.99138E-08   0.10697E+00 0.91366E+03 
c  nu_tilda     0.67933E-05      32   0.43441E-05   0.50085E-06 0.18940E+03 
c  TempC        0.39252E+02      27   0.25001E-03   0.56928E+01 0.27166E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0299          10.089          4.5729          4.5729
v  Velocity[Y]            -2.7924          7.2997        0.066426        0.066426
v  Velocity[Z]       -2.5091e-014     6.4145e-015    -1.7231e-017    -1.7231e-017
v  ǁVelocityǁ        0.00052963           10.09          5.1367          5.1367
v  Pressure               -38.566          17.032         -11.181         -11.181
v  nu_tilda           4.4134e-007       0.0042695       0.0015565       0.0015565
v  TempC                       21          73.263          21.955          21.955
v  TurbVisc           3.2287e-014       0.0050321       0.0018283       0.0018283
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1835:        0.21880E+01

===============================================================


 INSTANT    0.183600000E+04   TIME STEP NUMBER            1836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.21451E-02 0.89876E+00
   Friction velocity        uk    :  0.21451E-02 0.89876E+00
   Dimensionless distance   yplus :  0.17269E-01 0.72356E+01
   Friction thermal sca.    tstar : -0.64346E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12885E-01 0.53986E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97314E-02      33   0.26013E-03   0.49167E+01 0.17769E+03 
c  Velocity[X]                                      0.18353E+01 
c  Velocity[Y]                                      0.30814E+01 
c  Velocity[Z]                                      0.80859E-30 
c  Pressure     0.96596E-07     456   0.91185E-08   0.94925E-01 0.35448E+03 
c  nu_tilda     0.67957E-05      32   0.15194E-04   0.50149E-06 0.18950E+03 
c  TempC        0.39260E+02      27   0.37131E-03   0.39518E+01 0.24204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0269          10.088          4.5729          4.5729
v  Velocity[Y]            -2.7942          7.3102        0.066741        0.066741
v  Velocity[Z]       -2.4768e-014     6.5238e-015    -1.7231e-017    -1.7231e-017
v  ǁVelocityǁ        0.00059961          10.089          5.1367          5.1367
v  Pressure               -38.546           17.04         -11.195         -11.195
v  nu_tilda           4.4318e-007       0.0042695       0.0015569       0.0015569
v  TempC                       21          73.257          21.955          21.955
v  TurbVisc           3.3378e-014       0.0050321       0.0018288       0.0018288
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1836:        0.20210E+01

===============================================================


 INSTANT    0.183700000E+04   TIME STEP NUMBER            1837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75276E-02 0.89824E+00
   Friction velocity        uk    :  0.75276E-02 0.89824E+00
   Dimensionless distance   yplus :  0.60603E-01 0.72314E+01
   Friction thermal sca.    tstar : -0.63475E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45216E-01 0.53955E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97336E-02      33   0.28602E-03   0.49273E+01 0.17776E+03 
c  Velocity[X]                                      0.18442E+01 
c  Velocity[Y]                                      0.30831E+01 
c  Velocity[Z]                                      0.98776E-30 
c  Pressure     0.10268E-06     472   0.93136E-08   0.10337E+00 0.48260E+03 
c  nu_tilda     0.67980E-05      32   0.43225E-05   0.50209E-06 0.18959E+03 
c  TempC        0.39268E+02      27   0.29871E-03   0.68722E+01 0.29867E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0238          10.088          4.5729          4.5729
v  Velocity[Y]            -2.7959          7.2843        0.067057        0.067057
v  Velocity[Z]       -2.4517e-014     7.2846e-015    -1.7234e-017    -1.7234e-017
v  ǁVelocityǁ        0.00081542          10.088          5.1366          5.1366
v  Pressure               -38.509          16.982         -11.182         -11.182
v  nu_tilda           4.4326e-007       0.0042695       0.0015574       0.0015574
v  TempC                       21           73.25          21.955          21.955
v  TurbVisc           3.3937e-014       0.0050321       0.0018294       0.0018294
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1837:        0.20980E+01

===============================================================


 INSTANT    0.183800000E+04   TIME STEP NUMBER            1838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33731E-02 0.89671E+00
   Friction velocity        uk    :  0.33731E-02 0.89671E+00
   Dimensionless distance   yplus :  0.27156E-01 0.72191E+01
   Friction thermal sca.    tstar : -0.68999E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20261E-01 0.53863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97358E-02      33   0.28651E-03   0.49349E+01 0.17784E+03 
c  Velocity[X]                                      0.18429E+01 
c  Velocity[Y]                                      0.30920E+01 
c  Velocity[Z]                                      0.94152E-30 
c  Pressure     0.10017E-06     378   0.98206E-08   0.96922E-01 0.33520E+03 
c  nu_tilda     0.68004E-05      32   0.15199E-04   0.50273E-06 0.18969E+03 
c  TempC        0.39277E+02      27   0.32653E-03   0.48327E+01 0.24373E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.021          10.087          4.5729          4.5729
v  Velocity[Y]            -2.7974          7.2966        0.067374        0.067374
v  Velocity[Z]        -2.396e-014     6.8195e-015    -1.7234e-017    -1.7234e-017
v  ǁVelocityǁ        0.00091855          10.087          5.1366          5.1366
v  Pressure                -38.49          17.036         -11.189         -11.189
v  nu_tilda           4.4327e-007       0.0042695       0.0015578       0.0015578
v  TempC                       21          73.243          21.956          21.956
v  TurbVisc           3.3963e-014       0.0050321       0.0018299       0.0018299
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1838:        0.18470E+01

===============================================================


 INSTANT    0.183900000E+04   TIME STEP NUMBER            1839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76265E-02 0.89768E+00
   Friction velocity        uk    :  0.76265E-02 0.89768E+00
   Dimensionless distance   yplus :  0.61398E-01 0.72269E+01
   Friction thermal sca.    tstar : -0.64965E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45810E-01 0.53921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97380E-02      33   0.30123E-03   0.49288E+01 0.17791E+03 
c  Velocity[X]                                      0.18430E+01 
c  Velocity[Y]                                      0.30858E+01 
c  Velocity[Z]                                      0.11941E-29 
c  Pressure     0.88002E-07     457   0.96882E-08   0.87669E-01 0.49072E+03 
c  nu_tilda     0.68027E-05      32   0.42859E-05   0.50333E-06 0.18979E+03 
c  TempC        0.39285E+02      27   0.35526E-03   0.48881E+01 0.25789E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0182          10.086          4.5729          4.5729
v  Velocity[Y]            -2.7988          7.2746        0.067691        0.067691
v  Velocity[Z]       -2.3552e-014     7.2987e-015    -1.7237e-017    -1.7237e-017
v  ǁVelocityǁ         0.0010767          10.086          5.1366          5.1366
v  Pressure               -38.455          17.009         -11.171         -11.171
v  nu_tilda           4.4327e-007       0.0042695       0.0015583       0.0015583
v  TempC                       21          73.236          21.956          21.956
v  TurbVisc           3.3967e-014       0.0050321       0.0018304       0.0018304
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1839:        0.22650E+01

===============================================================


 INSTANT    0.184000000E+04   TIME STEP NUMBER            1840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12085E-02 0.89687E+00
   Friction velocity        uk    :  0.12085E-02 0.89687E+00
   Dimensionless distance   yplus :  0.97296E-02 0.72204E+01
   Friction thermal sca.    tstar : -0.64943E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72593E-02 0.53872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97402E-02      33   0.24913E-03   0.49562E+01 0.17807E+03 
c  Velocity[X]                                      0.18706E+01 
c  Velocity[Y]                                      0.30856E+01 
c  Velocity[Z]                                      0.77458E-30 
c  Pressure     0.11570E-06     378   0.93706E-08   0.11359E+00 0.32707E+03 
c  nu_tilda     0.68050E-05      32   0.15208E-04   0.50397E-06 0.18989E+03 
c  TempC        0.39293E+02      27   0.33227E-03   0.58883E+01 0.28086E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0152          10.085          4.5729          4.5729
v  Velocity[Y]            -2.8001          7.2999        0.068008        0.068008
v  Velocity[Z]       -2.3069e-014     6.8607e-015    -1.7239e-017    -1.7239e-017
v  ǁVelocityǁ         0.0013435          10.085          5.1365          5.1365
v  Pressure               -38.435          17.058         -11.178         -11.178
v  nu_tilda           4.4322e-007       0.0042695       0.0015587       0.0015587
v  TempC                       21          73.229          21.956          21.956
v  TurbVisc           3.3966e-014       0.0050321       0.0018309       0.0018309
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1840:        0.21690E+01

===============================================================


 INSTANT    0.184100000E+04   TIME STEP NUMBER            1841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76719E-02 0.89823E+00
   Friction velocity        uk    :  0.76719E-02 0.89823E+00
   Dimensionless distance   yplus :  0.61764E-01 0.72314E+01
   Friction thermal sca.    tstar : -0.63831E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46083E-01 0.53954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97424E-02      33   0.27003E-03   0.49487E+01 0.17807E+03 
c  Velocity[X]                                      0.18467E+01 
c  Velocity[Y]                                      0.31020E+01 
c  Velocity[Z]                                      0.90157E-30 
c  Pressure     0.11598E-06     490   0.99347E-08   0.11210E+00 0.72742E+03 
c  nu_tilda     0.68074E-05      32   0.42533E-05   0.50457E-06 0.18998E+03 
c  TempC        0.39301E+02      27   0.28728E-03   0.54023E+01 0.26114E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0122          10.084          4.5729          4.5729
v  Velocity[Y]            -2.8019          7.3024        0.068327        0.068327
v  Velocity[Z]       -2.2564e-014     6.4181e-015    -1.7244e-017    -1.7244e-017
v  ǁVelocityǁ         0.0014804          10.084          5.1365          5.1365
v  Pressure               -38.396          17.121          -11.14          -11.14
v  nu_tilda           4.4316e-007       0.0042695       0.0015592       0.0015592
v  TempC                       21          73.222          21.957          21.957
v  TurbVisc           3.3949e-014       0.0050321       0.0018315       0.0018315
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1841:        0.21180E+01

===============================================================


 INSTANT    0.184200000E+04   TIME STEP NUMBER            1842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75484E-02 0.89789E+00
   Friction velocity        uk    :  0.75484E-02 0.89789E+00
   Dimensionless distance   yplus :  0.60770E-01 0.72286E+01
   Friction thermal sca.    tstar : -0.63583E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45341E-01 0.53934E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97447E-02      33   0.26052E-03   0.49410E+01 0.17807E+03 
c  Velocity[X]                                      0.18505E+01 
c  Velocity[Y]                                      0.30904E+01 
c  Velocity[Z]                                      0.76898E-30 
c  Pressure     0.10368E-06     504   0.97879E-08   0.10317E+00 0.94065E+03 
c  nu_tilda     0.68097E-05      32   0.15214E-04   0.50521E-06 0.19008E+03 
c  TempC        0.39310E+02      27   0.29654E-03   0.38906E+01 0.23667E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0093          10.083          4.5729          4.5729
v  Velocity[Y]            -2.8037          7.2737        0.068647        0.068647
v  Velocity[Z]       -2.1841e-014     6.5725e-015    -1.7244e-017    -1.7244e-017
v  ǁVelocityǁ         0.0011447          10.083          5.1365          5.1365
v  Pressure               -38.377          16.977         -11.188         -11.188
v  nu_tilda           4.4315e-007       0.0042695       0.0015596       0.0015596
v  TempC                       21          73.215          21.957          21.957
v  TurbVisc           3.3931e-014       0.0050321        0.001832        0.001832
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1842:        0.21520E+01

===============================================================


 INSTANT    0.184300000E+04   TIME STEP NUMBER            1843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53298E-02 0.89648E+00
   Friction velocity        uk    :  0.53298E-02 0.89648E+00
   Dimensionless distance   yplus :  0.42909E-01 0.72173E+01
   Friction thermal sca.    tstar : -0.64243E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32015E-01 0.53849E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97469E-02      33   0.31867E-03   0.49239E+01 0.17807E+03 
c  Velocity[X]                                      0.18346E+01 
c  Velocity[Y]                                      0.30893E+01 
c  Velocity[Z]                                      0.87157E-30 
c  Pressure     0.10073E-06     536   0.96786E-08   0.99588E-01 0.11559E+04 
c  nu_tilda     0.68121E-05      32   0.42318E-05   0.50581E-06 0.19018E+03 
c  TempC        0.39318E+02      27   0.38149E-03   0.49466E+01 0.23327E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0064          10.082          4.5729          4.5729
v  Velocity[Y]            -2.8053          7.2965        0.068965        0.068965
v  Velocity[Z]        -2.129e-014     7.3143e-015    -1.7243e-017    -1.7243e-017
v  ǁVelocityǁ         0.0018032          10.082          5.1364          5.1364
v  Pressure                -38.34          17.138         -11.127         -11.127
v  nu_tilda           4.4315e-007       0.0042695       0.0015601       0.0015601
v  TempC                       21          73.208          21.957          21.957
v  TurbVisc            3.393e-014       0.0050321       0.0018325       0.0018325
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1843:        0.22250E+01

===============================================================


 INSTANT    0.184400000E+04   TIME STEP NUMBER            1844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57625E-02 0.89761E+00
   Friction velocity        uk    :  0.57625E-02 0.89761E+00
   Dimensionless distance   yplus :  0.46392E-01 0.72264E+01
   Friction thermal sca.    tstar : -0.63306E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34614E-01 0.53917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97491E-02      33   0.28115E-03   0.49884E+01 0.17840E+03 
c  Velocity[X]                                      0.18768E+01 
c  Velocity[Y]                                      0.31116E+01 
c  Velocity[Z]                                      0.10554E-29 
c  Pressure     0.12986E-06     489   0.99803E-08   0.12667E+00 0.11196E+04 
c  nu_tilda     0.68144E-05      32   0.15215E-04   0.50645E-06 0.19027E+03 
c  TempC        0.39326E+02      27   0.34544E-03   0.56962E+01 0.26149E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0036          10.081          4.5729          4.5729
v  Velocity[Y]            -2.8068          7.2681        0.069286        0.069286
v  Velocity[Z]       -2.0756e-014     6.7164e-015    -1.7244e-017    -1.7244e-017
v  ǁVelocityǁ         0.0018326          10.081          5.1364          5.1364
v  Pressure               -38.321          16.956         -11.184         -11.184
v  nu_tilda            4.432e-007       0.0042695       0.0015605       0.0015605
v  TempC                       21          73.201          21.958          21.958
v  TurbVisc            3.393e-014       0.0050321        0.001833        0.001833
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1844:        0.21210E+01

===============================================================


 INSTANT    0.184500000E+04   TIME STEP NUMBER            1845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.26654E-02 0.89718E+00
   Friction velocity        uk    :  0.26654E-02 0.89718E+00
   Dimensionless distance   yplus :  0.21459E-01 0.72229E+01
   Friction thermal sca.    tstar : -0.65210E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16010E-01 0.53891E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97513E-02      33   0.19100E-03   0.49447E+01 0.17825E+03 
c  Velocity[X]                                      0.18486E+01 
c  Velocity[Y]                                      0.30961E+01 
c  Velocity[Z]                                      0.76278E-30 
c  Pressure     0.94138E-07     521   0.94873E-08   0.92150E-01 0.11904E+04 
c  nu_tilda     0.68168E-05      32   0.41946E-05   0.50706E-06 0.19037E+03 
c  TempC        0.39335E+02      27   0.32177E-03   0.45592E+01 0.24654E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0005           10.08          4.5729          4.5729
v  Velocity[Y]            -2.8082          7.2957        0.069606        0.069606
v  Velocity[Z]       -2.0368e-014     6.3966e-015    -1.7247e-017    -1.7247e-017
v  ǁVelocityǁ         0.0019492           10.08          5.1364          5.1364
v  Pressure               -38.284          17.143         -11.123         -11.123
v  nu_tilda            4.432e-007       0.0042695        0.001561        0.001561
v  TempC                       21          73.193          21.958          21.958
v  TurbVisc           3.3946e-014       0.0050321       0.0018336       0.0018336
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1845:        0.22020E+01

===============================================================


 INSTANT    0.184600000E+04   TIME STEP NUMBER            1846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58165E-02 0.89852E+00
   Friction velocity        uk    :  0.58165E-02 0.89852E+00
   Dimensionless distance   yplus :  0.46826E-01 0.72337E+01
   Friction thermal sca.    tstar : -0.73347E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34938E-01 0.53971E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97535E-02      33   0.31542E-03   0.48963E+01 0.17807E+03 
c  Velocity[X]                                      0.18100E+01 
c  Velocity[Y]                                      0.30863E+01 
c  Velocity[Z]                                      0.10863E-29 
c  Pressure     0.90343E-07     456   0.92793E-08   0.88472E-01 0.47666E+03 
c  nu_tilda     0.68191E-05      32   0.15228E-04   0.50769E-06 0.19047E+03 
c  TempC        0.39343E+02      27   0.29021E-03   0.41149E+01 0.23642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9974          10.079          4.5729          4.5729
v  Velocity[Y]            -2.8095          7.3074        0.069928        0.069928
v  Velocity[Z]       -1.9811e-014     6.5005e-015    -1.7251e-017    -1.7251e-017
v  ǁVelocityǁ         0.0019523          10.079          5.1363          5.1363
v  Pressure               -38.261          17.106         -11.144         -11.144
v  nu_tilda           4.4317e-007       0.0042695       0.0015614       0.0015614
v  TempC                       21          73.186          21.959          21.959
v  TurbVisc           3.3946e-014       0.0050321       0.0018341       0.0018341
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1846:        0.20310E+01

===============================================================


 INSTANT    0.184700000E+04   TIME STEP NUMBER            1847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95234E-02 0.89810E+00
   Friction velocity        uk    :  0.95234E-02 0.89810E+00
   Dimensionless distance   yplus :  0.76670E-01 0.72303E+01
   Friction thermal sca.    tstar : -0.87768E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57205E-01 0.53946E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97557E-02      33   0.29897E-03   0.49594E+01 0.17842E+03 
c  Velocity[X]                                      0.18446E+01 
c  Velocity[Y]                                      0.31147E+01 
c  Velocity[Z]                                      0.11094E-29 
c  Pressure     0.12333E-06     424   0.96591E-08   0.12217E+00 0.47959E+03 
c  nu_tilda     0.68215E-05      32   0.41618E-05   0.50829E-06 0.19056E+03 
c  TempC        0.39351E+02      27   0.28181E-03   0.40544E+01 0.22805E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9944          10.078          4.5729          4.5729
v  Velocity[Y]            -2.8112          7.2737        0.070249        0.070249
v  Velocity[Z]       -1.9323e-014     7.2669e-015     -1.725e-017     -1.725e-017
v  ǁVelocityǁ         0.0019246          10.078          5.1363          5.1363
v  Pressure               -38.226          17.037         -11.135         -11.135
v  nu_tilda            4.432e-007       0.0042695       0.0015618       0.0015618
v  TempC                       21           73.18          21.959          21.959
v  TurbVisc           3.3936e-014       0.0050321       0.0018346       0.0018346
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1847:        0.19600E+01

===============================================================


 INSTANT    0.184800000E+04   TIME STEP NUMBER            1848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.33638E-02 0.89676E+00
   Friction velocity        uk    :  0.33638E-02 0.89676E+00
   Dimensionless distance   yplus :  0.27081E-01 0.72196E+01
   Friction thermal sca.    tstar : -0.12215E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20205E-01 0.53866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97580E-02      33   0.28077E-03   0.49640E+01 0.17851E+03 
c  Velocity[X]                                      0.18655E+01 
c  Velocity[Y]                                      0.30985E+01 
c  Velocity[Z]                                      0.94092E-30 
c  Pressure     0.10353E-06     392   0.94331E-08   0.10148E+00 0.39545E+03 
c  nu_tilda     0.68238E-05      32   0.15231E-04   0.50894E-06 0.19066E+03 
c  TempC        0.39360E+02      27   0.37955E-03   0.50985E+01 0.25702E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9916          10.077          4.5729          4.5729
v  Velocity[Y]            -2.8129          7.2952        0.070572        0.070572
v  Velocity[Z]       -1.8774e-014     6.7933e-015    -1.7255e-017    -1.7255e-017
v  ǁVelocityǁ         0.0019012          10.077          5.1363          5.1363
v  Pressure               -38.204          17.121         -11.133         -11.133
v  nu_tilda           4.4315e-007       0.0042695       0.0015622       0.0015622
v  TempC                       21          73.172          21.959          21.959
v  TurbVisc           3.3943e-014       0.0050321       0.0018351       0.0018351
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1848:        0.18990E+01

===============================================================


 INSTANT    0.184900000E+04   TIME STEP NUMBER            1849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76576E-02 0.89777E+00
   Friction velocity        uk    :  0.76576E-02 0.89777E+00
   Dimensionless distance   yplus :  0.61649E-01 0.72276E+01
   Friction thermal sca.    tstar : -0.34100E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45997E-01 0.53926E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97602E-02      33   0.29488E-03   0.49427E+01 0.17846E+03 
c  Velocity[X]                                      0.18522E+01 
c  Velocity[Y]                                      0.30905E+01 
c  Velocity[Z]                                      0.79873E-30 
c  Pressure     0.98048E-07     440   0.98985E-08   0.96840E-01 0.46515E+03 
c  nu_tilda     0.68262E-05      32   0.41350E-05   0.50954E-06 0.19076E+03 
c  TempC        0.39368E+02      27   0.31477E-03   0.72845E+01 0.30086E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9887          10.076          4.5729          4.5729
v  Velocity[Y]            -2.8146          7.2746        0.070894        0.070894
v  Velocity[Z]        -1.833e-014     7.2842e-015    -1.7252e-017    -1.7252e-017
v  ǁVelocityǁ         0.0019181          10.076          5.1363          5.1363
v  Pressure                -38.17          17.076         -11.121         -11.121
v  nu_tilda           4.4308e-007       0.0042695       0.0015627       0.0015627
v  TempC                       21          73.166           21.96           21.96
v  TurbVisc           3.3928e-014       0.0050321       0.0018357       0.0018357
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1849:        0.20130E+01

===============================================================


 INSTANT    0.185000000E+04   TIME STEP NUMBER            1850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91518E-03 0.89687E+00
   Friction velocity        uk    :  0.91518E-03 0.89687E+00
   Dimensionless distance   yplus :  0.73679E-02 0.72204E+01
   Friction thermal sca.    tstar : -0.14268E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54972E-02 0.53872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97624E-02      33   0.22978E-03   0.49523E+01 0.17849E+03 
c  Velocity[X]                                      0.18481E+01 
c  Velocity[Y]                                      0.31042E+01 
c  Velocity[Z]                                      0.92833E-30 
c  Pressure     0.11037E-06     377   0.94920E-08   0.10725E+00 0.33029E+03 
c  nu_tilda     0.68285E-05      32   0.15237E-04   0.51019E-06 0.19085E+03 
c  TempC        0.39376E+02      27   0.38384E-03   0.49634E+01 0.24961E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9857          10.075          4.5729          4.5729
v  Velocity[Y]            -2.8161          7.2933        0.071217        0.071217
v  Velocity[Z]       -1.7925e-014     6.8274e-015    -1.7258e-017    -1.7258e-017
v  ǁVelocityǁ         0.0018799          10.075          5.1362          5.1362
v  Pressure               -38.148          17.121         -11.126         -11.126
v  nu_tilda           4.4303e-007       0.0042695       0.0015631       0.0015631
v  TempC                       21          73.159           21.96           21.96
v  TurbVisc           3.3907e-014       0.0050321       0.0018362       0.0018362
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1850:        0.19480E+01

===============================================================


 INSTANT    0.185100000E+04   TIME STEP NUMBER            1851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74511E-02 0.89845E+00
   Friction velocity        uk    :  0.74511E-02 0.89845E+00
   Dimensionless distance   yplus :  0.59986E-01 0.72331E+01
   Friction thermal sca.    tstar : -0.99406E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44756E-01 0.53967E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97646E-02      33   0.25804E-03   0.49355E+01 0.17848E+03 
c  Velocity[X]                                      0.18369E+01 
c  Velocity[Y]                                      0.30986E+01 
c  Velocity[Z]                                      0.87698E-30 
c  Pressure     0.91781E-07     521   0.92726E-08   0.90614E-01 0.77619E+03 
c  nu_tilda     0.68309E-05      32   0.41027E-05   0.51079E-06 0.19095E+03 
c  TempC        0.39384E+02      27   0.27899E-03   0.63910E+01 0.27740E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9827          10.074          4.5729          4.5729
v  Velocity[Y]            -2.8174          7.3062        0.071541        0.071541
v  Velocity[Z]       -1.7387e-014     6.3821e-015    -1.7264e-017    -1.7264e-017
v  ǁVelocityǁ          0.001955          10.074          5.1362          5.1362
v  Pressure                -38.11          17.199         -11.086         -11.086
v  nu_tilda           4.4297e-007       0.0042695       0.0015636       0.0015636
v  TempC                       21          73.151           21.96           21.96
v  TurbVisc           3.3891e-014       0.0050321       0.0018367       0.0018367
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1851:        0.23870E+01

===============================================================


 INSTANT    0.185200000E+04   TIME STEP NUMBER            1852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61687E-02 0.89805E+00
   Friction velocity        uk    :  0.61687E-02 0.89805E+00
   Dimensionless distance   yplus :  0.49662E-01 0.72299E+01
   Friction thermal sca.    tstar : -0.77674E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37053E-01 0.53943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97668E-02      33   0.28033E-03   0.49342E+01 0.17851E+03 
c  Velocity[X]                                      0.18420E+01 
c  Velocity[Y]                                      0.30921E+01 
c  Velocity[Z]                                      0.69194E-30 
c  Pressure     0.11371E-06     504   0.96725E-08   0.11325E+00 0.95279E+03 
c  nu_tilda     0.68332E-05      32   0.15242E-04   0.51143E-06 0.19105E+03 
c  TempC        0.39393E+02      27   0.38465E-03   0.42206E+01 0.23835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9799          10.073          4.5729          4.5729
v  Velocity[Y]            -2.8187          7.2781        0.071866        0.071866
v  Velocity[Z]       -1.7026e-014     6.5539e-015    -1.7262e-017    -1.7262e-017
v  ǁVelocityǁ         0.0018489          10.073          5.1362          5.1362
v  Pressure               -38.091          17.054         -11.135         -11.135
v  nu_tilda           4.4294e-007       0.0042695        0.001564        0.001564
v  TempC                       21          73.144          21.961          21.961
v  TurbVisc           3.3874e-014       0.0050321       0.0018372       0.0018372
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1852:        0.21470E+01

===============================================================


 INSTANT    0.185300000E+04   TIME STEP NUMBER            1853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30851E-02 0.89640E+00
   Friction velocity        uk    :  0.30851E-02 0.89640E+00
   Dimensionless distance   yplus :  0.24837E-01 0.72166E+01
   Friction thermal sca.    tstar : -0.65837E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18531E-01 0.53844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97690E-02      33   0.28447E-03   0.49421E+01 0.17860E+03 
c  Velocity[X]                                      0.18312E+01 
c  Velocity[Y]                                      0.31109E+01 
c  Velocity[Z]                                      0.12831E-29 
c  Pressure     0.11809E-06     520   0.96413E-08   0.11537E+00 0.11074E+04 
c  nu_tilda     0.68356E-05      32   0.40858E-05   0.51203E-06 0.19114E+03 
c  TempC        0.39401E+02      27   0.36732E-03   0.58693E+01 0.26488E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9771          10.072          4.5729          4.5729
v  Velocity[Y]            -2.8203          7.2926        0.072191        0.072191
v  Velocity[Z]       -1.6602e-014     7.2814e-015    -1.7263e-017    -1.7263e-017
v  ǁVelocityǁ         0.0019559          10.072          5.1362          5.1362
v  Pressure               -38.056          17.208         -11.077         -11.077
v  nu_tilda            4.429e-007       0.0042695       0.0015645       0.0015645
v  TempC                       21          73.137          21.961          21.961
v  TurbVisc           3.3863e-014       0.0050321       0.0018378       0.0018378
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1853:        0.21860E+01

===============================================================


 INSTANT    0.185400000E+04   TIME STEP NUMBER            1854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34314E-02 0.89746E+00
   Friction velocity        uk    :  0.34314E-02 0.89746E+00
   Dimensionless distance   yplus :  0.27625E-01 0.72251E+01
   Friction thermal sca.    tstar : -0.64083E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20611E-01 0.53908E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97712E-02      33   0.29725E-03   0.49435E+01 0.17867E+03 
c  Velocity[X]                                      0.18416E+01 
c  Velocity[Y]                                      0.31019E+01 
c  Velocity[Z]                                      0.98141E-30 
c  Pressure     0.10162E-06     505   0.97325E-08   0.10094E+00 0.89855E+03 
c  nu_tilda     0.68379E-05      32   0.15242E-04   0.51267E-06 0.19124E+03 
c  TempC        0.39409E+02      27   0.32279E-03   0.66216E+01 0.28873E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9741          10.071          4.5729          4.5729
v  Velocity[Y]             -2.822          7.2691        0.072519        0.072519
v  Velocity[Z]       -1.6213e-014      6.687e-015    -1.7264e-017    -1.7264e-017
v  ǁVelocityǁ         0.0018651          10.071          5.1361          5.1361
v  Pressure               -38.036          17.076         -11.123         -11.123
v  nu_tilda           4.4295e-007       0.0042695       0.0015649       0.0015649
v  TempC                       21          73.129          21.961          21.961
v  TurbVisc           3.3853e-014       0.0050321       0.0018383       0.0018383
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1854:        0.21590E+01

===============================================================


 INSTANT    0.185500000E+04   TIME STEP NUMBER            1855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41524E-02 0.89664E+00
   Friction velocity        uk    :  0.41524E-02 0.89664E+00
   Dimensionless distance   yplus :  0.33430E-01 0.72186E+01
   Friction thermal sca.    tstar : -0.64713E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24943E-01 0.53858E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97734E-02      33   0.29373E-03   0.49649E+01 0.17883E+03 
c  Velocity[X]                                      0.18644E+01 
c  Velocity[Y]                                      0.31005E+01 
c  Velocity[Z]                                      0.75584E-30 
c  Pressure     0.11867E-06     506   0.97250E-08   0.11627E+00 0.98495E+03 
c  nu_tilda     0.68403E-05      32   0.40524E-05   0.51328E-06 0.19134E+03 
c  TempC        0.39418E+02      27   0.36339E-03   0.48890E+01 0.26229E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.971           10.07          4.5729          4.5729
v  Velocity[Y]            -2.8237          7.2969        0.072846        0.072846
v  Velocity[Z]       -1.5861e-014     6.3721e-015    -1.7266e-017    -1.7266e-017
v  ǁVelocityǁ         0.0019688           10.07          5.1361          5.1361
v  Pressure               -38.002          17.215         -11.074         -11.074
v  nu_tilda           4.4295e-007       0.0042695       0.0015654       0.0015654
v  TempC                       21          73.122          21.962          21.962
v  TurbVisc           3.3867e-014       0.0050321       0.0018388       0.0018388
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1855:        0.21440E+01

===============================================================


 INSTANT    0.185600000E+04   TIME STEP NUMBER            1856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52398E-02 0.89790E+00
   Friction velocity        uk    :  0.52398E-02 0.89790E+00
   Dimensionless distance   yplus :  0.42184E-01 0.72287E+01
   Friction thermal sca.    tstar : -0.63577E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31474E-01 0.53934E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97757E-02      33   0.27315E-03   0.49581E+01 0.17881E+03 
c  Velocity[X]                                      0.18433E+01 
c  Velocity[Y]                                      0.31149E+01 
c  Velocity[Z]                                      0.81815E-30 
c  Pressure     0.11907E-06     456   0.94827E-08   0.11545E+00 0.49560E+03 
c  nu_tilda     0.68426E-05      32   0.15248E-04   0.51392E-06 0.19143E+03 
c  TempC        0.39426E+02      27   0.27078E-03   0.60221E+01 0.27016E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9679          10.069          4.5729          4.5729
v  Velocity[Y]            -2.8251          7.2972        0.073175        0.073175
v  Velocity[Z]       -1.5425e-014     6.4664e-015    -1.7267e-017    -1.7267e-017
v  ǁVelocityǁ         0.0019533           10.07          5.1361          5.1361
v  Pressure               -37.978          17.177         -11.095         -11.095
v  nu_tilda           4.4293e-007       0.0042695       0.0015658       0.0015658
v  TempC                       21          73.114          21.962          21.962
v  TurbVisc           3.3868e-014       0.0050321       0.0018393       0.0018393
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1856:        0.20440E+01

===============================================================


 INSTANT    0.185700000E+04   TIME STEP NUMBER            1857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82066E-02 0.89758E+00
   Friction velocity        uk    :  0.82066E-02 0.89758E+00
   Dimensionless distance   yplus :  0.66069E-01 0.72261E+01
   Friction thermal sca.    tstar : -0.63000E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49295E-01 0.53915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97779E-02      33   0.26230E-03   0.49594E+01 0.17885E+03 
c  Velocity[X]                                      0.18477E+01 
c  Velocity[Y]                                      0.31118E+01 
c  Velocity[Z]                                      0.99825E-30 
c  Pressure     0.11259E-06     440   0.93632E-08   0.11380E+00 0.46852E+03 
c  nu_tilda     0.68450E-05      33   0.40181E-05   0.51453E-06 0.19153E+03 
c  TempC        0.39434E+02      27   0.36246E-03   0.60511E+01 0.25730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9651          10.068          4.5729          4.5729
v  Velocity[Y]            -2.8265           7.271        0.073504        0.073504
v  Velocity[Z]       -1.5141e-014     7.2601e-015     -1.726e-017     -1.726e-017
v  ǁVelocityǁ         0.0019283          10.069          5.1361          5.1361
v  Pressure               -37.946          17.145          -11.08          -11.08
v  nu_tilda           4.4298e-007       0.0042695       0.0015663       0.0015663
v  TempC                       21          73.105          21.962          21.962
v  TurbVisc           3.3861e-014       0.0050321       0.0018399       0.0018399
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1857:        0.20140E+01

===============================================================


 INSTANT    0.185800000E+04   TIME STEP NUMBER            1858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34688E-02 0.89615E+00
   Friction velocity        uk    :  0.34688E-02 0.89615E+00
   Dimensionless distance   yplus :  0.27926E-01 0.72146E+01
   Friction thermal sca.    tstar : -0.64956E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20836E-01 0.53829E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97801E-02      33   0.30749E-03   0.49263E+01 0.17876E+03 
c  Velocity[X]                                      0.18263E+01 
c  Velocity[Y]                                      0.30999E+01 
c  Velocity[Z]                                      0.86828E-30 
c  Pressure     0.92153E-07     298   0.96061E-08   0.90131E-01 0.34998E+03 
c  nu_tilda     0.68473E-05      33   0.15256E-04   0.51517E-06 0.19162E+03 
c  TempC        0.39442E+02      27   0.34373E-03   0.58426E+01 0.29145E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9623          10.067          4.5729          4.5729
v  Velocity[Y]            -2.8277          7.2917        0.073835        0.073835
v  Velocity[Z]       -1.4763e-014     6.7684e-015    -1.7255e-017    -1.7255e-017
v  ǁVelocityǁ         0.0019389          10.068           5.136           5.136
v  Pressure               -37.923          17.205         -11.083         -11.083
v  nu_tilda           4.4292e-007       0.0042695       0.0015667       0.0015667
v  TempC                       21          73.096          21.963          21.963
v  TurbVisc           3.3877e-014       0.0050321       0.0018404       0.0018404
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1858:        0.16650E+01

===============================================================


 INSTANT    0.185900000E+04   TIME STEP NUMBER            1859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72347E-02 0.89719E+00
   Friction velocity        uk    :  0.72347E-02 0.89719E+00
   Dimensionless distance   yplus :  0.58244E-01 0.72230E+01
   Friction thermal sca.    tstar : -0.63491E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43456E-01 0.53892E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97823E-02      33   0.29486E-03   0.49813E+01 0.17911E+03 
c  Velocity[X]                                      0.18584E+01 
c  Velocity[Y]                                      0.31229E+01 
c  Velocity[Z]                                      0.93856E-30 
c  Pressure     0.13552E-06     330   0.97180E-08   0.13290E+00 0.47949E+03 
c  nu_tilda     0.68496E-05      33   0.40136E-05   0.51577E-06 0.19172E+03 
c  TempC        0.39451E+02      27   0.26820E-03   0.51336E+01 0.25398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9593          10.066          4.5729          4.5729
v  Velocity[Y]            -2.8292           7.265        0.074166        0.074166
v  Velocity[Z]       -1.4419e-014     7.2533e-015    -1.7253e-017    -1.7253e-017
v  ǁVelocityǁ         0.0018936          10.067           5.136           5.136
v  Pressure               -37.891           17.12         -11.081         -11.081
v  nu_tilda           4.4287e-007       0.0042695       0.0015672       0.0015672
v  TempC                       21          73.089          21.963          21.963
v  TurbVisc           3.3859e-014       0.0050321       0.0018409       0.0018409
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1859:        0.19070E+01

===============================================================


 INSTANT    0.186000000E+04   TIME STEP NUMBER            1860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.20476E-02 0.89677E+00
   Friction velocity        uk    :  0.20476E-02 0.89677E+00
   Dimensionless distance   yplus :  0.16485E-01 0.72196E+01
   Friction thermal sca.    tstar : -0.65196E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12299E-01 0.53866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97845E-02      33   0.19613E-03   0.49676E+01 0.17905E+03 
c  Velocity[X]                                      0.18574E+01 
c  Velocity[Y]                                      0.31102E+01 
c  Velocity[Z]                                      0.10744E-29 
c  Pressure     0.11005E-06     425   0.97275E-08   0.10895E+00 0.43527E+03 
c  nu_tilda     0.68520E-05      33   0.15251E-04   0.51642E-06 0.19182E+03 
c  TempC        0.39459E+02      27   0.35806E-03   0.39639E+01 0.23271E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9563          10.065          4.5729          4.5729
v  Velocity[Y]             -2.831          7.2901        0.074497        0.074497
v  Velocity[Z]       -1.4081e-014      6.799e-015    -1.7252e-017    -1.7252e-017
v  ǁVelocityǁ         0.0018958          10.066           5.136           5.136
v  Pressure               -37.869           17.22         -11.075         -11.075
v  nu_tilda           4.4284e-007       0.0042695       0.0015676       0.0015676
v  TempC                       21           73.08          21.963          21.963
v  TurbVisc           3.3844e-014       0.0050321       0.0018414       0.0018414
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1860:        0.21580E+01

===============================================================


 INSTANT    0.186100000E+04   TIME STEP NUMBER            1861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83131E-02 0.89818E+00
   Friction velocity        uk    :  0.83131E-02 0.89818E+00
   Dimensionless distance   yplus :  0.66926E-01 0.72310E+01
   Friction thermal sca.    tstar : -0.63422E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49934E-01 0.53951E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97867E-02      33   0.30259E-03   0.49102E+01 0.17884E+03 
c  Velocity[X]                                      0.18077E+01 
c  Velocity[Y]                                      0.31025E+01 
c  Velocity[Z]                                      0.67469E-30 
c  Pressure     0.10012E-06     506   0.96083E-08   0.98969E-01 0.67689E+03 
c  nu_tilda     0.68543E-05      33   0.39842E-05   0.51703E-06 0.19191E+03 
c  TempC        0.39467E+02      27   0.32818E-03   0.62882E+01 0.29027E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9533          10.065          4.5729          4.5729
v  Velocity[Y]            -2.8325          7.3045        0.074831        0.074831
v  Velocity[Z]       -1.3853e-014     6.4028e-015    -1.7249e-017    -1.7249e-017
v  ǁVelocityǁ          0.001986          10.065           5.136           5.136
v  Pressure               -37.834          17.277         -11.042         -11.042
v  nu_tilda           4.4283e-007       0.0042695       0.0015681       0.0015681
v  TempC                       21          73.072          21.964          21.964
v  TurbVisc           3.3834e-014       0.0050321        0.001842        0.001842
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1861:        0.23770E+01

===============================================================


 INSTANT    0.186200000E+04   TIME STEP NUMBER            1862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.78561E-02 0.89773E+00
   Friction velocity        uk    :  0.78561E-02 0.89773E+00
   Dimensionless distance   yplus :  0.63247E-01 0.72273E+01
   Friction thermal sca.    tstar : -0.63361E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47189E-01 0.53924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97889E-02      33   0.29512E-03   0.49699E+01 0.17916E+03 
c  Velocity[X]                                      0.18457E+01 
c  Velocity[Y]                                      0.31243E+01 
c  Velocity[Z]                                      0.10825E-29 
c  Pressure     0.12720E-06     538   0.99333E-08   0.12424E+00 0.12499E+04 
c  nu_tilda     0.68567E-05      33   0.15261E-04   0.51767E-06 0.19201E+03 
c  TempC        0.39475E+02      27   0.31731E-03   0.57170E+01 0.26288E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9505          10.064          4.5729          4.5729
v  Velocity[Y]             -2.834          7.2685        0.075165        0.075165
v  Velocity[Z]       -1.3534e-014     6.5342e-015    -1.7243e-017    -1.7243e-017
v  ǁVelocityǁ         0.0015642          10.064           5.136           5.136
v  Pressure               -37.813          17.067         -11.103         -11.103
v  nu_tilda           4.4288e-007       0.0042695       0.0015685       0.0015685
v  TempC                       21          73.063          21.964          21.964
v  TurbVisc           3.3831e-014       0.0050321       0.0018425       0.0018425
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1862:        0.24290E+01

===============================================================


 INSTANT    0.186300000E+04   TIME STEP NUMBER            1863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42656E-02 0.89646E+00
   Friction velocity        uk    :  0.42656E-02 0.89646E+00
   Dimensionless distance   yplus :  0.34341E-01 0.72171E+01
   Friction thermal sca.    tstar : -0.65247E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25622E-01 0.53848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97911E-02      33   0.27349E-03   0.49767E+01 0.17926E+03 
c  Velocity[X]                                      0.18604E+01 
c  Velocity[Y]                                      0.31162E+01 
c  Velocity[Z]                                      0.10327E-29 
c  Pressure     0.11666E-06     552   0.98539E-08   0.11554E+00 0.14837E+04 
c  nu_tilda     0.68590E-05      33   0.39643E-05   0.51827E-06 0.19210E+03 
c  TempC        0.39484E+02      27   0.31136E-03   0.48366E+01 0.25023E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9477          10.063          4.5729          4.5729
v  Velocity[Y]            -2.8353          7.2918        0.075499        0.075499
v  Velocity[Z]        -1.318e-014     7.4511e-015    -1.7236e-017    -1.7236e-017
v  ǁVelocityǁ         0.0010862          10.063          5.1359          5.1359
v  Pressure               -37.779          17.306         -11.029         -11.029
v  nu_tilda           4.4287e-007       0.0042695        0.001569        0.001569
v  TempC                       21          73.053          21.964          21.964
v  TurbVisc           3.3847e-014       0.0050321        0.001843        0.001843
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1863:        0.27350E+01

===============================================================


 INSTANT    0.186400000E+04   TIME STEP NUMBER            1864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84483E-02 0.89738E+00
   Friction velocity        uk    :  0.84483E-02 0.89738E+00
   Dimensionless distance   yplus :  0.68014E-01 0.72245E+01
   Friction thermal sca.    tstar : -0.63608E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50746E-01 0.53903E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97933E-02      33   0.29825E-03   0.49565E+01 0.17918E+03 
c  Velocity[X]                                      0.18503E+01 
c  Velocity[Y]                                      0.31062E+01 
c  Velocity[Z]                                      0.78218E-30 
c  Pressure     0.10358E-06     506   0.98381E-08   0.10325E+00 0.11603E+04 
c  nu_tilda     0.68614E-05      33   0.15261E-04   0.51892E-06 0.19220E+03 
c  TempC        0.39492E+02      27   0.29637E-03   0.60175E+01 0.27131E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9447          10.062          4.5729          4.5729
v  Velocity[Y]            -2.8365          7.2694        0.075835        0.075835
v  Velocity[Z]       -1.2872e-014      6.768e-015    -1.7235e-017    -1.7235e-017
v  ǁVelocityǁ        0.00092415          10.062          5.1359          5.1359
v  Pressure               -37.757          17.116         -11.085         -11.085
v  nu_tilda           4.4286e-007       0.0042695       0.0015693       0.0015693
v  TempC                       21          73.046          21.965          21.965
v  TurbVisc           3.3844e-014       0.0050321       0.0018435       0.0018435
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1864:        0.21730E+01

===============================================================


 INSTANT    0.186500000E+04   TIME STEP NUMBER            1865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64262E-02 0.89655E+00
   Friction velocity        uk    :  0.64262E-02 0.89655E+00
   Dimensionless distance   yplus :  0.51735E-01 0.72178E+01
   Friction thermal sca.    tstar : -0.64852E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38600E-01 0.53853E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97955E-02      33   0.24312E-03   0.49666E+01 0.17926E+03 
c  Velocity[X]                                      0.18469E+01 
c  Velocity[Y]                                      0.31197E+01 
c  Velocity[Z]                                      0.91385E-30 
c  Pressure     0.11762E-06     536   0.94809E-08   0.11348E+00 0.10887E+04 
c  nu_tilda     0.68637E-05      33   0.39571E-05   0.51953E-06 0.19229E+03 
c  TempC        0.39500E+02      27   0.34205E-03   0.58591E+01 0.25262E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9415          10.061          4.5729          4.5729
v  Velocity[Y]             -2.838          7.2892        0.076171        0.076171
v  Velocity[Z]       -1.2586e-014        6.6e-015    -1.7235e-017    -1.7235e-017
v  ǁVelocityǁ        0.00066359          10.061          5.1359          5.1359
v  Pressure               -37.724          17.283         -11.031         -11.031
v  nu_tilda            4.428e-007       0.0042695       0.0015698       0.0015698
v  TempC                       21          73.047          21.965          21.965
v  TurbVisc           3.3841e-014       0.0050321        0.001844        0.001844
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1865:        0.22460E+01

===============================================================


 INSTANT    0.186600000E+04   TIME STEP NUMBER            1866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.43068E-02 0.89808E+00
   Friction velocity        uk    :  0.43068E-02 0.89808E+00
   Dimensionless distance   yplus :  0.34673E-01 0.72301E+01
   Friction thermal sca.    tstar : -0.96591E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25870E-01 0.53945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97977E-02      33   0.25662E-03   0.49492E+01 0.17923E+03 
c  Velocity[X]                                      0.18382E+01 
c  Velocity[Y]                                      0.31111E+01 
c  Velocity[Z]                                      0.83653E-30 
c  Pressure     0.10053E-06     457   0.92164E-08   0.98849E-01 0.43834E+03 
c  nu_tilda     0.68661E-05      33   0.15261E-04   0.52018E-06 0.19239E+03 
c  TempC        0.39508E+02      27   0.29062E-03   0.48927E+01 0.25735E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9387           10.06          4.5729          4.5729
v  Velocity[Y]            -2.8397          7.2989        0.076508        0.076508
v  Velocity[Z]       -1.2345e-014     6.6517e-015    -1.7227e-017    -1.7227e-017
v  ǁVelocityǁ        0.00059341           10.06          5.1359          5.1359
v  Pressure               -37.699           17.26         -11.048         -11.048
v  nu_tilda           4.4273e-007       0.0042695       0.0015702       0.0015702
v  TempC                       21          73.046          21.965          21.965
v  TurbVisc           3.3821e-014       0.0050321       0.0018446       0.0018446
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1866:        0.20460E+01

===============================================================


 INSTANT    0.186700000E+04   TIME STEP NUMBER            1867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60348E-02 0.89762E+00
   Friction velocity        uk    :  0.60348E-02 0.89762E+00
   Dimensionless distance   yplus :  0.48584E-01 0.72264E+01
   Friction thermal sca.    tstar : -0.69080E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36249E-01 0.53917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97999E-02      33   0.28023E-03   0.49518E+01 0.17928E+03 
c  Velocity[X]                                      0.18392E+01 
c  Velocity[Y]                                      0.31126E+01 
c  Velocity[Z]                                      0.11406E-29 
c  Pressure     0.11408E-06     440   0.93363E-08   0.11464E+00 0.45396E+03 
c  nu_tilda     0.68684E-05      33   0.39432E-05   0.52078E-06 0.19249E+03 
c  TempC        0.39517E+02      27   0.33882E-03   0.44745E+01 0.24795E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9358          10.059          4.5729          4.5729
v  Velocity[Y]            -2.8412          7.2718        0.076846        0.076846
v  Velocity[Z]       -1.2049e-014     7.4711e-015    -1.7216e-017    -1.7216e-017
v  ǁVelocityǁ         0.0014251          10.059          5.1359          5.1359
v  Pressure               -37.668          17.229         -11.034         -11.034
v  nu_tilda           4.4269e-007       0.0042695       0.0015707       0.0015707
v  TempC                       21          73.047          21.966          21.966
v  TurbVisc           3.3801e-014       0.0050321       0.0018451       0.0018451
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1867:        0.20090E+01

===============================================================


 INSTANT    0.186800000E+04   TIME STEP NUMBER            1868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.37383E-02 0.89604E+00
   Friction velocity        uk    :  0.37383E-02 0.89604E+00
   Dimensionless distance   yplus :  0.30096E-01 0.72137E+01
   Friction thermal sca.    tstar : -0.77523E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22455E-01 0.53823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98021E-02      33   0.30321E-03   0.49613E+01 0.17936E+03 
c  Velocity[X]                                      0.18391E+01 
c  Velocity[Y]                                      0.31222E+01 
c  Velocity[Z]                                      0.85879E-30 
c  Pressure     0.10683E-06     440   0.91215E-08   0.10339E+00 0.35936E+03 
c  nu_tilda     0.68708E-05      33   0.15266E-04   0.52143E-06 0.19258E+03 
c  TempC        0.39525E+02      27   0.33028E-03   0.49074E+01 0.25135E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9329          10.058          4.5729          4.5729
v  Velocity[Y]            -2.8427          7.2851        0.077185        0.077185
v  Velocity[Z]       -1.1744e-014      6.946e-015    -1.7209e-017    -1.7209e-017
v  ǁVelocityǁ         0.0014718          10.058          5.1359          5.1359
v  Pressure               -37.644          17.249         -11.044         -11.044
v  nu_tilda           4.4262e-007       0.0042695       0.0015711       0.0015711
v  TempC                       21          73.047          21.966          21.966
v  TurbVisc           3.3789e-014       0.0050321       0.0018456       0.0018456
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1868:        0.20230E+01

===============================================================


 INSTANT    0.186900000E+04   TIME STEP NUMBER            1869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91535E-02 0.89722E+00
   Friction velocity        uk    :  0.91535E-02 0.89722E+00
   Dimensionless distance   yplus :  0.73692E-01 0.72232E+01
   Friction thermal sca.    tstar : -0.87649E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54983E-01 0.53893E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98043E-02      33   0.26698E-03   0.49765E+01 0.17952E+03 
c  Velocity[X]                                      0.18619E+01 
c  Velocity[Y]                                      0.31145E+01 
c  Velocity[Z]                                      0.92888E-30 
c  Pressure     0.11519E-06     424   0.92208E-08   0.11466E+00 0.43810E+03 
c  nu_tilda     0.68731E-05      33   0.39306E-05   0.52202E-06 0.19267E+03 
c  TempC        0.39533E+02      27   0.23321E-03   0.46716E+01 0.23593E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.93          10.057          4.5729          4.5729
v  Velocity[Y]             -2.844           7.266        0.077524        0.077524
v  Velocity[Z]        -1.178e-014     6.4048e-015    -1.7207e-017    -1.7207e-017
v  ǁVelocityǁ         0.0016975          10.057          5.1358          5.1358
v  Pressure               -37.613          17.208         -11.033         -11.033
v  nu_tilda            4.426e-007       0.0042695       0.0015716       0.0015716
v  TempC                       21          73.047          21.966          21.966
v  TurbVisc           3.3767e-014       0.0050321       0.0018461       0.0018461
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1869:        0.22350E+01

===============================================================


 INSTANT    0.187000000E+04   TIME STEP NUMBER            1870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38165E-02 0.89647E+00
   Friction velocity        uk    :  0.38165E-02 0.89647E+00
   Dimensionless distance   yplus :  0.30726E-01 0.72172E+01
   Friction thermal sca.    tstar : -0.11632E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22925E-01 0.53849E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98065E-02      33   0.22547E-03   0.49451E+01 0.17938E+03 
c  Velocity[X]                                      0.18359E+01 
c  Velocity[Y]                                      0.31092E+01 
c  Velocity[Z]                                      0.75521E-30 
c  Pressure     0.10038E-06     426   0.99347E-08   0.98396E-01 0.44589E+03 
c  nu_tilda     0.68755E-05      33   0.15261E-04   0.52267E-06 0.19277E+03 
c  TempC        0.39541E+02      27   0.43076E-03   0.38235E+01 0.22741E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.927          10.056          4.5729          4.5729
v  Velocity[Y]            -2.8452          7.2911        0.077864        0.077864
v  Velocity[Z]       -1.1574e-014     6.6358e-015    -1.7203e-017    -1.7203e-017
v  ǁVelocityǁ         0.0014044          10.056          5.1358          5.1358
v  Pressure               -37.588          17.307         -11.026         -11.026
v  nu_tilda           4.4259e-007       0.0042695        0.001572        0.001572
v  TempC                       21          73.047          21.967          21.967
v  TurbVisc           3.3761e-014       0.0050321       0.0018467       0.0018467
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1870:        0.21300E+01

===============================================================


 INSTANT    0.187100000E+04   TIME STEP NUMBER            1871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34317E-02 0.89773E+00
   Friction velocity        uk    :  0.34317E-02 0.89773E+00
   Dimensionless distance   yplus :  0.27628E-01 0.72274E+01
   Friction thermal sca.    tstar : -0.23172E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20613E-01 0.53924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98087E-02      33   0.29618E-03   0.49348E+01 0.17942E+03 
c  Velocity[X]                                      0.18111E+01 
c  Velocity[Y]                                      0.31236E+01 
c  Velocity[Z]                                      0.88166E-30 
c  Pressure     0.10536E-06     488   0.95393E-08   0.10257E+00 0.56308E+03 
c  nu_tilda     0.68778E-05      33   0.39297E-05   0.52328E-06 0.19287E+03 
c  TempC        0.39550E+02      27   0.36891E-03   0.67170E+01 0.30401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9241          10.055          4.5729          4.5729
v  Velocity[Y]            -2.8465          7.2953        0.078206        0.078206
v  Velocity[Z]       -1.2156e-014      6.965e-015    -1.7189e-017    -1.7189e-017
v  ǁVelocityǁ         0.0020038          10.055          5.1358          5.1358
v  Pressure               -37.554           17.33             -11             -11
v  nu_tilda           4.4257e-007       0.0042695       0.0015725       0.0015725
v  TempC                       21          73.047          21.967          21.967
v  TurbVisc           3.3757e-014       0.0050321       0.0018472       0.0018472
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1871:        0.21160E+01

===============================================================


 INSTANT    0.187200000E+04   TIME STEP NUMBER            1872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90046E-02 0.89740E+00
   Friction velocity        uk    :  0.90046E-02 0.89740E+00
   Dimensionless distance   yplus :  0.72493E-01 0.72247E+01
   Friction thermal sca.    tstar : -0.16660E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54088E-01 0.53904E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98109E-02      33   0.25349E-03   0.49869E+01 0.17966E+03 
c  Velocity[X]                                      0.18687E+01 
c  Velocity[Y]                                      0.31183E+01 
c  Velocity[Z]                                      0.77446E-30 
c  Pressure     0.11241E-06     504   0.91314E-08   0.11176E+00 0.10098E+04 
c  nu_tilda     0.68802E-05      33   0.15264E-04   0.52393E-06 0.19296E+03 
c  TempC        0.39558E+02      27   0.33834E-03   0.66676E+01 0.28444E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9212          10.054          4.5729          4.5729
v  Velocity[Y]            -2.8482          7.2664        0.078548        0.078548
v  Velocity[Z]       -1.1756e-014     6.5064e-015    -1.7181e-017    -1.7181e-017
v  ǁVelocityǁ         0.0018428          10.054          5.1358          5.1358
v  Pressure               -37.531           17.17         -11.049         -11.049
v  nu_tilda           4.4262e-007       0.0042695       0.0015729       0.0015729
v  TempC                       21          73.046          21.967          21.967
v  TurbVisc           3.3751e-014       0.0050321       0.0018477       0.0018477
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1872:        0.21500E+01

===============================================================


 INSTANT    0.187300000E+04   TIME STEP NUMBER            1873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61428E-02 0.89594E+00
   Friction velocity        uk    :  0.61428E-02 0.89594E+00
   Dimensionless distance   yplus :  0.49453E-01 0.72130E+01
   Friction thermal sca.    tstar : -0.10191E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36898E-01 0.53817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98131E-02      33   0.28213E-03   0.49435E+01 0.17952E+03 
c  Velocity[X]                                      0.18274E+01 
c  Velocity[Y]                                      0.31162E+01 
c  Velocity[Z]                                      0.70704E-30 
c  Pressure     0.95693E-07     536   0.92346E-08   0.94581E-01 0.13671E+04 
c  nu_tilda     0.68825E-05      33   0.39141E-05   0.52454E-06 0.19306E+03 
c  TempC        0.39566E+02      27   0.34734E-03   0.53566E+01 0.26927E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9183          10.053          4.5729          4.5729
v  Velocity[Y]            -2.8497          7.2889         0.07889         0.07889
v  Velocity[Z]       -1.2014e-014     7.1397e-015    -1.7168e-017    -1.7168e-017
v  ǁVelocityǁ         0.0020122          10.053          5.1358          5.1358
v  Pressure               -37.499          17.386         -10.981         -10.981
v  nu_tilda           4.4264e-007       0.0042695       0.0015734       0.0015734
v  TempC                       21          73.047          21.968          21.968
v  TurbVisc           3.3768e-014       0.0050321       0.0018482       0.0018482
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1873:        0.22280E+01

===============================================================


 INSTANT    0.187400000E+04   TIME STEP NUMBER            1874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84019E-02 0.89681E+00
   Friction velocity        uk    :  0.84019E-02 0.89681E+00
   Dimensionless distance   yplus :  0.67641E-01 0.72199E+01
   Friction thermal sca.    tstar : -0.83250E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50468E-01 0.53869E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98153E-02      33   0.31052E-03   0.49689E+01 0.17967E+03 
c  Velocity[X]                                      0.18409E+01 
c  Velocity[Y]                                      0.31280E+01 
c  Velocity[Z]                                      0.11514E-29 
c  Pressure     0.11450E-06     553   0.99299E-08   0.11155E+00 0.12881E+04 
c  nu_tilda     0.68849E-05      33   0.15269E-04   0.52518E-06 0.19315E+03 
c  TempC        0.39574E+02      27   0.29111E-03   0.51712E+01 0.26009E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9153          10.052          4.5729          4.5729
v  Velocity[Y]            -2.8512          7.2591        0.079234        0.079234
v  Velocity[Z]       -1.1875e-014     7.4828e-015    -1.7162e-017    -1.7162e-017
v  ǁVelocityǁ         0.0018468          10.052          5.1358          5.1358
v  Pressure               -37.475          17.166         -11.042         -11.042
v  nu_tilda           4.4271e-007       0.0042695       0.0015738       0.0015738
v  TempC                       21          73.047          21.968          21.968
v  TurbVisc           3.3774e-014       0.0050321       0.0018488       0.0018488
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1874:        0.22670E+01

===============================================================


 INSTANT    0.187500000E+04   TIME STEP NUMBER            1875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52482E-02 0.89627E+00
   Friction velocity        uk    :  0.52482E-02 0.89627E+00
   Dimensionless distance   yplus :  0.42252E-01 0.72156E+01
   Friction thermal sca.    tstar : -0.74382E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31525E-01 0.53836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98174E-02      33   0.20422E-03   0.49792E+01 0.17979E+03 
c  Velocity[X]                                      0.18550E+01 
c  Velocity[Y]                                      0.31242E+01 
c  Velocity[Z]                                      0.82682E-30 
c  Pressure     0.11187E-06     554   0.96949E-08   0.11045E+00 0.13922E+04 
c  nu_tilda     0.68872E-05      33   0.39119E-05   0.52578E-06 0.19324E+03 
c  TempC        0.39583E+02      27   0.33849E-03   0.48515E+01 0.23316E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9122          10.051          4.5729          4.5729
v  Velocity[Y]            -2.8525          7.2876        0.079577        0.079577
v  Velocity[Z]       -1.1946e-014     7.8196e-015    -1.7157e-017    -1.7157e-017
v  ǁVelocityǁ         0.0020228          10.051          5.1358          5.1358
v  Pressure               -37.442          17.395         -10.974         -10.974
v  nu_tilda           4.4271e-007       0.0042695       0.0015743       0.0015743
v  TempC                       21          73.047          21.968          21.968
v  TurbVisc           3.3795e-014       0.0050321       0.0018493       0.0018493
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1875:        0.22930E+01

===============================================================


 INSTANT    0.187600000E+04   TIME STEP NUMBER            1876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15150E-02 0.89766E+00
   Friction velocity        uk    :  0.15150E-02 0.89766E+00
   Dimensionless distance   yplus :  0.12197E-01 0.72268E+01
   Friction thermal sca.    tstar : -0.63591E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91000E-02 0.53920E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98197E-02      33   0.28249E-03   0.49337E+01 0.17960E+03 
c  Velocity[X]                                      0.18172E+01 
c  Velocity[Y]                                      0.31165E+01 
c  Velocity[Z]                                      0.76106E-30 
c  Pressure     0.91738E-07     473   0.93579E-08   0.89934E-01 0.65102E+03 
c  nu_tilda     0.68896E-05      33   0.15260E-04   0.52643E-06 0.19334E+03 
c  TempC        0.39591E+02      27   0.30372E-03   0.39261E+01 0.23345E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9095           10.05          4.5729          4.5729
v  Velocity[Y]            -2.8537          7.2974        0.079922        0.079922
v  Velocity[Z]       -1.1704e-014     8.6848e-015    -1.7139e-017    -1.7139e-017
v  ǁVelocityǁ         0.0020253           10.05          5.1358          5.1358
v  Pressure               -37.415          17.321         -11.001         -11.001
v  nu_tilda           4.4263e-007       0.0042695       0.0015747       0.0015747
v  TempC                       21          73.047          21.969          21.969
v  TurbVisc           3.3793e-014       0.0050321       0.0018498       0.0018498
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1876:        0.20760E+01

===============================================================


 INSTANT    0.187700000E+04   TIME STEP NUMBER            1877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10099E-01 0.89725E+00
   Friction velocity        uk    :  0.10099E-01 0.89725E+00
   Dimensionless distance   yplus :  0.81304E-01 0.72235E+01
   Friction thermal sca.    tstar : -0.67440E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60662E-01 0.53895E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98218E-02      33   0.28901E-03   0.49777E+01 0.17984E+03 
c  Velocity[X]                                      0.18483E+01 
c  Velocity[Y]                                      0.31294E+01 
c  Velocity[Z]                                      0.73031E-30 
c  Pressure     0.12299E-06     394   0.98099E-08   0.12098E+00 0.43386E+03 
c  nu_tilda     0.68919E-05      33   0.39141E-05   0.52704E-06 0.19343E+03 
c  TempC        0.39599E+02      27   0.34070E-03   0.37005E+01 0.22329E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9067          10.049          4.5729          4.5729
v  Velocity[Y]            -2.8549          7.2643        0.080268        0.080268
v  Velocity[Z]       -1.1479e-014     9.3041e-015    -1.7133e-017    -1.7133e-017
v  ǁVelocityǁ         0.0019306          10.049          5.1357          5.1357
v  Pressure               -37.385          17.264         -10.997         -10.997
v  nu_tilda           4.4263e-007       0.0042695       0.0015752       0.0015752
v  TempC                       21          73.047          21.969          21.969
v  TurbVisc           3.3769e-014       0.0050321       0.0018503       0.0018503
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1877:        0.18950E+01

===============================================================


 INSTANT    0.187800000E+04   TIME STEP NUMBER            1878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49791E-02 0.89585E+00
   Friction velocity        uk    :  0.49791E-02 0.89585E+00
   Dimensionless distance   yplus :  0.40085E-01 0.72122E+01
   Friction thermal sca.    tstar : -0.65899E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29908E-01 0.53811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98240E-02      33   0.24900E-03   0.49776E+01 0.17987E+03 
c  Velocity[X]                                      0.18553E+01 
c  Velocity[Y]                                      0.31224E+01 
c  Velocity[Z]                                      0.81596E-30 
c  Pressure     0.10614E-06     426   0.96353E-08   0.10411E+00 0.40107E+03 
c  nu_tilda     0.68943E-05      33   0.15265E-04   0.52769E-06 0.19353E+03 
c  TempC        0.39607E+02      27   0.29279E-03   0.48884E+01 0.24271E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9038          10.048          4.5729          4.5729
v  Velocity[Y]            -2.8565          7.2843        0.080613        0.080613
v  Velocity[Z]       -1.1138e-014     9.1503e-015    -1.7125e-017    -1.7125e-017
v  ǁVelocityǁ         0.0019428          10.048          5.1357          5.1357
v  Pressure                -37.36          17.336          -10.99          -10.99
v  nu_tilda           4.4263e-007       0.0042695       0.0015755       0.0015755
v  TempC                       21          73.047          21.969          21.969
v  TurbVisc           3.3771e-014       0.0050321       0.0018508       0.0018508
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1878:        0.19700E+01

===============================================================


 INSTANT    0.187900000E+04   TIME STEP NUMBER            1879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88585E-02 0.89692E+00
   Friction velocity        uk    :  0.88585E-02 0.89692E+00
   Dimensionless distance   yplus :  0.71317E-01 0.72208E+01
   Friction thermal sca.    tstar : -0.64078E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53210E-01 0.53875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98262E-02      33   0.29253E-03   0.49497E+01 0.17982E+03 
c  Velocity[X]                                      0.18311E+01 
c  Velocity[Y]                                      0.31186E+01 
c  Velocity[Z]                                      0.69236E-30 
c  Pressure     0.10134E-06     457   0.92777E-08   0.10085E+00 0.42761E+03 
c  nu_tilda     0.68966E-05      33   0.39061E-05   0.52829E-06 0.19362E+03 
c  TempC        0.39615E+02      27   0.26105E-03   0.46940E+01 0.23996E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9008          10.047          4.5729          4.5729
v  Velocity[Y]            -2.8581          7.2647        0.080961        0.080961
v  Velocity[Z]       -1.0982e-014     8.9524e-015    -1.7122e-017    -1.7122e-017
v  ǁVelocityǁ         0.0019341          10.047          5.1357          5.1357
v  Pressure               -37.329          17.309          -10.98          -10.98
v  nu_tilda           4.4261e-007       0.0042695        0.001576        0.001576
v  TempC                       21          73.047          21.969          21.969
v  TurbVisc            3.377e-014       0.0050321       0.0018514       0.0018514
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1879:        0.20350E+01

===============================================================


 INSTANT    0.188000000E+04   TIME STEP NUMBER            1880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60137E-02 0.89596E+00
   Friction velocity        uk    :  0.60137E-02 0.89596E+00
   Dimensionless distance   yplus :  0.48414E-01 0.72131E+01
   Friction thermal sca.    tstar : -0.64751E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36122E-01 0.53817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98284E-02      33   0.23806E-03   0.49658E+01 0.17991E+03 
c  Velocity[X]                                      0.18347E+01 
c  Velocity[Y]                                      0.31311E+01 
c  Velocity[Z]                                      0.97644E-30 
c  Pressure     0.10963E-06     409   0.97344E-08   0.10721E+00 0.35835E+03 
c  nu_tilda     0.68990E-05      33   0.15261E-04   0.52894E-06 0.19372E+03 
c  TempC        0.39624E+02      27   0.38096E-03   0.48804E+01 0.25200E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8978          10.046          4.5729          4.5729
v  Velocity[Y]            -2.8595          7.2832        0.081308        0.081308
v  Velocity[Z]       -1.0727e-014     1.0347e-014    -1.7112e-017    -1.7112e-017
v  ǁVelocityǁ         0.0019237          10.046          5.1357          5.1357
v  Pressure               -37.302          17.323         -10.988         -10.988
v  nu_tilda           4.4261e-007       0.0042695       0.0015764       0.0015764
v  TempC                       21          73.047           21.97           21.97
v  TurbVisc           3.3765e-014       0.0050321       0.0018519       0.0018519
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1880:        0.19280E+01

===============================================================


 INSTANT    0.188100000E+04   TIME STEP NUMBER            1881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85154E-02 0.89759E+00
   Friction velocity        uk    :  0.85154E-02 0.89759E+00
   Dimensionless distance   yplus :  0.68555E-01 0.72262E+01
   Friction thermal sca.    tstar : -0.63937E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51149E-01 0.53915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98306E-02      33   0.29149E-03   0.49435E+01 0.17991E+03 
c  Velocity[X]                                      0.18170E+01 
c  Velocity[Y]                                      0.31265E+01 
c  Velocity[Z]                                      0.10127E-29 
c  Pressure     0.87422E-07     522   0.95019E-08   0.86001E-01 0.87822E+03 
c  nu_tilda     0.69013E-05      33   0.39193E-05   0.52954E-06 0.19381E+03 
c  TempC        0.39632E+02      27   0.28683E-03   0.62817E+01 0.29038E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.895          10.045          4.5729          4.5729
v  Velocity[Y]            -2.8609          7.2946        0.081657        0.081657
v  Velocity[Z]       -1.0525e-014     1.0303e-014    -1.7103e-017    -1.7103e-017
v  ǁVelocityǁ         0.0020553          10.045          5.1357          5.1357
v  Pressure               -37.269          17.436         -10.944         -10.944
v  nu_tilda            4.426e-007       0.0042695       0.0015769       0.0015769
v  TempC                       21          73.048           21.97           21.97
v  TurbVisc           3.3764e-014       0.0050321       0.0018524       0.0018524
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1881:        0.21960E+01

===============================================================


 INSTANT    0.188200000E+04   TIME STEP NUMBER            1882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.42430E-02 0.89716E+00
   Friction velocity        uk    :  0.42430E-02 0.89716E+00
   Dimensionless distance   yplus :  0.34159E-01 0.72227E+01
   Friction thermal sca.    tstar : -0.62786E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25486E-01 0.53890E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98328E-02      33   0.29295E-03   0.49977E+01 0.18016E+03 
c  Velocity[X]                                      0.18728E+01 
c  Velocity[Y]                                      0.31249E+01 
c  Velocity[Z]                                      0.74103E-30 
c  Pressure     0.12708E-06     521   0.99359E-08   0.12530E+00 0.12127E+04 
c  nu_tilda     0.69036E-05      33   0.15255E-04   0.53019E-06 0.19390E+03 
c  TempC        0.39640E+02      27   0.33042E-03   0.48654E+01 0.24758E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8921          10.044          4.5729          4.5729
v  Velocity[Y]            -2.8621          7.2672        0.082006        0.082006
v  Velocity[Z]       -1.0187e-014     1.0544e-014    -1.7102e-017    -1.7102e-017
v  ǁVelocityǁ          0.001857          10.044          5.1357          5.1357
v  Pressure               -37.244          17.233         -11.001         -11.001
v  nu_tilda           4.4261e-007       0.0042695       0.0015773       0.0015773
v  TempC                       21          73.047           21.97           21.97
v  TurbVisc           3.3761e-014       0.0050321       0.0018529       0.0018529
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1882:        0.21950E+01

===============================================================


 INSTANT    0.188300000E+04   TIME STEP NUMBER            1883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61089E-02 0.89580E+00
   Friction velocity        uk    :  0.61089E-02 0.89580E+00
   Dimensionless distance   yplus :  0.49181E-01 0.72118E+01
   Friction thermal sca.    tstar : -0.64462E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36695E-01 0.53808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98350E-02      33   0.26460E-03   0.49972E+01 0.18019E+03 
c  Velocity[X]                                      0.18531E+01 
c  Velocity[Y]                                      0.31441E+01 
c  Velocity[Z]                                      0.10560E-29 
c  Pressure     0.11870E-06     552   0.97397E-08   0.11552E+00 0.13015E+04 
c  nu_tilda     0.69060E-05      33   0.39163E-05   0.53079E-06 0.19400E+03 
c  TempC        0.39648E+02      27   0.32471E-03   0.51658E+01 0.25971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8891          10.043          4.5729          4.5729
v  Velocity[Y]            -2.8632          7.2806        0.082355        0.082355
v  Velocity[Z]       -9.9718e-015     1.0184e-014    -1.7091e-017    -1.7091e-017
v  ǁVelocityǁ         0.0019951          10.043          5.1357          5.1357
v  Pressure               -37.213          17.435         -10.936         -10.936
v  nu_tilda           4.4256e-007       0.0042695       0.0015778       0.0015778
v  TempC                       21          73.047          21.971          21.971
v  TurbVisc           3.3765e-014       0.0050321       0.0018534       0.0018534
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1883:        0.22580E+01

===============================================================


 INSTANT    0.188400000E+04   TIME STEP NUMBER            1884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77356E-02 0.89687E+00
   Friction velocity        uk    :  0.77356E-02 0.89687E+00
   Dimensionless distance   yplus :  0.62277E-01 0.72204E+01
   Friction thermal sca.    tstar : -0.63634E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46465E-01 0.53872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98372E-02      33   0.26489E-03   0.49695E+01 0.18009E+03 
c  Velocity[X]                                      0.18401E+01 
c  Velocity[Y]                                      0.31294E+01 
c  Velocity[Z]                                      0.80297E-30 
c  Pressure     0.10015E-06     537   0.99249E-08   0.99500E-01 0.11345E+04 
c  nu_tilda     0.69083E-05      33   0.15256E-04   0.53144E-06 0.19409E+03 
c  TempC        0.39656E+02      27   0.33198E-03   0.47408E+01 0.24657E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8861          10.042          4.5729          4.5729
v  Velocity[Y]            -2.8647          7.2581        0.082705        0.082705
v  Velocity[Z]       -9.6951e-015     1.0693e-014    -1.7088e-017    -1.7088e-017
v  ǁVelocityǁ          0.001871          10.042          5.1357          5.1357
v  Pressure               -37.188          17.255          -10.99          -10.99
v  nu_tilda           4.4254e-007       0.0042695       0.0015782       0.0015782
v  TempC                       21          73.048          21.971          21.971
v  TurbVisc           3.3748e-014       0.0050321        0.001854        0.001854
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1884:        0.22130E+01

===============================================================


 INSTANT    0.188500000E+04   TIME STEP NUMBER            1885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.55953E-02 0.89607E+00
   Friction velocity        uk    :  0.55953E-02 0.89607E+00
   Dimensionless distance   yplus :  0.45046E-01 0.72140E+01
   Friction thermal sca.    tstar : -0.69139E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33609E-01 0.53824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98393E-02      33   0.26086E-03   0.49458E+01 0.18006E+03 
c  Velocity[X]                                      0.18225E+01 
c  Velocity[Y]                                      0.31233E+01 
c  Velocity[Z]                                      0.69455E-30 
c  Pressure     0.84541E-07     538   0.94572E-08   0.83265E-01 0.12076E+04 
c  nu_tilda     0.69107E-05      33   0.39133E-05   0.53205E-06 0.19419E+03 
c  TempC        0.39665E+02      27   0.33961E-03   0.45574E+01 0.25245E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8832          10.041          4.5729          4.5729
v  Velocity[Y]            -2.8662          7.2871        0.083057        0.083057
v  Velocity[Z]       -9.5449e-015     1.0611e-014     -1.708e-017     -1.708e-017
v  ǁVelocityǁ         0.0020095          10.041          5.1357          5.1357
v  Pressure               -37.156          17.439         -10.931         -10.931
v  nu_tilda           4.4247e-007       0.0042695       0.0015787       0.0015787
v  TempC                       21          73.048          21.971          21.971
v  TurbVisc           3.3744e-014       0.0050321       0.0018545       0.0018545
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1885:        0.22350E+01

===============================================================


 INSTANT    0.188600000E+04   TIME STEP NUMBER            1886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82777E-02 0.89753E+00
   Friction velocity        uk    :  0.82777E-02 0.89753E+00
   Dimensionless distance   yplus :  0.66641E-01 0.72257E+01
   Friction thermal sca.    tstar : -0.65225E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49722E-01 0.53912E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98415E-02      33   0.29404E-03   0.49810E+01 0.18026E+03 
c  Velocity[X]                                      0.18359E+01 
c  Velocity[Y]                                      0.31451E+01 
c  Velocity[Z]                                      0.82426E-30 
c  Pressure     0.14231E-06     473   0.98505E-08   0.13707E+00 0.55923E+03 
c  nu_tilda     0.69130E-05      33   0.15252E-04   0.53270E-06 0.19428E+03 
c  TempC        0.39673E+02      27   0.33542E-03   0.54198E+01 0.27126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8804           10.04          4.5729          4.5729
v  Velocity[Y]            -2.8677          7.2889        0.083408        0.083408
v  Velocity[Z]       -9.3012e-015      1.123e-014     -1.708e-017     -1.708e-017
v  ǁVelocityǁ         0.0019684           10.04          5.1357          5.1357
v  Pressure               -37.127          17.379         -10.951         -10.951
v  nu_tilda            4.424e-007       0.0042695       0.0015791       0.0015791
v  TempC                       21          73.047          21.972          21.972
v  TurbVisc           3.3722e-014       0.0050321        0.001855        0.001855
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1886:        0.20820E+01

===============================================================


 INSTANT    0.188700000E+04   TIME STEP NUMBER            1887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94955E-02 0.89746E+00
   Friction velocity        uk    :  0.94955E-02 0.89746E+00
   Dimensionless distance   yplus :  0.76445E-01 0.72252E+01
   Friction thermal sca.    tstar : -0.64025E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57036E-01 0.53908E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98437E-02      33   0.25192E-03   0.49908E+01 0.18038E+03 
c  Velocity[X]                                      0.18572E+01 
c  Velocity[Y]                                      0.31336E+01 
c  Velocity[Z]                                      0.87504E-30 
c  Pressure     0.12670E-06     441   0.94352E-08   0.12655E+00 0.42677E+03 
c  nu_tilda     0.69154E-05      33   0.39258E-05   0.53330E-06 0.19437E+03 
c  TempC        0.39681E+02      27   0.30031E-03   0.61335E+01 0.28117E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8776          10.039          4.5729          4.5729
v  Velocity[Y]             -2.869           7.264         0.08376         0.08376
v  Velocity[Z]       -9.1158e-015     1.0438e-014     -1.708e-017     -1.708e-017
v  ǁVelocityǁ         0.0019465          10.039          5.1356          5.1356
v  Pressure               -37.098          17.362          -10.94          -10.94
v  nu_tilda            4.424e-007       0.0042695       0.0015796       0.0015796
v  TempC                       21          73.047          21.972          21.972
v  TurbVisc           3.3701e-014       0.0050321       0.0018555       0.0018555
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1887:        0.20190E+01

===============================================================


 INSTANT    0.188800000E+04   TIME STEP NUMBER            1888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61990E-02 0.89584E+00
   Friction velocity        uk    :  0.61990E-02 0.89584E+00
   Dimensionless distance   yplus :  0.49907E-01 0.72122E+01
   Friction thermal sca.    tstar : -0.64784E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37236E-01 0.53811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98459E-02      33   0.29898E-03   0.49458E+01 0.18016E+03 
c  Velocity[X]                                      0.18220E+01 
c  Velocity[Y]                                      0.31238E+01 
c  Velocity[Z]                                      0.86862E-30 
c  Pressure     0.96782E-07     378   0.96654E-08   0.94361E-01 0.34851E+03 
c  nu_tilda     0.69177E-05      33   0.15248E-04   0.53395E-06 0.19447E+03 
c  TempC        0.39689E+02      27   0.30270E-03   0.56581E+01 0.25916E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8746          10.038          4.5729          4.5729
v  Velocity[Y]            -2.8702          7.2848        0.084113        0.084113
v  Velocity[Z]       -8.8655e-015     1.0981e-014     -1.708e-017     -1.708e-017
v  ǁVelocityǁ         0.0019484          10.038          5.1356          5.1356
v  Pressure                -37.07          17.392         -10.944         -10.944
v  nu_tilda           4.4236e-007       0.0042695         0.00158         0.00158
v  TempC                       21          73.047          21.972          21.972
v  TurbVisc           3.3701e-014       0.0050321        0.001856        0.001856
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1888:        0.18580E+01

===============================================================


 INSTANT    0.188900000E+04   TIME STEP NUMBER            1889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89064E-02 0.89690E+00
   Friction velocity        uk    :  0.89064E-02 0.89690E+00
   Dimensionless distance   yplus :  0.71703E-01 0.72207E+01
   Friction thermal sca.    tstar : -0.68143E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53498E-01 0.53874E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98481E-02      33   0.30388E-03   0.49906E+01 0.18042E+03 
c  Velocity[X]                                      0.18401E+01 
c  Velocity[Y]                                      0.31505E+01 
c  Velocity[Z]                                      0.84436E-30 
c  Pressure     0.12241E-06     456   0.91954E-08   0.12106E+00 0.44029E+03 
c  nu_tilda     0.69201E-05      33   0.39243E-05   0.53455E-06 0.19456E+03 
c  TempC        0.39697E+02      27   0.31672E-03   0.45392E+01 0.24556E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8716          10.037          4.5729          4.5729
v  Velocity[Y]            -2.8714          7.2574        0.084466        0.084466
v  Velocity[Z]       -8.6873e-015      1.053e-014     -1.708e-017     -1.708e-017
v  ǁVelocityǁ         0.0019374          10.038          5.1356          5.1356
v  Pressure                -37.04          17.363         -10.931         -10.931
v  nu_tilda           4.4236e-007       0.0042695       0.0015804       0.0015804
v  TempC                       21          73.048          21.973          21.973
v  TurbVisc           3.3688e-014       0.0050321       0.0018566       0.0018566
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1889:        0.20400E+01

===============================================================


 INSTANT    0.189000000E+04   TIME STEP NUMBER            1890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.32999E-02 0.89606E+00
   Friction velocity        uk    :  0.32999E-02 0.89606E+00
   Dimensionless distance   yplus :  0.26567E-01 0.72139E+01
   Friction thermal sca.    tstar : -0.67682E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19822E-01 0.53824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98503E-02      33   0.22016E-03   0.50056E+01 0.18053E+03 
c  Velocity[X]                                      0.18700E+01 
c  Velocity[Y]                                      0.31356E+01 
c  Velocity[Z]                                      0.92411E-30 
c  Pressure     0.10720E-06     281   0.93338E-08   0.10519E+00 0.35807E+03 
c  nu_tilda     0.69224E-05      33   0.15248E-04   0.53520E-06 0.19465E+03 
c  TempC        0.39706E+02      27   0.33927E-03   0.53415E+01 0.26246E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8687          10.036          4.5729          4.5729
v  Velocity[Y]            -2.8726          7.2834        0.084821        0.084821
v  Velocity[Z]       -8.4507e-015     1.1283e-014    -1.7076e-017    -1.7076e-017
v  ǁVelocityǁ         0.0019307          10.037          5.1356          5.1356
v  Pressure               -37.012           17.41         -10.933         -10.933
v  nu_tilda           4.4241e-007       0.0042695       0.0015808       0.0015808
v  TempC                       21          73.047          21.973          21.973
v  TurbVisc           3.3687e-014       0.0050321       0.0018571       0.0018571
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1890:        0.16280E+01

===============================================================


 INSTANT    0.189100000E+04   TIME STEP NUMBER            1891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83494E-02 0.89763E+00
   Friction velocity        uk    :  0.83494E-02 0.89763E+00
   Dimensionless distance   yplus :  0.67219E-01 0.72265E+01
   Friction thermal sca.    tstar : -0.82823E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50153E-01 0.53918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98524E-02      33   0.28626E-03   0.49505E+01 0.18034E+03 
c  Velocity[X]                                      0.18199E+01 
c  Velocity[Y]                                      0.31305E+01 
c  Velocity[Z]                                      0.82341E-30 
c  Pressure     0.10408E-06     537   0.94445E-08   0.10238E+00 0.95925E+03 
c  nu_tilda     0.69248E-05      33   0.39235E-05   0.53580E-06 0.19475E+03 
c  TempC        0.39714E+02      27   0.33879E-03   0.56118E+01 0.27564E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8659          10.035          4.5729          4.5729
v  Velocity[Y]            -2.8742          7.2954        0.085175        0.085175
v  Velocity[Z]       -8.3268e-015     1.1009e-014    -1.7083e-017    -1.7083e-017
v  ǁVelocityǁ         0.0020802          10.036          5.1356          5.1356
v  Pressure               -36.979          17.534         -10.885         -10.885
v  nu_tilda            4.424e-007       0.0042695       0.0015813       0.0015813
v  TempC                       21          73.048          21.973          21.973
v  TurbVisc           3.3702e-014       0.0050321       0.0018576       0.0018576
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1891:        0.22310E+01

===============================================================


 INSTANT    0.189200000E+04   TIME STEP NUMBER            1892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82715E-02 0.89701E+00
   Friction velocity        uk    :  0.82715E-02 0.89701E+00
   Dimensionless distance   yplus :  0.66591E-01 0.72216E+01
   Friction thermal sca.    tstar : -0.95890E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49684E-01 0.53881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98546E-02      33   0.27823E-03   0.49865E+01 0.18052E+03 
c  Velocity[X]                                      0.18441E+01 
c  Velocity[Y]                                      0.31424E+01 
c  Velocity[Z]                                      0.88362E-30 
c  Pressure     0.11406E-06     584   0.94773E-08   0.11197E+00 0.13327E+04 
c  nu_tilda     0.69271E-05      33   0.15244E-04   0.53645E-06 0.19484E+03 
c  TempC        0.39722E+02      27   0.33781E-03   0.62560E+01 0.27245E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.863          10.034          4.5729          4.5729
v  Velocity[Y]            -2.8757          7.2595        0.085531        0.085531
v  Velocity[Z]       -8.1237e-015     1.1214e-014    -1.7082e-017    -1.7082e-017
v  ǁVelocityǁ         0.0018695          10.035          5.1356          5.1356
v  Pressure               -36.952          17.313         -10.946         -10.946
v  nu_tilda           4.4242e-007       0.0042695       0.0015817       0.0015817
v  TempC                       21          73.047          21.973          21.973
v  TurbVisc             3.37e-014       0.0050321       0.0018581       0.0018581
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1892:        0.23470E+01

===============================================================


 INSTANT    0.189300000E+04   TIME STEP NUMBER            1893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73270E-02 0.89572E+00
   Friction velocity        uk    :  0.73270E-02 0.89572E+00
   Dimensionless distance   yplus :  0.58988E-01 0.72112E+01
   Friction thermal sca.    tstar : -0.13632E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44011E-01 0.53804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98568E-02      33   0.26366E-03   0.49808E+01 0.18055E+03 
c  Velocity[X]                                      0.18458E+01 
c  Velocity[Y]                                      0.31350E+01 
c  Velocity[Z]                                      0.10568E-29 
c  Pressure     0.96460E-07     568   0.97198E-08   0.94932E-01 0.12138E+04 
c  nu_tilda     0.69295E-05      33   0.39374E-05   0.53705E-06 0.19493E+03 
c  TempC        0.39730E+02      27   0.28766E-03   0.59760E+01 0.28019E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8599          10.033          4.5729          4.5729
v  Velocity[Y]             -2.877          7.2825        0.085887        0.085887
v  Velocity[Z]       -8.0415e-015     1.1475e-014    -1.7082e-017    -1.7082e-017
v  ǁVelocityǁ         0.0020112          10.034          5.1356          5.1356
v  Pressure               -36.922            17.5         -10.887         -10.887
v  nu_tilda           4.4242e-007       0.0042695       0.0015822       0.0015822
v  TempC                       21          73.048          21.974          21.974
v  TurbVisc           3.3706e-014       0.0050321       0.0018586       0.0018586
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1893:        0.23050E+01

===============================================================


 INSTANT    0.189400000E+04   TIME STEP NUMBER            1894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36612E-02 0.89672E+00
   Friction velocity        uk    :  0.36612E-02 0.89672E+00
   Dimensionless distance   yplus :  0.29475E-01 0.72192E+01
   Friction thermal sca.    tstar : -0.66859E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21992E-01 0.53864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98590E-02      33   0.29507E-03   0.49812E+01 0.18053E+03 
c  Velocity[X]                                      0.18524E+01 
c  Velocity[Y]                                      0.31287E+01 
c  Velocity[Z]                                      0.91447E-30 
c  Pressure     0.11583E-06     538   0.95575E-08   0.11452E+00 0.99373E+03 
c  nu_tilda     0.69318E-05      33   0.15237E-04   0.53769E-06 0.19503E+03 
c  TempC        0.39738E+02      27   0.33178E-03   0.48279E+01 0.26042E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.857          10.032          4.5729          4.5729
v  Velocity[Y]            -2.8782          7.2544        0.086243        0.086243
v  Velocity[Z]       -7.7892e-015     1.1457e-014    -1.7086e-017    -1.7086e-017
v  ǁVelocityǁ         0.0018611          10.033          5.1356          5.1356
v  Pressure               -36.895          17.341         -10.932         -10.932
v  nu_tilda            4.424e-007       0.0042695       0.0015826       0.0015826
v  TempC                       21          73.047          21.974          21.974
v  TurbVisc           3.3706e-014       0.0050321       0.0018592       0.0018592
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1894:        0.22410E+01

===============================================================


 INSTANT    0.189500000E+04   TIME STEP NUMBER            1895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67871E-02 0.89597E+00
   Friction velocity        uk    :  0.67871E-02 0.89597E+00
   Dimensionless distance   yplus :  0.54641E-01 0.72132E+01
   Friction thermal sca.    tstar : -0.13458E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40768E-01 0.53818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98611E-02      33   0.24777E-03   0.49665E+01 0.18054E+03 
c  Velocity[X]                                      0.18342E+01 
c  Velocity[Y]                                      0.31323E+01 
c  Velocity[Z]                                      0.10473E-29 
c  Pressure     0.10394E-06     536   0.92402E-08   0.10310E+00 0.10880E+04 
c  nu_tilda     0.69342E-05      33   0.39335E-05   0.53830E-06 0.19512E+03 
c  TempC        0.39747E+02      27   0.33440E-03   0.56719E+01 0.26916E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8543          10.031          4.5729          4.5729
v  Velocity[Y]            -2.8794          7.2822        0.086601        0.086601
v  Velocity[Z]       -8.5611e-015     1.1809e-014    -1.7091e-017    -1.7091e-017
v  ǁVelocityǁ         0.0019843          10.032          5.1356          5.1356
v  Pressure               -36.863          17.504         -10.879         -10.879
v  nu_tilda           4.4235e-007       0.0042695       0.0015831       0.0015831
v  TempC                       21          73.048          21.974          21.974
v  TurbVisc           3.3699e-014       0.0050321       0.0018597       0.0018597
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1895:        0.22270E+01

===============================================================


 INSTANT    0.189600000E+04   TIME STEP NUMBER            1896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.60080E-02 0.89735E+00
   Friction velocity        uk    :  0.60080E-02 0.89735E+00
   Dimensionless distance   yplus :  0.48369E-01 0.72242E+01
   Friction thermal sca.    tstar : -0.10013E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36089E-01 0.53901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98633E-02      33   0.29165E-03   0.49558E+01 0.18057E+03 
c  Velocity[X]                                      0.18036E+01 
c  Velocity[Y]                                      0.31522E+01 
c  Velocity[Z]                                      0.79133E-30 
c  Pressure     0.10754E-06     409   0.95086E-08   0.10564E+00 0.38807E+03 
c  nu_tilda     0.69365E-05      33   0.15241E-04   0.53895E-06 0.19521E+03 
c  TempC        0.39755E+02      27   0.31961E-03   0.51463E+01 0.26055E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8515           10.03          4.5729          4.5729
v  Velocity[Y]            -2.8805          7.2902        0.086958        0.086958
v  Velocity[Z]       -9.5767e-015     1.1789e-014    -1.7102e-017    -1.7102e-017
v  ǁVelocityǁ         0.0020435          10.031          5.1356          5.1356
v  Pressure               -36.833          17.504         -10.887         -10.887
v  nu_tilda           4.4227e-007       0.0042695       0.0015835       0.0015835
v  TempC                       21          73.047          21.975          21.975
v  TurbVisc           3.3685e-014       0.0050321       0.0018602       0.0018602
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1896:        0.19350E+01

===============================================================


 INSTANT    0.189700000E+04   TIME STEP NUMBER            1897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10384E-01 0.89685E+00
   Friction velocity        uk    :  0.10384E-01 0.89685E+00
   Dimensionless distance   yplus :  0.83601E-01 0.72203E+01
   Friction thermal sca.    tstar : -0.79820E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62375E-01 0.53871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98655E-02      33   0.26931E-03   0.49958E+01 0.18079E+03 
c  Velocity[X]                                      0.18546E+01 
c  Velocity[Y]                                      0.31412E+01 
c  Velocity[Z]                                      0.74848E-30 
c  Pressure     0.12409E-06     378   0.92783E-08   0.12200E+00 0.53645E+03 
c  nu_tilda     0.69388E-05      33   0.39357E-05   0.53956E-06 0.19530E+03 
c  TempC        0.39763E+02      27   0.29037E-03   0.42879E+01 0.24978E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8485          10.029          4.5729          4.5729
v  Velocity[Y]             -2.882          7.2585        0.087317        0.087317
v  Velocity[Z]       -9.2712e-015     1.1733e-014    -1.7106e-017    -1.7106e-017
v  ǁVelocityǁ         0.0019348           10.03          5.1356          5.1356
v  Pressure               -36.803          17.394         -10.893         -10.893
v  nu_tilda           4.4232e-007       0.0042695        0.001584        0.001584
v  TempC                       21          73.047          21.975          21.975
v  TurbVisc            3.366e-014       0.0050321       0.0018607       0.0018607
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1897:        0.18720E+01

===============================================================


 INSTANT    0.189800000E+04   TIME STEP NUMBER            1898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.49571E-02 0.89566E+00
   Friction velocity        uk    :  0.49571E-02 0.89566E+00
   Dimensionless distance   yplus :  0.39908E-01 0.72107E+01
   Friction thermal sca.    tstar : -0.66994E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29776E-01 0.53800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98677E-02      33   0.27659E-03   0.49792E+01 0.18072E+03 
c  Velocity[X]                                      0.18452E+01 
c  Velocity[Y]                                      0.31340E+01 
c  Velocity[Z]                                      0.87539E-30 
c  Pressure     0.10360E-06     442   0.93398E-08   0.10185E+00 0.44803E+03 
c  nu_tilda     0.69412E-05      33   0.15236E-04   0.54021E-06 0.19540E+03 
c  TempC        0.39771E+02      27   0.30448E-03   0.56628E+01 0.25681E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8456          10.028          4.5729          4.5729
v  Velocity[Y]            -2.8835          7.2788        0.087676        0.087676
v  Velocity[Z]       -9.8849e-015     1.1573e-014    -1.7115e-017    -1.7115e-017
v  ǁVelocityǁ         0.0019832          10.029          5.1356          5.1356
v  Pressure               -36.774          17.486         -10.884         -10.884
v  nu_tilda           4.4237e-007       0.0042695       0.0015843       0.0015843
v  TempC                       21          73.047          21.975          21.975
v  TurbVisc           3.3675e-014       0.0050321       0.0018612       0.0018612
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1898:        0.20080E+01

===============================================================


 INSTANT    0.189900000E+04   TIME STEP NUMBER            1899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98959E-02 0.89664E+00
   Friction velocity        uk    :  0.98959E-02 0.89664E+00
   Dimensionless distance   yplus :  0.79668E-01 0.72186E+01
   Friction thermal sca.    tstar : -0.63974E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59442E-01 0.53859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98698E-02      33   0.26473E-03   0.49861E+01 0.18084E+03 
c  Velocity[X]                                      0.18264E+01 
c  Velocity[Y]                                      0.31597E+01 
c  Velocity[Z]                                      0.96305E-30 
c  Pressure     0.10343E-06     488   0.93252E-08   0.10347E+00 0.44295E+03 
c  nu_tilda     0.69435E-05      33   0.39456E-05   0.54080E-06 0.19549E+03 
c  TempC        0.39779E+02      27   0.38019E-03   0.45795E+01 0.25317E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8426          10.027          4.5729          4.5729
v  Velocity[Y]            -2.8848          7.2581        0.088035        0.088035
v  Velocity[Z]       -9.7175e-015     1.1578e-014    -1.7121e-017    -1.7121e-017
v  ǁVelocityǁ         0.0019491          10.028          5.1356          5.1356
v  Pressure               -36.745          17.463          -10.87          -10.87
v  nu_tilda           4.4236e-007       0.0042695       0.0015848       0.0015848
v  TempC                       21          73.048          21.975          21.975
v  TurbVisc           3.3691e-014       0.0050321       0.0018617       0.0018617
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1899:        0.24020E+01

===============================================================


 INSTANT    0.190000000E+04   TIME STEP NUMBER            1900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41296E-02 0.89572E+00
   Friction velocity        uk    :  0.41296E-02 0.89572E+00
   Dimensionless distance   yplus :  0.33246E-01 0.72111E+01
   Friction thermal sca.    tstar : -0.64817E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24805E-01 0.53803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98720E-02      33   0.23427E-03   0.49726E+01 0.18076E+03 
c  Velocity[X]                                      0.18311E+01 
c  Velocity[Y]                                      0.31415E+01 
c  Velocity[Z]                                      0.96451E-30 
c  Pressure     0.11274E-06     424   0.98463E-08   0.10849E+00 0.40934E+03 
c  nu_tilda     0.69459E-05      33   0.15231E-04   0.54144E-06 0.19558E+03 
c  TempC        0.39787E+02      27   0.33797E-03   0.63965E+01 0.28768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8398          10.026          4.5729          4.5729
v  Velocity[Y]             -2.886           7.277        0.088396        0.088396
v  Velocity[Z]       -1.0396e-014     1.1552e-014    -1.7125e-017    -1.7125e-017
v  ǁVelocityǁ         0.0019436          10.027          5.1356          5.1356
v  Pressure               -36.715          17.463         -10.882         -10.882
v  nu_tilda           4.4235e-007       0.0042695       0.0015852       0.0015852
v  TempC                       21          73.048          21.976          21.976
v  TurbVisc           3.3688e-014       0.0050321       0.0018623       0.0018623
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1900:        0.21240E+01

===============================================================


 INSTANT    0.190100000E+04   TIME STEP NUMBER            1901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48991E-02 0.89733E+00
   Friction velocity        uk    :  0.48991E-02 0.89733E+00
   Dimensionless distance   yplus :  0.39441E-01 0.72241E+01
   Friction thermal sca.    tstar : -0.68402E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29428E-01 0.53900E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98742E-02      33   0.30798E-03   0.49810E+01 0.18089E+03 
c  Velocity[X]                                      0.18415E+01 
c  Velocity[Y]                                      0.31394E+01 
c  Velocity[Z]                                      0.82258E-30 
c  Pressure     0.11030E-06     538   0.99659E-08   0.10925E+00 0.98113E+03 
c  nu_tilda     0.69482E-05      33   0.39431E-05   0.54205E-06 0.19567E+03 
c  TempC        0.39796E+02      27   0.28902E-03   0.53639E+01 0.26883E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8369          10.025          4.5729          4.5729
v  Velocity[Y]            -2.8871          7.2903        0.088756        0.088756
v  Velocity[Z]       -1.0869e-014     1.1146e-014    -1.7129e-017    -1.7129e-017
v  ǁVelocityǁ         0.0020845          10.026          5.1356          5.1356
v  Pressure               -36.683          17.593         -10.832         -10.832
v  nu_tilda            4.423e-007       0.0042695       0.0015857       0.0015857
v  TempC                       21          73.048          21.976          21.976
v  TurbVisc           3.3683e-014       0.0050321       0.0018628       0.0018628
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1901:        0.22260E+01

===============================================================


 INSTANT    0.190200000E+04   TIME STEP NUMBER            1902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98420E-02 0.89686E+00
   Friction velocity        uk    :  0.98420E-02 0.89686E+00
   Dimensionless distance   yplus :  0.79235E-01 0.72203E+01
   Friction thermal sca.    tstar : -0.64608E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59118E-01 0.53871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98764E-02      33   0.26196E-03   0.49975E+01 0.18099E+03 
c  Velocity[X]                                      0.18401E+01 
c  Velocity[Y]                                      0.31574E+01 
c  Velocity[Z]                                      0.98824E-30 
c  Pressure     0.10687E-06     537   0.95303E-08   0.10618E+00 0.11585E+04 
c  nu_tilda     0.69506E-05      33   0.15231E-04   0.54270E-06 0.19577E+03 
c  TempC        0.39804E+02      27   0.30572E-03   0.49687E+01 0.25075E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.834          10.024          4.5729          4.5729
v  Velocity[Y]            -2.8881          7.2601        0.089118        0.089118
v  Velocity[Z]        -1.044e-014     1.1095e-014    -1.7132e-017    -1.7132e-017
v  ǁVelocityǁ         0.0018867          10.025          5.1356          5.1356
v  Pressure               -36.655          17.403         -10.885         -10.885
v  nu_tilda           4.4228e-007       0.0042695       0.0015861       0.0015861
v  TempC                       21          73.047          21.976          21.976
v  TurbVisc            3.367e-014       0.0050321       0.0018633       0.0018633
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1902:        0.22310E+01

===============================================================


 INSTANT    0.190300000E+04   TIME STEP NUMBER            1903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53239E-02 0.89541E+00
   Friction velocity        uk    :  0.53239E-02 0.89541E+00
   Dimensionless distance   yplus :  0.42861E-01 0.72087E+01
   Friction thermal sca.    tstar : -0.65008E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31979E-01 0.53785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98785E-02      33   0.28598E-03   0.49707E+01 0.18088E+03 
c  Velocity[X]                                      0.18289E+01 
c  Velocity[Y]                                      0.31418E+01 
c  Velocity[Z]                                      0.78651E-30 
c  Pressure     0.11270E-06     537   0.92013E-08   0.10847E+00 0.11260E+04 
c  nu_tilda     0.69529E-05      33   0.39585E-05   0.54330E-06 0.19586E+03 
c  TempC        0.39812E+02      27   0.34618E-03   0.41127E+01 0.23270E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.831          10.023          4.5729          4.5729
v  Velocity[Y]            -2.8897          7.2763         0.08948         0.08948
v  Velocity[Z]       -1.0723e-014     1.0529e-014    -1.7144e-017    -1.7144e-017
v  ǁVelocityǁ         0.0020236          10.024          5.1356          5.1356
v  Pressure               -36.624          17.573          -10.83          -10.83
v  nu_tilda           4.4222e-007       0.0042695       0.0015866       0.0015866
v  TempC                       21          73.048          21.977          21.977
v  TurbVisc           3.3665e-014       0.0050321       0.0018638       0.0018638
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1903:        0.22360E+01

===============================================================


 INSTANT    0.190400000E+04   TIME STEP NUMBER            1904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67557E-02 0.89650E+00
   Friction velocity        uk    :  0.67557E-02 0.89650E+00
   Dimensionless distance   yplus :  0.54388E-01 0.72174E+01
   Friction thermal sca.    tstar : -0.63939E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40580E-01 0.53850E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98807E-02      33   0.29119E-03   0.50015E+01 0.18106E+03 
c  Velocity[X]                                      0.18636E+01 
c  Velocity[Y]                                      0.31380E+01 
c  Velocity[Z]                                      0.77811E-30 
c  Pressure     0.11358E-06     536   0.96763E-08   0.11325E+00 0.94355E+03 
c  nu_tilda     0.69553E-05      33   0.15222E-04   0.54395E-06 0.19595E+03 
c  TempC        0.39820E+02      27   0.30482E-03   0.62248E+01 0.26125E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8281          10.022          4.5729          4.5729
v  Velocity[Y]            -2.8911          7.2545        0.089842        0.089842
v  Velocity[Z]        -1.062e-014     1.0622e-014    -1.7144e-017    -1.7144e-017
v  ǁVelocityǁ         0.0018729          10.023          5.1356          5.1356
v  Pressure               -36.595          17.425         -10.871         -10.871
v  nu_tilda           4.4218e-007       0.0042695        0.001587        0.001587
v  TempC                       21          73.048          21.977          21.977
v  TurbVisc           3.3645e-014       0.0050321       0.0018643       0.0018643
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1904:        0.22220E+01

===============================================================


 INSTANT    0.190500000E+04   TIME STEP NUMBER            1905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71494E-02 0.89576E+00
   Friction velocity        uk    :  0.71494E-02 0.89576E+00
   Dimensionless distance   yplus :  0.57558E-01 0.72115E+01
   Friction thermal sca.    tstar : -0.65366E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42944E-01 0.53806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98828E-02      33   0.21574E-03   0.49838E+01 0.18108E+03 
c  Velocity[X]                                      0.18242E+01 
c  Velocity[Y]                                      0.31596E+01 
c  Velocity[Z]                                      0.83879E-30 
c  Pressure     0.86908E-07     554   0.99436E-08   0.85534E-01 0.11807E+04 
c  nu_tilda     0.69576E-05      33   0.39636E-05   0.54454E-06 0.19604E+03 
c  TempC        0.39828E+02      27   0.34727E-03   0.44375E+01 0.24034E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8254          10.022          4.5729          4.5729
v  Velocity[Y]            -2.8924          7.2805        0.090205        0.090205
v  Velocity[Z]       -1.1107e-014     1.0085e-014    -1.7151e-017    -1.7151e-017
v  ǁVelocityǁ         0.0020362          10.022          5.1356          5.1356
v  Pressure               -36.564          17.613         -10.814         -10.814
v  nu_tilda           4.4217e-007       0.0042695       0.0015875       0.0015875
v  TempC                       21          73.048          21.977          21.977
v  TurbVisc           3.3634e-014       0.0050321       0.0018648       0.0018648
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1905:        0.22650E+01

===============================================================


 INSTANT    0.190600000E+04   TIME STEP NUMBER            1906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88148E-02 0.89703E+00
   Friction velocity        uk    :  0.88148E-02 0.89703E+00
   Dimensionless distance   yplus :  0.70966E-01 0.72217E+01
   Friction thermal sca.    tstar : -0.63502E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52948E-01 0.53882E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98850E-02      33   0.27321E-03   0.49543E+01 0.18093E+03 
c  Velocity[X]                                      0.18106E+01 
c  Velocity[Y]                                      0.31437E+01 
c  Velocity[Z]                                      0.88176E-30 
c  Pressure     0.11039E-06     469   0.91138E-08   0.10741E+00 0.64447E+03 
c  nu_tilda     0.69600E-05      33   0.15221E-04   0.54519E-06 0.19613E+03 
c  TempC        0.39836E+02      27   0.26936E-03   0.51051E+01 0.26185E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8225          10.021          4.5729          4.5729
v  Velocity[Y]            -2.8936          7.2845        0.090568        0.090568
v  Velocity[Z]       -1.1153e-014     1.0236e-014    -1.7157e-017    -1.7157e-017
v  ǁVelocityǁ         0.0019884          10.021          5.1356          5.1356
v  Pressure               -36.532          17.534         -10.837         -10.837
v  nu_tilda           4.4213e-007       0.0042695       0.0015879       0.0015879
v  TempC                       21          73.048          21.977          21.977
v  TurbVisc           3.3629e-014       0.0050321       0.0018654       0.0018654
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1906:        0.20830E+01

===============================================================


 INSTANT    0.190700000E+04   TIME STEP NUMBER            1907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91395E-02 0.89681E+00
   Friction velocity        uk    :  0.91395E-02 0.89681E+00
   Dimensionless distance   yplus :  0.73579E-01 0.72199E+01
   Friction thermal sca.    tstar : -0.63306E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54898E-01 0.53869E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98872E-02      33   0.29501E-03   0.49981E+01 0.18119E+03 
c  Velocity[X]                                      0.18562E+01 
c  Velocity[Y]                                      0.31419E+01 
c  Velocity[Z]                                      0.88036E-30 
c  Pressure     0.11897E-06     458   0.94486E-08   0.11829E+00 0.44241E+03 
c  nu_tilda     0.69623E-05      33   0.39652E-05   0.54579E-06 0.19622E+03 
c  TempC        0.39844E+02      27   0.41145E-03   0.59422E+01 0.27000E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8195           10.02          4.5729          4.5729
v  Velocity[Y]            -2.8947          7.2598        0.090933        0.090933
v  Velocity[Z]       -1.0922e-014     9.5094e-015    -1.7166e-017    -1.7166e-017
v  ǁVelocityǁ         0.0019845           10.02          5.1356          5.1356
v  Pressure               -36.502          17.516         -10.823         -10.823
v  nu_tilda           4.4215e-007       0.0042695       0.0015883       0.0015883
v  TempC                       21          73.048          21.978          21.978
v  TurbVisc           3.3618e-014       0.0050321       0.0018659       0.0018659
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1907:        0.20500E+01

===============================================================


 INSTANT    0.190800000E+04   TIME STEP NUMBER            1908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.38351E-02 0.89535E+00
   Friction velocity        uk    :  0.38351E-02 0.89535E+00
   Dimensionless distance   yplus :  0.30875E-01 0.72082E+01
   Friction thermal sca.    tstar : -0.64832E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23036E-01 0.53781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98893E-02      33   0.27152E-03   0.49814E+01 0.18115E+03 
c  Velocity[X]                                      0.18220E+01 
c  Velocity[Y]                                      0.31593E+01 
c  Velocity[Z]                                      0.85486E-30 
c  Pressure     0.99772E-07     361   0.95294E-08   0.97439E-01 0.37601E+03 
c  nu_tilda     0.69646E-05      33   0.15221E-04   0.54644E-06 0.19632E+03 
c  TempC        0.39853E+02      27   0.35604E-03   0.78156E+01 0.31527E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8165          10.019          4.5729          4.5729
v  Velocity[Y]            -2.8957          7.2769        0.091298        0.091298
v  Velocity[Z]       -1.0958e-014     9.6932e-015    -1.7174e-017    -1.7174e-017
v  ǁVelocityǁ         0.0020377          10.019          5.1356          5.1356
v  Pressure               -36.472          17.576         -10.821         -10.821
v  nu_tilda           4.4217e-007       0.0042695       0.0015887       0.0015887
v  TempC                       21          73.047          21.978          21.978
v  TurbVisc           3.3625e-014       0.0050321       0.0018664       0.0018664
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1908:        0.18310E+01

===============================================================


 INSTANT    0.190900000E+04   TIME STEP NUMBER            1909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81394E-02 0.89626E+00
   Friction velocity        uk    :  0.81394E-02 0.89626E+00
   Dimensionless distance   yplus :  0.65528E-01 0.72155E+01
   Friction thermal sca.    tstar : -0.67546E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48891E-01 0.53836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98915E-02      33   0.29948E-03   0.49864E+01 0.18118E+03 
c  Velocity[X]                                      0.18356E+01 
c  Velocity[Y]                                      0.31508E+01 
c  Velocity[Z]                                      0.88224E-30 
c  Pressure     0.11840E-06     408   0.99057E-08   0.11690E+00 0.43331E+03 
c  nu_tilda     0.69670E-05      33   0.39851E-05   0.54704E-06 0.19641E+03 
c  TempC        0.39861E+02      27   0.35672E-03   0.50321E+01 0.25878E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8138          10.018          4.5729          4.5729
v  Velocity[Y]            -2.8972           7.252        0.091662        0.091662
v  Velocity[Z]       -1.1033e-014     8.9782e-015    -1.7182e-017    -1.7182e-017
v  ǁVelocityǁ         0.0019568          10.018          5.1356          5.1356
v  Pressure               -36.443          17.516         -10.815         -10.815
v  nu_tilda           4.4218e-007       0.0042695       0.0015892       0.0015892
v  TempC                       21          73.048          21.978          21.978
v  TurbVisc           3.3629e-014       0.0050321       0.0018669       0.0018669
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1909:        0.19190E+01

===============================================================


 INSTANT    0.191000000E+04   TIME STEP NUMBER            1910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63716E-02 0.89554E+00
   Friction velocity        uk    :  0.63716E-02 0.89554E+00
   Dimensionless distance   yplus :  0.51296E-01 0.72097E+01
   Friction thermal sca.    tstar : -0.66267E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38272E-01 0.53792E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98937E-02      33   0.23430E-03   0.50014E+01 0.18129E+03 
c  Velocity[X]                                      0.18584E+01 
c  Velocity[Y]                                      0.31429E+01 
c  Velocity[Z]                                      0.91469E-30 
c  Pressure     0.10736E-06     394   0.94826E-08   0.10537E+00 0.39890E+03 
c  nu_tilda     0.69693E-05      33   0.15210E-04   0.54768E-06 0.19650E+03 
c  TempC        0.39869E+02      27   0.29088E-03   0.53492E+01 0.27170E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8109          10.017          4.5729          4.5729
v  Velocity[Y]            -2.8986          7.2777        0.092029        0.092029
v  Velocity[Z]       -1.1237e-014       9.23e-015    -1.7194e-017    -1.7194e-017
v  ǁVelocityǁ          0.001995          10.017          5.1356          5.1356
v  Pressure                -36.41          17.579         -10.809         -10.809
v  nu_tilda           4.4219e-007       0.0042695       0.0015896       0.0015896
v  TempC                       21          73.048          21.979          21.979
v  TurbVisc           3.3634e-014       0.0050321       0.0018674       0.0018674
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1910:        0.19080E+01

===============================================================


 INSTANT    0.191100000E+04   TIME STEP NUMBER            1911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10135E-01 0.89712E+00
   Friction velocity        uk    :  0.10135E-01 0.89712E+00
   Dimensionless distance   yplus :  0.81594E-01 0.72225E+01
   Friction thermal sca.    tstar : -0.64150E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60878E-01 0.53888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98958E-02      33   0.26372E-03   0.49689E+01 0.18125E+03 
c  Velocity[X]                                      0.18042E+01 
c  Velocity[Y]                                      0.31647E+01 
c  Velocity[Z]                                      0.10926E-29 
c  Pressure     0.92572E-07     521   0.97656E-08   0.91046E-01 0.81059E+03 
c  nu_tilda     0.69717E-05      33   0.39895E-05   0.54829E-06 0.19659E+03 
c  TempC        0.39877E+02      27   0.29271E-03   0.42486E+01 0.24024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8079          10.016          4.5729          4.5729
v  Velocity[Y]            -2.8999          7.2882        0.092394        0.092394
v  Velocity[Z]       -1.1181e-014     8.4945e-015    -1.7203e-017    -1.7203e-017
v  ǁVelocityǁ         0.0020906          10.016          5.1356          5.1356
v  Pressure               -36.381           17.68         -10.771         -10.771
v  nu_tilda           4.4212e-007       0.0042695       0.0015901       0.0015901
v  TempC                       21          73.048          21.979          21.979
v  TurbVisc           3.3636e-014       0.0050321       0.0018679       0.0018679
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1911:        0.21800E+01

===============================================================


 INSTANT    0.191200000E+04   TIME STEP NUMBER            1912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41191E-02 0.89657E+00
   Friction velocity        uk    :  0.41191E-02 0.89657E+00
   Dimensionless distance   yplus :  0.33161E-01 0.72180E+01
   Friction thermal sca.    tstar : -0.64332E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24742E-01 0.53854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.98980E-02      33   0.27113E-03   0.49895E+01 0.18130E+03 
c  Velocity[X]                                      0.18391E+01 
c  Velocity[Y]                                      0.31504E+01 
c  Velocity[Z]                                      0.85355E-30 
c  Pressure     0.11617E-06     522   0.96204E-08   0.11378E+00 0.11990E+04 
c  nu_tilda     0.69740E-05      33   0.15211E-04   0.54893E-06 0.19668E+03 
c  TempC        0.39885E+02      27   0.34779E-03   0.42842E+01 0.24058E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.805          10.015          4.5729          4.5729
v  Velocity[Y]             -2.901          7.2535        0.092762        0.092762
v  Velocity[Z]       -1.1135e-014     8.7578e-015    -1.7215e-017    -1.7215e-017
v  ǁVelocityǁ         0.0018682          10.015          5.1356          5.1356
v  Pressure               -36.349          17.478         -10.822         -10.822
v  nu_tilda            4.421e-007       0.0042695       0.0015905       0.0015905
v  TempC                       21          73.047          21.979          21.979
v  TurbVisc           3.3614e-014       0.0050321       0.0018685       0.0018685
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1912:        0.22020E+01

===============================================================


 INSTANT    0.191300000E+04   TIME STEP NUMBER            1913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30758E-02 0.89527E+00
   Friction velocity        uk    :  0.30758E-02 0.89527E+00
   Dimensionless distance   yplus :  0.24762E-01 0.72076E+01
   Friction thermal sca.    tstar : -0.72073E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18475E-01 0.53776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99001E-02      33   0.29788E-03   0.49847E+01 0.18138E+03 
c  Velocity[X]                                      0.18410E+01 
c  Velocity[Y]                                      0.31437E+01 
c  Velocity[Z]                                      0.82894E-30 
c  Pressure     0.10097E-06     554   0.94121E-08   0.99242E-01 0.12605E+04 
c  nu_tilda     0.69764E-05      33   0.39935E-05   0.54953E-06 0.19677E+03 
c  TempC        0.39893E+02      27   0.33203E-03   0.53754E+01 0.26820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8022          10.014          4.5729          4.5729
v  Velocity[Y]            -2.9021          7.2771        0.093129        0.093129
v  Velocity[Z]       -1.1217e-014     7.9695e-015    -1.7224e-017    -1.7224e-017
v  ǁVelocityǁ         0.0020397          10.014          5.1356          5.1356
v  Pressure                -36.32           17.68         -10.762         -10.762
v  nu_tilda           4.4207e-007       0.0042695        0.001591        0.001591
v  TempC                       21          73.048          21.979          21.979
v  TurbVisc            3.361e-014       0.0050321        0.001869        0.001869
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1913:        0.22560E+01

===============================================================


 INSTANT    0.191400000E+04   TIME STEP NUMBER            1914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97027E-02 0.89625E+00
   Friction velocity        uk    :  0.97027E-02 0.89625E+00
   Dimensionless distance   yplus :  0.78114E-01 0.72154E+01
   Friction thermal sca.    tstar : -0.90887E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58282E-01 0.53835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99023E-02      33   0.27294E-03   0.49906E+01 0.18142E+03 
c  Velocity[X]                                      0.18288E+01 
c  Velocity[Y]                                      0.31618E+01 
c  Velocity[Z]                                      0.10556E-29 
c  Pressure     0.10384E-06     504   0.97971E-08   0.10361E+00 0.10314E+04 
c  nu_tilda     0.69787E-05      33   0.15204E-04   0.55017E-06 0.19686E+03 
c  TempC        0.39901E+02      27   0.29120E-03   0.52732E+01 0.27077E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7994          10.013          4.5729          4.5729
v  Velocity[Y]             -2.903          7.2521        0.093496        0.093496
v  Velocity[Z]       -1.1412e-014     7.5736e-015    -1.7238e-017    -1.7238e-017
v  ǁVelocityǁ         0.0018749          10.013          5.1356          5.1356
v  Pressure               -36.289          17.515         -10.805         -10.805
v  nu_tilda           4.4211e-007       0.0042695       0.0015914       0.0015914
v  TempC                       21          73.048           21.98           21.98
v  TurbVisc             3.36e-014       0.0050321       0.0018695       0.0018695
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1914:        0.21480E+01

===============================================================


 INSTANT    0.191500000E+04   TIME STEP NUMBER            1915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83628E-02 0.89534E+00
   Friction velocity        uk    :  0.83628E-02 0.89534E+00
   Dimensionless distance   yplus :  0.67326E-01 0.72081E+01
   Friction thermal sca.    tstar : -0.11116E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50233E-01 0.53780E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99045E-02      33   0.28138E-03   0.49827E+01 0.18139E+03 
c  Velocity[X]                                      0.18317E+01 
c  Velocity[Y]                                      0.31509E+01 
c  Velocity[Z]                                      0.72263E-30 
c  Pressure     0.11515E-06     521   0.94887E-08   0.11077E+00 0.11180E+04 
c  nu_tilda     0.69810E-05      33   0.40159E-05   0.55077E-06 0.19695E+03 
c  TempC        0.39909E+02      27   0.24237E-03   0.49251E+01 0.25150E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7966          10.012          4.5729          4.5729
v  Velocity[Y]            -2.9044           7.273        0.093865        0.093865
v  Velocity[Z]       -1.1582e-014     8.0484e-015    -1.7252e-017    -1.7252e-017
v  ǁVelocityǁ         0.0020348          10.012          5.1356          5.1356
v  Pressure               -36.257          17.682          -10.75          -10.75
v  nu_tilda           4.4215e-007       0.0042695       0.0015918       0.0015918
v  TempC                       21          73.049           21.98           21.98
v  TurbVisc           3.3612e-014       0.0050321         0.00187         0.00187
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1915:        0.21800E+01

===============================================================


 INSTANT    0.191600000E+04   TIME STEP NUMBER            1916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97180E-02 0.89665E+00
   Friction velocity        uk    :  0.97180E-02 0.89665E+00
   Dimensionless distance   yplus :  0.78237E-01 0.72187E+01
   Friction thermal sca.    tstar : -0.19713E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58374E-01 0.53859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99066E-02      33   0.28437E-03   0.49809E+01 0.18143E+03 
c  Velocity[X]                                      0.18358E+01 
c  Velocity[Y]                                      0.31451E+01 
c  Velocity[Z]                                      0.95013E-30 
c  Pressure     0.98700E-07     473   0.94822E-08   0.97198E-01 0.53236E+03 
c  nu_tilda     0.69834E-05      33   0.15196E-04   0.55141E-06 0.19704E+03 
c  TempC        0.39918E+02      27   0.38546E-03   0.58792E+01 0.26971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7936          10.011          4.5729          4.5729
v  Velocity[Y]            -2.9058          7.2819        0.094234        0.094234
v  Velocity[Z]       -1.1523e-014     7.2817e-015    -1.7262e-017    -1.7262e-017
v  ǁVelocityǁ         0.0020641          10.011          5.1356          5.1356
v  Pressure               -36.226          17.635         -10.769         -10.769
v  nu_tilda           4.4212e-007       0.0042695       0.0015922       0.0015922
v  TempC                       21          73.048           21.98           21.98
v  TurbVisc           3.3625e-014       0.0050321       0.0018705       0.0018705
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1916:        0.20830E+01

===============================================================


 INSTANT    0.191700000E+04   TIME STEP NUMBER            1917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82359E-02 0.89634E+00
   Friction velocity        uk    :  0.82359E-02 0.89634E+00
   Dimensionless distance   yplus :  0.66304E-01 0.72162E+01
   Friction thermal sca.    tstar : -0.21133E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49470E-01 0.53841E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99088E-02      33   0.25823E-03   0.49967E+01 0.18160E+03 
c  Velocity[X]                                      0.18295E+01 
c  Velocity[Y]                                      0.31672E+01 
c  Velocity[Z]                                      0.10060E-29 
c  Pressure     0.10176E-06     457   0.99071E-08   0.10160E+00 0.44939E+03 
c  nu_tilda     0.69857E-05      33   0.40172E-05   0.55202E-06 0.19713E+03 
c  TempC        0.39926E+02      27   0.27828E-03   0.69082E+01 0.30856E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7906           10.01          4.5729          4.5729
v  Velocity[Y]            -2.9071          7.2547        0.094603        0.094603
v  Velocity[Z]       -1.1579e-014     7.6479e-015    -1.7276e-017    -1.7276e-017
v  ǁVelocityǁ         0.0019793           10.01          5.1356          5.1356
v  Pressure               -36.195           17.61         -10.756         -10.756
v  nu_tilda           4.4214e-007       0.0042695       0.0015927       0.0015927
v  TempC                       21          73.048           21.98           21.98
v  TurbVisc           3.3615e-014       0.0050321        0.001871        0.001871
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1917:        0.20520E+01

===============================================================


 INSTANT    0.191800000E+04   TIME STEP NUMBER            1918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62716E-02 0.89485E+00
   Friction velocity        uk    :  0.62716E-02 0.89485E+00
   Dimensionless distance   yplus :  0.50491E-01 0.72041E+01
   Friction thermal sca.    tstar : -0.11249E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37672E-01 0.53751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99109E-02      33   0.27285E-03   0.49753E+01 0.18149E+03 
c  Velocity[X]                                      0.18229E+01 
c  Velocity[Y]                                      0.31523E+01 
c  Velocity[Z]                                      0.87096E-30 
c  Pressure     0.11328E-06     409   0.96546E-08   0.10935E+00 0.37692E+03 
c  nu_tilda     0.69881E-05      33   0.15201E-04   0.55266E-06 0.19722E+03 
c  TempC        0.39934E+02      27   0.34403E-03   0.42232E+01 0.23563E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7878          10.009          4.5729          4.5729
v  Velocity[Y]            -2.9082          7.2689        0.094974        0.094974
v  Velocity[Z]        -1.156e-014     6.8454e-015    -1.7284e-017    -1.7284e-017
v  ǁVelocityǁ         0.0020027          10.009          5.1356          5.1356
v  Pressure               -36.165           17.62         -10.764         -10.764
v  nu_tilda           4.4218e-007       0.0042695       0.0015931       0.0015931
v  TempC                       21          73.047          21.981          21.981
v  TurbVisc           3.3622e-014       0.0050321       0.0018715       0.0018715
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1918:        0.19460E+01

===============================================================


 INSTANT    0.191900000E+04   TIME STEP NUMBER            1919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.58556E-02 0.89613E+00
   Friction velocity        uk    :  0.58556E-02 0.89613E+00
   Dimensionless distance   yplus :  0.47142E-01 0.72144E+01
   Friction thermal sca.    tstar : -0.92686E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35173E-01 0.53828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99131E-02      33   0.30532E-03   0.50048E+01 0.18167E+03 
c  Velocity[X]                                      0.18527E+01 
c  Velocity[Y]                                      0.31521E+01 
c  Velocity[Z]                                      0.94354E-30 
c  Pressure     0.11955E-06     488   0.99673E-08   0.11898E+00 0.51187E+03 
c  nu_tilda     0.69904E-05      33   0.40255E-05   0.55325E-06 0.19731E+03 
c  TempC        0.39942E+02      27   0.36348E-03   0.56018E+01 0.27188E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7849          10.008          4.5729          4.5729
v  Velocity[Y]            -2.9093          7.2498        0.095343        0.095343
v  Velocity[Z]       -1.1719e-014      6.561e-015    -1.7299e-017    -1.7299e-017
v  ǁVelocityǁ          0.001986          10.008          5.1356          5.1356
v  Pressure               -36.134          17.624         -10.743         -10.743
v  nu_tilda           4.4212e-007       0.0042695       0.0015936       0.0015936
v  TempC                       21          73.048          21.981          21.981
v  TurbVisc           3.3633e-014       0.0050321       0.0018721       0.0018721
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1919:        0.21020E+01

===============================================================


 INSTANT    0.192000000E+04   TIME STEP NUMBER            1920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76212E-02 0.89525E+00
   Friction velocity        uk    :  0.76212E-02 0.89525E+00
   Dimensionless distance   yplus :  0.61356E-01 0.72074E+01
   Friction thermal sca.    tstar : -0.75132E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45779E-01 0.53775E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99152E-02      33   0.22030E-03   0.49907E+01 0.18164E+03 
c  Velocity[X]                                      0.18247E+01 
c  Velocity[Y]                                      0.31660E+01 
c  Velocity[Z]                                      0.78654E-30 
c  Pressure     0.99790E-07     297   0.92191E-08   0.97540E-01 0.37916E+03 
c  nu_tilda     0.69928E-05      33   0.15190E-04   0.55389E-06 0.19740E+03 
c  TempC        0.39950E+02      27   0.38621E-03   0.51666E+01 0.26650E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7821          10.007          4.5729          4.5729
v  Velocity[Y]            -2.9102          7.2738        0.095715        0.095715
v  Velocity[Z]       -1.1707e-014     7.0196e-015    -1.7306e-017    -1.7306e-017
v  ǁVelocityǁ         0.0020548          10.007          5.1356          5.1356
v  Pressure                 -36.1          17.667         -10.741         -10.741
v  nu_tilda           4.4203e-007       0.0042695        0.001594        0.001594
v  TempC                       21          73.048          21.981          21.981
v  TurbVisc           3.3614e-014       0.0050321       0.0018726       0.0018726
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1920:        0.16730E+01

===============================================================


 INSTANT    0.192100000E+04   TIME STEP NUMBER            1921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54266E-02 0.89680E+00
   Friction velocity        uk    :  0.54266E-02 0.89680E+00
   Dimensionless distance   yplus :  0.43688E-01 0.72199E+01
   Friction thermal sca.    tstar : -0.91341E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32596E-01 0.53868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99174E-02      33   0.28658E-03   0.49658E+01 0.18155E+03 
c  Velocity[X]                                      0.18087E+01 
c  Velocity[Y]                                      0.31571E+01 
c  Velocity[Z]                                      0.73213E-30 
c  Pressure     0.10938E-06     504   0.98003E-08   0.10674E+00 0.63229E+03 
c  nu_tilda     0.69951E-05      33   0.40422E-05   0.55449E-06 0.19749E+03 
c  TempC        0.39958E+02      27   0.27569E-03   0.71782E+01 0.29087E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7791          10.006          4.5729          4.5729
v  Velocity[Y]            -2.9115          7.2816        0.096086        0.096086
v  Velocity[Z]       -1.1585e-014     6.3556e-015    -1.7316e-017    -1.7316e-017
v  ǁVelocityǁ         0.0020806          10.006          5.1356          5.1356
v  Pressure               -36.071          17.721         -10.712         -10.712
v  nu_tilda             4.42e-007       0.0042695       0.0015945       0.0015945
v  TempC                       21          73.048          21.982          21.982
v  TurbVisc           3.3588e-014       0.0050321       0.0018731       0.0018731
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1921:        0.21600E+01

===============================================================


 INSTANT    0.192200000E+04   TIME STEP NUMBER            1922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.96898E-02 0.89657E+00
   Friction velocity        uk    :  0.96898E-02 0.89657E+00
   Dimensionless distance   yplus :  0.78009E-01 0.72180E+01
   Friction thermal sca.    tstar : -0.64969E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58204E-01 0.53854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99196E-02      33   0.27630E-03   0.50148E+01 0.18179E+03 
c  Velocity[X]                                      0.18627E+01 
c  Velocity[Y]                                      0.31521E+01 
c  Velocity[Z]                                      0.91602E-30 
c  Pressure     0.10807E-06     520   0.96912E-08   0.10751E+00 0.93203E+03 
c  nu_tilda     0.69974E-05      33   0.15186E-04   0.55513E-06 0.19758E+03 
c  TempC        0.39966E+02      27   0.29384E-03   0.45699E+01 0.25275E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7761          10.005          4.5729          4.5729
v  Velocity[Y]            -2.9129          7.2533        0.096458        0.096458
v  Velocity[Z]       -1.1362e-014     6.4022e-015    -1.7319e-017    -1.7319e-017
v  ǁVelocityǁ         0.0019221          10.005          5.1356          5.1356
v  Pressure               -36.037           17.58         -10.749         -10.749
v  nu_tilda           4.4204e-007       0.0042695       0.0015948       0.0015948
v  TempC                       21          73.047          21.982          21.982
v  TurbVisc           3.3577e-014       0.0050321       0.0018736       0.0018736
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1922:        0.21870E+01

===============================================================


 INSTANT    0.192300000E+04   TIME STEP NUMBER            1923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.79920E-02 0.89512E+00
   Friction velocity        uk    :  0.79920E-02 0.89512E+00
   Dimensionless distance   yplus :  0.64341E-01 0.72063E+01
   Friction thermal sca.    tstar : -0.64875E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48006E-01 0.53767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99217E-02      33   0.26516E-03   0.49848E+01 0.18176E+03 
c  Velocity[X]                                      0.18128E+01 
c  Velocity[Y]                                      0.31719E+01 
c  Velocity[Z]                                      0.10426E-29 
c  Pressure     0.92315E-07     536   0.95487E-08   0.90647E-01 0.12674E+04 
c  nu_tilda     0.69998E-05      33   0.40448E-05   0.55573E-06 0.19767E+03 
c  TempC        0.39974E+02      27   0.35155E-03   0.43235E+01 0.24181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7734          10.004          4.5729          4.5729
v  Velocity[Y]            -2.9141          7.2742         0.09683         0.09683
v  Velocity[Z]       -1.1179e-014     6.4633e-015    -1.7333e-017    -1.7333e-017
v  ǁVelocityǁ         0.0021002          10.004          5.1357          5.1357
v  Pressure               -36.009          17.777         -10.689         -10.689
v  nu_tilda           4.4204e-007       0.0042695       0.0015953       0.0015953
v  TempC                       21          73.048          21.982          21.982
v  TurbVisc            3.359e-014       0.0050321       0.0018741       0.0018741
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1923:        0.22280E+01

===============================================================


 INSTANT    0.192400000E+04   TIME STEP NUMBER            1924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10224E-01 0.89603E+00
   Friction velocity        uk    :  0.10224E-01 0.89603E+00
   Dimensionless distance   yplus :  0.82308E-01 0.72136E+01
   Friction thermal sca.    tstar : -0.63665E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61411E-01 0.53822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99239E-02      33   0.28129E-03   0.49840E+01 0.18174E+03 
c  Velocity[X]                                      0.18273E+01 
c  Velocity[Y]                                      0.31567E+01 
c  Velocity[Z]                                      0.81053E-30 
c  Pressure     0.11713E-06     569   0.98852E-08   0.11444E+00 0.13596E+04 
c  nu_tilda     0.70021E-05      33   0.15183E-04   0.55638E-06 0.19776E+03 
c  TempC        0.39982E+02      27   0.31730E-03   0.67225E+01 0.27571E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7706          10.003          4.5729          4.5729
v  Velocity[Y]            -2.9152          7.2462        0.097203        0.097203
v  Velocity[Z]       -1.1012e-014      6.295e-015    -1.7336e-017    -1.7336e-017
v  ǁVelocityǁ         0.0018742          10.003          5.1357          5.1357
v  Pressure               -35.975          17.553         -10.746         -10.746
v  nu_tilda           4.4209e-007       0.0042695       0.0015957       0.0015957
v  TempC                       21          73.046          21.982          21.982
v  TurbVisc            3.359e-014       0.0050321       0.0018746       0.0018746
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1924:        0.23260E+01

===============================================================


 INSTANT    0.192500000E+04   TIME STEP NUMBER            1925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75210E-02 0.89541E+00
   Friction velocity        uk    :  0.75210E-02 0.89541E+00
   Dimensionless distance   yplus :  0.60549E-01 0.72086E+01
   Friction thermal sca.    tstar : -0.65601E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45177E-01 0.53785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99260E-02      33   0.25964E-03   0.49995E+01 0.18188E+03 
c  Velocity[X]                                      0.18480E+01 
c  Velocity[Y]                                      0.31516E+01 
c  Velocity[Z]                                      0.86952E-30 
c  Pressure     0.10340E-06     553   0.97847E-08   0.10139E+00 0.15157E+04 
c  nu_tilda     0.70045E-05      33   0.40662E-05   0.55696E-06 0.19785E+03 
c  TempC        0.39990E+02      27   0.30455E-03   0.45580E+01 0.25626E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7677          10.002          4.5729          4.5729
v  Velocity[Y]            -2.9163          7.2737        0.097577        0.097577
v  Velocity[Z]       -1.0601e-014     6.3471e-015    -1.7346e-017    -1.7346e-017
v  ǁVelocityǁ          0.002093          10.002          5.1357          5.1357
v  Pressure               -35.942            17.8         -10.671         -10.671
v  nu_tilda           4.4209e-007       0.0042695       0.0015962       0.0015962
v  TempC                       21          73.047          21.983          21.983
v  TurbVisc           3.3606e-014       0.0050321       0.0018751       0.0018751
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1925:        0.25240E+01

===============================================================


 INSTANT    0.192600000E+04   TIME STEP NUMBER            1926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95747E-02 0.89656E+00
   Friction velocity        uk    :  0.95747E-02 0.89656E+00
   Dimensionless distance   yplus :  0.77083E-01 0.72179E+01
   Friction thermal sca.    tstar : -0.63387E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57513E-01 0.53854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99281E-02      33   0.28299E-03   0.49856E+01 0.18188E+03 
c  Velocity[X]                                      0.18166E+01 
c  Velocity[Y]                                      0.31691E+01 
c  Velocity[Z]                                      0.82048E-30 
c  Pressure     0.96469E-07     488   0.99531E-08   0.94974E-01 0.63552E+03 
c  nu_tilda     0.70068E-05      33   0.15172E-04   0.55760E-06 0.19794E+03 
c  TempC        0.39999E+02      27   0.26372E-03   0.62212E+01 0.27574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7647          10.001          4.5729          4.5729
v  Velocity[Y]            -2.9172          7.2807         0.09795         0.09795
v  Velocity[Z]       -1.0417e-014     6.3723e-015    -1.7344e-017    -1.7344e-017
v  ǁVelocityǁ         0.0020912          10.002          5.1357          5.1357
v  Pressure               -35.911          17.728         -10.696         -10.696
v  nu_tilda           4.4202e-007       0.0042695       0.0015966       0.0015966
v  TempC                       21          73.047          21.983          21.983
v  TurbVisc           3.3606e-014       0.0050321       0.0018757       0.0018757
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1926:        0.21180E+01

===============================================================


 INSTANT    0.192700000E+04   TIME STEP NUMBER            1927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71267E-02 0.89615E+00
   Friction velocity        uk    :  0.71267E-02 0.89615E+00
   Dimensionless distance   yplus :  0.57375E-01 0.72146E+01
   Friction thermal sca.    tstar : -0.63072E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42808E-01 0.53829E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99303E-02      33   0.26975E-03   0.49987E+01 0.18191E+03 
c  Velocity[X]                                      0.18396E+01 
c  Velocity[Y]                                      0.31592E+01 
c  Velocity[Z]                                      0.65168E-30 
c  Pressure     0.12795E-06     424   0.94216E-08   0.12523E+00 0.44420E+03 
c  nu_tilda     0.70092E-05      33   0.40762E-05   0.55820E-06 0.19803E+03 
c  TempC        0.40007E+02      27   0.37240E-03   0.51804E+01 0.25218E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7618              10          4.5729          4.5729
v  Velocity[Y]            -2.9184           7.249        0.098325        0.098325
v  Velocity[Z]       -1.0416e-014     6.1962e-015    -1.7354e-017    -1.7354e-017
v  ǁVelocityǁ         0.0019674          10.001          5.1357          5.1357
v  Pressure                -35.88          17.681         -10.687         -10.687
v  nu_tilda           4.4201e-007       0.0042695       0.0015971       0.0015971
v  TempC                       21          73.048          21.983          21.983
v  TurbVisc           3.3584e-014       0.0050321       0.0018762       0.0018762
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1927:        0.19710E+01

===============================================================


 INSTANT    0.192800000E+04   TIME STEP NUMBER            1928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.67945E-02 0.89483E+00
   Friction velocity        uk    :  0.67945E-02 0.89483E+00
   Dimensionless distance   yplus :  0.54700E-01 0.72040E+01
   Friction thermal sca.    tstar : -0.64524E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40813E-01 0.53750E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99324E-02      33   0.27485E-03   0.49897E+01 0.18189E+03 
c  Velocity[X]                                      0.18382E+01 
c  Velocity[Y]                                      0.31515E+01 
c  Velocity[Z]                                      0.87178E-30 
c  Pressure     0.10437E-06     393   0.92649E-08   0.10275E+00 0.39642E+03 
c  nu_tilda     0.70115E-05      33   0.15175E-04   0.55885E-06 0.19812E+03 
c  TempC        0.40015E+02      27   0.32375E-03   0.70431E+01 0.30277E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.759          9.9993          4.5729          4.5729
v  Velocity[Y]            -2.9197            7.27        0.098698        0.098698
v  Velocity[Z]       -1.0531e-014     6.4674e-015    -1.7356e-017    -1.7356e-017
v  ǁVelocityǁ          0.002023          9.9996          5.1357          5.1357
v  Pressure               -35.846          17.743          -10.68          -10.68
v  nu_tilda             4.42e-007       0.0042695       0.0015974       0.0015974
v  TempC                       21          73.047          21.983          21.983
v  TurbVisc           3.3582e-014       0.0050321       0.0018767       0.0018767
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1928:        0.19280E+01

===============================================================


 INSTANT    0.192900000E+04   TIME STEP NUMBER            1929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10121E-01 0.89598E+00
   Friction velocity        uk    :  0.10121E-01 0.89598E+00
   Dimensionless distance   yplus :  0.81482E-01 0.72132E+01
   Friction thermal sca.    tstar : -0.67848E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60794E-01 0.53819E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99346E-02      33   0.27251E-03   0.49877E+01 0.18200E+03 
c  Velocity[X]                                      0.18156E+01 
c  Velocity[Y]                                      0.31721E+01 
c  Velocity[Z]                                      0.11002E-29 
c  Pressure     0.10533E-06     456   0.95981E-08   0.10513E+00 0.46245E+03 
c  nu_tilda     0.70138E-05      33   0.40831E-05   0.55944E-06 0.19821E+03 
c  TempC        0.40023E+02      27   0.34083E-03   0.52594E+01 0.25863E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7562          9.9984          4.5729          4.5729
v  Velocity[Y]            -2.9209          7.2493        0.099074        0.099074
v  Velocity[Z]       -1.0798e-014     6.2416e-015    -1.7367e-017    -1.7367e-017
v  ǁVelocityǁ         0.0019803          9.9986          5.1357          5.1357
v  Pressure               -35.812          17.715         -10.666         -10.666
v  nu_tilda           4.4204e-007       0.0042695       0.0015979       0.0015979
v  TempC                       21          73.047          21.984          21.984
v  TurbVisc           3.3579e-014       0.0050321       0.0018772       0.0018772
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1929:        0.23280E+01

===============================================================


 INSTANT    0.193000000E+04   TIME STEP NUMBER            1930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46661E-02 0.89506E+00
   Friction velocity        uk    :  0.46661E-02 0.89506E+00
   Dimensionless distance   yplus :  0.37565E-01 0.72058E+01
   Friction thermal sca.    tstar : -0.65921E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28028E-01 0.53764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99367E-02      33   0.22726E-03   0.49758E+01 0.18191E+03 
c  Velocity[X]                                      0.18186E+01 
c  Velocity[Y]                                      0.31572E+01 
c  Velocity[Z]                                      0.97819E-30 
c  Pressure     0.11363E-06     314   0.98444E-08   0.10996E+00 0.39229E+03 
c  nu_tilda     0.70162E-05      33   0.15166E-04   0.56008E-06 0.19829E+03 
c  TempC        0.40031E+02      27   0.28675E-03   0.55194E+01 0.26893E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7532          9.9974          4.5729          4.5729
v  Velocity[Y]             -2.922          7.2687         0.09945         0.09945
v  Velocity[Z]       -1.0997e-014     6.0925e-015    -1.7367e-017    -1.7367e-017
v  ǁVelocityǁ         0.0020044          9.9976          5.1357          5.1357
v  Pressure               -35.774          17.741         -10.663         -10.663
v  nu_tilda           4.4204e-007       0.0042695       0.0015983       0.0015983
v  TempC                       21          73.046          21.984          21.984
v  TurbVisc           3.3591e-014       0.0050321       0.0018777       0.0018777
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1930:        0.18090E+01

===============================================================


 INSTANT    0.193100000E+04   TIME STEP NUMBER            1931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10249E-01 0.89668E+00
   Friction velocity        uk    :  0.10249E-01 0.89668E+00
   Dimensionless distance   yplus :  0.82508E-01 0.72189E+01
   Friction thermal sca.    tstar : -0.64209E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61560E-01 0.53861E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99388E-02      33   0.30078E-03   0.49717E+01 0.18196E+03 
c  Velocity[X]                                      0.18139E+01 
c  Velocity[Y]                                      0.31578E+01 
c  Velocity[Z]                                      0.81468E-30 
c  Pressure     0.10976E-06     521   0.93587E-08   0.10800E+00 0.90286E+03 
c  nu_tilda     0.70185E-05      33   0.41070E-05   0.56067E-06 0.19838E+03 
c  TempC        0.40039E+02      27   0.23911E-03   0.59497E+01 0.26506E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7503          9.9964          4.5729          4.5729
v  Velocity[Y]            -2.9231          7.2819        0.099825        0.099825
v  Velocity[Z]       -1.0814e-014     6.3312e-015    -1.7375e-017    -1.7375e-017
v  ǁVelocityǁ         0.0021153          9.9967          5.1357          5.1357
v  Pressure               -35.741          17.857         -10.618         -10.618
v  nu_tilda           4.4198e-007       0.0042695       0.0015988       0.0015988
v  TempC                       21          73.047          21.984          21.984
v  TurbVisc           3.3592e-014       0.0050321       0.0018782       0.0018782
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1931:        0.21860E+01

===============================================================


 INSTANT    0.193200000E+04   TIME STEP NUMBER            1932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35423E-02 0.89625E+00
   Friction velocity        uk    :  0.35423E-02 0.89625E+00
   Dimensionless distance   yplus :  0.28518E-01 0.72154E+01
   Friction thermal sca.    tstar : -0.63453E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21277E-01 0.53835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99410E-02      33   0.27204E-03   0.50121E+01 0.18219E+03 
c  Velocity[X]                                      0.18389E+01 
c  Velocity[Y]                                      0.31732E+01 
c  Velocity[Z]                                      0.89227E-30 
c  Pressure     0.11340E-06     522   0.92865E-08   0.11273E+00 0.10782E+04 
c  nu_tilda     0.70209E-05      33   0.15157E-04   0.56131E-06 0.19847E+03 
c  TempC        0.40047E+02      27   0.37518E-03   0.43783E+01 0.23119E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7475          9.9955          4.5729          4.5729
v  Velocity[Y]             -2.924          7.2518          0.1002          0.1002
v  Velocity[Z]       -1.0968e-014      6.288e-015    -1.7372e-017    -1.7372e-017
v  ǁVelocityǁ         0.0019285          9.9957          5.1357          5.1357
v  Pressure               -35.704          17.685         -10.659         -10.659
v  nu_tilda             4.42e-007       0.0042695       0.0015992       0.0015992
v  TempC                       21          73.047          21.984          21.984
v  TurbVisc           3.3571e-014       0.0050321       0.0018787       0.0018787
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1932:        0.21770E+01

===============================================================


 INSTANT    0.193300000E+04   TIME STEP NUMBER            1933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73359E-02 0.89480E+00
   Friction velocity        uk    :  0.73359E-02 0.89480E+00
   Dimensionless distance   yplus :  0.59059E-01 0.72038E+01
   Friction thermal sca.    tstar : -0.64950E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44065E-01 0.53748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99431E-02      33   0.27175E-03   0.49840E+01 0.18207E+03 
c  Velocity[X]                                      0.18203E+01 
c  Velocity[Y]                                      0.31637E+01 
c  Velocity[Z]                                      0.75059E-30 
c  Pressure     0.10569E-06     538   0.99351E-08   0.10306E+00 0.11222E+04 
c  nu_tilda     0.70232E-05      33   0.41125E-05   0.56190E-06 0.19856E+03 
c  TempC        0.40055E+02      27   0.33275E-03   0.56651E+01 0.28419E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7448          9.9945          4.5729          4.5729
v  Velocity[Y]             -2.925          7.2684         0.10058         0.10058
v  Velocity[Z]       -1.0987e-014     6.3219e-015    -1.7379e-017    -1.7379e-017
v  ǁVelocityǁ         0.0020677          9.9948          5.1357          5.1357
v  Pressure               -35.672           17.85         -10.604         -10.604
v  nu_tilda           4.4205e-007       0.0042695       0.0015997       0.0015997
v  TempC                       21          73.048          21.985          21.985
v  TurbVisc           3.3579e-014       0.0050321       0.0018792       0.0018792
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1933:        0.22340E+01

===============================================================


 INSTANT    0.193400000E+04   TIME STEP NUMBER            1934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82584E-02 0.89589E+00
   Friction velocity        uk    :  0.82584E-02 0.89589E+00
   Dimensionless distance   yplus :  0.66486E-01 0.72125E+01
   Friction thermal sca.    tstar : -0.63747E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49606E-01 0.53813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99453E-02      33   0.28598E-03   0.50018E+01 0.18215E+03 
c  Velocity[X]                                      0.18446E+01 
c  Velocity[Y]                                      0.31571E+01 
c  Velocity[Z]                                      0.82890E-30 
c  Pressure     0.98995E-07     505   0.97113E-08   0.98407E-01 0.92838E+03 
c  nu_tilda     0.70255E-05      33   0.15157E-04   0.56254E-06 0.19865E+03 
c  TempC        0.40063E+02      27   0.31288E-03   0.53060E+01 0.26222E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7418          9.9935          4.5729          4.5729
v  Velocity[Y]            -2.9264          7.2459         0.10096         0.10096
v  Velocity[Z]       -1.1293e-014     6.3696e-015    -1.7377e-017    -1.7377e-017
v  ǁVelocityǁ         0.0019148          9.9938          5.1357          5.1357
v  Pressure               -35.634          17.711         -10.637         -10.637
v  nu_tilda           4.4213e-007       0.0042695          0.0016          0.0016
v  TempC                       21          73.047          21.985          21.985
v  TurbVisc           3.3593e-014       0.0050321       0.0018797       0.0018797
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1934:        0.21500E+01

===============================================================


 INSTANT    0.193500000E+04   TIME STEP NUMBER            1935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87182E-02 0.89509E+00
   Friction velocity        uk    :  0.87182E-02 0.89509E+00
   Dimensionless distance   yplus :  0.70187E-01 0.72061E+01
   Friction thermal sca.    tstar : -0.69584E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52368E-01 0.53766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99474E-02      33   0.25852E-03   0.49873E+01 0.18221E+03 
c  Velocity[X]                                      0.18132E+01 
c  Velocity[Y]                                      0.31741E+01 
c  Velocity[Z]                                      0.10702E-29 
c  Pressure     0.96955E-07     536   0.96361E-08   0.94343E-01 0.12701E+04 
c  nu_tilda     0.70279E-05      33   0.41220E-05   0.56313E-06 0.19873E+03 
c  TempC        0.40071E+02      27   0.35402E-03   0.42273E+01 0.24264E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7389          9.9925          4.5729          4.5729
v  Velocity[Y]            -2.9276          7.2711         0.10133         0.10133
v  Velocity[Z]       -1.1224e-014     6.2011e-015    -1.7386e-017    -1.7386e-017
v  ǁVelocityǁ         0.0021176          9.9928          5.1357          5.1357
v  Pressure               -35.602          17.909         -10.575         -10.575
v  nu_tilda           4.4214e-007       0.0042695       0.0016005       0.0016005
v  TempC                       21          73.048          21.985          21.985
v  TurbVisc           3.3618e-014       0.0050321       0.0018802       0.0018802
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1935:        0.22210E+01

===============================================================


 INSTANT    0.193600000E+04   TIME STEP NUMBER            1936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10651E-01 0.89623E+00
   Friction velocity        uk    :  0.10651E-01 0.89623E+00
   Dimensionless distance   yplus :  0.85747E-01 0.72153E+01
   Friction thermal sca.    tstar : -0.75615E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63977E-01 0.53834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99495E-02      33   0.27626E-03   0.49577E+01 0.18205E+03 
c  Velocity[X]                                      0.17977E+01 
c  Velocity[Y]                                      0.31600E+01 
c  Velocity[Z]                                      0.76414E-30 
c  Pressure     0.10564E-06     490   0.92788E-08   0.10252E+00 0.69945E+03 
c  nu_tilda     0.70302E-05      33   0.15147E-04   0.56377E-06 0.19882E+03 
c  TempC        0.40079E+02      27   0.34250E-03   0.49094E+01 0.24315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.736          9.9916          4.5729          4.5729
v  Velocity[Y]            -2.9287          7.2736         0.10171         0.10171
v  Velocity[Z]       -1.1215e-014     6.2637e-015    -1.7382e-017    -1.7382e-017
v  ǁVelocityǁ         0.0020766          9.9918          5.1357          5.1357
v  Pressure               -35.563          17.824         -10.597         -10.597
v  nu_tilda           4.4208e-007       0.0042695       0.0016009       0.0016009
v  TempC                       21          73.047          21.985          21.985
v  TurbVisc           3.3621e-014       0.0050321       0.0018808       0.0018808
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1936:        0.21130E+01

===============================================================


 INSTANT    0.193700000E+04   TIME STEP NUMBER            1937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11028E-01 0.89601E+00
   Friction velocity        uk    :  0.11028E-01 0.89601E+00
   Dimensionless distance   yplus :  0.88786E-01 0.72135E+01
   Friction thermal sca.    tstar : -0.89020E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66244E-01 0.53821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99517E-02      33   0.29394E-03   0.49986E+01 0.18229E+03 
c  Velocity[X]                                      0.18400E+01 
c  Velocity[Y]                                      0.31586E+01 
c  Velocity[Z]                                      0.89755E-30 
c  Pressure     0.11153E-06     457   0.95929E-08   0.11157E+00 0.46959E+03 
c  nu_tilda     0.70325E-05      33   0.41429E-05   0.56436E-06 0.19891E+03 
c  TempC        0.40087E+02      27   0.29280E-03   0.52108E+01 0.24387E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7331          9.9906          4.5729          4.5729
v  Velocity[Y]            -2.9297          7.2493         0.10209         0.10209
v  Velocity[Z]         -1.11e-014     6.1376e-015    -1.7388e-017    -1.7388e-017
v  ǁVelocityǁ         0.0019816          9.9909          5.1358          5.1358
v  Pressure               -35.531          17.813         -10.579         -10.579
v  nu_tilda           4.4203e-007       0.0042695       0.0016014       0.0016014
v  TempC                       21          73.048          21.986          21.986
v  TurbVisc           3.3603e-014       0.0050321       0.0018813       0.0018813
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1937:        0.20420E+01

===============================================================


 INSTANT    0.193800000E+04   TIME STEP NUMBER            1938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72965E-02 0.89462E+00
   Friction velocity        uk    :  0.72965E-02 0.89462E+00
   Dimensionless distance   yplus :  0.58742E-01 0.72023E+01
   Friction thermal sca.    tstar : -0.12521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43828E-01 0.53737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99538E-02      33   0.27457E-03   0.49986E+01 0.18236E+03 
c  Velocity[X]                                      0.18243E+01 
c  Velocity[Y]                                      0.31743E+01 
c  Velocity[Z]                                      0.97165E-30 
c  Pressure     0.10129E-06     360   0.94986E-08   0.98765E-01 0.39946E+03 
c  nu_tilda     0.70349E-05      33   0.15143E-04   0.56500E-06 0.19900E+03 
c  TempC        0.40095E+02      27   0.41013E-03   0.49003E+01 0.25763E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7303          9.9896          4.5729          4.5729
v  Velocity[Y]            -2.9305          7.2676         0.10247         0.10247
v  Velocity[Z]       -1.1311e-014     6.3612e-015    -1.7387e-017    -1.7387e-017
v  ǁVelocityǁ         0.0020355          9.9899          5.1358          5.1358
v  Pressure               -35.492          17.853         -10.575         -10.575
v  nu_tilda           4.4198e-007       0.0042695       0.0016018       0.0016018
v  TempC                       21          73.048          21.986          21.986
v  TurbVisc           3.3586e-014       0.0050321       0.0018818       0.0018818
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1938:        0.18150E+01

===============================================================


 INSTANT    0.193900000E+04   TIME STEP NUMBER            1939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70313E-02 0.89573E+00
   Friction velocity        uk    :  0.70313E-02 0.89573E+00
   Dimensionless distance   yplus :  0.56607E-01 0.72112E+01
   Friction thermal sca.    tstar : -0.22834E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42235E-01 0.53804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99559E-02      33   0.27683E-03   0.49950E+01 0.18231E+03 
c  Velocity[X]                                      0.18278E+01 
c  Velocity[Y]                                      0.31672E+01 
c  Velocity[Z]                                      0.73428E-30 
c  Pressure     0.13026E-06     474   0.95225E-08   0.12779E+00 0.55841E+03 
c  nu_tilda     0.70372E-05      33   0.41466E-05   0.56559E-06 0.19908E+03 
c  TempC        0.40103E+02      27   0.31050E-03   0.68694E+01 0.29943E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7274          9.9886          4.5729          4.5729
v  Velocity[Y]            -2.9315          7.2422         0.10285         0.10285
v  Velocity[Z]       -1.1133e-014     6.3225e-015    -1.7393e-017    -1.7393e-017
v  ǁVelocityǁ         0.0019772           9.989          5.1358          5.1358
v  Pressure               -35.455          17.845         -10.549         -10.549
v  nu_tilda           4.4198e-007       0.0042695       0.0016023       0.0016023
v  TempC                       21          73.048          21.986          21.986
v  TurbVisc           3.3572e-014       0.0050321       0.0018823       0.0018823
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1939:        0.20670E+01

===============================================================


 INSTANT    0.194000000E+04   TIME STEP NUMBER            1940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75811E-02 0.89501E+00
   Friction velocity        uk    :  0.75811E-02 0.89501E+00
   Dimensionless distance   yplus :  0.61033E-01 0.72054E+01
   Friction thermal sca.    tstar : -0.18753E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45538E-01 0.53760E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99581E-02      33   0.22725E-03   0.49973E+01 0.18234E+03 
c  Velocity[X]                                      0.18381E+01 
c  Velocity[Y]                                      0.31592E+01 
c  Velocity[Z]                                      0.80431E-30 
c  Pressure     0.96227E-07     280   0.96151E-08   0.94196E-01 0.39702E+03 
c  nu_tilda     0.70396E-05      33   0.15143E-04   0.56623E-06 0.19917E+03 
c  TempC        0.40111E+02      27   0.22302E-03   0.52542E+01 0.25429E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7245          9.9877          4.5729          4.5729
v  Velocity[Y]            -2.9328          7.2683         0.10323         0.10323
v  Velocity[Z]       -1.0985e-014     6.4275e-015    -1.7392e-017    -1.7392e-017
v  ǁVelocityǁ         0.0020439           9.988          5.1358          5.1358
v  Pressure               -35.417          17.881         -10.549         -10.549
v  nu_tilda           4.4194e-007       0.0042695       0.0016026       0.0016026
v  TempC                       21          73.048          21.986          21.986
v  TurbVisc           3.3571e-014       0.0050321       0.0018828       0.0018828
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1940:        0.16490E+01

===============================================================


 INSTANT    0.194100000E+04   TIME STEP NUMBER            1941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10771E-01 0.89660E+00
   Friction velocity        uk    :  0.10771E-01 0.89660E+00
   Dimensionless distance   yplus :  0.86710E-01 0.72183E+01
   Friction thermal sca.    tstar : -0.11049E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64696E-01 0.53856E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99602E-02      33   0.26067E-03   0.49680E+01 0.18232E+03 
c  Velocity[X]                                      0.17888E+01 
c  Velocity[Y]                                      0.31792E+01 
c  Velocity[Z]                                      0.95261E-30 
c  Pressure     0.98947E-07     521   0.94493E-08   0.98010E-01 0.98070E+03 
c  nu_tilda     0.70419E-05      33   0.41612E-05   0.56681E-06 0.19926E+03 
c  TempC        0.40119E+02      27   0.32681E-03   0.30328E+01 0.20716E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7217          9.9867          4.5729          4.5729
v  Velocity[Y]             -2.934          7.2796          0.1036          0.1036
v  Velocity[Z]       -1.0756e-014     6.3258e-015      -1.74e-017      -1.74e-017
v  ǁVelocityǁ         0.0021504           9.987          5.1358          5.1358
v  Pressure                -35.38          18.002         -10.497         -10.497
v  nu_tilda           4.4188e-007       0.0042695       0.0016031       0.0016031
v  TempC                       21          73.048          21.987          21.987
v  TurbVisc           3.3559e-014       0.0050321       0.0018833       0.0018833
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1941:        0.21940E+01

===============================================================


 INSTANT    0.194200000E+04   TIME STEP NUMBER            1942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10910E-01 0.89607E+00
   Friction velocity        uk    :  0.10910E-01 0.89607E+00
   Dimensionless distance   yplus :  0.87834E-01 0.72140E+01
   Friction thermal sca.    tstar : -0.86267E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65534E-01 0.53824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99623E-02      33   0.27252E-03   0.49869E+01 0.18237E+03 
c  Velocity[X]                                      0.18220E+01 
c  Velocity[Y]                                      0.31649E+01 
c  Velocity[Z]                                      0.82336E-30 
c  Pressure     0.11110E-06     536   0.95379E-08   0.10912E+00 0.12629E+04 
c  nu_tilda     0.70442E-05      33   0.15131E-04   0.56745E-06 0.19935E+03 
c  TempC        0.40127E+02      27   0.33969E-03   0.43093E+01 0.24506E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7189          9.9857          4.5729          4.5729
v  Velocity[Y]            -2.9351          7.2456         0.10398         0.10398
v  Velocity[Z]       -1.0584e-014     6.2738e-015    -1.7404e-017    -1.7404e-017
v  ǁVelocityǁ         0.0019128           9.986          5.1358          5.1358
v  Pressure               -35.343          17.793         -10.548         -10.548
v  nu_tilda           4.4193e-007       0.0042695       0.0016035       0.0016035
v  TempC                       21          73.047          21.987          21.987
v  TurbVisc           3.3543e-014       0.0050321       0.0018838       0.0018838
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1942:        0.22090E+01

===============================================================


 INSTANT    0.194300000E+04   TIME STEP NUMBER            1943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64491E-02 0.89479E+00
   Friction velocity        uk    :  0.64491E-02 0.89479E+00
   Dimensionless distance   yplus :  0.51920E-01 0.72037E+01
   Friction thermal sca.    tstar : -0.77324E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38738E-01 0.53747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99644E-02      33   0.29901E-03   0.49880E+01 0.18245E+03 
c  Velocity[X]                                      0.18254E+01 
c  Velocity[Y]                                      0.31626E+01 
c  Velocity[Z]                                      0.88877E-30 
c  Pressure     0.10616E-06     536   0.93942E-08   0.10435E+00 0.13954E+04 
c  nu_tilda     0.70466E-05      33   0.41715E-05   0.56804E-06 0.19943E+03 
c  TempC        0.40136E+02      27   0.30667E-03   0.47824E+01 0.24841E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.716          9.9847          4.5729          4.5729
v  Velocity[Y]            -2.9361           7.269         0.10436         0.10436
v  Velocity[Z]       -1.0418e-014     6.3979e-015    -1.7406e-017    -1.7406e-017
v  ǁVelocityǁ         0.0021016          9.9851          5.1358          5.1358
v  Pressure               -35.308          18.009         -10.478         -10.478
v  nu_tilda            4.419e-007       0.0042695        0.001604        0.001604
v  TempC                       21          73.048          21.987          21.987
v  TurbVisc           3.3558e-014       0.0050321       0.0018843       0.0018843
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1943:        0.22590E+01

===============================================================


 INSTANT    0.194400000E+04   TIME STEP NUMBER            1944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10362E-01 0.89578E+00
   Friction velocity        uk    :  0.10362E-01 0.89578E+00
   Dimensionless distance   yplus :  0.83421E-01 0.72116E+01
   Friction thermal sca.    tstar : -0.66270E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62242E-01 0.53807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99666E-02      33   0.28117E-03   0.50109E+01 0.18261E+03 
c  Velocity[X]                                      0.18314E+01 
c  Velocity[Y]                                      0.31795E+01 
c  Velocity[Z]                                      0.90545E-30 
c  Pressure     0.11045E-06     490   0.98783E-08   0.10942E+00 0.10212E+04 
c  nu_tilda     0.70489E-05      33   0.15130E-04   0.56867E-06 0.19952E+03 
c  TempC        0.40144E+02      27   0.28446E-03   0.44620E+01 0.23753E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7131          9.9838          4.5729          4.5729
v  Velocity[Y]            -2.9369          7.2441         0.10474         0.10474
v  Velocity[Z]       -1.0191e-014     6.3889e-015    -1.7414e-017    -1.7414e-017
v  ǁVelocityǁ         0.0019413          9.9841          5.1358          5.1358
v  Pressure               -35.264          17.855         -10.512         -10.512
v  nu_tilda           4.4189e-007       0.0042695       0.0016044       0.0016044
v  TempC                       21          73.048          21.987          21.987
v  TurbVisc           3.3547e-014       0.0050321       0.0018848       0.0018848
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1944:        0.21270E+01

===============================================================


 INSTANT    0.194500000E+04   TIME STEP NUMBER            1945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92748E-02 0.89487E+00
   Friction velocity        uk    :  0.92748E-02 0.89487E+00
   Dimensionless distance   yplus :  0.74668E-01 0.72043E+01
   Friction thermal sca.    tstar : -0.68893E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55711E-01 0.53752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99687E-02      33   0.21496E-03   0.49857E+01 0.18249E+03 
c  Velocity[X]                                      0.18201E+01 
c  Velocity[Y]                                      0.31656E+01 
c  Velocity[Z]                                      0.72086E-30 
c  Pressure     0.11559E-06     520   0.92901E-08   0.11135E+00 0.10778E+04 
c  nu_tilda     0.70512E-05      33   0.41794E-05   0.56926E-06 0.19961E+03 
c  TempC        0.40152E+02      27   0.29356E-03   0.46809E+01 0.24383E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7101          9.9828          4.5729          4.5729
v  Velocity[Y]            -2.9378          7.2656         0.10513         0.10513
v  Velocity[Z]       -9.9178e-015     6.1869e-015    -1.7415e-017    -1.7415e-017
v  ǁVelocityǁ         0.0020831          9.9831          5.1358          5.1358
v  Pressure                -35.23           18.01         -10.458         -10.458
v  nu_tilda           4.4189e-007       0.0042695       0.0016048       0.0016048
v  TempC                       21          73.048          21.988          21.988
v  TurbVisc           3.3544e-014       0.0050321       0.0018853       0.0018853
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1945:        0.21920E+01

===============================================================


 INSTANT    0.194600000E+04   TIME STEP NUMBER            1946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62034E-02 0.89627E+00
   Friction velocity        uk    :  0.62034E-02 0.89627E+00
   Dimensionless distance   yplus :  0.49941E-01 0.72156E+01
   Friction thermal sca.    tstar : -0.65068E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37262E-01 0.53836E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99708E-02      33   0.28151E-03   0.49756E+01 0.18246E+03 
c  Velocity[X]                                      0.18163E+01 
c  Velocity[Y]                                      0.31593E+01 
c  Velocity[Z]                                      0.84632E-30 
c  Pressure     0.98538E-07     361   0.95782E-08   0.97290E-01 0.43427E+03 
c  nu_tilda     0.70536E-05      33   0.15122E-04   0.56989E-06 0.19969E+03 
c  TempC        0.40160E+02      27   0.35806E-03   0.54379E+01 0.26062E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7074          9.9818          4.5729          4.5729
v  Velocity[Y]            -2.9391          7.2745         0.10551         0.10551
v  Velocity[Z]       -9.6854e-015     6.4426e-015    -1.7424e-017    -1.7424e-017
v  ǁVelocityǁ         0.0021228          9.9821          5.1358          5.1358
v  Pressure               -35.188          18.001         -10.458         -10.458
v  nu_tilda           4.4181e-007       0.0042695       0.0016052       0.0016052
v  TempC                       21          73.048          21.988          21.988
v  TurbVisc           3.3544e-014       0.0050321       0.0018859       0.0018859
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1946:        0.18240E+01

===============================================================


 INSTANT    0.194700000E+04   TIME STEP NUMBER            1947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88451E-02 0.89589E+00
   Friction velocity        uk    :  0.88451E-02 0.89589E+00
   Dimensionless distance   yplus :  0.71209E-01 0.72125E+01
   Friction thermal sca.    tstar : -0.63589E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53130E-01 0.53814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99729E-02      33   0.25913E-03   0.49959E+01 0.18265E+03 
c  Velocity[X]                                      0.18156E+01 
c  Velocity[Y]                                      0.31803E+01 
c  Velocity[Z]                                      0.90695E-30 
c  Pressure     0.11721E-06     425   0.92034E-08   0.11614E+00 0.45595E+03 
c  nu_tilda     0.70559E-05      33   0.42036E-05   0.57048E-06 0.19978E+03 
c  TempC        0.40168E+02      27   0.31011E-03   0.55779E+01 0.28507E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7045          9.9809          4.5729          4.5729
v  Velocity[Y]            -2.9403          7.2466         0.10589         0.10589
v  Velocity[Z]       -9.4666e-015     6.2972e-015    -1.7425e-017    -1.7425e-017
v  ǁVelocityǁ         0.0020053          9.9812          5.1358          5.1358
v  Pressure               -35.153          17.968         -10.445         -10.445
v  nu_tilda           4.4178e-007       0.0042695       0.0016057       0.0016057
v  TempC                       21          73.048          21.988          21.988
v  TurbVisc           3.3521e-014       0.0050321       0.0018864       0.0018864
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1947:        0.19680E+01

===============================================================


 INSTANT    0.194800000E+04   TIME STEP NUMBER            1948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.81280E-02 0.89429E+00
   Friction velocity        uk    :  0.81280E-02 0.89429E+00
   Dimensionless distance   yplus :  0.65436E-01 0.71997E+01
   Friction thermal sca.    tstar : -0.64339E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48822E-01 0.53718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99751E-02      33   0.27545E-03   0.49722E+01 0.18253E+03 
c  Velocity[X]                                      0.18085E+01 
c  Velocity[Y]                                      0.31638E+01 
c  Velocity[Z]                                      0.79334E-30 
c  Pressure     0.10486E-06     263   0.99572E-08   0.10105E+00 0.41633E+03 
c  nu_tilda     0.70583E-05      33   0.15116E-04   0.57111E-06 0.19987E+03 
c  TempC        0.40176E+02      27   0.35824E-03   0.52390E+01 0.26474E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7015          9.9799          4.5729          4.5729
v  Velocity[Y]            -2.9413          7.2614         0.10627         0.10627
v  Velocity[Z]        -9.286e-015     6.3553e-015    -1.7434e-017    -1.7434e-017
v  ǁVelocityǁ         0.0020052          9.9802          5.1359          5.1359
v  Pressure               -35.111          17.979         -10.442         -10.442
v  nu_tilda           4.4179e-007       0.0042695       0.0016061       0.0016061
v  TempC                       21          73.047          21.988          21.988
v  TurbVisc           3.3511e-014       0.0050321       0.0018869       0.0018869
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1948:        0.15950E+01

===============================================================


 INSTANT    0.194900000E+04   TIME STEP NUMBER            1949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71729E-02 0.89566E+00
   Friction velocity        uk    :  0.71729E-02 0.89566E+00
   Dimensionless distance   yplus :  0.57747E-01 0.72107E+01
   Friction thermal sca.    tstar : -0.64434E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43086E-01 0.53800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99772E-02      33   0.30506E-03   0.49958E+01 0.18268E+03 
c  Velocity[X]                                      0.18310E+01 
c  Velocity[Y]                                      0.31648E+01 
c  Velocity[Z]                                      0.11253E-29 
c  Pressure     0.11762E-06     504   0.96337E-08   0.11794E+00 0.72710E+03 
c  nu_tilda     0.70606E-05      33   0.42061E-05   0.57170E-06 0.19995E+03 
c  TempC        0.40184E+02      27   0.29949E-03   0.79232E+01 0.30852E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6986          9.9789          4.5729          4.5729
v  Velocity[Y]            -2.9423          7.2428         0.10665         0.10665
v  Velocity[Z]         -9.11e-015     6.1385e-015    -1.7445e-017    -1.7445e-017
v  ǁVelocityǁ         0.0020008          9.9793          5.1359          5.1359
v  Pressure               -35.071          18.025         -10.403         -10.403
v  nu_tilda           4.4182e-007       0.0042695       0.0016066       0.0016066
v  TempC                       21          73.047          21.989          21.989
v  TurbVisc           3.3514e-014       0.0050321       0.0018874       0.0018874
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1949:        0.21580E+01

===============================================================


 INSTANT    0.195000000E+04   TIME STEP NUMBER            1950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83016E-02 0.89479E+00
   Friction velocity        uk    :  0.83016E-02 0.89479E+00
   Dimensionless distance   yplus :  0.66833E-01 0.72037E+01
   Friction thermal sca.    tstar : -0.64516E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49865E-01 0.53748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99793E-02      33   0.22096E-03   0.50068E+01 0.18279E+03 
c  Velocity[X]                                      0.18244E+01 
c  Velocity[Y]                                      0.31824E+01 
c  Velocity[Z]                                      0.84549E-30 
c  Pressure     0.10638E-06     393   0.99747E-08   0.10389E+00 0.44780E+03 
c  nu_tilda     0.70629E-05      33   0.15115E-04   0.57234E-06 0.20004E+03 
c  TempC        0.40192E+02      27   0.32844E-03   0.52537E+01 0.26166E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6959          9.9779          4.5729          4.5729
v  Velocity[Y]            -2.9431          7.2668         0.10703         0.10703
v  Velocity[Z]       -8.8944e-015     6.2936e-015    -1.7448e-017    -1.7448e-017
v  ǁVelocityǁ         0.0020708          9.9783          5.1359          5.1359
v  Pressure               -35.031          18.035         -10.409         -10.409
v  nu_tilda            4.418e-007       0.0042695       0.0016069       0.0016069
v  TempC                       21          73.047          21.989          21.989
v  TurbVisc           3.3524e-014       0.0050321       0.0018879       0.0018879
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1950:        0.18940E+01

===============================================================


 INSTANT    0.195100000E+04   TIME STEP NUMBER            1951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11012E-01 0.89634E+00
   Friction velocity        uk    :  0.11012E-01 0.89634E+00
   Dimensionless distance   yplus :  0.88656E-01 0.72162E+01
   Friction thermal sca.    tstar : -0.63507E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66147E-01 0.53841E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99814E-02      33   0.26950E-03   0.49671E+01 0.18260E+03 
c  Velocity[X]                                      0.17989E+01 
c  Velocity[Y]                                      0.31682E+01 
c  Velocity[Z]                                      0.78871E-30 
c  Pressure     0.11682E-06     505   0.93390E-08   0.11249E+00 0.82825E+03 
c  nu_tilda     0.70653E-05      33   0.42186E-05   0.57291E-06 0.20012E+03 
c  TempC        0.40200E+02      27   0.31197E-03   0.55233E+01 0.26558E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.693          9.9769          4.5729          4.5729
v  Velocity[Y]            -2.9439           7.274         0.10741         0.10741
v  Velocity[Z]       -9.3042e-015     6.2225e-015    -1.7452e-017    -1.7452e-017
v  ǁVelocityǁ         0.0021083          9.9773          5.1359          5.1359
v  Pressure               -34.994          18.117         -10.364         -10.364
v  nu_tilda           4.4177e-007       0.0042695       0.0016074       0.0016074
v  TempC                       21          73.048          21.989          21.989
v  TurbVisc           3.3517e-014       0.0050321       0.0018884       0.0018884
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1951:        0.21500E+01

===============================================================


 INSTANT    0.195200000E+04   TIME STEP NUMBER            1952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.73937E-02 0.89606E+00
   Friction velocity        uk    :  0.73937E-02 0.89606E+00
   Dimensionless distance   yplus :  0.59525E-01 0.72139E+01
   Friction thermal sca.    tstar : -0.63524E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44412E-01 0.53824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99835E-02      33   0.27467E-03   0.50065E+01 0.18277E+03 
c  Velocity[X]                                      0.18436E+01 
c  Velocity[Y]                                      0.31629E+01 
c  Velocity[Z]                                      0.83559E-30 
c  Pressure     0.10526E-06     506   0.93279E-08   0.10518E+00 0.88917E+03 
c  nu_tilda     0.70676E-05      33   0.15106E-04   0.57355E-06 0.20021E+03 
c  TempC        0.40208E+02      27   0.28348E-03   0.58397E+01 0.27656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6901           9.976          4.5729          4.5729
v  Velocity[Y]            -2.9452          7.2457          0.1078          0.1078
v  Velocity[Z]       -9.2172e-015     6.4405e-015    -1.7455e-017    -1.7455e-017
v  ǁVelocityǁ         0.0019484          9.9763          5.1359          5.1359
v  Pressure               -34.953          17.985         -10.394         -10.394
v  nu_tilda           4.4183e-007       0.0042695       0.0016078       0.0016078
v  TempC                       21          73.047          21.989          21.989
v  TurbVisc           3.3508e-014       0.0050321       0.0018889       0.0018889
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1952:        0.21530E+01

===============================================================


 INSTANT    0.195300000E+04   TIME STEP NUMBER            1953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89219E-02 0.89465E+00
   Friction velocity        uk    :  0.89219E-02 0.89465E+00
   Dimensionless distance   yplus :  0.71827E-01 0.72026E+01
   Friction thermal sca.    tstar : -0.68841E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53591E-01 0.53739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99856E-02      33   0.26927E-03   0.49822E+01 0.18280E+03 
c  Velocity[X]                                      0.18002E+01 
c  Velocity[Y]                                      0.31819E+01 
c  Velocity[Z]                                      0.82926E-30 
c  Pressure     0.87656E-07     536   0.99420E-08   0.86103E-01 0.12505E+04 
c  nu_tilda     0.70699E-05      33   0.42337E-05   0.57413E-06 0.20029E+03 
c  TempC        0.40216E+02      27   0.34770E-03   0.42938E+01 0.23870E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6872           9.975          4.5729          4.5729
v  Velocity[Y]            -2.9463          7.2671         0.10818         0.10818
v  Velocity[Z]       -9.8054e-015     6.2304e-015     -1.746e-017     -1.746e-017
v  ǁVelocityǁ         0.0021387          9.9753          5.1359          5.1359
v  Pressure               -34.913          18.172         -10.329         -10.329
v  nu_tilda           4.4184e-007       0.0042695       0.0016083       0.0016083
v  TempC                       21          73.048           21.99           21.99
v  TurbVisc           3.3525e-014       0.0050321       0.0018894       0.0018894
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1953:        0.22310E+01

===============================================================


 INSTANT    0.195400000E+04   TIME STEP NUMBER            1954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10865E-01 0.89554E+00
   Friction velocity        uk    :  0.10865E-01 0.89554E+00
   Dimensionless distance   yplus :  0.87468E-01 0.72097E+01
   Friction thermal sca.    tstar : -0.64761E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65261E-01 0.53793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99878E-02      33   0.28582E-03   0.49806E+01 0.18275E+03 
c  Velocity[X]                                      0.18143E+01 
c  Velocity[Y]                                      0.31663E+01 
c  Velocity[Z]                                      0.76820E-30 
c  Pressure     0.11445E-06     488   0.96910E-08   0.11252E+00 0.10297E+04 
c  nu_tilda     0.70723E-05      33   0.15100E-04   0.57476E-06 0.20038E+03 
c  TempC        0.40224E+02      27   0.33576E-03   0.44897E+01 0.24703E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6843           9.974          4.5729          4.5729
v  Velocity[Y]            -2.9474          7.2386         0.10856         0.10856
v  Velocity[Z]       -1.0295e-014     6.4535e-015    -1.7464e-017    -1.7464e-017
v  ǁVelocityǁ         0.0019218          9.9744          5.1359          5.1359
v  Pressure               -34.865          18.006         -10.359         -10.359
v  nu_tilda           4.4188e-007       0.0042695       0.0016086       0.0016086
v  TempC                       21          73.047           21.99           21.99
v  TurbVisc           3.3529e-014       0.0050321       0.0018899       0.0018899
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1954:        0.21050E+01

===============================================================


 INSTANT    0.195500000E+04   TIME STEP NUMBER            1955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61582E-02 0.89487E+00
   Friction velocity        uk    :  0.61582E-02 0.89487E+00
   Dimensionless distance   yplus :  0.49577E-01 0.72043E+01
   Friction thermal sca.    tstar : -0.65097E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36990E-01 0.53752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99899E-02      33   0.29578E-03   0.49891E+01 0.18285E+03 
c  Velocity[X]                                      0.18244E+01 
c  Velocity[Y]                                      0.31647E+01 
c  Velocity[Z]                                      0.86204E-30 
c  Pressure     0.10577E-06     569   0.95297E-08   0.10323E+00 0.13443E+04 
c  nu_tilda     0.70746E-05      33   0.42383E-05   0.57534E-06 0.20046E+03 
c  TempC        0.40232E+02      27   0.31231E-03   0.49783E+01 0.25212E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6814           9.973          4.5729          4.5729
v  Velocity[Y]            -2.9483          7.2663         0.10894         0.10894
v  Velocity[Z]       -9.8597e-015     6.2538e-015    -1.7463e-017    -1.7463e-017
v  ǁVelocityǁ         0.0021264          9.9734          5.1359          5.1359
v  Pressure               -34.827          18.215         -10.291         -10.291
v  nu_tilda           4.4182e-007       0.0042695       0.0016091       0.0016091
v  TempC                       21          73.048           21.99           21.99
v  TurbVisc           3.3543e-014       0.0050321       0.0018904       0.0018904
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1955:        0.22980E+01

===============================================================


 INSTANT    0.195600000E+04   TIME STEP NUMBER            1956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61659E-02 0.89607E+00
   Friction velocity        uk    :  0.61659E-02 0.89607E+00
   Dimensionless distance   yplus :  0.49640E-01 0.72140E+01
   Friction thermal sca.    tstar : -0.63759E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37037E-01 0.53824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99920E-02      33   0.27045E-03   0.49843E+01 0.18289E+03 
c  Velocity[X]                                      0.18026E+01 
c  Velocity[Y]                                      0.31817E+01 
c  Velocity[Z]                                      0.73566E-30 
c  Pressure     0.10135E-06     362   0.97433E-08   0.99673E-01 0.49272E+03 
c  nu_tilda     0.70769E-05      33   0.15097E-04   0.57597E-06 0.20055E+03 
c  TempC        0.40240E+02      27   0.26924E-03   0.52647E+01 0.24796E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6786           9.972          4.5729          4.5729
v  Velocity[Y]            -2.9491          7.2722         0.10932         0.10932
v  Velocity[Z]       -1.0176e-014     6.3016e-015    -1.7466e-017    -1.7466e-017
v  ǁVelocityǁ         0.0021791          9.9724          5.1359          5.1359
v  Pressure                -34.78          18.191         -10.292         -10.292
v  nu_tilda            4.417e-007       0.0042695       0.0016095       0.0016095
v  TempC                       21          73.048           21.99           21.99
v  TurbVisc           3.3525e-014       0.0050321       0.0018909       0.0018909
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1956:        0.18170E+01

===============================================================


 INSTANT    0.195700000E+04   TIME STEP NUMBER            1957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11919E-01 0.89557E+00
   Friction velocity        uk    :  0.11919E-01 0.89557E+00
   Dimensionless distance   yplus :  0.95957E-01 0.72100E+01
   Friction thermal sca.    tstar : -0.63490E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71594E-01 0.53795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99941E-02      33   0.26251E-03   0.49955E+01 0.18292E+03 
c  Velocity[X]                                      0.18235E+01 
c  Velocity[Y]                                      0.31721E+01 
c  Velocity[Z]                                      0.87960E-30 
c  Pressure     0.12193E-06     295   0.86147E-08   0.11976E+00 0.53710E+03 
c  nu_tilda     0.70793E-05      33   0.42611E-05   0.57656E-06 0.20064E+03 
c  TempC        0.40248E+02      27   0.29183E-03   0.46812E+01 0.24556E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6757           9.971          4.5729          4.5729
v  Velocity[Y]            -2.9498          7.2417         0.10971         0.10971
v  Velocity[Z]       -1.0101e-014     6.2645e-015    -1.7463e-017    -1.7463e-017
v  ǁVelocityǁ          0.001975          9.9714          5.1359          5.1359
v  Pressure               -34.742          18.102         -10.288         -10.288
v  nu_tilda           4.4171e-007       0.0042695         0.00161         0.00161
v  TempC                       21          73.048          21.991          21.991
v  TurbVisc           3.3488e-014       0.0050321       0.0018914       0.0018914
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1957:        0.16620E+01

===============================================================


 INSTANT    0.195800000E+04   TIME STEP NUMBER            1958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70679E-02 0.89434E+00
   Friction velocity        uk    :  0.70679E-02 0.89434E+00
   Dimensionless distance   yplus :  0.56901E-01 0.72001E+01
   Friction thermal sca.    tstar : -0.67219E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42455E-01 0.53721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99962E-02      33   0.27069E-03   0.49873E+01 0.18289E+03 
c  Velocity[X]                                      0.18247E+01 
c  Velocity[Y]                                      0.31626E+01 
c  Velocity[Z]                                      0.94010E-30 
c  Pressure     0.99078E-07     442   0.97529E-08   0.97043E-01 0.56350E+03 
c  nu_tilda     0.70816E-05      33   0.15089E-04   0.57718E-06 0.20072E+03 
c  TempC        0.40256E+02      27   0.34812E-03   0.41877E+01 0.23933E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6728          9.9701          4.5729          4.5729
v  Velocity[Y]            -2.9511           7.262         0.11009         0.11009
v  Velocity[Z]       -1.0177e-014       6.24e-015    -1.7461e-017    -1.7461e-017
v  ǁVelocityǁ         0.0020581          9.9704          5.1359          5.1359
v  Pressure               -34.697          18.199         -10.265         -10.265
v  nu_tilda           4.4178e-007       0.0042695       0.0016104       0.0016104
v  TempC                       21          73.047          21.991          21.991
v  TurbVisc           3.3491e-014       0.0050321       0.0018919       0.0018919
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1958:        0.20040E+01

===============================================================


 INSTANT    0.195900000E+04   TIME STEP NUMBER            1959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10605E-01 0.89547E+00
   Friction velocity        uk    :  0.10605E-01 0.89547E+00
   Dimensionless distance   yplus :  0.85374E-01 0.72091E+01
   Friction thermal sca.    tstar : -0.75175E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63699E-01 0.53788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99983E-02      33   0.26755E-03   0.49912E+01 0.18300E+03 
c  Velocity[X]                                      0.18043E+01 
c  Velocity[Y]                                      0.31870E+01 
c  Velocity[Z]                                      0.82118E-30 
c  Pressure     0.11270E-06     474   0.99205E-08   0.11193E+00 0.52300E+03 
c  nu_tilda     0.70839E-05      33   0.42691E-05   0.57776E-06 0.20080E+03 
c  TempC        0.40263E+02      27   0.29503E-03   0.62068E+01 0.28744E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.67          9.9691          4.5729          4.5729
v  Velocity[Y]            -2.9522          7.2406         0.11047         0.11047
v  Velocity[Z]       -9.8736e-015     6.3127e-015    -1.7465e-017    -1.7465e-017
v  ǁVelocityǁ         0.0020118          9.9695          5.1359          5.1359
v  Pressure               -34.659          18.191         -10.241         -10.241
v  nu_tilda           4.4186e-007       0.0042695       0.0016108       0.0016108
v  TempC                       21          73.048          21.991          21.991
v  TurbVisc           3.3511e-014       0.0050321       0.0018924       0.0018924
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1959:        0.21790E+01

===============================================================


 INSTANT    0.196000000E+04   TIME STEP NUMBER            1960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.40465E-02 0.89454E+00
   Friction velocity        uk    :  0.40465E-02 0.89454E+00
   Dimensionless distance   yplus :  0.32577E-01 0.72016E+01
   Friction thermal sca.    tstar : -0.94576E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24306E-01 0.53732E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10000E-01      33   0.22607E-03   0.49763E+01 0.18291E+03 
c  Velocity[X]                                      0.18056E+01 
c  Velocity[Y]                                      0.31708E+01 
c  Velocity[Z]                                      0.74694E-30 
c  Pressure     0.11004E-06     330   0.99480E-08   0.10629E+00 0.44597E+03 
c  nu_tilda     0.70862E-05      33   0.15086E-04   0.57838E-06 0.20089E+03 
c  TempC        0.40271E+02      27   0.36356E-03   0.56402E+01 0.25742E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6672          9.9681          4.5729          4.5729
v  Velocity[Y]            -2.9532          7.2608         0.11086         0.11086
v  Velocity[Z]       -1.0134e-014     6.2818e-015    -1.7459e-017    -1.7459e-017
v  ǁVelocityǁ         0.0020382          9.9685           5.136           5.136
v  Pressure               -34.613          18.203         -10.237         -10.237
v  nu_tilda           4.4187e-007       0.0042695       0.0016112       0.0016112
v  TempC                       21          73.047          21.991          21.991
v  TurbVisc           3.3534e-014       0.0050321       0.0018929       0.0018929
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1960:        0.19670E+01

===============================================================


 INSTANT    0.196100000E+04   TIME STEP NUMBER            1961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63518E-02 0.89632E+00
   Friction velocity        uk    :  0.63518E-02 0.89632E+00
   Dimensionless distance   yplus :  0.51136E-01 0.72160E+01
   Friction thermal sca.    tstar : -0.11716E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38153E-01 0.53840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10003E-01      33   0.30261E-03   0.49708E+01 0.18296E+03 
c  Velocity[X]                                      0.18023E+01 
c  Velocity[Y]                                      0.31685E+01 
c  Velocity[Z]                                      0.89449E-30 
c  Pressure     0.10745E-06     536   0.96345E-08   0.10621E+00 0.10370E+04 
c  nu_tilda     0.70886E-05      33   0.42777E-05   0.57896E-06 0.20097E+03 
c  TempC        0.40279E+02      27   0.33947E-03   0.61469E+01 0.28550E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6643          9.9671          4.5729          4.5729
v  Velocity[Y]            -2.9541          7.2744         0.11124         0.11124
v  Velocity[Z]       -1.0109e-014     6.4353e-015    -1.7463e-017    -1.7463e-017
v  ǁVelocityǁ         0.0021638          9.9675           5.136           5.136
v  Pressure               -34.573          18.337         -10.182         -10.182
v  nu_tilda           4.4181e-007       0.0042695       0.0016117       0.0016117
v  TempC                       21          73.048          21.992          21.992
v  TurbVisc           3.3537e-014       0.0050321       0.0018934       0.0018934
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1961:        0.22920E+01

===============================================================


 INSTANT    0.196200000E+04   TIME STEP NUMBER            1962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11089E-01 0.89586E+00
   Friction velocity        uk    :  0.11089E-01 0.89586E+00
   Dimensionless distance   yplus :  0.89276E-01 0.72123E+01
   Friction thermal sca.    tstar : -0.21759E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66610E-01 0.53812E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10005E-01      33   0.26302E-03   0.50149E+01 0.18321E+03 
c  Velocity[X]                                      0.18295E+01 
c  Velocity[Y]                                      0.31854E+01 
c  Velocity[Z]                                      0.79659E-30 
c  Pressure     0.11424E-06     474   0.93114E-08   0.11358E+00 0.10719E+04 
c  nu_tilda     0.70909E-05      33   0.15080E-04   0.57960E-06 0.20106E+03 
c  TempC        0.40287E+02      27   0.31636E-03   0.57057E+01 0.27571E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6614          9.9661          4.5729          4.5729
v  Velocity[Y]             -2.955          7.2445         0.11162         0.11162
v  Velocity[Z]       -1.0536e-014     6.3115e-015    -1.7459e-017    -1.7459e-017
v  ǁVelocityǁ         0.0019587          9.9665           5.136           5.136
v  Pressure               -34.525           18.17         -10.215         -10.215
v  nu_tilda           4.4185e-007       0.0042695       0.0016121       0.0016121
v  TempC                       21          73.047          21.992          21.992
v  TurbVisc            3.352e-014       0.0050321       0.0018939       0.0018939
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1962:        0.20790E+01

===============================================================


 INSTANT    0.196300000E+04   TIME STEP NUMBER            1963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91364E-02 0.89440E+00
   Friction velocity        uk    :  0.91364E-02 0.89440E+00
   Dimensionless distance   yplus :  0.73554E-01 0.72005E+01
   Friction thermal sca.    tstar : -0.19471E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54879E-01 0.53724E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10007E-01      33   0.26741E-03   0.49805E+01 0.18305E+03 
c  Velocity[X]                                      0.18094E+01 
c  Velocity[Y]                                      0.31711E+01 
c  Velocity[Z]                                      0.72857E-30 
c  Pressure     0.12014E-06     520   0.96377E-08   0.11532E+00 0.12805E+04 
c  nu_tilda     0.70932E-05      33   0.43007E-05   0.58017E-06 0.20114E+03 
c  TempC        0.40295E+02      27   0.33403E-03   0.45260E+01 0.25797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6584          9.9651          4.5729          4.5729
v  Velocity[Y]            -2.9556          7.2605           0.112           0.112
v  Velocity[Z]       -1.0565e-014      6.129e-015    -1.7461e-017    -1.7461e-017
v  ǁVelocityǁ         0.0021062          9.9655           5.136           5.136
v  Pressure               -34.482           18.35         -10.146         -10.146
v  nu_tilda           4.4185e-007       0.0042695       0.0016125       0.0016125
v  TempC                       21          73.048          21.992          21.992
v  TurbVisc           3.3531e-014       0.0050321       0.0018944       0.0018944
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1963:        0.21960E+01

===============================================================


 INSTANT    0.196400000E+04   TIME STEP NUMBER            1964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10436E-01 0.89545E+00
   Friction velocity        uk    :  0.10436E-01 0.89545E+00
   Dimensionless distance   yplus :  0.84017E-01 0.72090E+01
   Friction thermal sca.    tstar : -0.12059E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62686E-01 0.53787E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10009E-01      33   0.28168E-03   0.49990E+01 0.18312E+03 
c  Velocity[X]                                      0.18327E+01 
c  Velocity[Y]                                      0.31663E+01 
c  Velocity[Z]                                      0.75059E-30 
c  Pressure     0.11013E-06     473   0.98451E-08   0.10972E+00 0.89115E+03 
c  nu_tilda     0.70956E-05      33   0.15070E-04   0.58081E-06 0.20122E+03 
c  TempC        0.40303E+02      27   0.26963E-03   0.60333E+01 0.28312E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6555          9.9641          4.5729          4.5729
v  Velocity[Y]            -2.9568          7.2387         0.11239         0.11239
v  Velocity[Z]       -1.0543e-014     6.3666e-015    -1.7455e-017    -1.7455e-017
v  ǁVelocityǁ         0.0019407          9.9646           5.136           5.136
v  Pressure               -34.436          18.218         -10.172         -10.172
v  nu_tilda           4.4184e-007       0.0042695       0.0016129       0.0016129
v  TempC                       21          73.048          21.992          21.992
v  TurbVisc           3.3531e-014       0.0050321        0.001895        0.001895
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1964:        0.20760E+01

===============================================================


 INSTANT    0.196500000E+04   TIME STEP NUMBER            1965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76058E-02 0.89471E+00
   Friction velocity        uk    :  0.76058E-02 0.89471E+00
   Dimensionless distance   yplus :  0.61232E-01 0.72030E+01
   Friction thermal sca.    tstar : -0.89346E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45686E-01 0.53742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10011E-01      33   0.21326E-03   0.49839E+01 0.18317E+03 
c  Velocity[X]                                      0.17984E+01 
c  Velocity[Y]                                      0.31856E+01 
c  Velocity[Z]                                      0.10202E-29 
c  Pressure     0.97758E-07     521   0.99719E-08   0.95739E-01 0.13144E+04 
c  nu_tilda     0.70979E-05      33   0.43033E-05   0.58137E-06 0.20131E+03 
c  TempC        0.40311E+02      27   0.37983E-03   0.57589E+01 0.26937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6527          9.9631          4.5729          4.5729
v  Velocity[Y]            -2.9579          7.2644         0.11277         0.11277
v  Velocity[Z]       -1.0516e-014     6.1733e-015    -1.7454e-017    -1.7454e-017
v  ǁVelocityǁ         0.0021572          9.9636           5.136           5.136
v  Pressure               -34.396          18.419         -10.104         -10.104
v  nu_tilda           4.4182e-007       0.0042695       0.0016134       0.0016134
v  TempC                       21          73.048          21.992          21.992
v  TurbVisc           3.3531e-014       0.0050321       0.0018954       0.0018954
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1965:        0.21740E+01

===============================================================


 INSTANT    0.196600000E+04   TIME STEP NUMBER            1966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10274E-01 0.89587E+00
   Friction velocity        uk    :  0.10274E-01 0.89587E+00
   Dimensionless distance   yplus :  0.82716E-01 0.72124E+01
   Friction thermal sca.    tstar : -0.75017E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61715E-01 0.53813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10013E-01      33   0.27745E-03   0.49540E+01 0.18301E+03 
c  Velocity[X]                                      0.17840E+01 
c  Velocity[Y]                                      0.31700E+01 
c  Velocity[Z]                                      0.78126E-30 
c  Pressure     0.11929E-06     442   0.92586E-08   0.11465E+00 0.70702E+03 
c  nu_tilda     0.71002E-05      33   0.15070E-04   0.58200E-06 0.20139E+03 
c  TempC        0.40319E+02      27   0.26489E-03   0.73228E+01 0.31284E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6499          9.9622          4.5729          4.5729
v  Velocity[Y]            -2.9589          7.2668         0.11315         0.11315
v  Velocity[Z]       -1.0678e-014     6.2543e-015    -1.7445e-017    -1.7445e-017
v  ǁVelocityǁ         0.0021274          9.9626           5.136           5.136
v  Pressure               -34.374          18.338         -10.121         -10.121
v  nu_tilda           4.4176e-007       0.0042695       0.0016138       0.0016138
v  TempC                       21          73.047          21.993          21.993
v  TurbVisc           3.3525e-014       0.0050321        0.001896        0.001896
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1966:        0.20080E+01

===============================================================


 INSTANT    0.196700000E+04   TIME STEP NUMBER            1967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11668E-01 0.89561E+00
   Friction velocity        uk    :  0.11668E-01 0.89561E+00
   Dimensionless distance   yplus :  0.93936E-01 0.72103E+01
   Friction thermal sca.    tstar : -0.70987E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70086E-01 0.53797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10015E-01      33   0.29970E-03   0.50002E+01 0.18326E+03 
c  Velocity[X]                                      0.18295E+01 
c  Velocity[Y]                                      0.31707E+01 
c  Velocity[Z]                                      0.78069E-30 
c  Pressure     0.13439E-06     504   0.93677E-08   0.13396E+00 0.68780E+03 
c  nu_tilda     0.71026E-05      33   0.43146E-05   0.58257E-06 0.20147E+03 
c  TempC        0.40327E+02      27   0.34653E-03   0.45482E+01 0.24440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6469          9.9612          4.5729          4.5729
v  Velocity[Y]            -2.9598          7.2422         0.11354         0.11354
v  Velocity[Z]       -1.0892e-014     6.3733e-015     -1.745e-017     -1.745e-017
v  ǁVelocityǁ         0.0020159          9.9616           5.136           5.136
v  Pressure               -34.309          18.364         -10.083         -10.083
v  nu_tilda           4.4173e-007       0.0042695       0.0016143       0.0016143
v  TempC                       21          73.047          21.993          21.993
v  TurbVisc           3.3505e-014       0.0050321       0.0018965       0.0018965
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1967:        0.21470E+01

===============================================================


 INSTANT    0.196800000E+04   TIME STEP NUMBER            1968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.84408E-02 0.89423E+00
   Friction velocity        uk    :  0.84408E-02 0.89423E+00
   Dimensionless distance   yplus :  0.67954E-01 0.71991E+01
   Friction thermal sca.    tstar : -0.64359E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50702E-01 0.53714E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10017E-01      33   0.27211E-03   0.50002E+01 0.18333E+03 
c  Velocity[X]                                      0.18150E+01 
c  Velocity[Y]                                      0.31852E+01 
c  Velocity[Z]                                      0.79058E-30 
c  Pressure     0.10368E-06     409   0.91663E-08   0.10097E+00 0.46398E+03 
c  nu_tilda     0.71049E-05      33   0.15062E-04   0.58320E-06 0.20156E+03 
c  TempC        0.40335E+02      27   0.28093E-03   0.64255E+01 0.28276E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6439          9.9602          4.5729          4.5729
v  Velocity[Y]            -2.9606           7.261         0.11392         0.11392
v  Velocity[Z]       -1.1103e-014     6.3176e-015     -1.744e-017     -1.744e-017
v  ǁVelocityǁ         0.0020749          9.9606           5.136           5.136
v  Pressure               -34.259          18.401         -10.074         -10.074
v  nu_tilda           4.4172e-007       0.0042695       0.0016146       0.0016146
v  TempC                       21          73.047          21.993          21.993
v  TurbVisc           3.3495e-014       0.0050321        0.001897        0.001897
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1968:        0.19320E+01

===============================================================


 INSTANT    0.196900000E+04   TIME STEP NUMBER            1969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.28919E-02 0.89537E+00
   Friction velocity        uk    :  0.28919E-02 0.89537E+00
   Dimensionless distance   yplus :  0.23282E-01 0.72083E+01
   Friction thermal sca.    tstar : -0.67712E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17371E-01 0.53782E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10019E-01      33   0.27005E-03   0.49851E+01 0.18324E+03 
c  Velocity[X]                                      0.18117E+01 
c  Velocity[Y]                                      0.31734E+01 
c  Velocity[Z]                                      0.83929E-30 
c  Pressure     0.11564E-06     472   0.95057E-08   0.11329E+00 0.52162E+03 
c  nu_tilda     0.71072E-05      33   0.43287E-05   0.58377E-06 0.20164E+03 
c  TempC        0.40343E+02      27   0.24987E-03   0.53557E+01 0.26394E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6412          9.9592          4.5729          4.5729
v  Velocity[Y]            -2.9613          7.2359          0.1143          0.1143
v  Velocity[Z]       -1.0907e-014     6.3329e-015    -1.7444e-017    -1.7444e-017
v  ǁVelocityǁ         0.0020103          9.9597           5.136           5.136
v  Pressure               -34.218          18.372         -10.051         -10.051
v  nu_tilda           4.4176e-007       0.0042695       0.0016151       0.0016151
v  TempC                       21          73.048          21.993          21.993
v  TurbVisc           3.3493e-014       0.0050321       0.0018975       0.0018975
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1969:        0.20680E+01

===============================================================


 INSTANT    0.197000000E+04   TIME STEP NUMBER            1970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70222E-02 0.89460E+00
   Friction velocity        uk    :  0.70222E-02 0.89460E+00
   Dimensionless distance   yplus :  0.56533E-01 0.72021E+01
   Friction thermal sca.    tstar : -0.65962E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42180E-01 0.53736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10021E-01      33   0.22473E-03   0.49900E+01 0.18326E+03 
c  Velocity[X]                                      0.18228E+01 
c  Velocity[Y]                                      0.31673E+01 
c  Velocity[Z]                                      0.85227E-30 
c  Pressure     0.10523E-06     456   0.94315E-08   0.10400E+00 0.57343E+03 
c  nu_tilda     0.71095E-05      33   0.15058E-04   0.58439E-06 0.20172E+03 
c  TempC        0.40351E+02      27   0.38331E-03   0.40538E+01 0.24261E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6384          9.9582          4.5729          4.5729
v  Velocity[Y]            -2.9623          7.2618         0.11468         0.11468
v  Velocity[Z]       -1.0871e-014     6.2293e-015    -1.7435e-017    -1.7435e-017
v  ǁVelocityǁ         0.0020924          9.9587           5.136           5.136
v  Pressure               -34.167          18.458         -10.025         -10.025
v  nu_tilda           4.4175e-007       0.0042695       0.0016155       0.0016155
v  TempC                       21          73.048          21.994          21.994
v  TurbVisc           3.3506e-014       0.0050321        0.001898        0.001898
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1970:        0.20480E+01

===============================================================


 INSTANT    0.197100000E+04   TIME STEP NUMBER            1971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10863E-01 0.89609E+00
   Friction velocity        uk    :  0.10863E-01 0.89609E+00
   Dimensionless distance   yplus :  0.87455E-01 0.72142E+01
   Friction thermal sca.    tstar : -0.64102E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65251E-01 0.53826E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10023E-01      33   0.26015E-03   0.49647E+01 0.18328E+03 
c  Velocity[X]                                      0.17770E+01 
c  Velocity[Y]                                      0.31876E+01 
c  Velocity[Z]                                      0.78802E-30 
c  Pressure     0.10188E-06     505   0.97039E-08   0.99428E-01 0.75063E+03 
c  nu_tilda     0.71119E-05      33   0.43351E-05   0.58498E-06 0.20181E+03 
c  TempC        0.40359E+02      27   0.30670E-03   0.65969E+01 0.30726E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6354          9.9572          4.5729          4.5729
v  Velocity[Y]            -2.9634          7.2722         0.11507         0.11507
v  Velocity[Z]       -1.0872e-014     6.0418e-015     -1.743e-017     -1.743e-017
v  ǁVelocityǁ         0.0022329          9.9577           5.136           5.136
v  Pressure               -34.128          18.539         -9.9862         -9.9862
v  nu_tilda           4.4168e-007       0.0042695        0.001616        0.001616
v  TempC                       21          73.049          21.994          21.994
v  TurbVisc           3.3502e-014       0.0050321       0.0018985       0.0018985
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1971:        0.21400E+01

===============================================================


 INSTANT    0.197200000E+04   TIME STEP NUMBER            1972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11837E-01 0.89554E+00
   Friction velocity        uk    :  0.11837E-01 0.89554E+00
   Dimensionless distance   yplus :  0.95299E-01 0.72097E+01
   Friction thermal sca.    tstar : -0.63139E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71104E-01 0.53793E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10026E-01      33   0.26655E-03   0.49825E+01 0.18330E+03 
c  Velocity[X]                                      0.18099E+01 
c  Velocity[Y]                                      0.31726E+01 
c  Velocity[Z]                                      0.77377E-30 
c  Pressure     0.11524E-06     504   0.98418E-08   0.11267E+00 0.11210E+04 
c  nu_tilda     0.71142E-05      33   0.15054E-04   0.58559E-06 0.20189E+03 
c  TempC        0.40367E+02      27   0.39004E-03   0.57277E+01 0.26232E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6324          9.9563          4.5729          4.5729
v  Velocity[Y]            -2.9644          7.2387         0.11545         0.11545
v  Velocity[Z]       -1.0819e-014     6.3556e-015     -1.743e-017     -1.743e-017
v  ǁVelocityǁ         0.0019378          9.9567           5.136           5.136
v  Pressure                -34.17          18.356         -10.018         -10.018
v  nu_tilda           4.4171e-007       0.0042695       0.0016163       0.0016163
v  TempC                       21          73.047          21.994          21.994
v  TurbVisc            3.348e-014       0.0050321        0.001899        0.001899
v  total_pressure     1.0129e+005     1.0134e+005     1.0131e+005     1.0131e+005


 TIME FOR THE TIME STEP             1972:        0.21480E+01

===============================================================


 INSTANT    0.197300000E+04   TIME STEP NUMBER            1973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92005E-02 0.89434E+00
   Friction velocity        uk    :  0.92005E-02 0.89434E+00
   Dimensionless distance   yplus :  0.74071E-01 0.72001E+01
   Friction thermal sca.    tstar : -0.65213E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55265E-01 0.53721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10028E-01      33   0.29390E-03   0.49814E+01 0.18336E+03 
c  Velocity[X]                                      0.18095E+01 
c  Velocity[Y]                                      0.31719E+01 
c  Velocity[Z]                                      0.93247E-30 
c  Pressure     0.10668E-06     520   0.99794E-08   0.10519E+00 0.15202E+04 
c  nu_tilda     0.71165E-05      33   0.43566E-05   0.58615E-06 0.20197E+03 
c  TempC        0.40375E+02      27   0.31132E-03   0.74785E+01 0.30990E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6296          9.9553          4.5729          4.5729
v  Velocity[Y]            -2.9653           7.262         0.11583         0.11583
v  Velocity[Z]       -1.0555e-014     6.3039e-015    -1.7427e-017    -1.7427e-017
v  ǁVelocityǁ         0.0021056          9.9557           5.136           5.136
v  Pressure               -34.037          18.588         -9.9399         -9.9399
v  nu_tilda           4.4165e-007       0.0042695       0.0016168       0.0016168
v  TempC                       21          73.048          21.994          21.994
v  TurbVisc           3.3491e-014       0.0050321       0.0018995       0.0018995
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1973:        0.21920E+01

===============================================================


 INSTANT    0.197400000E+04   TIME STEP NUMBER            1974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23148E-02 0.89529E+00
   Friction velocity        uk    :  0.23148E-02 0.89529E+00
   Dimensionless distance   yplus :  0.18635E-01 0.72077E+01
   Friction thermal sca.    tstar : -0.63465E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13904E-01 0.53777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10030E-01      33   0.28195E-03   0.50037E+01 0.18351E+03 
c  Velocity[X]                                      0.18169E+01 
c  Velocity[Y]                                      0.31868E+01 
c  Velocity[Z]                                      0.90927E-30 
c  Pressure     0.11077E-06     488   0.91996E-08   0.10966E+00 0.10204E+04 
c  nu_tilda     0.71189E-05      33   0.15042E-04   0.58677E-06 0.20205E+03 
c  TempC        0.40383E+02      27   0.29190E-03   0.58844E+01 0.27136E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6268          9.9543          4.5729          4.5729
v  Velocity[Y]             -2.966          7.2377         0.11622         0.11622
v  Velocity[Z]       -1.0326e-014     6.3933e-015    -1.7425e-017    -1.7425e-017
v  ǁVelocityǁ         0.0019285          9.9547          5.1361          5.1361
v  Pressure               -34.028          18.436         -9.9684         -9.9684
v  nu_tilda           4.4161e-007       0.0042695       0.0016172       0.0016172
v  TempC                       21          73.048          21.995          21.995
v  TurbVisc           3.3472e-014       0.0050321          0.0019          0.0019
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1974:        0.21020E+01

===============================================================


 INSTANT    0.197500000E+04   TIME STEP NUMBER            1975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89018E-02 0.89445E+00
   Friction velocity        uk    :  0.89018E-02 0.89445E+00
   Dimensionless distance   yplus :  0.71665E-01 0.72009E+01
   Friction thermal sca.    tstar : -0.64387E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53470E-01 0.53727E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10032E-01      33   0.26581E-03   0.49832E+01 0.18342E+03 
c  Velocity[X]                                      0.18090E+01 
c  Velocity[Y]                                      0.31742E+01 
c  Velocity[Z]                                      0.78394E-30 
c  Pressure     0.12047E-06     489   0.99448E-08   0.11536E+00 0.12266E+04 
c  nu_tilda     0.71212E-05      33   0.43635E-05   0.58734E-06 0.20214E+03 
c  TempC        0.40390E+02      27   0.34486E-03   0.42514E+01 0.24401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6239          9.9533          4.5729          4.5729
v  Velocity[Y]            -2.9667          7.2583          0.1166          0.1166
v  Velocity[Z]       -1.0069e-014     6.0922e-015    -1.7424e-017    -1.7424e-017
v  ǁVelocityǁ         0.0020938          9.9538          5.1361          5.1361
v  Pressure               -33.993          18.612         -9.9048         -9.9048
v  nu_tilda           4.4159e-007       0.0042695       0.0016176       0.0016176
v  TempC                       21          73.049          21.995          21.995
v  TurbVisc            3.346e-014       0.0050321       0.0019005       0.0019005
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1975:        0.20930E+01

===============================================================


 INSTANT    0.197600000E+04   TIME STEP NUMBER            1976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10591E-01 0.89574E+00
   Friction velocity        uk    :  0.10591E-01 0.89574E+00
   Dimensionless distance   yplus :  0.85262E-01 0.72113E+01
   Friction thermal sca.    tstar : -0.63614E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63615E-01 0.53805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10034E-01      33   0.27704E-03   0.49727E+01 0.18338E+03 
c  Velocity[X]                                      0.18048E+01 
c  Velocity[Y]                                      0.31679E+01 
c  Velocity[Z]                                      0.76781E-30 
c  Pressure     0.10071E-06     361   0.92815E-08   0.99045E-01 0.51420E+03 
c  nu_tilda     0.71235E-05      33   0.15042E-04   0.58797E-06 0.20222E+03 
c  TempC        0.40398E+02      27   0.28657E-03   0.57833E+01 0.26624E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6209          9.9523          4.5729          4.5729
v  Velocity[Y]            -2.9676          7.2672         0.11698         0.11698
v  Velocity[Z]       -9.9004e-015     6.3046e-015    -1.7417e-017    -1.7417e-017
v  ǁVelocityǁ          0.002152          9.9528          5.1361          5.1361
v  Pressure               -34.053          18.589         -9.9036         -9.9036
v  nu_tilda           4.4155e-007       0.0042695        0.001618        0.001618
v  TempC                       21          73.048          21.995          21.995
v  TurbVisc           3.3454e-014       0.0050321        0.001901        0.001901
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1976:        0.18150E+01

===============================================================


 INSTANT    0.197700000E+04   TIME STEP NUMBER            1977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12209E-01 0.89541E+00
   Friction velocity        uk    :  0.12209E-01 0.89541E+00
   Dimensionless distance   yplus :  0.98287E-01 0.72086E+01
   Friction thermal sca.    tstar : -0.67425E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73333E-01 0.53785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10036E-01      33   0.25086E-03   0.49882E+01 0.18353E+03 
c  Velocity[X]                                      0.18001E+01 
c  Velocity[Y]                                      0.31882E+01 
c  Velocity[Z]                                      0.86776E-30 
c  Pressure     0.10979E-06     504   0.93690E-08   0.10960E+00 0.57777E+03 
c  nu_tilda     0.71258E-05      33   0.43722E-05   0.58854E-06 0.20230E+03 
c  TempC        0.40406E+02      27   0.37240E-03   0.44348E+01 0.24646E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6179          9.9513          4.5729          4.5729
v  Velocity[Y]            -2.9687          7.2405         0.11736         0.11736
v  Velocity[Z]       -9.6622e-015     6.1562e-015    -1.7423e-017    -1.7423e-017
v  ǁVelocityǁ         0.0020066          9.9518          5.1361          5.1361
v  Pressure               -33.856          18.572         -9.8761         -9.8761
v  nu_tilda           4.4159e-007       0.0042695       0.0016185       0.0016185
v  TempC                       21          73.048          21.995          21.995
v  TurbVisc           3.3441e-014       0.0050321       0.0019015       0.0019015
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1977:        0.21500E+01

===============================================================


 INSTANT    0.197800000E+04   TIME STEP NUMBER            1978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.69638E-02 0.89392E+00
   Friction velocity        uk    :  0.69638E-02 0.89392E+00
   Dimensionless distance   yplus :  0.56063E-01 0.71967E+01
   Friction thermal sca.    tstar : -0.65686E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41829E-01 0.53695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10038E-01      33   0.27345E-03   0.49659E+01 0.18341E+03 
c  Velocity[X]                                      0.17922E+01 
c  Velocity[Y]                                      0.31737E+01 
c  Velocity[Z]                                      0.74934E-30 
c  Pressure     0.11617E-06     360   0.91760E-08   0.11158E+00 0.45522E+03 
c  nu_tilda     0.71282E-05      33   0.15035E-04   0.58917E-06 0.20238E+03 
c  TempC        0.40414E+02      27   0.30668E-03   0.60667E+01 0.27562E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6152          9.9503          4.5729          4.5729
v  Velocity[Y]            -2.9697          7.2543         0.11775         0.11775
v  Velocity[Z]       -9.7009e-015      6.388e-015     -1.742e-017     -1.742e-017
v  ǁVelocityǁ         0.0020767          9.9508          5.1361          5.1361
v  Pressure               -34.039          18.594         -9.8706         -9.8706
v  nu_tilda           4.4166e-007       0.0042695       0.0016189       0.0016189
v  TempC                       21          73.047          21.995          21.995
v  TurbVisc           3.3455e-014       0.0050321        0.001902        0.001902
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1978:        0.18190E+01

===============================================================


 INSTANT    0.197900000E+04   TIME STEP NUMBER            1979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75634E-02 0.89517E+00
   Friction velocity        uk    :  0.75634E-02 0.89517E+00
   Dimensionless distance   yplus :  0.60891E-01 0.72067E+01
   Friction thermal sca.    tstar : -0.63834E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45431E-01 0.53770E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10040E-01      33   0.30248E-03   0.49894E+01 0.18357E+03 
c  Velocity[X]                                      0.18167E+01 
c  Velocity[Y]                                      0.31727E+01 
c  Velocity[Z]                                      0.82899E-30 
c  Pressure     0.13241E-06     505   0.96488E-08   0.13176E+00 0.72236E+03 
c  nu_tilda     0.71305E-05      33   0.43927E-05   0.58972E-06 0.20246E+03 
c  TempC        0.40422E+02      27   0.31630E-03   0.45445E+01 0.23877E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6123          9.9493          4.5729          4.5729
v  Velocity[Y]            -2.9705          7.2362         0.11813         0.11813
v  Velocity[Z]       -1.0483e-014     6.3151e-015    -1.7424e-017    -1.7424e-017
v  ǁVelocityǁ          0.002027          9.9498          5.1361          5.1361
v  Pressure               -33.824          18.623         -9.8306         -9.8306
v  nu_tilda            4.417e-007       0.0042695       0.0016193       0.0016193
v  TempC                       21          73.047          21.996          21.996
v  TurbVisc           3.3474e-014       0.0050321       0.0019025       0.0019025
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1979:        0.21530E+01

===============================================================


 INSTANT    0.198000000E+04   TIME STEP NUMBER            1980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92121E-02 0.89441E+00
   Friction velocity        uk    :  0.92121E-02 0.89441E+00
   Dimensionless distance   yplus :  0.74164E-01 0.72006E+01
   Friction thermal sca.    tstar : -0.64832E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55334E-01 0.53725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10042E-01      33   0.20895E-03   0.49982E+01 0.18366E+03 
c  Velocity[X]                                      0.18106E+01 
c  Velocity[Y]                                      0.31876E+01 
c  Velocity[Z]                                      0.76217E-30 
c  Pressure     0.10824E-06     362   0.99554E-08   0.10555E+00 0.45104E+03 
c  nu_tilda     0.71328E-05      33   0.15026E-04   0.59033E-06 0.20254E+03 
c  TempC        0.40430E+02      27   0.32863E-03   0.42628E+01 0.22953E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6093          9.9483          4.5729          4.5729
v  Velocity[Y]            -2.9713          7.2601         0.11851         0.11851
v  Velocity[Z]       -1.0504e-014     6.3834e-015    -1.7415e-017    -1.7415e-017
v  ǁVelocityǁ         0.0021595          9.9488          5.1361          5.1361
v  Pressure               -33.883          18.665         -9.8221         -9.8221
v  nu_tilda           4.4167e-007       0.0042695       0.0016197       0.0016197
v  TempC                       21          73.047          21.996          21.996
v  TurbVisc           3.3487e-014       0.0050321        0.001903        0.001903
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1980:        0.18270E+01

===============================================================


 INSTANT    0.198100000E+04   TIME STEP NUMBER            1981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71628E-02 0.89597E+00
   Friction velocity        uk    :  0.71628E-02 0.89597E+00
   Dimensionless distance   yplus :  0.57666E-01 0.72132E+01
   Friction thermal sca.    tstar : -0.68525E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43025E-01 0.53818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10044E-01      33   0.26551E-03   0.49610E+01 0.18348E+03 
c  Velocity[X]                                      0.17827E+01 
c  Velocity[Y]                                      0.31783E+01 
c  Velocity[Z]                                      0.88435E-30 
c  Pressure     0.11947E-06     474   0.93237E-08   0.11644E+00 0.92747E+03 
c  nu_tilda     0.71351E-05      33   0.43959E-05   0.59091E-06 0.20263E+03 
c  TempC        0.40438E+02      27   0.28048E-03   0.43452E+01 0.24402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6064          9.9473          4.5729          4.5729
v  Velocity[Y]            -2.9719          7.2671         0.11889         0.11889
v  Velocity[Z]       -1.1181e-014     6.2897e-015    -1.7413e-017    -1.7413e-017
v  ǁVelocityǁ         0.0022138          9.9479          5.1361          5.1361
v  Pressure                -33.86          18.761          -9.771          -9.771
v  nu_tilda            4.416e-007       0.0042695       0.0016202       0.0016202
v  TempC                       21          73.048          21.996          21.996
v  TurbVisc           3.3479e-014       0.0050321       0.0019035       0.0019035
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1981:        0.20650E+01

===============================================================


 INSTANT    0.198200000E+04   TIME STEP NUMBER            1982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95859E-02 0.89560E+00
   Friction velocity        uk    :  0.95859E-02 0.89560E+00
   Dimensionless distance   yplus :  0.77173E-01 0.72102E+01
   Friction thermal sca.    tstar : -0.72834E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57580E-01 0.53796E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10046E-01      33   0.26928E-03   0.49975E+01 0.18364E+03 
c  Velocity[X]                                      0.18265E+01 
c  Velocity[Y]                                      0.31710E+01 
c  Velocity[Z]                                      0.93568E-30 
c  Pressure     0.10807E-06     472   0.95267E-08   0.10765E+00 0.99943E+03 
c  nu_tilda     0.71374E-05      33   0.15028E-04   0.59152E-06 0.20271E+03 
c  TempC        0.40446E+02      27   0.33586E-03   0.42314E+01 0.24327E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6035          9.9463          4.5729          4.5729
v  Velocity[Y]            -2.9728          7.2396         0.11927         0.11927
v  Velocity[Z]       -1.2265e-014     6.2286e-015    -1.7421e-017    -1.7421e-017
v  ǁVelocityǁ         0.0019937          9.9469          5.1361          5.1361
v  Pressure                -33.87          18.611         -9.7959         -9.7959
v  nu_tilda           4.4158e-007       0.0042695       0.0016205       0.0016205
v  TempC                       21          73.048          21.996          21.996
v  TurbVisc           3.3455e-014       0.0050321        0.001904        0.001904
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1982:        0.20730E+01

===============================================================


 INSTANT    0.198300000E+04   TIME STEP NUMBER            1983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76733E-02 0.89420E+00
   Friction velocity        uk    :  0.76733E-02 0.89420E+00
   Dimensionless distance   yplus :  0.61775E-01 0.71989E+01
   Friction thermal sca.    tstar : -0.84610E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46091E-01 0.53712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10048E-01      33   0.26702E-03   0.49774E+01 0.18366E+03 
c  Velocity[X]                                      0.17866E+01 
c  Velocity[Y]                                      0.31908E+01 
c  Velocity[Z]                                      0.96978E-30 
c  Pressure     0.99612E-07     520   0.95990E-08   0.97637E-01 0.14536E+04 
c  nu_tilda     0.71398E-05      33   0.44107E-05   0.59207E-06 0.20279E+03 
c  TempC        0.40454E+02      27   0.30140E-03   0.68190E+01 0.28243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6006          9.9454          4.5729          4.5729
v  Velocity[Y]            -2.9738          7.2593         0.11966         0.11966
v  Velocity[Z]       -1.2192e-014     6.3718e-015    -1.7412e-017    -1.7412e-017
v  ǁVelocityǁ          0.002219          9.9458          5.1361          5.1361
v  Pressure               -33.682          18.829         -9.7205         -9.7205
v  nu_tilda           4.4156e-007       0.0042695        0.001621        0.001621
v  TempC                       21          73.048          21.997          21.997
v  TurbVisc           3.3452e-014       0.0050321       0.0019044       0.0019044
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1983:        0.22030E+01

===============================================================


 INSTANT    0.198400000E+04   TIME STEP NUMBER            1984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75708E-02 0.89499E+00
   Friction velocity        uk    :  0.75708E-02 0.89499E+00
   Dimensionless distance   yplus :  0.60950E-01 0.72053E+01
   Friction thermal sca.    tstar : -0.11067E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45476E-01 0.53759E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10051E-01      33   0.28268E-03   0.49754E+01 0.18362E+03 
c  Velocity[X]                                      0.17995E+01 
c  Velocity[Y]                                      0.31759E+01 
c  Velocity[Z]                                      0.83083E-30 
c  Pressure     0.11525E-06     489   0.99245E-08   0.11260E+00 0.12729E+04 
c  nu_tilda     0.71421E-05      33   0.15015E-04   0.59269E-06 0.20287E+03 
c  TempC        0.40461E+02      27   0.34654E-03   0.61569E+01 0.27909E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5977          9.9444          4.5729          4.5729
v  Velocity[Y]            -2.9748          7.2318         0.12004         0.12004
v  Velocity[Z]       -1.2937e-014     6.3816e-015    -1.7413e-017    -1.7413e-017
v  ǁVelocityǁ         0.0019448          9.9448          5.1361          5.1361
v  Pressure               -33.848          18.624         -9.7587         -9.7587
v  nu_tilda           4.4156e-007       0.0042695       0.0016214       0.0016214
v  TempC                       21          73.047          21.997          21.997
v  TurbVisc           3.3444e-014       0.0050321        0.001905        0.001905
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1984:        0.21140E+01

===============================================================


 INSTANT    0.198500000E+04   TIME STEP NUMBER            1985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90914E-02 0.89444E+00
   Friction velocity        uk    :  0.90914E-02 0.89444E+00
   Dimensionless distance   yplus :  0.73192E-01 0.72008E+01
   Friction thermal sca.    tstar : -0.16001E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54609E-01 0.53726E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10053E-01      33   0.24989E-03   0.49800E+01 0.18371E+03 
c  Velocity[X]                                      0.18082E+01 
c  Velocity[Y]                                      0.31718E+01 
c  Velocity[Z]                                      0.86703E-30 
c  Pressure     0.11344E-06     506   0.97711E-08   0.11069E+00 0.14602E+04 
c  nu_tilda     0.71444E-05      33   0.44191E-05   0.59327E-06 0.20295E+03 
c  TempC        0.40469E+02      27   0.29806E-03   0.48658E+01 0.25074E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5947          9.9434          4.5729          4.5729
v  Velocity[Y]            -2.9756          7.2597         0.12042         0.12042
v  Velocity[Z]       -1.2868e-014     6.1857e-015    -1.7402e-017    -1.7402e-017
v  ǁVelocityǁ         0.0021618          9.9439          5.1361          5.1361
v  Pressure               -33.716           18.85         -9.6847         -9.6847
v  nu_tilda           4.4154e-007       0.0042695       0.0016219       0.0016219
v  TempC                       21          73.048          21.997          21.997
v  TurbVisc           3.3446e-014       0.0050321       0.0019054       0.0019054
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1985:        0.21450E+01

===============================================================


 INSTANT    0.198600000E+04   TIME STEP NUMBER            1986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10895E-01 0.89571E+00
   Friction velocity        uk    :  0.10895E-01 0.89571E+00
   Dimensionless distance   yplus :  0.87710E-01 0.72111E+01
   Friction thermal sca.    tstar : -0.32063E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65441E-01 0.53803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10055E-01      33   0.26980E-03   0.49756E+01 0.18374E+03 
c  Velocity[X]                                      0.17884E+01 
c  Velocity[Y]                                      0.31872E+01 
c  Velocity[Z]                                      0.85335E-30 
c  Pressure     0.11276E-06     329   0.93028E-08   0.11094E+00 0.50791E+03 
c  nu_tilda     0.71467E-05      33   0.15014E-04   0.59388E-06 0.20303E+03 
c  TempC        0.40477E+02      27   0.25350E-03   0.47041E+01 0.23560E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5918          9.9423          4.5729          4.5729
v  Velocity[Y]            -2.9764          7.2661          0.1208          0.1208
v  Velocity[Z]       -1.3625e-014     6.4219e-015    -1.7404e-017    -1.7404e-017
v  ǁVelocityǁ         0.0022097          9.9429          5.1361          5.1361
v  Pressure               -33.741          18.838         -9.6771         -9.6771
v  nu_tilda           4.4151e-007       0.0042695       0.0016222       0.0016222
v  TempC                       21          73.048          21.997          21.997
v  TurbVisc           3.3438e-014       0.0050321       0.0019059       0.0019059
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1986:        0.17450E+01

===============================================================


 INSTANT    0.198700000E+04   TIME STEP NUMBER            1987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.29713E-02 0.89522E+00
   Friction velocity        uk    :  0.29713E-02 0.89522E+00
   Dimensionless distance   yplus :  0.23921E-01 0.72071E+01
   Friction thermal sca.    tstar : -0.13542E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17848E-01 0.53773E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10057E-01      33   0.26353E-03   0.49888E+01 0.18377E+03 
c  Velocity[X]                                      0.18119E+01 
c  Velocity[Y]                                      0.31769E+01 
c  Velocity[Z]                                      0.71238E-30 
c  Pressure     0.13603E-06     426   0.93064E-08   0.13251E+00 0.52208E+03 
c  nu_tilda     0.71491E-05      33   0.44277E-05   0.59444E-06 0.20311E+03 
c  TempC        0.40485E+02      27   0.36470E-03   0.52419E+01 0.25721E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.589          9.9414          4.5729          4.5729
v  Velocity[Y]             -2.977          7.2348         0.12118         0.12118
v  Velocity[Z]       -1.3508e-014     6.3025e-015    -1.7389e-017    -1.7389e-017
v  ǁVelocityǁ         0.0020051          9.9419          5.1361          5.1361
v  Pressure               -33.704          18.776         -9.6635         -9.6635
v  nu_tilda           4.4155e-007       0.0042695       0.0016227       0.0016227
v  TempC                       21          73.049          21.997          21.997
v  TurbVisc           3.3429e-014       0.0050321       0.0019064       0.0019064
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1987:        0.19620E+01

===============================================================


 INSTANT    0.198800000E+04   TIME STEP NUMBER            1988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62543E-02 0.89395E+00
   Friction velocity        uk    :  0.62543E-02 0.89395E+00
   Dimensionless distance   yplus :  0.50351E-01 0.71969E+01
   Friction thermal sca.    tstar : -0.10177E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37568E-01 0.53697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10059E-01      33   0.26722E-03   0.49788E+01 0.18373E+03 
c  Velocity[X]                                      0.18110E+01 
c  Velocity[Y]                                      0.31678E+01 
c  Velocity[Z]                                      0.80124E-30 
c  Pressure     0.98463E-07     442   0.94478E-08   0.96248E-01 0.56083E+03 
c  nu_tilda     0.71514E-05      33   0.15010E-04   0.59504E-06 0.20319E+03 
c  TempC        0.40493E+02      27   0.27445E-03   0.67705E+01 0.29168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5861          9.9404          4.5729          4.5729
v  Velocity[Y]            -2.9777          7.2558         0.12156         0.12156
v  Velocity[Z]       -1.3823e-014     6.3265e-015    -1.7383e-017    -1.7383e-017
v  ǁVelocityǁ         0.0020792          9.9409          5.1361          5.1361
v  Pressure               -33.714          18.858         -9.6398         -9.6398
v  nu_tilda           4.4159e-007       0.0042695       0.0016231       0.0016231
v  TempC                       21          73.048          21.998          21.998
v  TurbVisc           3.3441e-014       0.0050321       0.0019069       0.0019069
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1988:        0.20010E+01

===============================================================


 INSTANT    0.198900000E+04   TIME STEP NUMBER            1989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44493E-02 0.89511E+00
   Friction velocity        uk    :  0.44493E-02 0.89511E+00
   Dimensionless distance   yplus :  0.35820E-01 0.72063E+01
   Friction thermal sca.    tstar : -0.80510E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26726E-01 0.53767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10061E-01      33   0.26757E-03   0.49786E+01 0.18383E+03 
c  Velocity[X]                                      0.17874E+01 
c  Velocity[Y]                                      0.31912E+01 
c  Velocity[Z]                                      0.94080E-30 
c  Pressure     0.11493E-06     504   0.98949E-08   0.11508E+00 0.64328E+03 
c  nu_tilda     0.71537E-05      33   0.44491E-05   0.59559E-06 0.20327E+03 
c  TempC        0.40501E+02      27   0.30519E-03   0.41709E+01 0.23871E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5831          9.9394          4.5729          4.5729
v  Velocity[Y]            -2.9788          7.2348         0.12194         0.12194
v  Velocity[Z]         -1.38e-014     6.1108e-015    -1.7373e-017    -1.7373e-017
v  ǁVelocityǁ         0.0020411          9.9399          5.1361          5.1361
v  Pressure               -33.507          18.871         -9.6057         -9.6057
v  nu_tilda           4.4164e-007       0.0042695       0.0016235       0.0016235
v  TempC                       21          73.049          21.998          21.998
v  TurbVisc           3.3453e-014       0.0050321       0.0019074       0.0019074
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1989:        0.21530E+01

===============================================================


 INSTANT    0.199000000E+04   TIME STEP NUMBER            1990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83558E-02 0.89414E+00
   Friction velocity        uk    :  0.83558E-02 0.89414E+00
   Dimensionless distance   yplus :  0.67270E-01 0.71984E+01
   Friction thermal sca.    tstar : -0.69803E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50191E-01 0.53708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10063E-01      33   0.22395E-03   0.49664E+01 0.18374E+03 
c  Velocity[X]                                      0.17910E+01 
c  Velocity[Y]                                      0.31754E+01 
c  Velocity[Z]                                      0.82035E-30 
c  Pressure     0.11467E-06     378   0.94517E-08   0.11057E+00 0.53832E+03 
c  nu_tilda     0.71560E-05      33   0.14998E-04   0.59620E-06 0.20335E+03 
c  TempC        0.40509E+02      27   0.33495E-03   0.42863E+01 0.25039E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5802          9.9384          4.5729          4.5729
v  Velocity[Y]            -2.9797          7.2546         0.12233         0.12233
v  Velocity[Z]       -1.4235e-014     6.2863e-015    -1.7362e-017    -1.7362e-017
v  ǁVelocityǁ         0.0020731          9.9389          5.1361          5.1361
v  Pressure               -33.709          18.862         -9.6051         -9.6051
v  nu_tilda           4.4165e-007       0.0042695       0.0016239       0.0016239
v  TempC                       21          73.047          21.998          21.998
v  TurbVisc           3.3469e-014       0.0050321       0.0019079       0.0019079
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1990:        0.20370E+01

===============================================================


 INSTANT    0.199100000E+04   TIME STEP NUMBER            1991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10698E-01 0.89584E+00
   Friction velocity        uk    :  0.10698E-01 0.89584E+00
   Dimensionless distance   yplus :  0.86128E-01 0.72121E+01
   Friction thermal sca.    tstar : -0.66981E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64261E-01 0.53811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10065E-01      33   0.30059E-03   0.49578E+01 0.18378E+03 
c  Velocity[X]                                      0.17880E+01 
c  Velocity[Y]                                      0.31698E+01 
c  Velocity[Z]                                      0.81468E-30 
c  Pressure     0.11326E-06     536   0.94180E-08   0.11066E+00 0.12083E+04 
c  nu_tilda     0.71583E-05      33   0.44503E-05   0.59677E-06 0.20343E+03 
c  TempC        0.40516E+02      27   0.36004E-03   0.57882E+01 0.27346E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5772          9.9374          4.5729          4.5729
v  Velocity[Y]            -2.9806          7.2676         0.12271         0.12271
v  Velocity[Z]       -1.4256e-014      6.219e-015    -1.7354e-017    -1.7354e-017
v  ǁVelocityǁ         0.0013144          9.9379          5.1361          5.1361
v  Pressure               -33.542          19.012         -9.5383         -9.5383
v  nu_tilda           4.4155e-007       0.0042695       0.0016244       0.0016244
v  TempC                       21          73.048          21.998          21.998
v  TurbVisc           3.3472e-014       0.0050321       0.0019084       0.0019084
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1991:        0.24920E+01

===============================================================


 INSTANT    0.199200000E+04   TIME STEP NUMBER            1992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.70259E-02 0.89538E+00
   Friction velocity        uk    :  0.70259E-02 0.89538E+00
   Dimensionless distance   yplus :  0.56563E-01 0.72084E+01
   Friction thermal sca.    tstar : -0.62737E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42203E-01 0.53783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10067E-01      33   0.26116E-03   0.50052E+01 0.18403E+03 
c  Velocity[X]                                      0.18147E+01 
c  Velocity[Y]                                      0.31905E+01 
c  Velocity[Z]                                      0.89065E-30 
c  Pressure     0.11689E-06     520   0.92114E-08   0.11648E+00 0.10378E+04 
c  nu_tilda     0.71607E-05      33   0.15001E-04   0.59740E-06 0.20351E+03 
c  TempC        0.40524E+02      27   0.29236E-03   0.73338E+01 0.29642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5743          9.9363          4.5729          4.5729
v  Velocity[Y]            -2.9813          7.2376         0.12309         0.12309
v  Velocity[Z]       -1.3858e-014     6.4119e-015    -1.7339e-017    -1.7339e-017
v  ǁVelocityǁ         0.0020147          9.9369          5.1361          5.1361
v  Pressure               -33.557          18.857         -9.5668         -9.5668
v  nu_tilda           4.4152e-007       0.0042695       0.0016247       0.0016247
v  TempC                       21          73.046          21.998          21.998
v  TurbVisc           3.3442e-014       0.0050321       0.0019089       0.0019089
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1992:        0.22120E+01

===============================================================


 INSTANT    0.199300000E+04   TIME STEP NUMBER            1993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10466E-01 0.89395E+00
   Friction velocity        uk    :  0.10466E-01 0.89395E+00
   Dimensionless distance   yplus :  0.84256E-01 0.71969E+01
   Friction thermal sca.    tstar : -0.64707E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62864E-01 0.53697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10069E-01      33   0.26465E-03   0.49681E+01 0.18385E+03 
c  Velocity[X]                                      0.17908E+01 
c  Velocity[Y]                                      0.31773E+01 
c  Velocity[Z]                                      0.79533E-30 
c  Pressure     0.11077E-06     521   0.96089E-08   0.10716E+00 0.11647E+04 
c  nu_tilda     0.71630E-05      33   0.44642E-05   0.59794E-06 0.20359E+03 
c  TempC        0.40532E+02      27   0.35369E-03   0.52547E+01 0.26391E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5714          9.9354          4.5729          4.5729
v  Velocity[Y]            -2.9819          7.2547         0.12347         0.12347
v  Velocity[Z]       -1.3751e-014     6.2922e-015    -1.7324e-017    -1.7324e-017
v  ǁVelocityǁ          0.002094          9.9359          5.1361          5.1361
v  Pressure               -33.519          19.012         -9.5051         -9.5051
v  nu_tilda           4.4151e-007       0.0042695       0.0016252       0.0016252
v  TempC                       21          73.047          21.999          21.999
v  TurbVisc           3.3433e-014       0.0050321       0.0019094       0.0019094
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1993:        0.21950E+01

===============================================================


 INSTANT    0.199400000E+04   TIME STEP NUMBER            1994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.31187E-02 0.89509E+00
   Friction velocity        uk    :  0.31187E-02 0.89509E+00
   Dimensionless distance   yplus :  0.25107E-01 0.72061E+01
   Friction thermal sca.    tstar : -0.63754E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18733E-01 0.53766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10071E-01      33   0.27975E-03   0.49845E+01 0.18393E+03 
c  Velocity[X]                                      0.18150E+01 
c  Velocity[Y]                                      0.31694E+01 
c  Velocity[Z]                                      0.77560E-30 
c  Pressure     0.11106E-06     472   0.97541E-08   0.10997E+00 0.89572E+03 
c  nu_tilda     0.71653E-05      33   0.14989E-04   0.59854E-06 0.20367E+03 
c  TempC        0.40540E+02      27   0.35016E-03   0.52089E+01 0.26735E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5684          9.9344          4.5729          4.5729
v  Velocity[Y]            -2.9825          7.2321         0.12385         0.12385
v  Velocity[Z]       -1.3805e-014     6.1356e-015    -1.7308e-017    -1.7308e-017
v  ǁVelocityǁ         0.0019451          9.9349          5.1361          5.1361
v  Pressure               -33.559          18.891         -9.5269         -9.5269
v  nu_tilda           4.4149e-007       0.0042695       0.0016256       0.0016256
v  TempC                       21          73.048          21.999          21.999
v  TurbVisc           3.3429e-014       0.0050321       0.0019099       0.0019099
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1994:        0.20700E+01

===============================================================


 INSTANT    0.199500000E+04   TIME STEP NUMBER            1995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92219E-02 0.89424E+00
   Friction velocity        uk    :  0.92219E-02 0.89424E+00
   Dimensionless distance   yplus :  0.74242E-01 0.71992E+01
   Friction thermal sca.    tstar : -0.64428E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55393E-01 0.53714E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10073E-01      33   0.25163E-03   0.49747E+01 0.18397E+03 
c  Velocity[X]                                      0.17840E+01 
c  Velocity[Y]                                      0.31907E+01 
c  Velocity[Z]                                      0.95727E-30 
c  Pressure     0.11517E-06     521   0.95150E-08   0.11253E+00 0.15922E+04 
c  nu_tilda     0.71676E-05      33   0.44725E-05   0.59910E-06 0.20374E+03 
c  TempC        0.40548E+02      27   0.32235E-03   0.57586E+01 0.27935E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5655          9.9334          4.5729          4.5729
v  Velocity[Y]            -2.9836          7.2573         0.12423         0.12423
v  Velocity[Z]       -1.3951e-014     6.4123e-015    -1.7301e-017    -1.7301e-017
v  ǁVelocityǁ         0.0021687          9.9339          5.1361          5.1361
v  Pressure               -33.338           19.12         -9.4437         -9.4437
v  nu_tilda           4.4147e-007       0.0042695       0.0016261       0.0016261
v  TempC                       21          73.048          21.999          21.999
v  TurbVisc           3.3425e-014       0.0050321       0.0019104       0.0019104
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1995:        0.21930E+01

===============================================================


 INSTANT    0.199600000E+04   TIME STEP NUMBER            1996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50134E-02 0.89538E+00
   Friction velocity        uk    :  0.50134E-02 0.89538E+00
   Dimensionless distance   yplus :  0.40362E-01 0.72084E+01
   Friction thermal sca.    tstar : -0.62934E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30114E-01 0.53783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10075E-01      33   0.27390E-03   0.49416E+01 0.18380E+03 
c  Velocity[X]                                      0.17680E+01 
c  Velocity[Y]                                      0.31736E+01 
c  Velocity[Z]                                      0.85765E-30 
c  Pressure     0.10984E-06     456   0.98061E-08   0.10584E+00 0.78594E+03 
c  nu_tilda     0.71699E-05      33   0.14987E-04   0.59970E-06 0.20382E+03 
c  TempC        0.40556E+02      27   0.29542E-03   0.49486E+01 0.26311E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5626          9.9324          4.5729          4.5729
v  Velocity[Y]            -2.9845          7.2604         0.12461         0.12461
v  Velocity[Z]       -1.4009e-014     6.1645e-015    -1.7289e-017    -1.7289e-017
v  ǁVelocityǁ         0.0021468           9.933          5.1361          5.1361
v  Pressure               -33.551          19.033         -9.4565         -9.4565
v  nu_tilda           4.4147e-007       0.0042695       0.0016264       0.0016264
v  TempC                       21          73.048          21.999          21.999
v  TurbVisc           3.3416e-014       0.0050321       0.0019109       0.0019109
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1996:        0.20320E+01

===============================================================


 INSTANT    0.199700000E+04   TIME STEP NUMBER            1997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.64205E-03 0.89522E+00
   Friction velocity        uk    :  0.64205E-03 0.89522E+00
   Dimensionless distance   yplus :  0.51689E-02 0.72071E+01
   Friction thermal sca.    tstar : -0.63437E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38566E-02 0.53773E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10077E-01      33   0.29408E-03   0.49871E+01 0.18404E+03 
c  Velocity[X]                                      0.18130E+01 
c  Velocity[Y]                                      0.31742E+01 
c  Velocity[Z]                                      0.88261E-30 
c  Pressure     0.12503E-06     472   0.93178E-08   0.12528E+00 0.68120E+03 
c  nu_tilda     0.71722E-05      33   0.44803E-05   0.60026E-06 0.20390E+03 
c  TempC        0.40563E+02      27   0.29809E-03   0.50976E+01 0.26131E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5597          9.9314          4.5729          4.5729
v  Velocity[Y]            -2.9853          7.2359         0.12499         0.12499
v  Velocity[Z]        -1.377e-014     6.3409e-015    -1.7275e-017    -1.7275e-017
v  ǁVelocityǁ         0.0020232           9.932          5.1361          5.1361
v  Pressure               -33.368          19.055         -9.4193         -9.4193
v  nu_tilda           4.4152e-007       0.0042695       0.0016269       0.0016269
v  TempC                       21          73.048              22              22
v  TurbVisc           3.3416e-014       0.0050321       0.0019114       0.0019114
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1997:        0.20620E+01

===============================================================


 INSTANT    0.199800000E+04   TIME STEP NUMBER            1998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.93179E-02 0.89379E+00
   Friction velocity        uk    :  0.93179E-02 0.89379E+00
   Dimensionless distance   yplus :  0.75015E-01 0.71956E+01
   Friction thermal sca.    tstar : -0.64435E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55970E-01 0.53687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10079E-01      33   0.27087E-03   0.49878E+01 0.18411E+03 
c  Velocity[X]                                      0.17979E+01 
c  Velocity[Y]                                      0.31899E+01 
c  Velocity[Z]                                      0.81054E-30 
c  Pressure     0.10240E-06     394   0.92180E-08   0.99955E-01 0.50125E+03 
c  nu_tilda     0.71746E-05      33   0.14982E-04   0.60086E-06 0.20398E+03 
c  TempC        0.40571E+02      27   0.34344E-03   0.50412E+01 0.25081E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5568          9.9304          4.5729          4.5729
v  Velocity[Y]             -2.986           7.254         0.12537         0.12537
v  Velocity[Z]       -1.3764e-014      6.274e-015    -1.7265e-017    -1.7265e-017
v  ǁVelocityǁ         0.0021583           9.931          5.1361          5.1361
v  Pressure               -33.402          19.104         -9.4048         -9.4048
v  nu_tilda           4.4158e-007       0.0042695       0.0016272       0.0016272
v  TempC                       21          73.047              22              22
v  TurbVisc           3.3431e-014       0.0050321       0.0019119       0.0019119
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1998:        0.18870E+01

===============================================================


 INSTANT    0.199900000E+04   TIME STEP NUMBER            1999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77594E-02 0.89485E+00
   Friction velocity        uk    :  0.77594E-02 0.89485E+00
   Dimensionless distance   yplus :  0.62468E-01 0.72042E+01
   Friction thermal sca.    tstar : -0.63360E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46608E-01 0.53751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10081E-01      33   0.26735E-03   0.49781E+01 0.18404E+03 
c  Velocity[X]                                      0.17964E+01 
c  Velocity[Y]                                      0.31816E+01 
c  Velocity[Z]                                      0.62805E-30 
c  Pressure     0.13160E-06     457   0.91664E-08   0.12874E+00 0.57401E+03 
c  nu_tilda     0.71769E-05      33   0.45015E-05   0.60142E-06 0.20406E+03 
c  TempC        0.40579E+02      27   0.27534E-03   0.49487E+01 0.26186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5538          9.9294          4.5729          4.5729
v  Velocity[Y]            -2.9866          7.2295         0.12575         0.12575
v  Velocity[Z]       -1.3651e-014     6.2511e-015    -1.7259e-017    -1.7259e-017
v  ǁVelocityǁ         0.0020268          9.9299          5.1361          5.1361
v  Pressure               -33.327          19.073         -9.3783         -9.3783
v  nu_tilda           4.4166e-007       0.0042695       0.0016277       0.0016277
v  TempC                       21          73.047              22              22
v  TurbVisc           3.3452e-014       0.0050321       0.0019124       0.0019124
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             1999:        0.20320E+01

===============================================================


 INSTANT    0.200000000E+04   TIME STEP NUMBER            2000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92094E-02 0.89422E+00
   Friction velocity        uk    :  0.92094E-02 0.89422E+00
   Dimensionless distance   yplus :  0.74142E-01 0.71990E+01
   Friction thermal sca.    tstar : -0.64403E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55318E-01 0.53713E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10084E-01      33   0.22082E-03   0.49792E+01 0.18404E+03 
c  Velocity[X]                                      0.18071E+01 
c  Velocity[Y]                                      0.31721E+01 
c  Velocity[Z]                                      0.79052E-30 
c  Pressure     0.10128E-06     441   0.95565E-08   0.99131E-01 0.56939E+03 
c  nu_tilda     0.71792E-05      33   0.14972E-04   0.60202E-06 0.20414E+03 
c  TempC        0.40587E+02      27   0.40365E-03   0.53106E+01 0.25797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5508          9.9284          4.5729          4.5729
v  Velocity[Y]            -2.9872           7.255         0.12612         0.12612
v  Velocity[Z]       -1.3603e-014     6.3196e-015    -1.7244e-017    -1.7244e-017
v  ǁVelocityǁ         0.0021911          9.9289          5.1361          5.1361
v  Pressure               -33.375          19.156         -9.3552         -9.3552
v  nu_tilda           4.4161e-007       0.0042695       0.0016281       0.0016281
v  TempC                       21          73.047              22              22
v  TurbVisc           3.3476e-014       0.0050321       0.0019129       0.0019129
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2000:        0.19890E+01

===============================================================


 INSTANT    0.200100000E+04   TIME STEP NUMBER            2001
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11874E-01 0.89574E+00
   Friction velocity        uk    :  0.11874E-01 0.89574E+00
   Dimensionless distance   yplus :  0.95591E-01 0.72113E+01
   Friction thermal sca.    tstar : -0.63228E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71322E-01 0.53805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10086E-01      33   0.25806E-03   0.49477E+01 0.18404E+03 
c  Velocity[X]                                      0.17596E+01 
c  Velocity[Y]                                      0.31881E+01 
c  Velocity[Z]                                      0.10519E-29 
c  Pressure     0.99899E-07     489   0.94977E-08   0.98066E-01 0.90839E+03 
c  nu_tilda     0.71815E-05      33   0.45030E-05   0.60257E-06 0.20422E+03 
c  TempC        0.40595E+02      27   0.27960E-03   0.80968E+01 0.33691E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5479          9.9273          4.5729          4.5729
v  Velocity[Y]            -2.9882          7.2667          0.1265          0.1265
v  Velocity[Z]       -1.3402e-014     6.1629e-015    -1.7235e-017    -1.7235e-017
v  ǁVelocityǁ         0.0022672           9.928          5.1361          5.1361
v  Pressure               -33.229          19.251         -9.3061         -9.3061
v  nu_tilda           4.4151e-007       0.0042695       0.0016286       0.0016286
v  TempC                       21          73.048              22              22
v  TurbVisc           3.3461e-014       0.0050321       0.0019133       0.0019133
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2001:        0.21190E+01

===============================================================


 INSTANT    0.200200000E+04   TIME STEP NUMBER            2002
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11877E-01 0.89524E+00
   Friction velocity        uk    :  0.11877E-01 0.89524E+00
   Dimensionless distance   yplus :  0.95614E-01 0.72073E+01
   Friction thermal sca.    tstar : -0.62441E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71339E-01 0.53774E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10088E-01      33   0.26500E-03   0.49689E+01 0.18406E+03 
c  Velocity[X]                                      0.17940E+01 
c  Velocity[Y]                                      0.31749E+01 
c  Velocity[Z]                                      0.78065E-30 
c  Pressure     0.12082E-06     474   0.99078E-08   0.11901E+00 0.10678E+04 
c  nu_tilda     0.71838E-05      33   0.14973E-04   0.60318E-06 0.20429E+03 
c  TempC        0.40602E+02      27   0.34303E-03   0.42859E+01 0.25417E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.545          9.9263          4.5729          4.5729
v  Velocity[Y]            -2.9891          7.2324         0.12688         0.12688
v  Velocity[Z]       -1.3338e-014     6.1967e-015    -1.7219e-017    -1.7219e-017
v  ǁVelocityǁ         0.0020092           9.927          5.1361          5.1361
v  Pressure               -33.366          19.087         -9.3312         -9.3312
v  nu_tilda           4.4154e-007       0.0042695       0.0016289       0.0016289
v  TempC                       21          73.047          22.001          22.001
v  TurbVisc           3.3429e-014       0.0050321       0.0019138       0.0019138
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2002:        0.20840E+01

===============================================================


 INSTANT    0.200300000E+04   TIME STEP NUMBER            2003
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98130E-02 0.89392E+00
   Friction velocity        uk    :  0.98130E-02 0.89392E+00
   Dimensionless distance   yplus :  0.79001E-01 0.71966E+01
   Friction thermal sca.    tstar : -0.64351E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58944E-01 0.53695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10090E-01      33   0.29197E-03   0.49653E+01 0.18412E+03 
c  Velocity[X]                                      0.17931E+01 
c  Velocity[Y]                                      0.31722E+01 
c  Velocity[Z]                                      0.80333E-30 
c  Pressure     0.10741E-06     537   0.91522E-08   0.10486E+00 0.13675E+04 
c  nu_tilda     0.71861E-05      33   0.45161E-05   0.60372E-06 0.20437E+03 
c  TempC        0.40610E+02      27   0.29352E-03   0.56041E+01 0.27333E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.542          9.9253          4.5729          4.5729
v  Velocity[Y]            -2.9899          7.2562         0.12726         0.12726
v  Velocity[Z]       -1.3018e-014     6.0978e-015     -1.721e-017     -1.721e-017
v  ǁVelocityǁ         0.0021954           9.926          5.1361          5.1361
v  Pressure               -33.193          19.284          -9.261          -9.261
v  nu_tilda           4.4158e-007       0.0042695       0.0016294       0.0016294
v  TempC                       21          73.048          22.001          22.001
v  TurbVisc           3.3437e-014       0.0050321       0.0019143       0.0019143
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2003:        0.22090E+01

===============================================================


 INSTANT    0.200400000E+04   TIME STEP NUMBER            2004
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74455E-02 0.89492E+00
   Friction velocity        uk    :  0.74455E-02 0.89492E+00
   Dimensionless distance   yplus :  0.59941E-01 0.72047E+01
   Friction thermal sca.    tstar : -0.67081E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44723E-01 0.53755E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10092E-01      33   0.27984E-03   0.49887E+01 0.18427E+03 
c  Velocity[X]                                      0.18003E+01 
c  Velocity[Y]                                      0.31884E+01 
c  Velocity[Z]                                      0.72226E-30 
c  Pressure     0.11135E-06     472   0.99101E-08   0.11056E+00 0.92103E+03 
c  nu_tilda     0.71884E-05      33   0.14962E-04   0.60431E-06 0.20445E+03 
c  TempC        0.40618E+02      27   0.26458E-03   0.55082E+01 0.26584E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.539          9.9243          4.5729          4.5729
v  Velocity[Y]            -2.9906          7.2314         0.12764         0.12764
v  Velocity[Z]       -1.2833e-014     6.4154e-015    -1.7204e-017    -1.7204e-017
v  ǁVelocityǁ         0.0020286          9.9249          5.1361          5.1361
v  Pressure               -33.211          19.159         -9.2788         -9.2788
v  nu_tilda           4.4162e-007       0.0042695       0.0016297       0.0016297
v  TempC                       21          73.047          22.001          22.001
v  TurbVisc            3.345e-014       0.0050321       0.0019148       0.0019148
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2004:        0.20760E+01

===============================================================


 INSTANT    0.200500000E+04   TIME STEP NUMBER            2005
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.77152E-02 0.89404E+00
   Friction velocity        uk    :  0.77152E-02 0.89404E+00
   Dimensionless distance   yplus :  0.62113E-01 0.71976E+01
   Friction thermal sca.    tstar : -0.68785E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46343E-01 0.53702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10094E-01      33   0.21615E-03   0.49692E+01 0.18416E+03 
c  Velocity[X]                                      0.17920E+01 
c  Velocity[Y]                                      0.31772E+01 
c  Velocity[Z]                                      0.67897E-30 
c  Pressure     0.11907E-06     504   0.91282E-08   0.11482E+00 0.13262E+04 
c  nu_tilda     0.71908E-05      33   0.45246E-05   0.60487E-06 0.20452E+03 
c  TempC        0.40626E+02      27   0.41000E-03   0.50372E+01 0.25690E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5361          9.9233          4.5729          4.5729
v  Velocity[Y]            -2.9912          7.2531         0.12802         0.12802
v  Velocity[Z]       -1.2861e-014     6.2009e-015    -1.7189e-017    -1.7189e-017
v  ǁVelocityǁ         0.0021515          9.9239          5.1361          5.1361
v  Pressure               -33.174          19.336         -9.2075         -9.2075
v  nu_tilda           4.4164e-007       0.0042695       0.0016302       0.0016302
v  TempC                       21          73.048          22.001          22.001
v  TurbVisc           3.3463e-014       0.0050321       0.0019153       0.0019153
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2005:        0.21980E+01

===============================================================


 INSTANT    0.200600000E+04   TIME STEP NUMBER            2006
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11320E-02 0.89546E+00
   Friction velocity        uk    :  0.11320E-02 0.89546E+00
   Dimensionless distance   yplus :  0.91134E-02 0.72091E+01
   Friction thermal sca.    tstar : -0.81884E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67996E-02 0.53788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10096E-01      33   0.27495E-03   0.49592E+01 0.18413E+03 
c  Velocity[X]                                      0.17867E+01 
c  Velocity[Y]                                      0.31725E+01 
c  Velocity[Z]                                      0.84629E-30 
c  Pressure     0.99616E-07     378   0.96545E-08   0.97466E-01 0.55259E+03 
c  nu_tilda     0.71931E-05      33   0.14961E-04   0.60548E-06 0.20460E+03 
c  TempC        0.40633E+02      27   0.28858E-03   0.81490E+01 0.31634E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5332          9.9223          4.5729          4.5729
v  Velocity[Y]            -2.9917          7.2613         0.12839         0.12839
v  Velocity[Z]       -1.2936e-014     6.1678e-015    -1.7175e-017    -1.7175e-017
v  ǁVelocityǁ         0.0022179           9.923          5.1361          5.1361
v  Pressure               -33.246          19.315         -9.2071         -9.2071
v  nu_tilda           4.4162e-007       0.0042695       0.0016306       0.0016306
v  TempC                       21          73.048          22.001          22.001
v  TurbVisc            3.347e-014       0.0050321       0.0019158       0.0019158
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2006:        0.20250E+01

===============================================================


 INSTANT    0.200700000E+04   TIME STEP NUMBER            2007
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12364E-01 0.89502E+00
   Friction velocity        uk    :  0.12364E-01 0.89502E+00
   Dimensionless distance   yplus :  0.99542E-01 0.72056E+01
   Friction thermal sca.    tstar : -0.92297E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74269E-01 0.53762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10098E-01      33   0.24888E-03   0.49771E+01 0.18428E+03 
c  Velocity[X]                                      0.17835E+01 
c  Velocity[Y]                                      0.31935E+01 
c  Velocity[Z]                                      0.99057E-30 
c  Pressure     0.12503E-06     489   0.95738E-08   0.12435E+00 0.61979E+03 
c  nu_tilda     0.71954E-05      33   0.45325E-05   0.60602E-06 0.20468E+03 
c  TempC        0.40641E+02      27   0.35366E-03   0.45399E+01 0.24566E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5302          9.9213          4.5729          4.5729
v  Velocity[Y]            -2.9926          7.2343         0.12877         0.12877
v  Velocity[Z]       -1.2913e-014     6.1173e-015    -1.7162e-017    -1.7162e-017
v  ǁVelocityǁ         0.0020777           9.922          5.1361          5.1361
v  Pressure                -33.02          19.307         -9.1757         -9.1757
v  nu_tilda           4.4162e-007       0.0042695        0.001631        0.001631
v  TempC                       21          73.049          22.002          22.002
v  TurbVisc           3.3464e-014       0.0050321       0.0019163       0.0019163
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2007:        0.27410E+01

===============================================================


 INSTANT    0.200800000E+04   TIME STEP NUMBER            2008
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99846E-02 0.89351E+00
   Friction velocity        uk    :  0.99846E-02 0.89351E+00
   Dimensionless distance   yplus :  0.80383E-01 0.71934E+01
   Friction thermal sca.    tstar : -0.12498E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59974E-01 0.53671E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10100E-01      33   0.27039E-03   0.49508E+01 0.18414E+03 
c  Velocity[X]                                      0.17763E+01 
c  Velocity[Y]                                      0.31745E+01 
c  Velocity[Z]                                      0.83333E-30 
c  Pressure     0.11559E-06     394   0.99342E-08   0.11121E+00 0.49679E+03 
c  nu_tilda     0.71977E-05      33   0.14955E-04   0.60661E-06 0.20476E+03 
c  TempC        0.40649E+02      28   0.32093E-03   0.55691E+01 0.27091E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5272          9.9203          4.5729          4.5729
v  Velocity[Y]            -2.9935          7.2483         0.12915         0.12915
v  Velocity[Z]       -1.2971e-014     6.3383e-015    -1.7144e-017    -1.7144e-017
v  ǁVelocityǁ         0.0021359           9.921          5.1361          5.1361
v  Pressure               -33.183          19.337         -9.1624         -9.1624
v  nu_tilda           4.4162e-007       0.0042695       0.0016314       0.0016314
v  TempC                       21          73.048          22.002          22.002
v  TurbVisc           3.3462e-014       0.0050321       0.0019168       0.0019168
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2008:        0.22060E+01

===============================================================


 INSTANT    0.200900000E+04   TIME STEP NUMBER            2009
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94646E-02 0.89478E+00
   Friction velocity        uk    :  0.94646E-02 0.89478E+00
   Dimensionless distance   yplus :  0.76197E-01 0.72036E+01
   Friction thermal sca.    tstar : -0.19164E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56851E-01 0.53747E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10102E-01      33   0.29840E-03   0.49701E+01 0.18429E+03 
c  Velocity[X]                                      0.17999E+01 
c  Velocity[Y]                                      0.31701E+01 
c  Velocity[Z]                                      0.82608E-30 
c  Pressure     0.12079E-06     458   0.96382E-08   0.11978E+00 0.63256E+03 
c  nu_tilda     0.72000E-05      33   0.45519E-05   0.60715E-06 0.20483E+03 
c  TempC        0.40657E+02      27   0.32907E-03   0.48095E+01 0.25519E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5242          9.9193          4.5729          4.5729
v  Velocity[Y]            -2.9943          7.2303         0.12952         0.12952
v  Velocity[Z]       -1.2921e-014     6.2151e-015    -1.7131e-017    -1.7131e-017
v  ǁVelocityǁ         0.0020203            9.92          5.1361          5.1361
v  Pressure               -33.025          19.338           -9.13           -9.13
v  nu_tilda           4.4162e-007       0.0042695       0.0016319       0.0016319
v  TempC                       21          73.049          22.002          22.002
v  TurbVisc           3.3463e-014       0.0050321       0.0019173       0.0019173
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2009:        0.21580E+01

===============================================================


 INSTANT    0.201000000E+04   TIME STEP NUMBER            2010
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88966E-02 0.89400E+00
   Friction velocity        uk    :  0.88966E-02 0.89400E+00
   Dimensionless distance   yplus :  0.71623E-01 0.71973E+01
   Friction thermal sca.    tstar : -0.20384E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53439E-01 0.53700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10104E-01      33   0.20804E-03   0.49810E+01 0.18439E+03 
c  Velocity[X]                                      0.17933E+01 
c  Velocity[Y]                                      0.31877E+01 
c  Velocity[Z]                                      0.90567E-30 
c  Pressure     0.10724E-06     440   0.99482E-08   0.10555E+00 0.58763E+03 
c  nu_tilda     0.72023E-05      33   0.14945E-04   0.60775E-06 0.20491E+03 
c  TempC        0.40664E+02      27   0.32358E-03   0.52811E+01 0.26787E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5213          9.9183          4.5729          4.5729
v  Velocity[Y]             -2.995           7.254          0.1299          0.1299
v  Velocity[Z]       -1.2902e-014     6.3285e-015    -1.7122e-017    -1.7122e-017
v  ǁVelocityǁ         0.0021665          9.9189          5.1361          5.1361
v  Pressure               -33.038          19.423         -9.1046         -9.1046
v  nu_tilda           4.4158e-007       0.0042695       0.0016322       0.0016322
v  TempC                       21          73.048          22.002          22.002
v  TurbVisc           3.3462e-014       0.0050321       0.0019178       0.0019178
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2010:        0.21260E+01

===============================================================


 INSTANT    0.201100000E+04   TIME STEP NUMBER            2011
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53117E-02 0.89552E+00
   Friction velocity        uk    :  0.53117E-02 0.89552E+00
   Dimensionless distance   yplus :  0.42763E-01 0.72095E+01
   Friction thermal sca.    tstar : -0.12744E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31906E-01 0.53791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10106E-01      33   0.26440E-03   0.49428E+01 0.18421E+03 
c  Velocity[X]                                      0.17669E+01 
c  Velocity[Y]                                      0.31759E+01 
c  Velocity[Z]                                      0.67896E-30 
c  Pressure     0.12308E-06     490   0.93597E-08   0.11812E+00 0.78388E+03 
c  nu_tilda     0.72046E-05      33   0.45544E-05   0.60829E-06 0.20499E+03 
c  TempC        0.40672E+02      27   0.30000E-03   0.47745E+01 0.25684E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5184          9.9173          4.5729          4.5729
v  Velocity[Y]            -2.9956          7.2607         0.13028         0.13028
v  Velocity[Z]       -1.2776e-014     6.1633e-015    -1.7107e-017    -1.7107e-017
v  ǁVelocityǁ         0.0022207          9.9179          5.1361          5.1361
v  Pressure               -33.025           19.48         -9.0613         -9.0613
v  nu_tilda            4.415e-007       0.0042695       0.0016327       0.0016327
v  TempC                       21          73.048          22.002          22.002
v  TurbVisc            3.345e-014       0.0050321       0.0019182       0.0019182
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2011:        0.21180E+01

===============================================================


 INSTANT    0.201200000E+04   TIME STEP NUMBER            2012
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11815E-01 0.89519E+00
   Friction velocity        uk    :  0.11815E-01 0.89519E+00
   Dimensionless distance   yplus :  0.95118E-01 0.72069E+01
   Friction thermal sca.    tstar : -0.93579E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70969E-01 0.53771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10108E-01      33   0.26911E-03   0.49809E+01 0.18436E+03 
c  Velocity[X]                                      0.18122E+01 
c  Velocity[Y]                                      0.31687E+01 
c  Velocity[Z]                                      0.73577E-30 
c  Pressure     0.10890E-06     458   0.97765E-08   0.10800E+00 0.87462E+03 
c  nu_tilda     0.72069E-05      33   0.14948E-04   0.60889E-06 0.20506E+03 
c  TempC        0.40680E+02      27   0.30688E-03   0.44717E+01 0.25460E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5154          9.9163          4.5729          4.5729
v  Velocity[Y]            -2.9961          7.2327         0.13065         0.13065
v  Velocity[Z]       -1.2694e-014      6.186e-015    -1.7097e-017    -1.7097e-017
v  ǁVelocityǁ         0.0020402          9.9169          5.1361          5.1361
v  Pressure               -33.039          19.364         -9.0782         -9.0782
v  nu_tilda           4.4148e-007       0.0042695        0.001633        0.001633
v  TempC                       21          73.048          22.003          22.003
v  TurbVisc           3.3426e-014       0.0050321       0.0019187       0.0019187
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2012:        0.20440E+01

===============================================================


 INSTANT    0.201300000E+04   TIME STEP NUMBER            2013
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10757E-01 0.89379E+00
   Friction velocity        uk    :  0.10757E-01 0.89379E+00
   Dimensionless distance   yplus :  0.86598E-01 0.71956E+01
   Friction thermal sca.    tstar : -0.83258E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64612E-01 0.53687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10110E-01      33   0.26515E-03   0.49620E+01 0.18438E+03 
c  Velocity[X]                                      0.17684E+01 
c  Velocity[Y]                                      0.31936E+01 
c  Velocity[Z]                                      0.90216E-30 
c  Pressure     0.10997E-06     536   0.93827E-08   0.10837E+00 0.15581E+04 
c  nu_tilda     0.72092E-05      33   0.45675E-05   0.60944E-06 0.20514E+03 
c  TempC        0.40688E+02      27   0.30364E-03   0.50348E+01 0.25287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5123          9.9153          4.5729          4.5729
v  Velocity[Y]            -2.9969          7.2543         0.13103         0.13103
v  Velocity[Z]       -1.2584e-014     6.1483e-015    -1.7095e-017    -1.7095e-017
v  ǁVelocityǁ         0.0022152          9.9159          5.1361          5.1361
v  Pressure                -32.83           19.58         -8.9967         -8.9967
v  nu_tilda           4.4146e-007       0.0042695       0.0016335       0.0016335
v  TempC                       21          73.049          22.003          22.003
v  TurbVisc           3.3421e-014       0.0050321       0.0019192       0.0019192
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2013:        0.22770E+01

===============================================================


 INSTANT    0.201400000E+04   TIME STEP NUMBER            2014
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.62303E-02 0.89471E+00
   Friction velocity        uk    :  0.62303E-02 0.89471E+00
   Dimensionless distance   yplus :  0.50158E-01 0.72030E+01
   Friction thermal sca.    tstar : -0.70135E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37423E-01 0.53743E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10112E-01      33   0.28089E-03   0.49587E+01 0.18433E+03 
c  Velocity[X]                                      0.17826E+01 
c  Velocity[Y]                                      0.31760E+01 
c  Velocity[Z]                                      0.78948E-30 
c  Pressure     0.12288E-06     489   0.94946E-08   0.11963E+00 0.13010E+04 
c  nu_tilda     0.72115E-05      33   0.14933E-04   0.61002E-06 0.20521E+03 
c  TempC        0.40695E+02      27   0.33748E-03   0.49831E+01 0.25006E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5094          9.9144          4.5729          4.5729
v  Velocity[Y]            -2.9978          7.2258          0.1314          0.1314
v  Velocity[Z]       -1.2443e-014     6.2202e-015    -1.7085e-017    -1.7085e-017
v  ǁVelocityǁ         0.0019831          9.9149          5.1361          5.1361
v  Pressure               -33.018          19.386         -9.0317         -9.0317
v  nu_tilda           4.4145e-007       0.0042695       0.0016339       0.0016339
v  TempC                       21          73.048          22.003          22.003
v  TurbVisc           3.3414e-014       0.0050321       0.0019197       0.0019197
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2014:        0.21050E+01

===============================================================


 INSTANT    0.201500000E+04   TIME STEP NUMBER            2015
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95656E-02 0.89403E+00
   Friction velocity        uk    :  0.95656E-02 0.89403E+00
   Dimensionless distance   yplus :  0.77010E-01 0.71975E+01
   Friction thermal sca.    tstar : -0.66329E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57458E-01 0.53702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10114E-01      33   0.29013E-03   0.49647E+01 0.18442E+03 
c  Velocity[X]                                      0.17945E+01 
c  Velocity[Y]                                      0.31702E+01 
c  Velocity[Z]                                      0.85971E-30 
c  Pressure     0.11694E-06     537   0.97919E-08   0.11358E+00 0.16046E+04 
c  nu_tilda     0.72138E-05      33   0.45747E-05   0.61056E-06 0.20529E+03 
c  TempC        0.40703E+02      27   0.27363E-03   0.60632E+01 0.28210E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5064          9.9134          4.5729          4.5729
v  Velocity[Y]            -2.9986          7.2536         0.13178         0.13178
v  Velocity[Z]       -1.2222e-014     6.2487e-015    -1.7081e-017    -1.7081e-017
v  ǁVelocityǁ         0.0022141          9.9139          5.1361          5.1361
v  Pressure               -32.829          19.618         -8.9496         -8.9496
v  nu_tilda           4.4141e-007       0.0042695       0.0016343       0.0016343
v  TempC                       21          73.049          22.003          22.003
v  TurbVisc            3.341e-014       0.0050321       0.0019202       0.0019202
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2015:        0.22370E+01

===============================================================


 INSTANT    0.201600000E+04   TIME STEP NUMBER            2016
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.46242E-02 0.89524E+00
   Friction velocity        uk    :  0.46242E-02 0.89524E+00
   Dimensionless distance   yplus :  0.37228E-01 0.72073E+01
   Friction thermal sca.    tstar : -0.66282E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27776E-01 0.53775E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10116E-01      33   0.26552E-03   0.49579E+01 0.18444E+03 
c  Velocity[X]                                      0.17711E+01 
c  Velocity[Y]                                      0.31868E+01 
c  Velocity[Z]                                      0.75361E-30 
c  Pressure     0.10766E-06     393   0.97370E-08   0.10541E+00 0.60093E+03 
c  nu_tilda     0.72162E-05      33   0.14933E-04   0.61115E-06 0.20536E+03 
c  TempC        0.40711E+02      27   0.34533E-03   0.41452E+01 0.24983E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5035          9.9124          4.5729          4.5729
v  Velocity[Y]            -2.9992            7.26         0.13215         0.13215
v  Velocity[Z]       -1.2029e-014     6.3166e-015    -1.7069e-017    -1.7069e-017
v  ǁVelocityǁ         0.0022827          9.9129          5.1361          5.1361
v  Pressure               -32.887          19.584         -8.9487         -8.9487
v  nu_tilda           4.4138e-007       0.0042695       0.0016347       0.0016347
v  TempC                       21          73.048          22.004          22.004
v  TurbVisc           3.3398e-014       0.0050321       0.0019207       0.0019207
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2016:        0.18990E+01

===============================================================


 INSTANT    0.201700000E+04   TIME STEP NUMBER            2017
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13105E-01 0.89483E+00
   Friction velocity        uk    :  0.13105E-01 0.89483E+00
   Dimensionless distance   yplus :  0.10550E+00 0.72040E+01
   Friction thermal sca.    tstar : -0.66586E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78715E-01 0.53750E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10118E-01      33   0.25774E-03   0.49675E+01 0.18446E+03 
c  Velocity[X]                                      0.17906E+01 
c  Velocity[Y]                                      0.31769E+01 
c  Velocity[Z]                                      0.72141E-30 
c  Pressure     0.12351E-06     441   0.97164E-08   0.12110E+00 0.54575E+03 
c  nu_tilda     0.72185E-05      33   0.45829E-05   0.61169E-06 0.20544E+03 
c  TempC        0.40719E+02      27   0.32637E-03   0.53396E+01 0.25328E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5004          9.9114          4.5729          4.5729
v  Velocity[Y]            -2.9998          7.2293         0.13252         0.13252
v  Velocity[Z]       -1.1825e-014     6.2175e-015    -1.7063e-017    -1.7063e-017
v  ǁVelocityǁ         0.0020386          9.9119          5.1361          5.1361
v  Pressure               -32.845          19.528         -8.9312         -8.9312
v  nu_tilda           4.4138e-007       0.0042695       0.0016352       0.0016352
v  TempC                       21          73.048          22.004          22.004
v  TurbVisc           3.3389e-014       0.0050321       0.0019212       0.0019212
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2017:        0.19950E+01

===============================================================


 INSTANT    0.201800000E+04   TIME STEP NUMBER            2018
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82163E-02 0.89355E+00
   Friction velocity        uk    :  0.82163E-02 0.89355E+00
   Dimensionless distance   yplus :  0.66147E-01 0.71937E+01
   Friction thermal sca.    tstar : -0.68161E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49353E-01 0.53673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10120E-01      33   0.26596E-03   0.49605E+01 0.18442E+03 
c  Velocity[X]                                      0.17924E+01 
c  Velocity[Y]                                      0.31681E+01 
c  Velocity[Z]                                      0.81956E-30 
c  Pressure     0.10450E-06     472   0.91540E-08   0.10187E+00 0.65123E+03 
c  nu_tilda     0.72208E-05      33   0.14929E-04   0.61228E-06 0.20552E+03 
c  TempC        0.40726E+02      27   0.33832E-03   0.50933E+01 0.23910E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4973          9.9104          4.5729          4.5729
v  Velocity[Y]            -3.0003          7.2496          0.1329          0.1329
v  Velocity[Z]        -1.186e-014      6.223e-015    -1.7054e-017    -1.7054e-017
v  ǁVelocityǁ         0.0021577           9.911          5.1361          5.1361
v  Pressure               -32.859          19.617         -8.9002         -8.9002
v  nu_tilda           4.4136e-007       0.0042695       0.0016355       0.0016355
v  TempC                       21          73.048          22.004          22.004
v  TurbVisc           3.3389e-014       0.0050321       0.0019216       0.0019216
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2018:        0.20740E+01

===============================================================


 INSTANT    0.201900000E+04   TIME STEP NUMBER            2019
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17876E-02 0.89468E+00
   Friction velocity        uk    :  0.17876E-02 0.89468E+00
   Dimensionless distance   yplus :  0.14392E-01 0.72028E+01
   Friction thermal sca.    tstar : -0.69783E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10738E-01 0.53741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10122E-01      33   0.26216E-03   0.49612E+01 0.18451E+03 
c  Velocity[X]                                      0.17714E+01 
c  Velocity[Y]                                      0.31897E+01 
c  Velocity[Z]                                      0.88031E-30 
c  Pressure     0.13007E-06     506   0.98793E-08   0.12897E+00 0.73245E+03 
c  nu_tilda     0.72231E-05      33   0.46017E-05   0.61281E-06 0.20559E+03 
c  TempC        0.40734E+02      27   0.28251E-03   0.47837E+01 0.24041E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4945          9.9095          4.5729          4.5729
v  Velocity[Y]             -3.001          7.2282         0.13327         0.13327
v  Velocity[Z]       -1.1749e-014     6.3641e-015    -1.7049e-017    -1.7049e-017
v  ǁVelocityǁ         0.0020927            9.91           5.136           5.136
v  Pressure               -32.633          19.643         -8.8597         -8.8597
v  nu_tilda           4.4137e-007       0.0042695        0.001636        0.001636
v  TempC                       21          73.048          22.004          22.004
v  TurbVisc           3.3384e-014       0.0050321       0.0019221       0.0019221
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2019:        0.21440E+01

===============================================================


 INSTANT    0.202000000E+04   TIME STEP NUMBER            2020
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.36726E-02 0.89371E+00
   Friction velocity        uk    :  0.36726E-02 0.89371E+00
   Dimensionless distance   yplus :  0.29567E-01 0.71950E+01
   Friction thermal sca.    tstar : -0.66755E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22060E-01 0.53683E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10124E-01      33   0.22223E-03   0.49475E+01 0.18442E+03 
c  Velocity[X]                                      0.17722E+01 
c  Velocity[Y]                                      0.31753E+01 
c  Velocity[Z]                                      0.81867E-30 
c  Pressure     0.11908E-06     376   0.95606E-08   0.11461E+00 0.53958E+03 
c  nu_tilda     0.72254E-05      33   0.14918E-04   0.61342E-06 0.20567E+03 
c  TempC        0.40742E+02      27   0.22953E-03   0.36967E+01 0.22448E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4915          9.9085          4.5729          4.5729
v  Velocity[Y]            -3.0019          7.2483         0.13364         0.13364
v  Velocity[Z]       -1.1589e-014     6.1056e-015    -1.7043e-017    -1.7043e-017
v  ǁVelocityǁ         0.0021481           9.909           5.136           5.136
v  Pressure               -32.816          19.652         -8.8509         -8.8509
v  nu_tilda           4.4137e-007       0.0042695       0.0016363       0.0016363
v  TempC                       21          73.049          22.004          22.004
v  TurbVisc           3.3386e-014       0.0050321       0.0019226       0.0019226
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2020:        0.21100E+01

===============================================================


 INSTANT    0.202100000E+04   TIME STEP NUMBER            2021
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.27836E-02 0.89549E+00
   Friction velocity        uk    :  0.27836E-02 0.89549E+00
   Dimensionless distance   yplus :  0.22410E-01 0.72093E+01
   Friction thermal sca.    tstar : -0.67732E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16720E-01 0.53789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10126E-01      33   0.29739E-03   0.49430E+01 0.18447E+03 
c  Velocity[X]                                      0.17698E+01 
c  Velocity[Y]                                      0.31732E+01 
c  Velocity[Z]                                      0.10256E-29 
c  Pressure     0.11759E-06     505   0.98715E-08   0.11591E+00 0.10913E+04 
c  nu_tilda     0.72277E-05      33   0.46029E-05   0.61394E-06 0.20574E+03 
c  TempC        0.40749E+02      27   0.35788E-03   0.39631E+01 0.23766E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4885          9.9075          4.5729          4.5729
v  Velocity[Y]            -3.0026          7.2623         0.13401         0.13401
v  Velocity[Z]        -1.138e-014     6.3136e-015    -1.7034e-017    -1.7034e-017
v  ǁVelocityǁ         0.0022382           9.908           5.136           5.136
v  Pressure               -32.688          19.777         -8.7923         -8.7923
v  nu_tilda           4.4135e-007       0.0042695       0.0016368       0.0016368
v  TempC                       21          73.048          22.005          22.005
v  TurbVisc           3.3387e-014       0.0050321       0.0019231       0.0019231
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2021:        0.23220E+01

===============================================================


 INSTANT    0.202200000E+04   TIME STEP NUMBER            2022
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11924E-01 0.89512E+00
   Friction velocity        uk    :  0.11924E-01 0.89512E+00
   Dimensionless distance   yplus :  0.95999E-01 0.72063E+01
   Friction thermal sca.    tstar : -0.65753E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71626E-01 0.53767E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10128E-01      33   0.25949E-03   0.49854E+01 0.18469E+03 
c  Velocity[X]                                      0.17970E+01 
c  Velocity[Y]                                      0.31885E+01 
c  Velocity[Z]                                      0.87909E-30 
c  Pressure     0.12026E-06     474   0.95875E-08   0.11921E+00 0.10170E+04 
c  nu_tilda     0.72300E-05      33   0.14920E-04   0.61454E-06 0.20582E+03 
c  TempC        0.40757E+02      27   0.30676E-03   0.65300E+01 0.28342E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4854          9.9065          4.5729          4.5729
v  Velocity[Y]            -3.0033          7.2317         0.13439         0.13439
v  Velocity[Z]       -1.1243e-014      6.364e-015    -1.7031e-017    -1.7031e-017
v  ǁVelocityǁ         0.0020521           9.907           5.136           5.136
v  Pressure               -32.698          19.639         -8.8131         -8.8131
v  nu_tilda           4.4143e-007       0.0042695       0.0016372       0.0016372
v  TempC                       21          73.048          22.005          22.005
v  TurbVisc            3.338e-014       0.0050321       0.0019236       0.0019236
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2022:        0.20740E+01

===============================================================


 INSTANT    0.202300000E+04   TIME STEP NUMBER            2023
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10614E-01 0.89355E+00
   Friction velocity        uk    :  0.10614E-01 0.89355E+00
   Dimensionless distance   yplus :  0.85449E-01 0.71937E+01
   Friction thermal sca.    tstar : -0.68899E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63755E-01 0.53673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10130E-01      33   0.25842E-03   0.49529E+01 0.18452E+03 
c  Velocity[X]                                      0.17756E+01 
c  Velocity[Y]                                      0.31773E+01 
c  Velocity[Z]                                      0.72626E-30 
c  Pressure     0.12331E-06     521   0.94990E-08   0.11880E+00 0.13230E+04 
c  nu_tilda     0.72323E-05      33   0.46174E-05   0.61506E-06 0.20589E+03 
c  TempC        0.40765E+02      27   0.34363E-03   0.47412E+01 0.25505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4824          9.9055          4.5729          4.5729
v  Velocity[Y]            -3.0039          7.2486         0.13476         0.13476
v  Velocity[Z]       -1.1087e-014     6.2348e-015    -1.7032e-017    -1.7032e-017
v  ǁVelocityǁ         0.0021773          9.9061           5.136           5.136
v  Pressure               -32.626          19.804         -8.7425         -8.7425
v  nu_tilda           4.4151e-007       0.0042695       0.0016376       0.0016376
v  TempC                       21          73.048          22.005          22.005
v  TurbVisc           3.3404e-014       0.0050321       0.0019241       0.0019241
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2023:        0.21970E+01

===============================================================


 INSTANT    0.202400000E+04   TIME STEP NUMBER            2024
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91186E-02 0.89470E+00
   Friction velocity        uk    :  0.91186E-02 0.89470E+00
   Dimensionless distance   yplus :  0.73411E-01 0.72030E+01
   Friction thermal sca.    tstar : -0.68176E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54773E-01 0.53742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10132E-01      33   0.27550E-03   0.49688E+01 0.18459E+03 
c  Velocity[X]                                      0.17990E+01 
c  Velocity[Y]                                      0.31698E+01 
c  Velocity[Z]                                      0.79428E-30 
c  Pressure     0.11022E-06     488   0.94002E-08   0.10903E+00 0.92727E+03 
c  nu_tilda     0.72346E-05      33   0.14908E-04   0.61565E-06 0.20596E+03 
c  TempC        0.40773E+02      27   0.31990E-03   0.55971E+01 0.27121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4794          9.9045          4.5729          4.5729
v  Velocity[Y]            -3.0044          7.2264         0.13513         0.13513
v  Velocity[Z]       -1.0917e-014     6.4479e-015    -1.7026e-017    -1.7026e-017
v  ǁVelocityǁ         0.0020259          9.9051           5.136           5.136
v  Pressure               -32.661          19.687         -8.7602         -8.7602
v  nu_tilda           4.4153e-007       0.0042695        0.001638        0.001638
v  TempC                       21          73.047          22.005          22.005
v  TurbVisc           3.3428e-014       0.0050321       0.0019245       0.0019245
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2024:        0.21160E+01

===============================================================


 INSTANT    0.202500000E+04   TIME STEP NUMBER            2025
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.63470E-02 0.89390E+00
   Friction velocity        uk    :  0.63470E-02 0.89390E+00
   Dimensionless distance   yplus :  0.51098E-01 0.71965E+01
   Friction thermal sca.    tstar : -0.72627E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38125E-01 0.53694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10134E-01      33   0.20955E-03   0.49508E+01 0.18463E+03 
c  Velocity[X]                                      0.17647E+01 
c  Velocity[Y]                                      0.31861E+01 
c  Velocity[Z]                                      0.78864E-30 
c  Pressure     0.10773E-06     520   0.91891E-08   0.10480E+00 0.14598E+04 
c  nu_tilda     0.72369E-05      33   0.46236E-05   0.61618E-06 0.20604E+03 
c  TempC        0.40780E+02      27   0.38522E-03   0.47356E+01 0.25220E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4764          9.9036          4.5729          4.5729
v  Velocity[Y]             -3.005          7.2521          0.1355          0.1355
v  Velocity[Z]       -1.0746e-014     6.2308e-015    -1.7025e-017    -1.7025e-017
v  ǁVelocityǁ          0.002226          9.9041           5.136           5.136
v  Pressure               -32.493          19.891         -8.6841         -8.6841
v  nu_tilda           4.4148e-007       0.0042695       0.0016384       0.0016384
v  TempC                       21          73.048          22.005          22.005
v  TurbVisc           3.3434e-014       0.0050321        0.001925        0.001925
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2025:        0.22000E+01

===============================================================


 INSTANT    0.202600000E+04   TIME STEP NUMBER            2026
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11814E-01 0.89507E+00
   Friction velocity        uk    :  0.11814E-01 0.89507E+00
   Dimensionless distance   yplus :  0.95108E-01 0.72059E+01
   Friction thermal sca.    tstar : -0.72404E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70961E-01 0.53764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10136E-01      33   0.27287E-03   0.49215E+01 0.18446E+03 
c  Velocity[X]                                      0.17504E+01 
c  Velocity[Y]                                      0.31711E+01 
c  Velocity[Z]                                      0.82998E-30 
c  Pressure     0.12265E-06     424   0.97282E-08   0.11888E+00 0.65571E+03 
c  nu_tilda     0.72392E-05      33   0.14906E-04   0.61676E-06 0.20611E+03 
c  TempC        0.40788E+02      27   0.30994E-03   0.54702E+01 0.26207E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4733          9.9026          4.5729          4.5729
v  Velocity[Y]            -3.0058          7.2548         0.13587         0.13587
v  Velocity[Z]       -1.0552e-014     6.4349e-015    -1.7022e-017    -1.7022e-017
v  ǁVelocityǁ         0.0022218          9.9031           5.136           5.136
v  Pressure               -32.675          19.834         -8.6866         -8.6866
v  nu_tilda           4.4138e-007       0.0042695       0.0016388       0.0016388
v  TempC                       21          73.048          22.005          22.005
v  TurbVisc           3.3419e-014       0.0050321       0.0019255       0.0019255
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2026:        0.19690E+01

===============================================================


 INSTANT    0.202700000E+04   TIME STEP NUMBER            2027
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87724E-02 0.89484E+00
   Friction velocity        uk    :  0.87724E-02 0.89484E+00
   Dimensionless distance   yplus :  0.70624E-01 0.72041E+01
   Friction thermal sca.    tstar : -0.71726E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52693E-01 0.53751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10138E-01      33   0.29450E-03   0.49669E+01 0.18471E+03 
c  Velocity[X]                                      0.17948E+01 
c  Velocity[Y]                                      0.31721E+01 
c  Velocity[Z]                                      0.96330E-30 
c  Pressure     0.13553E-06     474   0.98893E-08   0.13381E+00 0.69567E+03 
c  nu_tilda     0.72415E-05      33   0.46306E-05   0.61731E-06 0.20619E+03 
c  TempC        0.40796E+02      27   0.33927E-03   0.52401E+01 0.25785E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4703          9.9016          4.5729          4.5729
v  Velocity[Y]            -3.0066          7.2304         0.13624         0.13624
v  Velocity[Z]        -1.043e-014     6.2212e-015    -1.7022e-017    -1.7022e-017
v  ǁVelocityǁ         0.0021001          9.9021           5.136           5.136
v  Pressure               -32.482          19.846         -8.6491         -8.6491
v  nu_tilda           4.4135e-007       0.0042695       0.0016393       0.0016393
v  TempC                       21          73.049          22.006          22.006
v  TurbVisc           3.3391e-014       0.0050321        0.001926        0.001926
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2027:        0.20860E+01

===============================================================


 INSTANT    0.202800000E+04   TIME STEP NUMBER            2028
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10315E-01 0.89348E+00
   Friction velocity        uk    :  0.10315E-01 0.89348E+00
   Dimensionless distance   yplus :  0.83044E-01 0.71931E+01
   Friction thermal sca.    tstar : -0.70972E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61960E-01 0.53669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10140E-01      33   0.26571E-03   0.49676E+01 0.18476E+03 
c  Velocity[X]                                      0.17811E+01 
c  Velocity[Y]                                      0.31864E+01 
c  Velocity[Z]                                      0.82793E-30 
c  Pressure     0.11030E-06     441   0.94668E-08   0.10797E+00 0.57901E+03 
c  nu_tilda     0.72438E-05      33   0.14901E-04   0.61788E-06 0.20626E+03 
c  TempC        0.40803E+02      27   0.36603E-03   0.54570E+01 0.26794E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4674          9.9006          4.5729          4.5729
v  Velocity[Y]            -3.0072          7.2486         0.13661         0.13661
v  Velocity[Z]       -1.0268e-014     6.5013e-015    -1.7026e-017    -1.7026e-017
v  ǁVelocityǁ         0.0022531          9.9012           5.136           5.136
v  Pressure                -32.51           19.91         -8.6262         -8.6262
v  nu_tilda           4.4129e-007       0.0042695       0.0016396       0.0016396
v  TempC                       21          73.048          22.006          22.006
v  TurbVisc            3.338e-014       0.0050321       0.0019265       0.0019265
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2028:        0.19950E+01

===============================================================


 INSTANT    0.202900000E+04   TIME STEP NUMBER            2029
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11012E-01 0.89453E+00
   Friction velocity        uk    :  0.11012E-01 0.89453E+00
   Dimensionless distance   yplus :  0.88657E-01 0.72016E+01
   Friction thermal sca.    tstar : -0.70926E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66148E-01 0.53732E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10142E-01      33   0.26474E-03   0.49514E+01 0.18466E+03 
c  Velocity[X]                                      0.17768E+01 
c  Velocity[Y]                                      0.31746E+01 
c  Velocity[Z]                                      0.80725E-30 
c  Pressure     0.12332E-06     473   0.97189E-08   0.12051E+00 0.57377E+03 
c  nu_tilda     0.72461E-05      33   0.46496E-05   0.61841E-06 0.20633E+03 
c  TempC        0.40811E+02      27   0.25576E-03   0.60388E+01 0.27477E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4644          9.8996          4.5729          4.5729
v  Velocity[Y]            -3.0078          7.2243         0.13698         0.13698
v  Velocity[Z]       -1.0119e-014     6.4178e-015    -1.7025e-017    -1.7025e-017
v  ǁVelocityǁ         0.0020383          9.9002          5.1359          5.1359
v  Pressure               -32.452          19.866         -8.6027         -8.6027
v  nu_tilda           4.4133e-007       0.0042695       0.0016401       0.0016401
v  TempC                       21          73.048          22.006          22.006
v  TurbVisc           3.3363e-014       0.0050321       0.0019269       0.0019269
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2029:        0.20640E+01

===============================================================


 INSTANT    0.203000000E+04   TIME STEP NUMBER            2030
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91834E-02 0.89384E+00
   Friction velocity        uk    :  0.91834E-02 0.89384E+00
   Dimensionless distance   yplus :  0.73933E-01 0.71960E+01
   Friction thermal sca.    tstar : -0.80831E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55162E-01 0.53690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10144E-01      33   0.22006E-03   0.49546E+01 0.18467E+03 
c  Velocity[X]                                      0.17890E+01 
c  Velocity[Y]                                      0.31656E+01 
c  Velocity[Z]                                      0.87566E-30 
c  Pressure     0.11867E-06     457   0.91859E-08   0.11583E+00 0.62167E+03 
c  nu_tilda     0.72484E-05      33   0.14892E-04   0.61898E-06 0.20641E+03 
c  TempC        0.40819E+02      27   0.36507E-03   0.48471E+01 0.25361E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4613          9.8986          4.5729          4.5729
v  Velocity[Y]            -3.0084          7.2499         0.13735         0.13735
v  Velocity[Z]       -9.9771e-015     6.5026e-015    -1.7022e-017    -1.7022e-017
v  ǁVelocityǁ         0.0021737          9.8992          5.1359          5.1359
v  Pressure               -32.485          19.951         -8.5752         -8.5752
v  nu_tilda           4.4141e-007       0.0042695       0.0016404       0.0016404
v  TempC                       21          73.047          22.006          22.006
v  TurbVisc           3.3374e-014       0.0050321       0.0019274       0.0019274
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2030:        0.20250E+01

===============================================================


 INSTANT    0.203100000E+04   TIME STEP NUMBER            2031
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.75977E-02 0.89531E+00
   Friction velocity        uk    :  0.75977E-02 0.89531E+00
   Dimensionless distance   yplus :  0.61167E-01 0.72079E+01
   Friction thermal sca.    tstar : -0.89784E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45637E-01 0.53779E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10146E-01      33   0.25507E-03   0.49314E+01 0.18467E+03 
c  Velocity[X]                                      0.17431E+01 
c  Velocity[Y]                                      0.31883E+01 
c  Velocity[Z]                                      0.82640E-30 
c  Pressure     0.11471E-06     520   0.97501E-08   0.11246E+00 0.11672E+04 
c  nu_tilda     0.72507E-05      33   0.46500E-05   0.61951E-06 0.20648E+03 
c  TempC        0.40826E+02      27   0.27167E-03   0.65103E+01 0.29957E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4582          9.8977          4.5729          4.5729
v  Velocity[Y]            -3.0088          7.2603         0.13771         0.13771
v  Velocity[Z]       -9.8129e-015     6.4542e-015    -1.7031e-017    -1.7031e-017
v  ǁVelocityǁ         0.0023247          9.8982          5.1359          5.1359
v  Pressure               -32.295           20.08         -8.5117         -8.5117
v  nu_tilda           4.4141e-007       0.0042695       0.0016409       0.0016409
v  TempC                       21          73.047          22.006          22.006
v  TurbVisc           3.3399e-014       0.0050321       0.0019279       0.0019279
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2031:        0.21860E+01

===============================================================


 INSTANT    0.203200000E+04   TIME STEP NUMBER            2032
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12791E-01 0.89477E+00
   Friction velocity        uk    :  0.12791E-01 0.89477E+00
   Dimensionless distance   yplus :  0.10298E+00 0.72035E+01
   Friction thermal sca.    tstar : -0.11767E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76834E-01 0.53746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10148E-01      33   0.26159E-03   0.49467E+01 0.18469E+03 
c  Velocity[X]                                      0.17751E+01 
c  Velocity[Y]                                      0.31716E+01 
c  Velocity[Z]                                      0.74664E-30 
c  Pressure     0.11578E-06     489   0.94503E-08   0.11304E+00 0.13519E+04 
c  nu_tilda     0.72530E-05      33   0.14892E-04   0.62009E-06 0.20655E+03 
c  TempC        0.40834E+02      27   0.28559E-03   0.51432E+01 0.24891E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4552          9.8967          4.5729          4.5729
v  Velocity[Y]            -3.0096          7.2266         0.13808         0.13808
v  Velocity[Z]       -9.6199e-015      6.783e-015    -1.7027e-017    -1.7027e-017
v  ǁVelocityǁ         0.0020228          9.8972          5.1359          5.1359
v  Pressure               -32.463          19.879         -8.5457         -8.5457
v  nu_tilda           4.4146e-007       0.0042695       0.0016412       0.0016412
v  TempC                       21          73.047          22.007          22.007
v  TurbVisc           3.3398e-014       0.0050321       0.0019284       0.0019284
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2032:        0.21130E+01

===============================================================


 INSTANT    0.203300000E+04   TIME STEP NUMBER            2033
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10550E-01 0.89353E+00
   Friction velocity        uk    :  0.10550E-01 0.89353E+00
   Dimensionless distance   yplus :  0.84938E-01 0.71936E+01
   Friction thermal sca.    tstar : -0.17542E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63373E-01 0.53672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10150E-01      33   0.28929E-03   0.49415E+01 0.18474E+03 
c  Velocity[X]                                      0.17744E+01 
c  Velocity[Y]                                      0.31671E+01 
c  Velocity[Z]                                      0.79804E-30 
c  Pressure     0.10876E-06     522   0.98608E-08   0.10639E+00 0.16197E+04 
c  nu_tilda     0.72553E-05      33   0.46644E-05   0.62062E-06 0.20663E+03 
c  TempC        0.40841E+02      27   0.32374E-03   0.51355E+01 0.24914E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4522          9.8957          4.5729          4.5729
v  Velocity[Y]            -3.0104          7.2504         0.13845         0.13845
v  Velocity[Z]       -9.4513e-015     6.6987e-015    -1.7027e-017    -1.7027e-017
v  ǁVelocityǁ         0.0021977          9.8963          5.1359          5.1359
v  Pressure               -32.287          20.106         -8.4632         -8.4632
v  nu_tilda           4.4146e-007       0.0042695       0.0016417       0.0016417
v  TempC                       21          73.048          22.007          22.007
v  TurbVisc           3.3413e-014       0.0050321       0.0019289       0.0019289
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2033:        0.21870E+01

===============================================================


 INSTANT    0.203400000E+04   TIME STEP NUMBER            2034
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.25587E-02 0.89455E+00
   Friction velocity        uk    :  0.25587E-02 0.89455E+00
   Dimensionless distance   yplus :  0.20599E-01 0.72018E+01
   Friction thermal sca.    tstar : -0.28288E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15369E-01 0.53733E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10152E-01      33   0.27798E-03   0.49702E+01 0.18490E+03 
c  Velocity[X]                                      0.17821E+01 
c  Velocity[Y]                                      0.31881E+01 
c  Velocity[Z]                                      0.76227E-30 
c  Pressure     0.11831E-06     474   0.95852E-08   0.11756E+00 0.95511E+03 
c  nu_tilda     0.72576E-05      33   0.14880E-04   0.62121E-06 0.20670E+03 
c  TempC        0.40849E+02      27   0.27471E-03   0.51436E+01 0.26443E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4491          9.8947          4.5729          4.5729
v  Velocity[Y]             -3.011          7.2255         0.13881         0.13881
v  Velocity[Z]       -9.5965e-015     6.6204e-015    -1.7027e-017    -1.7027e-017
v  ǁVelocityǁ         0.0020543          9.8953          5.1359          5.1359
v  Pressure               -32.301          19.983         -8.4794         -8.4794
v  nu_tilda           4.4142e-007       0.0042695        0.001642        0.001642
v  TempC                       21          73.047          22.007          22.007
v  TurbVisc           3.3413e-014       0.0050321       0.0019293       0.0019293
v  total_pressure     1.0129e+005     1.0134e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2034:        0.20680E+01

===============================================================


 INSTANT    0.203500000E+04   TIME STEP NUMBER            2035
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10673E-01 0.89363E+00
   Friction velocity        uk    :  0.10673E-01 0.89363E+00
   Dimensionless distance   yplus :  0.85924E-01 0.71943E+01
   Friction thermal sca.    tstar : -0.14112E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64109E-01 0.53678E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10154E-01      33   0.26033E-03   0.49480E+01 0.18479E+03 
c  Velocity[X]                                      0.17742E+01 
c  Velocity[Y]                                      0.31738E+01 
c  Velocity[Z]                                      0.83686E-30 
c  Pressure     0.13349E-06     506   0.96701E-08   0.12762E+00 0.12609E+04 
c  nu_tilda     0.72599E-05      33   0.46700E-05   0.62172E-06 0.20677E+03 
c  TempC        0.40857E+02      27   0.33021E-03   0.50555E+01 0.25021E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.446          9.8937          4.5729          4.5729
v  Velocity[Y]            -3.0116          7.2468         0.13918         0.13918
v  Velocity[Z]        -9.488e-015     6.4616e-015    -1.7026e-017    -1.7026e-017
v  ǁVelocityǁ          0.002209          9.8943          5.1359          5.1359
v  Pressure               -32.262          20.143         -8.4137         -8.4137
v  nu_tilda           4.4137e-007       0.0042695       0.0016425       0.0016425
v  TempC                       21          73.048          22.007          22.007
v  TurbVisc           3.3402e-014       0.0050321       0.0019298       0.0019298
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2035:        0.21330E+01

===============================================================


 INSTANT    0.203600000E+04   TIME STEP NUMBER            2036
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18087E-02 0.89503E+00
   Friction velocity        uk    :  0.18087E-02 0.89503E+00
   Dimensionless distance   yplus :  0.14561E-01 0.72056E+01
   Friction thermal sca.    tstar : -0.10045E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10864E-01 0.53762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10156E-01      33   0.27087E-03   0.49343E+01 0.18473E+03 
c  Velocity[X]                                      0.17690E+01 
c  Velocity[Y]                                      0.31653E+01 
c  Velocity[Z]                                      0.90600E-30 
c  Pressure     0.10412E-06     344   0.96717E-08   0.10148E+00 0.58640E+03 
c  nu_tilda     0.72622E-05      33   0.14881E-04   0.62230E-06 0.20684E+03 
c  TempC        0.40864E+02      27   0.28685E-03   0.58856E+01 0.26084E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4429          9.8927          4.5729          4.5729
v  Velocity[Y]            -3.0121          7.2557         0.13955         0.13955
v  Velocity[Z]       -9.8694e-015      6.326e-015    -1.7032e-017    -1.7032e-017
v  ǁVelocityǁ         0.0022962          9.8933          5.1358          5.1358
v  Pressure               -32.317          20.135         -8.4039         -8.4039
v  nu_tilda           4.4136e-007       0.0042695       0.0016428       0.0016428
v  TempC                       21          73.048          22.007          22.007
v  TurbVisc           3.3388e-014       0.0050321       0.0019303       0.0019303
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2036:        0.17750E+01

===============================================================


 INSTANT    0.203700000E+04   TIME STEP NUMBER            2037
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13208E-01 0.89468E+00
   Friction velocity        uk    :  0.13208E-01 0.89468E+00
   Dimensionless distance   yplus :  0.10633E+00 0.72028E+01
   Friction thermal sca.    tstar : -0.87592E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79336E-01 0.53741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10158E-01      33   0.24597E-03   0.49538E+01 0.18488E+03 
c  Velocity[X]                                      0.17657E+01 
c  Velocity[Y]                                      0.31881E+01 
c  Velocity[Z]                                      0.90310E-30 
c  Pressure     0.12420E-06     506   0.97197E-08   0.12392E+00 0.68065E+03 
c  nu_tilda     0.72644E-05      33   0.46776E-05   0.62282E-06 0.20692E+03 
c  TempC        0.40872E+02      27   0.33200E-03   0.48806E+01 0.24745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4399          9.8917          4.5729          4.5729
v  Velocity[Y]            -3.0125          7.2286         0.13991         0.13991
v  Velocity[Z]       -9.5973e-015     6.2035e-015    -1.7031e-017    -1.7031e-017
v  ǁVelocityǁ         0.0021113          9.8923          5.1358          5.1358
v  Pressure                -32.11           20.14         -8.3676         -8.3676
v  nu_tilda           4.4142e-007       0.0042695       0.0016433       0.0016433
v  TempC                       21          73.048          22.008          22.008
v  TurbVisc           3.3383e-014       0.0050321       0.0019308       0.0019308
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2037:        0.21590E+01

===============================================================


 INSTANT    0.203800000E+04   TIME STEP NUMBER            2038
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10397E-01 0.89312E+00
   Friction velocity        uk    :  0.10397E-01 0.89312E+00
   Dimensionless distance   yplus :  0.83699E-01 0.71903E+01
   Friction thermal sca.    tstar : -0.76771E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62449E-01 0.53647E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10160E-01      33   0.26680E-03   0.49270E+01 0.18474E+03 
c  Velocity[X]                                      0.17573E+01 
c  Velocity[Y]                                      0.31697E+01 
c  Velocity[Z]                                      0.89470E-30 
c  Pressure     0.11313E-06     394   0.93431E-08   0.10878E+00 0.56785E+03 
c  nu_tilda     0.72667E-05      33   0.14874E-04   0.62340E-06 0.20699E+03 
c  TempC        0.40880E+02      27   0.35823E-03   0.60990E+01 0.28139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4369          9.8907          4.5729          4.5729
v  Velocity[Y]            -3.0132          7.2429         0.14028         0.14028
v  Velocity[Z]       -9.6776e-015     6.1368e-015    -1.7034e-017    -1.7034e-017
v  ǁVelocityǁ         0.0021578          9.8913          5.1358          5.1358
v  Pressure               -32.284          20.151         -8.3563         -8.3563
v  nu_tilda           4.4146e-007       0.0042695       0.0016436       0.0016436
v  TempC                       21          73.047          22.008          22.008
v  TurbVisc           3.3403e-014       0.0050321       0.0019313       0.0019313
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2038:        0.19040E+01

===============================================================


 INSTANT    0.203900000E+04   TIME STEP NUMBER            2039
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.48817E-02 0.89444E+00
   Friction velocity        uk    :  0.48817E-02 0.89444E+00
   Dimensionless distance   yplus :  0.39301E-01 0.72008E+01
   Friction thermal sca.    tstar : -0.81879E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29323E-01 0.53726E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10162E-01      33   0.29485E-03   0.49466E+01 0.18489E+03 
c  Velocity[X]                                      0.17813E+01 
c  Velocity[Y]                                      0.31653E+01 
c  Velocity[Z]                                      0.82976E-30 
c  Pressure     0.13132E-06     489   0.95026E-08   0.12908E+00 0.71333E+03 
c  nu_tilda     0.72690E-05      33   0.46941E-05   0.62391E-06 0.20706E+03 
c  TempC        0.40887E+02      27   0.32659E-03   0.58499E+01 0.28024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4338          9.8897          4.5729          4.5729
v  Velocity[Y]             -3.014          7.2248         0.14064         0.14064
v  Velocity[Z]       -9.5939e-015     6.2682e-015    -1.7037e-017    -1.7037e-017
v  ǁVelocityǁ         0.0020769          9.8904          5.1358          5.1358
v  Pressure               -32.094          20.172         -8.3177         -8.3177
v  nu_tilda           4.4151e-007       0.0042695       0.0016441       0.0016441
v  TempC                       21          73.048          22.008          22.008
v  TurbVisc           3.3416e-014       0.0050321       0.0019317       0.0019317
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2039:        0.21170E+01

===============================================================


 INSTANT    0.204000000E+04   TIME STEP NUMBER            2040
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.53632E-02 0.89368E+00
   Friction velocity        uk    :  0.53632E-02 0.89368E+00
   Dimensionless distance   yplus :  0.43177E-01 0.71947E+01
   Friction thermal sca.    tstar : -0.88879E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32215E-01 0.53681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10164E-01      33   0.21434E-03   0.49574E+01 0.18497E+03 
c  Velocity[X]                                      0.17747E+01 
c  Velocity[Y]                                      0.31826E+01 
c  Velocity[Z]                                      0.72798E-30 
c  Pressure     0.11509E-06     458   0.97316E-08   0.11289E+00 0.67358E+03 
c  nu_tilda     0.72713E-05      33   0.14865E-04   0.62448E-06 0.20713E+03 
c  TempC        0.40895E+02      27   0.28739E-03   0.57915E+01 0.26288E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4307          9.8887          4.5729          4.5729
v  Velocity[Y]            -3.0147          7.2481           0.141           0.141
v  Velocity[Z]       -9.9173e-015     6.2857e-015    -1.7037e-017    -1.7037e-017
v  ǁVelocityǁ         0.0022632          9.8893          5.1358          5.1358
v  Pressure               -32.111          20.262         -8.2859         -8.2859
v  nu_tilda            4.415e-007       0.0042695       0.0016445       0.0016445
v  TempC                       21          73.047          22.008          22.008
v  TurbVisc           3.3429e-014       0.0050321       0.0019322       0.0019322
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2040:        0.20210E+01

===============================================================


 INSTANT    0.204100000E+04   TIME STEP NUMBER            2041
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12976E-01 0.89516E+00
   Friction velocity        uk    :  0.12976E-01 0.89516E+00
   Dimensionless distance   yplus :  0.10446E+00 0.72067E+01
   Friction thermal sca.    tstar : -0.83704E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77940E-01 0.53770E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10166E-01      33   0.26104E-03   0.49214E+01 0.18481E+03 
c  Velocity[X]                                      0.17470E+01 
c  Velocity[Y]                                      0.31744E+01 
c  Velocity[Z]                                      0.93462E-30 
c  Pressure     0.12345E-06     488   0.97762E-08   0.11901E+00 0.80784E+03 
c  nu_tilda     0.72736E-05      33   0.46954E-05   0.62502E-06 0.20720E+03 
c  TempC        0.40902E+02      27   0.31077E-03   0.45055E+01 0.25432E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4276          9.8877          4.5729          4.5729
v  Velocity[Y]            -3.0152           7.256         0.14137         0.14137
v  Velocity[Z]       -9.9362e-015      6.167e-015    -1.7031e-017    -1.7031e-017
v  ǁVelocityǁ         0.0022406          9.8883          5.1358          5.1358
v  Pressure               -32.106          20.313         -8.2416         -8.2416
v  nu_tilda            4.414e-007       0.0042695       0.0016449       0.0016449
v  TempC                       21          73.048          22.008          22.008
v  TurbVisc           3.3425e-014       0.0050321       0.0019327       0.0019327
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2041:        0.21020E+01

===============================================================


 INSTANT    0.204200000E+04   TIME STEP NUMBER            2042
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11965E-01 0.89491E+00
   Friction velocity        uk    :  0.11965E-01 0.89491E+00
   Dimensionless distance   yplus :  0.96324E-01 0.72046E+01
   Friction thermal sca.    tstar : -0.87148E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71868E-01 0.53754E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10168E-01      33   0.26264E-03   0.49554E+01 0.18494E+03 
c  Velocity[X]                                      0.17912E+01 
c  Velocity[Y]                                      0.31642E+01 
c  Velocity[Z]                                      0.85012E-30 
c  Pressure     0.11385E-06     456   0.93581E-08   0.11294E+00 0.87769E+03 
c  nu_tilda     0.72759E-05      33   0.14866E-04   0.62559E-06 0.20728E+03 
c  TempC        0.40910E+02      27   0.32641E-03   0.56711E+01 0.27233E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4246          9.8867          4.5729          4.5729
v  Velocity[Y]            -3.0157          7.2277         0.14173         0.14173
v  Velocity[Z]       -9.9478e-015     6.2704e-015    -1.7028e-017    -1.7028e-017
v  ǁVelocityǁ         0.0020645          9.8873          5.1357          5.1357
v  Pressure               -32.109          20.205         -8.2537         -8.2537
v  nu_tilda            4.414e-007       0.0042695       0.0016453       0.0016453
v  TempC                       21          73.048          22.009          22.009
v  TurbVisc           3.3397e-014       0.0050321       0.0019332       0.0019332
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2042:        0.20370E+01

===============================================================


 INSTANT    0.204300000E+04   TIME STEP NUMBER            2043
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10805E-01 0.89340E+00
   Friction velocity        uk    :  0.10805E-01 0.89340E+00
   Dimensionless distance   yplus :  0.86990E-01 0.71925E+01
   Friction thermal sca.    tstar : -0.92302E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64904E-01 0.53664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10170E-01      33   0.26272E-03   0.49354E+01 0.18495E+03 
c  Velocity[X]                                      0.17502E+01 
c  Velocity[Y]                                      0.31853E+01 
c  Velocity[Z]                                      0.82843E-30 
c  Pressure     0.11665E-06     536   0.96402E-08   0.11412E+00 0.16319E+04 
c  nu_tilda     0.72782E-05      33   0.47103E-05   0.62610E-06 0.20735E+03 
c  TempC        0.40918E+02      27   0.31296E-03   0.54085E+01 0.26494E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4215          9.8857          4.5729          4.5729
v  Velocity[Y]            -3.0161          7.2483         0.14209         0.14209
v  Velocity[Z]       -9.9602e-015     6.0717e-015    -1.7026e-017    -1.7026e-017
v  ǁVelocityǁ         0.0022815          9.8864          5.1357          5.1357
v  Pressure               -31.883          20.423         -8.1693         -8.1693
v  nu_tilda           4.4139e-007       0.0042695       0.0016457       0.0016457
v  TempC                       21          73.048          22.009          22.009
v  TurbVisc           3.3397e-014       0.0050321       0.0019336       0.0019336
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2043:        0.22260E+01

===============================================================


 INSTANT    0.204400000E+04   TIME STEP NUMBER            2044
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89912E-02 0.89431E+00
   Friction velocity        uk    :  0.89912E-02 0.89431E+00
   Dimensionless distance   yplus :  0.72386E-01 0.71998E+01
   Friction thermal sca.    tstar : -0.78209E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54008E-01 0.53718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10172E-01      33   0.27777E-03   0.49334E+01 0.18490E+03 
c  Velocity[X]                                      0.17638E+01 
c  Velocity[Y]                                      0.31695E+01 
c  Velocity[Z]                                      0.10030E-29 
c  Pressure     0.12059E-06     504   0.97409E-08   0.11732E+00 0.14124E+04 
c  nu_tilda     0.72805E-05      33   0.14853E-04   0.62667E-06 0.20742E+03 
c  TempC        0.40925E+02      27   0.31522E-03   0.54538E+01 0.26037E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4184          9.8847          4.5729          4.5729
v  Velocity[Y]            -3.0168            7.22         0.14245         0.14245
v  Velocity[Z]       -1.0091e-014     6.2402e-015     -1.702e-017     -1.702e-017
v  ǁVelocityǁ         0.0020236          9.8854          5.1357          5.1357
v  Pressure               -32.083          20.221         -8.2064         -8.2064
v  nu_tilda            4.414e-007       0.0042695       0.0016461       0.0016461
v  TempC                       21          73.047          22.009          22.009
v  TurbVisc           3.3392e-014       0.0050321       0.0019341       0.0019341
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2044:        0.21630E+01

===============================================================


 INSTANT    0.204500000E+04   TIME STEP NUMBER            2045
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10544E-01 0.89365E+00
   Friction velocity        uk    :  0.10544E-01 0.89365E+00
   Dimensionless distance   yplus :  0.84884E-01 0.71945E+01
   Friction thermal sca.    tstar : -0.89686E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63333E-01 0.53679E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10174E-01      33   0.24548E-03   0.49375E+01 0.18497E+03 
c  Velocity[X]                                      0.17732E+01 
c  Velocity[Y]                                      0.31643E+01 
c  Velocity[Z]                                      0.78974E-30 
c  Pressure     0.11041E-06     552   0.96083E-08   0.10774E+00 0.17294E+04 
c  nu_tilda     0.72828E-05      33   0.47138E-05   0.62719E-06 0.20749E+03 
c  TempC        0.40933E+02      27   0.36420E-03   0.59308E+01 0.27741E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4153          9.8837          4.5729          4.5729
v  Velocity[Y]            -3.0175          7.2484         0.14281         0.14281
v  Velocity[Z]       -1.0134e-014     6.2895e-015     -1.702e-017     -1.702e-017
v  ǁVelocityǁ         0.0022579          9.8844          5.1357          5.1357
v  Pressure               -31.908          20.463          -8.119          -8.119
v  nu_tilda           4.4136e-007       0.0042695       0.0016465       0.0016465
v  TempC                       21          73.048          22.009          22.009
v  TurbVisc           3.3396e-014       0.0050321       0.0019346       0.0019346
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2045:        0.22610E+01

===============================================================


 INSTANT    0.204600000E+04   TIME STEP NUMBER            2046
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11015E-01 0.89494E+00
   Friction velocity        uk    :  0.11015E-01 0.89494E+00
   Dimensionless distance   yplus :  0.88679E-01 0.72049E+01
   Friction thermal sca.    tstar : -0.93951E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66165E-01 0.53756E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10176E-01      33   0.26455E-03   0.49335E+01 0.18500E+03 
c  Velocity[X]                                      0.17529E+01 
c  Velocity[Y]                                      0.31807E+01 
c  Velocity[Z]                                      0.70534E-30 
c  Pressure     0.10949E-06     360   0.99918E-08   0.10733E+00 0.61849E+03 
c  nu_tilda     0.72851E-05      33   0.14853E-04   0.62776E-06 0.20756E+03 
c  TempC        0.40940E+02      27   0.33898E-03   0.64259E+01 0.29913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4123          9.8828          4.5729          4.5729
v  Velocity[Y]            -3.0182          7.2548         0.14317         0.14317
v  Velocity[Z]       -1.0314e-014     6.3629e-015    -1.7007e-017    -1.7007e-017
v  ǁVelocityǁ         0.0023229          9.8834          5.1357          5.1357
v  Pressure                -31.96          20.434          -8.115          -8.115
v  nu_tilda           4.4132e-007       0.0042695       0.0016469       0.0016469
v  TempC                       21          73.047          22.009          22.009
v  TurbVisc           3.3385e-014       0.0050321        0.001935        0.001935
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2046:        0.18180E+01

===============================================================


 INSTANT    0.204700000E+04   TIME STEP NUMBER            2047
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13381E-01 0.89449E+00
   Friction velocity        uk    :  0.13381E-01 0.89449E+00
   Dimensionless distance   yplus :  0.10773E+00 0.72013E+01
   Friction thermal sca.    tstar : -0.92854E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80375E-01 0.53730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10178E-01      33   0.25502E-03   0.49429E+01 0.18502E+03 
c  Velocity[X]                                      0.17730E+01 
c  Velocity[Y]                                      0.31699E+01 
c  Velocity[Z]                                      0.85714E-30 
c  Pressure     0.13215E-06     472   0.98669E-08   0.12868E+00 0.63493E+03 
c  nu_tilda     0.72873E-05      33   0.47220E-05   0.62828E-06 0.20763E+03 
c  TempC        0.40948E+02      27   0.31127E-03   0.58339E+01 0.28532E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4092          9.8818          4.5729          4.5729
v  Velocity[Y]            -3.0187           7.224         0.14353         0.14353
v  Velocity[Z]       -1.0254e-014     6.1641e-015    -1.7005e-017    -1.7005e-017
v  ǁVelocityǁ         0.0020615          9.8824          5.1356          5.1356
v  Pressure               -31.891          20.391         -8.0874         -8.0874
v  nu_tilda           4.4138e-007       0.0042695       0.0016473       0.0016473
v  TempC                       21          73.047           22.01           22.01
v  TurbVisc           3.3373e-014       0.0050321       0.0019355       0.0019355
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2047:        0.20890E+01

===============================================================


 INSTANT    0.204800000E+04   TIME STEP NUMBER            2048
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.39601E-02 0.89321E+00
   Friction velocity        uk    :  0.39601E-02 0.89321E+00
   Dimensionless distance   yplus :  0.31882E-01 0.71910E+01
   Friction thermal sca.    tstar : -0.97417E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23787E-01 0.53653E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10180E-01      33   0.26323E-03   0.49386E+01 0.18500E+03 
c  Velocity[X]                                      0.17735E+01 
c  Velocity[Y]                                      0.31651E+01 
c  Velocity[Z]                                      0.10511E-29 
c  Pressure     0.10820E-06     473   0.94414E-08   0.10536E+00 0.63749E+03 
c  nu_tilda     0.72896E-05      33   0.14848E-04   0.62886E-06 0.20771E+03 
c  TempC        0.40955E+02      27   0.30601E-03   0.50893E+01 0.25472E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.406          9.8807          4.5729          4.5729
v  Velocity[Y]            -3.0192          7.2446         0.14389         0.14389
v  Velocity[Z]       -1.0239e-014     6.2593e-015    -1.6989e-017    -1.6989e-017
v  ǁVelocityǁ         0.0021721          9.8814          5.1356          5.1356
v  Pressure               -31.914          20.474         -8.0595         -8.0595
v  nu_tilda           4.4138e-007       0.0042695       0.0016477       0.0016477
v  TempC                       21          73.047           22.01           22.01
v  TurbVisc            3.339e-014       0.0050321        0.001936        0.001936
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2048:        0.20820E+01

===============================================================


 INSTANT    0.204900000E+04   TIME STEP NUMBER            2049
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11811E-01 0.89434E+00
   Friction velocity        uk    :  0.11811E-01 0.89434E+00
   Dimensionless distance   yplus :  0.95089E-01 0.72001E+01
   Friction thermal sca.    tstar : -0.10573E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70947E-01 0.53721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10182E-01      33   0.26270E-03   0.49353E+01 0.18507E+03 
c  Velocity[X]                                      0.17514E+01 
c  Velocity[Y]                                      0.31839E+01 
c  Velocity[Z]                                      0.91997E-30 
c  Pressure     0.12452E-06     490   0.95899E-08   0.12423E+00 0.75287E+03 
c  nu_tilda     0.72919E-05      33   0.47371E-05   0.62936E-06 0.20778E+03 
c  TempC        0.40963E+02      27   0.28761E-03   0.55201E+01 0.26555E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4028          9.8797          4.5729          4.5729
v  Velocity[Y]            -3.0196          7.2236         0.14425         0.14425
v  Velocity[Z]        -1.019e-014     6.2784e-015    -1.6981e-017    -1.6981e-017
v  ǁVelocityǁ         0.0021052          9.8804          5.1356          5.1356
v  Pressure               -31.706          20.493         -8.0187         -8.0187
v  nu_tilda           4.4137e-007       0.0042695       0.0016481       0.0016481
v  TempC                       21          73.048           22.01           22.01
v  TurbVisc           3.3389e-014       0.0050321       0.0019365       0.0019365
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2049:        0.21150E+01

===============================================================


 INSTANT    0.205000000E+04   TIME STEP NUMBER            2050
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97164E-02 0.89339E+00
   Friction velocity        uk    :  0.97164E-02 0.89339E+00
   Dimensionless distance   yplus :  0.78224E-01 0.71924E+01
   Friction thermal sca.    tstar : -0.95495E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58363E-01 0.53664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10184E-01      33   0.21797E-03   0.49199E+01 0.18495E+03 
c  Velocity[X]                                      0.17546E+01 
c  Velocity[Y]                                      0.31653E+01 
c  Velocity[Z]                                      0.89866E-30 
c  Pressure     0.12544E-06     410   0.98160E-08   0.12067E+00 0.58044E+03 
c  nu_tilda     0.72942E-05      33   0.14838E-04   0.62993E-06 0.20785E+03 
c  TempC        0.40970E+02      27   0.35468E-03   0.47117E+01 0.24976E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3998          9.8787          4.5729          4.5729
v  Velocity[Y]            -3.0201          7.2429         0.14461         0.14461
v  Velocity[Z]        -1.021e-014     6.2855e-015    -1.6968e-017    -1.6968e-017
v  ǁVelocityǁ          0.002186          9.8794          5.1356          5.1356
v  Pressure               -31.888          20.511         -8.0039         -8.0039
v  nu_tilda            4.414e-007       0.0042695       0.0016485       0.0016485
v  TempC                       21          73.048           22.01           22.01
v  TurbVisc           3.3387e-014       0.0050321       0.0019369       0.0019369
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2050:        0.21490E+01

===============================================================


 INSTANT    0.205100000E+04   TIME STEP NUMBER            2051
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11959E-01 0.89511E+00
   Friction velocity        uk    :  0.11959E-01 0.89511E+00
   Dimensionless distance   yplus :  0.96276E-01 0.72062E+01
   Friction thermal sca.    tstar : -0.10435E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71833E-01 0.53766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10186E-01      33   0.29522E-03   0.49130E+01 0.18500E+03 
c  Velocity[X]                                      0.17513E+01 
c  Velocity[Y]                                      0.31617E+01 
c  Velocity[Z]                                      0.83714E-30 
c  Pressure     0.11799E-06     521   0.93596E-08   0.11492E+00 0.11602E+04 
c  nu_tilda     0.72965E-05      33   0.47379E-05   0.63045E-06 0.20792E+03 
c  TempC        0.40978E+02      27   0.26580E-03   0.48207E+01 0.25008E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3967          9.8778          4.5729          4.5729
v  Velocity[Y]            -3.0209          7.2563         0.14496         0.14496
v  Velocity[Z]       -9.9658e-015     6.1657e-015     -1.695e-017     -1.695e-017
v  ǁVelocityǁ         0.0023535          9.8784          5.1355          5.1355
v  Pressure               -31.733          20.643          -7.943          -7.943
v  nu_tilda           4.4134e-007       0.0042695       0.0016489       0.0016489
v  TempC                       21          73.048           22.01           22.01
v  TurbVisc           3.3395e-014       0.0050321       0.0019374       0.0019374
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2051:        0.23780E+01

===============================================================


 INSTANT    0.205200000E+04   TIME STEP NUMBER            2052
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.88366E-02 0.89467E+00
   Friction velocity        uk    :  0.88366E-02 0.89467E+00
   Dimensionless distance   yplus :  0.71141E-01 0.72027E+01
   Friction thermal sca.    tstar : -0.10389E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53079E-01 0.53740E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10188E-01      33   0.25675E-03   0.49599E+01 0.18523E+03 
c  Velocity[X]                                      0.17804E+01 
c  Velocity[Y]                                      0.31796E+01 
c  Velocity[Z]                                      0.73237E-30 
c  Pressure     0.12174E-06     472   0.97037E-08   0.12116E+00 0.94652E+03 
c  nu_tilda     0.72988E-05      33   0.14839E-04   0.63101E-06 0.20799E+03 
c  TempC        0.40986E+02      27   0.29770E-03   0.39140E+01 0.22211E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3936          9.8767          4.5729          4.5729
v  Velocity[Y]            -3.0215          7.2264         0.14532         0.14532
v  Velocity[Z]       -1.0239e-014       6.23e-015     -1.694e-017     -1.694e-017
v  ǁVelocityǁ         0.0021298          9.8774          5.1355          5.1355
v  Pressure               -31.722          20.519         -7.9551         -7.9551
v  nu_tilda           4.4133e-007       0.0042695       0.0016493       0.0016493
v  TempC                       21          73.048           22.01           22.01
v  TurbVisc           3.3378e-014       0.0050321       0.0019379       0.0019379
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2052:        0.20840E+01

===============================================================


 INSTANT    0.205300000E+04   TIME STEP NUMBER            2053
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35351E-02 0.89328E+00
   Friction velocity        uk    :  0.35351E-02 0.89328E+00
   Dimensionless distance   yplus :  0.28460E-01 0.71915E+01
   Friction thermal sca.    tstar : -0.98859E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21235E-01 0.53657E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10190E-01      33   0.25640E-03   0.49233E+01 0.18506E+03 
c  Velocity[X]                                      0.17557E+01 
c  Velocity[Y]                                      0.31676E+01 
c  Velocity[Z]                                      0.78204E-30 
c  Pressure     0.11305E-06     520   0.93487E-08   0.10890E+00 0.11686E+04 
c  nu_tilda     0.73011E-05      33   0.47521E-05   0.63152E-06 0.20806E+03 
c  TempC        0.40993E+02      27   0.32436E-03   0.37605E+01 0.23088E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3904          9.8757          4.5729          4.5729
v  Velocity[Y]            -3.0221          7.2436         0.14568         0.14568
v  Velocity[Z]       -1.0277e-014     6.0366e-015    -1.6923e-017    -1.6923e-017
v  ǁVelocityǁ         0.0022091          9.8764          5.1355          5.1355
v  Pressure               -31.705          20.665         -7.8949         -7.8949
v  nu_tilda           4.4132e-007       0.0042695       0.0016497       0.0016497
v  TempC                       21          73.049          22.011          22.011
v  TurbVisc           3.3375e-014       0.0050321       0.0019383       0.0019383
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2053:        0.21780E+01

===============================================================


 INSTANT    0.205400000E+04   TIME STEP NUMBER            2054
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11742E-01 0.89438E+00
   Friction velocity        uk    :  0.11742E-01 0.89438E+00
   Dimensionless distance   yplus :  0.94533E-01 0.72004E+01
   Friction thermal sca.    tstar : -0.96150E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70532E-01 0.53723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10192E-01      33   0.27293E-03   0.49393E+01 0.18512E+03 
c  Velocity[X]                                      0.17795E+01 
c  Velocity[Y]                                      0.31599E+01 
c  Velocity[Z]                                      0.94359E-30 
c  Pressure     0.10497E-06     456   0.96225E-08   0.10371E+00 0.91919E+03 
c  nu_tilda     0.73033E-05      33   0.14827E-04   0.63209E-06 0.20813E+03 
c  TempC        0.41001E+02      27   0.26263E-03   0.51953E+01 0.25746E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3872          9.8747          4.5729          4.5729
v  Velocity[Y]            -3.0225          7.2216         0.14604         0.14604
v  Velocity[Z]       -1.0391e-014     6.3002e-015    -1.6909e-017    -1.6909e-017
v  ǁVelocityǁ         0.0020029          9.8754          5.1355          5.1355
v  Pressure               -31.716          20.549         -7.9073         -7.9073
v  nu_tilda           4.4134e-007       0.0042695         0.00165         0.00165
v  TempC                       21          73.048          22.011          22.011
v  TurbVisc           3.3372e-014       0.0050321       0.0019388       0.0019388
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2054:        0.20120E+01

===============================================================


 INSTANT    0.205500000E+04   TIME STEP NUMBER            2055
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99715E-02 0.89360E+00
   Friction velocity        uk    :  0.99715E-02 0.89360E+00
   Dimensionless distance   yplus :  0.80277E-01 0.71941E+01
   Friction thermal sca.    tstar : -0.11358E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59896E-01 0.53676E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10194E-01      33   0.19810E-03   0.49346E+01 0.18520E+03 
c  Velocity[X]                                      0.17477E+01 
c  Velocity[Y]                                      0.31869E+01 
c  Velocity[Z]                                      0.88551E-30 
c  Pressure     0.11396E-06     538   0.92654E-08   0.11116E+00 0.16254E+04 
c  nu_tilda     0.73056E-05      33   0.47553E-05   0.63263E-06 0.20820E+03 
c  TempC        0.41008E+02      27   0.32993E-03   0.40186E+01 0.23725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3842          9.8737          4.5729          4.5729
v  Velocity[Y]            -3.0229          7.2464         0.14639         0.14639
v  Velocity[Z]       -1.0206e-014     6.2402e-015    -1.6887e-017    -1.6887e-017
v  ǁVelocityǁ         0.0022389          9.8745          5.1354          5.1354
v  Pressure               -31.512          20.774         -7.8271         -7.8271
v  nu_tilda           4.4134e-007       0.0042695       0.0016505       0.0016505
v  TempC                       21          73.049          22.011          22.011
v  TurbVisc           3.3378e-014       0.0050321       0.0019393       0.0019393
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2055:        0.22300E+01

===============================================================


 INSTANT    0.205600000E+04   TIME STEP NUMBER            2056
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11813E-01 0.89465E+00
   Friction velocity        uk    :  0.11813E-01 0.89465E+00
   Dimensionless distance   yplus :  0.95106E-01 0.72026E+01
   Friction thermal sca.    tstar : -0.95969E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70960E-01 0.53739E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10196E-01      33   0.26814E-03   0.48977E+01 0.18502E+03 
c  Velocity[X]                                      0.17310E+01 
c  Velocity[Y]                                      0.31667E+01 
c  Velocity[Z]                                      0.77806E-30 
c  Pressure     0.10949E-06     473   0.93840E-08   0.10533E+00 0.89749E+03 
c  nu_tilda     0.73079E-05      33   0.14825E-04   0.63318E-06 0.20827E+03 
c  TempC        0.41016E+02      27   0.30067E-03   0.63149E+01 0.28886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3811          9.8727          4.5729          4.5729
v  Velocity[Y]            -3.0234          7.2492         0.14675         0.14675
v  Velocity[Z]       -1.0479e-014     6.1871e-015    -1.6872e-017    -1.6872e-017
v  ǁVelocityǁ         0.0022526          9.8734          5.1354          5.1354
v  Pressure               -31.732          20.678         -7.8413         -7.8413
v  nu_tilda           4.4135e-007       0.0042695       0.0016508       0.0016508
v  TempC                       21          73.049          22.011          22.011
v  TurbVisc           3.3378e-014       0.0050321       0.0019398       0.0019398
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2056:        0.20720E+01

===============================================================


 INSTANT    0.205700000E+04   TIME STEP NUMBER            2057
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30116E-02 0.89446E+00
   Friction velocity        uk    :  0.30116E-02 0.89446E+00
   Dimensionless distance   yplus :  0.24245E-01 0.72010E+01
   Friction thermal sca.    tstar : -0.12336E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18090E-01 0.53728E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10198E-01      33   0.28799E-03   0.49363E+01 0.18524E+03 
c  Velocity[X]                                      0.17746E+01 
c  Velocity[Y]                                      0.31617E+01 
c  Velocity[Z]                                      0.81877E-30 
c  Pressure     0.11651E-06     489   0.94467E-08   0.11565E+00 0.67874E+03 
c  nu_tilda     0.73102E-05      33   0.47641E-05   0.63368E-06 0.20834E+03 
c  TempC        0.41023E+02      27   0.35970E-03   0.50500E+01 0.25998E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3779          9.8717          4.5729          4.5729
v  Velocity[Y]            -3.0241          7.2252         0.14711         0.14711
v  Velocity[Z]        -1.048e-014     6.2761e-015    -1.6856e-017    -1.6856e-017
v  ǁVelocityǁ         0.0021081          9.8724          5.1354          5.1354
v  Pressure               -31.552          20.688         -7.8064         -7.8064
v  nu_tilda            4.414e-007       0.0042695       0.0016513       0.0016513
v  TempC                       21          73.049          22.011          22.011
v  TurbVisc           3.3382e-014       0.0050321       0.0019402       0.0019402
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2057:        0.21200E+01

===============================================================


 INSTANT    0.205800000E+04   TIME STEP NUMBER            2058
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10477E-01 0.89310E+00
   Friction velocity        uk    :  0.10477E-01 0.89310E+00
   Dimensionless distance   yplus :  0.84350E-01 0.71901E+01
   Friction thermal sca.    tstar : -0.24823E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62934E-01 0.53646E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10199E-01      33   0.26402E-03   0.49396E+01 0.18530E+03 
c  Velocity[X]                                      0.17615E+01 
c  Velocity[Y]                                      0.31781E+01 
c  Velocity[Z]                                      0.77839E-30 
c  Pressure     0.10856E-06     472   0.97602E-08   0.10658E+00 0.66009E+03 
c  nu_tilda     0.73125E-05      33   0.14820E-04   0.63425E-06 0.20841E+03 
c  TempC        0.41031E+02      27   0.32741E-03   0.53553E+01 0.26949E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3747          9.8707          4.5729          4.5729
v  Velocity[Y]            -3.0247          7.2428         0.14747         0.14747
v  Velocity[Z]       -1.0809e-014     6.2735e-015    -1.6839e-017    -1.6839e-017
v  ǁVelocityǁ          0.002285          9.8714          5.1354          5.1354
v  Pressure               -31.555          20.776         -7.7772         -7.7772
v  nu_tilda           4.4137e-007       0.0042695       0.0016516       0.0016516
v  TempC                       21          73.048          22.012          22.012
v  TurbVisc           3.3396e-014       0.0050321       0.0019407       0.0019407
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2058:        0.20570E+01

===============================================================


 INSTANT    0.205900000E+04   TIME STEP NUMBER            2059
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13001E-01 0.89411E+00
   Friction velocity        uk    :  0.13001E-01 0.89411E+00
   Dimensionless distance   yplus :  0.10467E+00 0.71982E+01
   Friction thermal sca.    tstar : -0.21504E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78093E-01 0.53707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10201E-01      33   0.26708E-03   0.49261E+01 0.18521E+03 
c  Velocity[X]                                      0.17598E+01 
c  Velocity[Y]                                      0.31664E+01 
c  Velocity[Z]                                      0.86502E-30 
c  Pressure     0.12625E-06     473   0.91641E-08   0.12263E+00 0.64131E+03 
c  nu_tilda     0.73147E-05      33   0.47803E-05   0.63476E-06 0.20848E+03 
c  TempC        0.41038E+02      27   0.26389E-03   0.52524E+01 0.26010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3717          9.8697          4.5729          4.5729
v  Velocity[Y]            -3.0253          7.2184         0.14782         0.14782
v  Velocity[Z]       -1.0772e-014     6.0155e-015    -1.6823e-017    -1.6823e-017
v  ǁVelocityǁ         0.0020868          9.8704          5.1353          5.1353
v  Pressure               -31.485          20.733         -7.7493         -7.7493
v  nu_tilda           4.4136e-007       0.0042695       0.0016521       0.0016521
v  TempC                       21          73.048          22.012          22.012
v  TurbVisc           3.3388e-014       0.0050321       0.0019411       0.0019411
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2059:        0.20770E+01

===============================================================


 INSTANT    0.206000000E+04   TIME STEP NUMBER            2060
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.52331E-02 0.89348E+00
   Friction velocity        uk    :  0.52331E-02 0.89348E+00
   Dimensionless distance   yplus :  0.42130E-01 0.71931E+01
   Friction thermal sca.    tstar : -0.12887E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31434E-01 0.53669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10203E-01      33   0.21782E-03   0.49301E+01 0.18522E+03 
c  Velocity[X]                                      0.17713E+01 
c  Velocity[Y]                                      0.31587E+01 
c  Velocity[Z]                                      0.91741E-30 
c  Pressure     0.10683E-06     457   0.93723E-08   0.10431E+00 0.59516E+03 
c  nu_tilda     0.73170E-05      33   0.14812E-04   0.63533E-06 0.20855E+03 
c  TempC        0.41046E+02      27   0.37039E-03   0.42329E+01 0.23931E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3686          9.8687          4.5729          4.5729
v  Velocity[Y]            -3.0257          7.2444         0.14818         0.14818
v  Velocity[Z]       -1.0731e-014     6.2547e-015    -1.6799e-017    -1.6799e-017
v  ǁVelocityǁ          0.002251          9.8694          5.1353          5.1353
v  Pressure               -31.538          20.807         -7.7268         -7.7268
v  nu_tilda           4.4128e-007       0.0042695       0.0016524       0.0016524
v  TempC                       21          73.048          22.012          22.012
v  TurbVisc           3.3383e-014       0.0050321       0.0019416       0.0019416
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2060:        0.20360E+01

===============================================================


 INSTANT    0.206100000E+04   TIME STEP NUMBER            2061
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11598E-01 0.89507E+00
   Friction velocity        uk    :  0.11598E-01 0.89507E+00
   Dimensionless distance   yplus :  0.93369E-01 0.72059E+01
   Friction thermal sca.    tstar : -0.12562E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69664E-01 0.53764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10205E-01      33   0.25243E-03   0.49046E+01 0.18522E+03 
c  Velocity[X]                                      0.17245E+01 
c  Velocity[Y]                                      0.31801E+01 
c  Velocity[Z]                                      0.79369E-30 
c  Pressure     0.96849E-07     521   0.95998E-08   0.95656E-01 0.11616E+04 
c  nu_tilda     0.73193E-05      33   0.47833E-05   0.63584E-06 0.20862E+03 
c  TempC        0.41053E+02      27   0.32685E-03   0.56679E+01 0.27804E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3654          9.8677          4.5729          4.5729
v  Velocity[Y]            -3.0261          7.2555         0.14854         0.14854
v  Velocity[Z]       -1.0674e-014     6.2561e-015     -1.678e-017     -1.678e-017
v  ǁVelocityǁ         0.0024108          9.8684          5.1353          5.1353
v  Pressure               -31.377          20.933         -7.6655         -7.6655
v  nu_tilda           4.4115e-007       0.0042695       0.0016529       0.0016529
v  TempC                       21          73.049          22.012          22.012
v  TurbVisc           3.3359e-014       0.0050321       0.0019421       0.0019421
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2061:        0.21760E+01

===============================================================


 INSTANT    0.206200000E+04   TIME STEP NUMBER            2062
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89391E-02 0.89450E+00
   Friction velocity        uk    :  0.89391E-02 0.89450E+00
   Dimensionless distance   yplus :  0.71966E-01 0.72013E+01
   Friction thermal sca.    tstar : -0.10944E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53695E-01 0.53730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10207E-01      33   0.25961E-03   0.49249E+01 0.18527E+03 
c  Velocity[X]                                      0.17570E+01 
c  Velocity[Y]                                      0.31679E+01 
c  Velocity[Z]                                      0.78840E-30 
c  Pressure     0.11866E-06     489   0.93797E-08   0.11598E+00 0.13679E+04 
c  nu_tilda     0.73216E-05      33   0.14811E-04   0.63642E-06 0.20869E+03 
c  TempC        0.41061E+02      27   0.30962E-03   0.77871E+01 0.28090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3622          9.8667          4.5729          4.5729
v  Velocity[Y]            -3.0264           7.222          0.1489          0.1489
v  Velocity[Z]       -1.0734e-014     6.2257e-015    -1.6756e-017    -1.6756e-017
v  ǁVelocityǁ         0.0020645          9.8674          5.1353          5.1353
v  Pressure               -31.532          20.731         -7.6996         -7.6996
v  nu_tilda           4.4116e-007       0.0042695       0.0016532       0.0016532
v  TempC                       21          73.048          22.012          22.012
v  TurbVisc            3.332e-014       0.0050321       0.0019426       0.0019426
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2062:        0.21060E+01

===============================================================


 INSTANT    0.206300000E+04   TIME STEP NUMBER            2063
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11158E-01 0.89325E+00
   Friction velocity        uk    :  0.11158E-01 0.89325E+00
   Dimensionless distance   yplus :  0.89829E-01 0.71912E+01
   Friction thermal sca.    tstar : -0.13736E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67022E-01 0.53655E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10209E-01      33   0.28698E-03   0.49189E+01 0.18530E+03 
c  Velocity[X]                                      0.17578E+01 
c  Velocity[Y]                                      0.31611E+01 
c  Velocity[Z]                                      0.77263E-30 
c  Pressure     0.10647E-06     570   0.99063E-08   0.10358E+00 0.17608E+04 
c  nu_tilda     0.73238E-05      33   0.47998E-05   0.63693E-06 0.20876E+03 
c  TempC        0.41068E+02      27   0.27145E-03   0.48657E+01 0.25169E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3591          9.8657          4.5729          4.5729
v  Velocity[Y]            -3.0272          7.2447         0.14925         0.14925
v  Velocity[Z]       -1.0647e-014     6.2494e-015    -1.6741e-017    -1.6741e-017
v  ǁVelocityǁ         0.0022623          9.8664          5.1352          5.1352
v  Pressure               -31.342          20.977         -7.6126         -7.6126
v  nu_tilda            4.412e-007       0.0042695       0.0016537       0.0016537
v  TempC                       21          73.048          22.013          22.013
v  TurbVisc           3.3324e-014       0.0050321        0.001943        0.001943
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2063:        0.22970E+01

===============================================================


 INSTANT    0.206400000E+04   TIME STEP NUMBER            2064
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12314E-01 0.89416E+00
   Friction velocity        uk    :  0.12314E-01 0.89416E+00
   Dimensionless distance   yplus :  0.99140E-01 0.71986E+01
   Friction thermal sca.    tstar : -0.13100E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73970E-01 0.53709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10211E-01      33   0.27485E-03   0.49429E+01 0.18544E+03 
c  Velocity[X]                                      0.17654E+01 
c  Velocity[Y]                                      0.31775E+01 
c  Velocity[Z]                                      0.73309E-30 
c  Pressure     0.11774E-06     505   0.92922E-08   0.11694E+00 0.11011E+04 
c  nu_tilda     0.73261E-05      33   0.14799E-04   0.63749E-06 0.20883E+03 
c  TempC        0.41076E+02      27   0.33172E-03   0.43883E+01 0.24672E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.356          9.8646          4.5729          4.5729
v  Velocity[Y]            -3.0278          7.2204         0.14961         0.14961
v  Velocity[Z]       -1.0579e-014     6.2885e-015    -1.6714e-017    -1.6714e-017
v  ǁVelocityǁ         0.0020378          9.8654          5.1352          5.1352
v  Pressure               -31.359          20.827         -7.6354         -7.6354
v  nu_tilda           4.4127e-007       0.0042695        0.001654        0.001654
v  TempC                       21          73.048          22.013          22.013
v  TurbVisc           3.3335e-014       0.0050321       0.0019435       0.0019435
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2064:        0.21560E+01

===============================================================


 INSTANT    0.206500000E+04   TIME STEP NUMBER            2065
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10510E-01 0.89332E+00
   Friction velocity        uk    :  0.10510E-01 0.89332E+00
   Dimensionless distance   yplus :  0.84614E-01 0.71918E+01
   Friction thermal sca.    tstar : -0.13838E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63131E-01 0.53659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10213E-01      33   0.21201E-03   0.49216E+01 0.18534E+03 
c  Velocity[X]                                      0.17557E+01 
c  Velocity[Y]                                      0.31659E+01 
c  Velocity[Z]                                      0.76250E-30 
c  Pressure     0.11663E-06     537   0.93471E-08   0.11232E+00 0.13923E+04 
c  nu_tilda     0.73284E-05      33   0.48053E-05   0.63800E-06 0.20890E+03 
c  TempC        0.41083E+02      27   0.27231E-03   0.70797E+01 0.28435E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3528          9.8636          4.5729          4.5729
v  Velocity[Y]            -3.0283          7.2422         0.14997         0.14997
v  Velocity[Z]       -1.0442e-014     6.0197e-015    -1.6696e-017    -1.6696e-017
v  ǁVelocityǁ         0.0021961          9.8644          5.1352          5.1352
v  Pressure                -31.33          21.003         -7.5643         -7.5643
v  nu_tilda            4.413e-007       0.0042695       0.0016544       0.0016544
v  TempC                       21          73.048          22.013          22.013
v  TurbVisc           3.3358e-014       0.0050321       0.0019439       0.0019439
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2065:        0.22180E+01

===============================================================


 INSTANT    0.206600000E+04   TIME STEP NUMBER            2066
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11342E-01 0.89477E+00
   Friction velocity        uk    :  0.11342E-01 0.89477E+00
   Dimensionless distance   yplus :  0.91310E-01 0.72035E+01
   Friction thermal sca.    tstar : -0.11737E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68128E-01 0.53746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10215E-01      33   0.26989E-03   0.49108E+01 0.18529E+03 
c  Velocity[X]                                      0.17521E+01 
c  Velocity[Y]                                      0.31587E+01 
c  Velocity[Z]                                      0.82434E-30 
c  Pressure     0.94576E-07     281   0.94727E-08   0.92350E-01 0.57912E+03 
c  nu_tilda     0.73307E-05      33   0.14799E-04   0.63855E-06 0.20897E+03 
c  TempC        0.41090E+02      27   0.28696E-03   0.53509E+01 0.25088E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3496          9.8627          4.5729          4.5729
v  Velocity[Y]            -3.0288          7.2505         0.15032         0.15032
v  Velocity[Z]       -1.0412e-014     6.2396e-015     -1.668e-017     -1.668e-017
v  ǁVelocityǁ         0.0023566          9.8634          5.1351          5.1351
v  Pressure               -31.391          20.999         -7.5567         -7.5567
v  nu_tilda           4.4129e-007       0.0042695       0.0016548       0.0016548
v  TempC                       21          73.047          22.013          22.013
v  TurbVisc           3.3366e-014       0.0050321       0.0019444       0.0019444
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2066:        0.16290E+01

===============================================================


 INSTANT    0.206700000E+04   TIME STEP NUMBER            2067
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.18173E-02 0.89431E+00
   Friction velocity        uk    :  0.18173E-02 0.89431E+00
   Dimensionless distance   yplus :  0.14630E-01 0.71998E+01
   Friction thermal sca.    tstar : -0.13473E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10916E-01 0.53719E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10217E-01      33   0.24784E-03   0.49327E+01 0.18546E+03 
c  Velocity[X]                                      0.17510E+01 
c  Velocity[Y]                                      0.31817E+01 
c  Velocity[Z]                                      0.79776E-30 
c  Pressure     0.12064E-06     473   0.92630E-08   0.11976E+00 0.68616E+03 
c  nu_tilda     0.73329E-05      33   0.48144E-05   0.63905E-06 0.20904E+03 
c  TempC        0.41098E+02      27   0.32303E-03   0.40530E+01 0.23193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3464          9.8616          4.5729          4.5729
v  Velocity[Y]            -3.0291          7.2236         0.15067         0.15067
v  Velocity[Z]        -1.033e-014     6.1904e-015    -1.6664e-017    -1.6664e-017
v  ǁVelocityǁ           0.00217          9.8624          5.1351          5.1351
v  Pressure               -31.167          20.989         -7.5219         -7.5219
v  nu_tilda           4.4131e-007       0.0042695       0.0016552       0.0016552
v  TempC                       21          73.047          22.013          22.013
v  TurbVisc           3.3363e-014       0.0050321       0.0019449       0.0019449
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2067:        0.20730E+01

===============================================================


 INSTANT    0.206800000E+04   TIME STEP NUMBER            2068
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11228E-01 0.89287E+00
   Friction velocity        uk    :  0.11228E-01 0.89287E+00
   Dimensionless distance   yplus :  0.90395E-01 0.71882E+01
   Friction thermal sca.    tstar : -0.11766E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67445E-01 0.53632E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10219E-01      33   0.26527E-03   0.49042E+01 0.18531E+03 
c  Velocity[X]                                      0.17418E+01 
c  Velocity[Y]                                      0.31624E+01 
c  Velocity[Z]                                      0.85795E-30 
c  Pressure     0.10671E-06     440   0.93511E-08   0.10269E+00 0.58617E+03 
c  nu_tilda     0.73352E-05      33   0.14792E-04   0.63962E-06 0.20911E+03 
c  TempC        0.41105E+02      27   0.32995E-03   0.47811E+01 0.24973E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3434          9.8606          4.5729          4.5729
v  Velocity[Y]            -3.0294          7.2385         0.15103         0.15103
v  Velocity[Z]       -1.0154e-014     6.2729e-015    -1.6637e-017    -1.6637e-017
v  ǁVelocityǁ         0.0022641          9.8614          5.1351          5.1351
v  Pressure               -31.334          21.023          -7.505          -7.505
v  nu_tilda           4.4126e-007       0.0042695       0.0016556       0.0016556
v  TempC                       21          73.047          22.013          22.013
v  TurbVisc            3.337e-014       0.0050321       0.0019453       0.0019453
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2068:        0.20070E+01

===============================================================


 INSTANT    0.206900000E+04   TIME STEP NUMBER            2069
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12803E-01 0.89418E+00
   Friction velocity        uk    :  0.12803E-01 0.89418E+00
   Dimensionless distance   yplus :  0.10307E+00 0.71988E+01
   Friction thermal sca.    tstar : -0.11611E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76902E-01 0.53711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10221E-01      33   0.29181E-03   0.49233E+01 0.18546E+03 
c  Velocity[X]                                      0.17654E+01 
c  Velocity[Y]                                      0.31578E+01 
c  Velocity[Z]                                      0.79860E-30 
c  Pressure     0.11552E-06     505   0.92620E-08   0.11450E+00 0.70766E+03 
c  nu_tilda     0.73375E-05      33   0.48289E-05   0.64012E-06 0.20918E+03 
c  TempC        0.41113E+02      27   0.24954E-03   0.57584E+01 0.25864E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3402          9.8596          4.5729          4.5729
v  Velocity[Y]            -3.0301          7.2204         0.15138         0.15138
v  Velocity[Z]       -1.0037e-014     6.2401e-015    -1.6622e-017    -1.6622e-017
v  ǁVelocityǁ         0.0021307          9.8604           5.135           5.135
v  Pressure               -31.164           21.03         -7.4679         -7.4679
v  nu_tilda           4.4125e-007       0.0042695        0.001656        0.001656
v  TempC                       21          73.048          22.014          22.014
v  TurbVisc           3.3355e-014       0.0050321       0.0019458       0.0019458
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2069:        0.21490E+01

===============================================================


 INSTANT    0.207000000E+04   TIME STEP NUMBER            2070
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71275E-02 0.89337E+00
   Friction velocity        uk    :  0.71275E-02 0.89337E+00
   Dimensionless distance   yplus :  0.57381E-01 0.71922E+01
   Friction thermal sca.    tstar : -0.13170E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42813E-01 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10223E-01      33   0.21427E-03   0.49392E+01 0.18557E+03 
c  Velocity[X]                                      0.17594E+01 
c  Velocity[Y]                                      0.31798E+01 
c  Velocity[Z]                                      0.71655E-30 
c  Pressure     0.11049E-06     456   0.92486E-08   0.10877E+00 0.64504E+03 
c  nu_tilda     0.73397E-05      33   0.14784E-04   0.64069E-06 0.20925E+03 
c  TempC        0.41120E+02      27   0.32107E-03   0.40880E+01 0.23771E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3371          9.8586          4.5729          4.5729
v  Velocity[Y]            -3.0307          7.2432         0.15174         0.15174
v  Velocity[Z]       -1.0175e-014     6.8642e-015    -1.6596e-017    -1.6596e-017
v  ǁVelocityǁ         0.0023188          9.8594           5.135           5.135
v  Pressure               -31.177          21.109         -7.4407         -7.4407
v  nu_tilda           4.4128e-007       0.0042695       0.0016563       0.0016563
v  TempC                       21          73.048          22.014          22.014
v  TurbVisc            3.335e-014       0.0050321       0.0019463       0.0019463
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2070:        0.20430E+01

===============================================================


 INSTANT    0.207100000E+04   TIME STEP NUMBER            2071
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13184E-01 0.89477E+00
   Friction velocity        uk    :  0.13184E-01 0.89477E+00
   Dimensionless distance   yplus :  0.10614E+00 0.72035E+01
   Friction thermal sca.    tstar : -0.13084E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79195E-01 0.53746E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10225E-01      33   0.25842E-03   0.48972E+01 0.18537E+03 
c  Velocity[X]                                      0.17326E+01 
c  Velocity[Y]                                      0.31646E+01 
c  Velocity[Z]                                      0.74740E-30 
c  Pressure     0.11999E-06     488   0.94757E-08   0.11523E+00 0.84074E+03 
c  nu_tilda     0.73420E-05      33   0.48329E-05   0.64118E-06 0.20932E+03 
c  TempC        0.41128E+02      27   0.35193E-03   0.44646E+01 0.23351E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3338          9.8576          4.5729          4.5729
v  Velocity[Y]            -3.0312          7.2503         0.15209         0.15209
v  Velocity[Z]       -1.0154e-014     6.7156e-015    -1.6576e-017    -1.6576e-017
v  ǁVelocityǁ         0.0023545          9.8584           5.135           5.135
v  Pressure               -31.157          21.169         -7.3963         -7.3963
v  nu_tilda            4.413e-007       0.0042695       0.0016568       0.0016568
v  TempC                       21          73.049          22.014          22.014
v  TurbVisc           3.3359e-014       0.0050321       0.0019467       0.0019467
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2071:        0.21130E+01

===============================================================


 INSTANT    0.207200000E+04   TIME STEP NUMBER            2072
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.57541E-02 0.89451E+00
   Friction velocity        uk    :  0.57541E-02 0.89451E+00
   Dimensionless distance   yplus :  0.46324E-01 0.72014E+01
   Friction thermal sca.    tstar : -0.13542E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34563E-01 0.53730E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10226E-01      33   0.26014E-03   0.49318E+01 0.18550E+03 
c  Velocity[X]                                      0.17760E+01 
c  Velocity[Y]                                      0.31558E+01 
c  Velocity[Z]                                      0.75803E-30 
c  Pressure     0.10812E-06     472   0.96655E-08   0.10723E+00 0.98599E+03 
c  nu_tilda     0.73443E-05      33   0.14784E-04   0.64173E-06 0.20938E+03 
c  TempC        0.41135E+02      27   0.31244E-03   0.45681E+01 0.24286E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3307          9.8566          4.5729          4.5729
v  Velocity[Y]            -3.0317          7.2221         0.15245         0.15245
v  Velocity[Z]       -1.0199e-014     7.4156e-015    -1.6554e-017    -1.6554e-017
v  ǁVelocityǁ         0.0021245          9.8574          5.1349          5.1349
v  Pressure                -31.17          21.047         -7.4107         -7.4107
v  nu_tilda           4.4134e-007       0.0042695       0.0016571       0.0016571
v  TempC                       21          73.048          22.014          22.014
v  TurbVisc           3.3365e-014       0.0050321       0.0019472       0.0019472
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2072:        0.20730E+01

===============================================================


 INSTANT    0.207300000E+04   TIME STEP NUMBER            2073
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11812E-01 0.89307E+00
   Friction velocity        uk    :  0.11812E-01 0.89307E+00
   Dimensionless distance   yplus :  0.95095E-01 0.71898E+01
   Friction thermal sca.    tstar : -0.15194E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70952E-01 0.53644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10228E-01      33   0.25992E-03   0.49118E+01 0.18552E+03 
c  Velocity[X]                                      0.17344E+01 
c  Velocity[Y]                                      0.31775E+01 
c  Velocity[Z]                                      0.82864E-30 
c  Pressure     0.94855E-07     538   0.98457E-08   0.93378E-01 0.15808E+04 
c  nu_tilda     0.73466E-05      33   0.48499E-05   0.64221E-06 0.20945E+03 
c  TempC        0.41142E+02      27   0.29183E-03   0.51936E+01 0.25812E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3276          9.8556          4.5729          4.5729
v  Velocity[Y]             -3.032          7.2431          0.1528          0.1528
v  Velocity[Z]       -1.0071e-014     7.7584e-015    -1.6536e-017    -1.6536e-017
v  ǁVelocityǁ         0.0022916          9.8563          5.1349          5.1349
v  Pressure               -30.981          21.257         -7.3326         -7.3326
v  nu_tilda           4.4133e-007       0.0042695       0.0016576       0.0016576
v  TempC                       21          73.049          22.014          22.014
v  TurbVisc           3.3377e-014       0.0050321       0.0019476       0.0019476
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2073:        0.22350E+01

===============================================================


 INSTANT    0.207400000E+04   TIME STEP NUMBER            2074
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71044E-02 0.89396E+00
   Friction velocity        uk    :  0.71044E-02 0.89396E+00
   Dimensionless distance   yplus :  0.57195E-01 0.71970E+01
   Friction thermal sca.    tstar : -0.13451E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42674E-01 0.53698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10230E-01      33   0.27529E-03   0.49105E+01 0.18547E+03 
c  Velocity[X]                                      0.17502E+01 
c  Velocity[Y]                                      0.31602E+01 
c  Velocity[Z]                                      0.82441E-30 
c  Pressure     0.11767E-06     490   0.93852E-08   0.11498E+00 0.12197E+04 
c  nu_tilda     0.73488E-05      33   0.14770E-04   0.64275E-06 0.20951E+03 
c  TempC        0.41150E+02      27   0.29275E-03   0.53946E+01 0.26161E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3244          9.8545          4.5729          4.5729
v  Velocity[Y]            -3.0322          7.2152         0.15315         0.15315
v  Velocity[Z]       -1.0096e-014     7.8331e-015    -1.6515e-017    -1.6515e-017
v  ǁVelocityǁ         0.0020093          9.8553          5.1349          5.1349
v  Pressure               -31.134          21.085         -7.3576         -7.3576
v  nu_tilda           4.4138e-007       0.0042695       0.0016579       0.0016579
v  TempC                       21          73.048          22.014          22.014
v  TurbVisc           3.3375e-014       0.0050321       0.0019481       0.0019481
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2074:        0.21150E+01

===============================================================


 INSTANT    0.207500000E+04   TIME STEP NUMBER            2075
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10139E-01 0.89337E+00
   Friction velocity        uk    :  0.10139E-01 0.89337E+00
   Dimensionless distance   yplus :  0.81627E-01 0.71922E+01
   Friction thermal sca.    tstar : -0.13447E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60903E-01 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10232E-01      33   0.28485E-03   0.49147E+01 0.18555E+03 
c  Velocity[X]                                      0.17584E+01 
c  Velocity[Y]                                      0.31563E+01 
c  Velocity[Z]                                      0.73202E-30 
c  Pressure     0.10764E-06     568   0.97485E-08   0.10444E+00 0.16699E+04 
c  nu_tilda     0.73511E-05      33   0.48533E-05   0.64322E-06 0.20958E+03 
c  TempC        0.41157E+02      27   0.29154E-03   0.52891E+01 0.25855E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3211          9.8535          4.5729          4.5729
v  Velocity[Y]            -3.0329          7.2428         0.15351         0.15351
v  Velocity[Z]       -9.9985e-015     8.5176e-015    -1.6503e-017    -1.6503e-017
v  ǁVelocityǁ         0.0022536          9.8544          5.1348          5.1348
v  Pressure               -30.965          21.315         -7.2761         -7.2761
v  nu_tilda           4.4141e-007       0.0042695       0.0016584       0.0016584
v  TempC                       21          73.049          22.015          22.015
v  TurbVisc           3.3389e-014       0.0050321       0.0019486       0.0019486
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2075:        0.22890E+01

===============================================================


 INSTANT    0.207600000E+04   TIME STEP NUMBER            2076
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11986E-01 0.89457E+00
   Friction velocity        uk    :  0.11986E-01 0.89457E+00
   Dimensionless distance   yplus :  0.96495E-01 0.72019E+01
   Friction thermal sca.    tstar : -0.13204E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71996E-01 0.53734E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10234E-01      33   0.26101E-03   0.49125E+01 0.18558E+03 
c  Velocity[X]                                      0.17385E+01 
c  Velocity[Y]                                      0.31740E+01 
c  Velocity[Z]                                      0.66167E-30 
c  Pressure     0.99794E-07     392   0.99234E-08   0.97887E-01 0.67264E+03 
c  nu_tilda     0.73533E-05      33   0.14771E-04   0.64375E-06 0.20964E+03 
c  TempC        0.41165E+02      27   0.33596E-03   0.46042E+01 0.24060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.318          9.8525          4.5729          4.5729
v  Velocity[Y]            -3.0335          7.2491         0.15386         0.15386
v  Velocity[Z]        -9.971e-015     8.2408e-015     -1.648e-017     -1.648e-017
v  ǁVelocityǁ         0.0023618          9.8533          5.1348          5.1348
v  Pressure               -31.029          21.282         -7.2726         -7.2726
v  nu_tilda           4.4136e-007       0.0042695       0.0016587       0.0016587
v  TempC                       21          73.049          22.015          22.015
v  TurbVisc           3.3398e-014       0.0050321        0.001949        0.001949
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2076:        0.18810E+01

===============================================================


 INSTANT    0.207700000E+04   TIME STEP NUMBER            2077
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.61263E-02 0.89412E+00
   Friction velocity        uk    :  0.61263E-02 0.89412E+00
   Dimensionless distance   yplus :  0.49321E-01 0.71983E+01
   Friction thermal sca.    tstar : -0.12516E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36799E-01 0.53707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10236E-01      33   0.25200E-03   0.49265E+01 0.18564E+03 
c  Velocity[X]                                      0.17580E+01 
c  Velocity[Y]                                      0.31686E+01 
c  Velocity[Z]                                      0.71786E-30 
c  Pressure     0.11746E-06     457   0.99268E-08   0.11525E+00 0.59450E+03 
c  nu_tilda     0.73556E-05      33   0.48632E-05   0.64425E-06 0.20971E+03 
c  TempC        0.41172E+02      27   0.33028E-03   0.63349E+01 0.27312E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3149          9.8515          4.5729          4.5729
v  Velocity[Y]             -3.034          7.2192         0.15421         0.15421
v  Velocity[Z]       -9.8033e-015     8.5005e-015    -1.6468e-017    -1.6468e-017
v  ǁVelocityǁ         0.0021083          9.8523          5.1348          5.1348
v  Pressure               -30.968          21.226         -7.2511         -7.2511
v  nu_tilda           4.4132e-007       0.0042695       0.0016591       0.0016591
v  TempC                       21          73.049          22.015          22.015
v  TurbVisc           3.3383e-014       0.0050321       0.0019495       0.0019495
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2077:        0.20310E+01

===============================================================


 INSTANT    0.207800000E+04   TIME STEP NUMBER            2078
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97245E-02 0.89292E+00
   Friction velocity        uk    :  0.97245E-02 0.89292E+00
   Dimensionless distance   yplus :  0.78289E-01 0.71886E+01
   Friction thermal sca.    tstar : -0.14533E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58412E-01 0.53635E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10238E-01      33   0.26114E-03   0.49144E+01 0.18557E+03 
c  Velocity[X]                                      0.17591E+01 
c  Velocity[Y]                                      0.31554E+01 
c  Velocity[Z]                                      0.77358E-30 
c  Pressure     0.10655E-06     473   0.94571E-08   0.10373E+00 0.68101E+03 
c  nu_tilda     0.73579E-05      33   0.14765E-04   0.64477E-06 0.20977E+03 
c  TempC        0.41179E+02      27   0.27763E-03   0.54364E+01 0.27782E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3117          9.8505          4.5729          4.5729
v  Velocity[Y]            -3.0344          7.2391         0.15456         0.15456
v  Velocity[Z]        -9.708e-015     8.2775e-015    -1.6452e-017    -1.6452e-017
v  ǁVelocityǁ          0.002313          9.8513          5.1347          5.1347
v  Pressure               -31.003          21.321         -7.2222         -7.2222
v  nu_tilda           4.4127e-007       0.0042695       0.0016595       0.0016595
v  TempC                       21          73.049          22.015          22.015
v  TurbVisc           3.3372e-014       0.0050321       0.0019499       0.0019499
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2078:        0.20660E+01

===============================================================


 INSTANT    0.207900000E+04   TIME STEP NUMBER            2079
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12964E-01 0.89397E+00
   Friction velocity        uk    :  0.12964E-01 0.89397E+00
   Dimensionless distance   yplus :  0.10437E+00 0.71971E+01
   Friction thermal sca.    tstar : -0.17807E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77873E-01 0.53698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10240E-01      33   0.25337E-03   0.49154E+01 0.18566E+03 
c  Velocity[X]                                      0.17383E+01 
c  Velocity[Y]                                      0.31772E+01 
c  Velocity[Z]                                      0.10385E-29 
c  Pressure     0.12294E-06     520   0.94501E-08   0.12215E+00 0.71511E+03 
c  nu_tilda     0.73601E-05      33   0.48764E-05   0.64523E-06 0.20983E+03 
c  TempC        0.41187E+02      27   0.36326E-03   0.42540E+01 0.24619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3084          9.8495          4.5729          4.5729
v  Velocity[Y]            -3.0347          7.2181         0.15491         0.15491
v  Velocity[Z]       -9.5857e-015     8.7017e-015     -1.644e-017     -1.644e-017
v  ǁVelocityǁ         0.0021972          9.8503          5.1347          5.1347
v  Pressure               -30.772          21.327         -7.1854         -7.1854
v  nu_tilda           4.4123e-007       0.0042695       0.0016599       0.0016599
v  TempC                       21           73.05          22.015          22.015
v  TurbVisc           3.3357e-014       0.0050321       0.0019504       0.0019504
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2079:        0.21870E+01

===============================================================


 INSTANT    0.208000000E+04   TIME STEP NUMBER            2080
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11223E-01 0.89306E+00
   Friction velocity        uk    :  0.11223E-01 0.89306E+00
   Dimensionless distance   yplus :  0.90356E-01 0.71897E+01
   Friction thermal sca.    tstar : -0.13268E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67416E-01 0.53644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10242E-01      33   0.21883E-03   0.48991E+01 0.18555E+03 
c  Velocity[X]                                      0.17405E+01 
c  Velocity[Y]                                      0.31585E+01 
c  Velocity[Z]                                      0.83319E-30 
c  Pressure     0.11544E-06     378   0.97180E-08   0.11114E+00 0.59469E+03 
c  nu_tilda     0.73624E-05      33   0.14758E-04   0.64573E-06 0.20989E+03 
c  TempC        0.41194E+02      27   0.32280E-03   0.68820E+01 0.29130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3052          9.8484          4.5729          4.5729
v  Velocity[Y]             -3.035           7.238         0.15526         0.15526
v  Velocity[Z]        -9.523e-015     8.6684e-015     -1.642e-017     -1.642e-017
v  ǁVelocityǁ         0.0022629          9.8493          5.1347          5.1347
v  Pressure               -30.964          21.338         -7.1752         -7.1752
v  nu_tilda            4.412e-007       0.0042695       0.0016602       0.0016602
v  TempC                       21          73.049          22.015          22.015
v  TurbVisc           3.3346e-014       0.0050321       0.0019509       0.0019509
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2080:        0.20870E+01

===============================================================


 INSTANT    0.208100000E+04   TIME STEP NUMBER            2081
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12087E-01 0.89484E+00
   Friction velocity        uk    :  0.12087E-01 0.89484E+00
   Dimensionless distance   yplus :  0.97311E-01 0.72040E+01
   Friction thermal sca.    tstar : -0.14866E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72605E-01 0.53750E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10243E-01      33   0.29187E-03   0.48924E+01 0.18559E+03 
c  Velocity[X]                                      0.17381E+01 
c  Velocity[Y]                                      0.31543E+01 
c  Velocity[Z]                                      0.71846E-30 
c  Pressure     0.10215E-06     552   0.98860E-08   0.10017E+00 0.13143E+04 
c  nu_tilda     0.73647E-05      33   0.48799E-05   0.64620E-06 0.20995E+03 
c  TempC        0.41201E+02      27   0.29873E-03   0.58145E+01 0.26869E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3021          9.8474          4.5729          4.5729
v  Velocity[Y]            -3.0356          7.2517         0.15561         0.15561
v  Velocity[Z]       -9.3761e-015     9.1225e-015    -1.6413e-017    -1.6413e-017
v  ǁVelocityǁ         0.0023573          9.8483          5.1346          5.1346
v  Pressure               -30.824          21.486         -7.1066         -7.1066
v  nu_tilda           4.4114e-007       0.0042695       0.0016607       0.0016607
v  TempC                       21          73.049          22.016          22.016
v  TurbVisc           3.3335e-014       0.0050321       0.0019513       0.0019513
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2081:        0.24660E+01

===============================================================


 INSTANT    0.208200000E+04   TIME STEP NUMBER            2082
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12706E-01 0.89441E+00
   Friction velocity        uk    :  0.12706E-01 0.89441E+00
   Dimensionless distance   yplus :  0.10229E+00 0.72006E+01
   Friction thermal sca.    tstar : -0.14230E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76323E-01 0.53725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10245E-01      33   0.25558E-03   0.49393E+01 0.18582E+03 
c  Velocity[X]                                      0.17669E+01 
c  Velocity[Y]                                      0.31725E+01 
c  Velocity[Z]                                      0.69557E-30 
c  Pressure     0.12117E-06     489   0.96200E-08   0.12101E+00 0.10882E+04 
c  nu_tilda     0.73669E-05      33   0.14755E-04   0.64672E-06 0.21002E+03 
c  TempC        0.41209E+02      27   0.33423E-03   0.52582E+01 0.26758E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2989          9.8464          4.5729          4.5729
v  Velocity[Y]            -3.0361          7.2219         0.15596         0.15596
v  Velocity[Z]       -9.2093e-015      8.574e-015    -1.6397e-017    -1.6397e-017
v  ǁVelocityǁ         0.0021002          9.8473          5.1346          5.1346
v  Pressure               -30.819          21.342         -7.1263         -7.1263
v  nu_tilda           4.4122e-007       0.0042695        0.001661        0.001661
v  TempC                       21          73.048          22.016          22.016
v  TurbVisc           3.3318e-014       0.0050321       0.0019518       0.0019518
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2082:        0.21290E+01

===============================================================


 INSTANT    0.208300000E+04   TIME STEP NUMBER            2083
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10953E-01 0.89294E+00
   Friction velocity        uk    :  0.10953E-01 0.89294E+00
   Dimensionless distance   yplus :  0.88181E-01 0.71888E+01
   Friction thermal sca.    tstar : -0.16678E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65793E-01 0.53637E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10247E-01      33   0.25316E-03   0.49034E+01 0.18565E+03 
c  Velocity[X]                                      0.17434E+01 
c  Velocity[Y]                                      0.31599E+01 
c  Velocity[Z]                                      0.66165E-30 
c  Pressure     0.11245E-06     538   0.95304E-08   0.10791E+00 0.13365E+04 
c  nu_tilda     0.73692E-05      33   0.48987E-05   0.64717E-06 0.21008E+03 
c  TempC        0.41216E+02      27   0.26328E-03   0.67606E+01 0.28773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2957          9.8454          4.5729          4.5729
v  Velocity[Y]            -3.0366          7.2381         0.15631         0.15631
v  Velocity[Z]       -9.0374e-015     8.9466e-015    -1.6387e-017    -1.6387e-017
v  ǁVelocityǁ         0.0022331          9.8462          5.1345          5.1345
v  Pressure               -30.774          21.506         -7.0589         -7.0589
v  nu_tilda           4.4126e-007       0.0042695       0.0016614       0.0016614
v  TempC                       21          73.049          22.016          22.016
v  TurbVisc           3.3343e-014       0.0050321       0.0019522       0.0019522
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2083:        0.22280E+01

===============================================================


 INSTANT    0.208400000E+04   TIME STEP NUMBER            2084
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99173E-02 0.89400E+00
   Friction velocity        uk    :  0.99173E-02 0.89400E+00
   Dimensionless distance   yplus :  0.79841E-01 0.71973E+01
   Friction thermal sca.    tstar : -0.35040E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59570E-01 0.53700E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10249E-01      33   0.27024E-03   0.49244E+01 0.18575E+03 
c  Velocity[X]                                      0.17671E+01 
c  Velocity[Y]                                      0.31573E+01 
c  Velocity[Z]                                      0.72563E-30 
c  Pressure     0.10885E-06     458   0.99423E-08   0.10769E+00 0.97106E+03 
c  nu_tilda     0.73714E-05      33   0.14745E-04   0.64770E-06 0.21014E+03 
c  TempC        0.41224E+02      27   0.36262E-03   0.52801E+01 0.26674E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2924          9.8443          4.5729          4.5729
v  Velocity[Y]             -3.037          7.2164         0.15666         0.15666
v  Velocity[Z]       -8.8876e-015      9.118e-015    -1.6379e-017    -1.6379e-017
v  ǁVelocityǁ          0.002072          9.8452          5.1345          5.1345
v  Pressure               -30.782          21.385         -7.0718         -7.0718
v  nu_tilda           4.4129e-007       0.0042695       0.0016618       0.0016618
v  TempC                       21          73.048          22.016          22.016
v  TurbVisc           3.3354e-014       0.0050321       0.0019527       0.0019527
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2084:        0.20440E+01

===============================================================


 INSTANT    0.208500000E+04   TIME STEP NUMBER            2085
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10810E-01 0.89326E+00
   Friction velocity        uk    :  0.10810E-01 0.89326E+00
   Dimensionless distance   yplus :  0.87031E-01 0.71914E+01
   Friction thermal sca.    tstar : -0.17000E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64935E-01 0.53656E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10251E-01      33   0.20519E-03   0.49111E+01 0.18578E+03 
c  Velocity[X]                                      0.17351E+01 
c  Velocity[Y]                                      0.31759E+01 
c  Velocity[Z]                                      0.81321E-30 
c  Pressure     0.98749E-07     538   0.96134E-08   0.96900E-01 0.16626E+04 
c  nu_tilda     0.73737E-05      33   0.49001E-05   0.64814E-06 0.21020E+03 
c  TempC        0.41231E+02      27   0.29845E-03   0.64903E+01 0.30747E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2893          9.8433          4.5729          4.5729
v  Velocity[Y]            -3.0374          7.2415         0.15701         0.15701
v  Velocity[Z]       -8.7328e-015     8.6164e-015    -1.6371e-017    -1.6371e-017
v  ǁVelocityǁ         0.0023839          9.8442          5.1345          5.1345
v  Pressure               -30.614          21.613         -6.9904         -6.9904
v  nu_tilda            4.412e-007       0.0042695       0.0016622       0.0016622
v  TempC                       21          73.049          22.016          22.016
v  TurbVisc           3.3362e-014       0.0050321       0.0019531       0.0019531
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2085:        0.22280E+01

===============================================================


 INSTANT    0.208600000E+04   TIME STEP NUMBER            2086
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71660E-02 0.89434E+00
   Friction velocity        uk    :  0.71660E-02 0.89434E+00
   Dimensionless distance   yplus :  0.57691E-01 0.72001E+01
   Friction thermal sca.    tstar : -0.13163E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43044E-01 0.53721E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10253E-01      33   0.26818E-03   0.48770E+01 0.18559E+03 
c  Velocity[X]                                      0.17203E+01 
c  Velocity[Y]                                      0.31567E+01 
c  Velocity[Z]                                      0.88351E-30 
c  Pressure     0.11177E-06     458   0.94075E-08   0.10767E+00 0.85567E+03 
c  nu_tilda     0.73759E-05      33   0.14744E-04   0.64864E-06 0.21026E+03 
c  TempC        0.41238E+02      27   0.35797E-03   0.62778E+01 0.28465E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2861          9.8423          4.5729          4.5729
v  Velocity[Y]            -3.0376          7.2444         0.15736         0.15736
v  Velocity[Z]       -8.5896e-015     8.9222e-015    -1.6359e-017    -1.6359e-017
v  ǁVelocityǁ         0.0023554          9.8432          5.1344          5.1344
v  Pressure               -30.811          21.525         -6.9995         -6.9995
v  nu_tilda           4.4108e-007       0.0042695       0.0016625       0.0016625
v  TempC                       21          73.048          22.017          22.017
v  TurbVisc           3.3337e-014       0.0050321       0.0019536       0.0019536
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2086:        0.20380E+01

===============================================================


 INSTANT    0.208700000E+04   TIME STEP NUMBER            2087
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11554E-01 0.89414E+00
   Friction velocity        uk    :  0.11554E-01 0.89414E+00
   Dimensionless distance   yplus :  0.93021E-01 0.71984E+01
   Friction thermal sca.    tstar : -0.14445E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69404E-01 0.53708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10255E-01      33   0.28620E-03   0.49157E+01 0.18582E+03 
c  Velocity[X]                                      0.17625E+01 
c  Velocity[Y]                                      0.31532E+01 
c  Velocity[Z]                                      0.89617E-30 
c  Pressure     0.12565E-06     474   0.99213E-08   0.12423E+00 0.68701E+03 
c  nu_tilda     0.73782E-05      33   0.49103E-05   0.64908E-06 0.21032E+03 
c  TempC        0.41245E+02      27   0.26421E-03   0.62557E+01 0.28626E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2829          9.8413          4.5729          4.5729
v  Velocity[Y]            -3.0381          7.2203         0.15771         0.15771
v  Velocity[Z]       -8.4079e-015     9.0536e-015    -1.6348e-017    -1.6348e-017
v  ǁVelocityǁ         0.0021231          9.8422          5.1344          5.1344
v  Pressure               -30.626          21.527         -6.9655         -6.9655
v  nu_tilda           4.4108e-007       0.0042695        0.001663        0.001663
v  TempC                       21          73.049          22.017          22.017
v  TurbVisc             3.33e-014       0.0050321        0.001954        0.001954
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2087:        0.20600E+01

===============================================================


 INSTANT    0.208800000E+04   TIME STEP NUMBER            2088
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10871E-01 0.89277E+00
   Friction velocity        uk    :  0.10871E-01 0.89277E+00
   Dimensionless distance   yplus :  0.87520E-01 0.71874E+01
   Friction thermal sca.    tstar : -0.16659E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65300E-01 0.53626E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10257E-01      33   0.26048E-03   0.49179E+01 0.18587E+03 
c  Velocity[X]                                      0.17486E+01 
c  Velocity[Y]                                      0.31693E+01 
c  Velocity[Z]                                      0.72204E-30 
c  Pressure     0.11080E-06     474   0.95927E-08   0.10875E+00 0.72868E+03 
c  nu_tilda     0.73805E-05      33   0.14737E-04   0.64959E-06 0.21037E+03 
c  TempC        0.41253E+02      27   0.25580E-03   0.40026E+01 0.24332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2796          9.8403          4.5729          4.5729
v  Velocity[Y]            -3.0387           7.238         0.15805         0.15805
v  Velocity[Z]       -8.2949e-015     9.1923e-015    -1.6338e-017    -1.6338e-017
v  ǁVelocityǁ         0.0023121          9.8411          5.1343          5.1343
v  Pressure               -30.624          21.621         -6.9319         -6.9319
v  nu_tilda           4.4112e-007       0.0042695       0.0016633       0.0016633
v  TempC                       21          73.048          22.017          22.017
v  TurbVisc           3.3299e-014       0.0050321       0.0019545       0.0019545
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2088:        0.20820E+01

===============================================================


 INSTANT    0.208900000E+04   TIME STEP NUMBER            2089
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13364E-01 0.89380E+00
   Friction velocity        uk    :  0.13364E-01 0.89380E+00
   Dimensionless distance   yplus :  0.10759E+00 0.71957E+01
   Friction thermal sca.    tstar : -0.17489E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80273E-01 0.53688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10259E-01      33   0.26526E-03   0.49054E+01 0.18579E+03 
c  Velocity[X]                                      0.17475E+01 
c  Velocity[Y]                                      0.31579E+01 
c  Velocity[Z]                                      0.70317E-30 
c  Pressure     0.11693E-06     458   0.96341E-08   0.11438E+00 0.63495E+03 
c  nu_tilda     0.73827E-05      33   0.49205E-05   0.65001E-06 0.21043E+03 
c  TempC        0.41260E+02      27   0.34952E-03   0.73382E+01 0.27908E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2764          9.8392          4.5729          4.5729
v  Velocity[Y]            -3.0391          7.2137          0.1584          0.1584
v  Velocity[Z]       -8.1792e-015     9.1557e-015    -1.6331e-017    -1.6331e-017
v  ǁVelocityǁ         0.0021055          9.8401          5.1343          5.1343
v  Pressure               -30.586          21.568         -6.9091         -6.9091
v  nu_tilda           4.4123e-007       0.0042695       0.0016638       0.0016638
v  TempC                       21          73.049          22.017          22.017
v  TurbVisc           3.3311e-014       0.0050321       0.0019549       0.0019549
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2089:        0.20450E+01

===============================================================


 INSTANT    0.209000000E+04   TIME STEP NUMBER            2090
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10816E-01 0.89311E+00
   Friction velocity        uk    :  0.10816E-01 0.89311E+00
   Dimensionless distance   yplus :  0.87078E-01 0.71902E+01
   Friction thermal sca.    tstar : -0.26013E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64970E-01 0.53647E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10260E-01      33   0.21312E-03   0.49093E+01 0.18580E+03 
c  Velocity[X]                                      0.17594E+01 
c  Velocity[Y]                                      0.31499E+01 
c  Velocity[Z]                                      0.67876E-30 
c  Pressure     0.96890E-07     489   0.94642E-08   0.94907E-01 0.70597E+03 
c  nu_tilda     0.73850E-05      33   0.14733E-04   0.65051E-06 0.21049E+03 
c  TempC        0.41267E+02      27   0.28940E-03   0.69454E+01 0.27701E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2732          9.8382          4.5729          4.5729
v  Velocity[Y]            -3.0395          7.2396         0.15875         0.15875
v  Velocity[Z]       -8.0351e-015     9.1331e-015    -1.6319e-017    -1.6319e-017
v  ǁVelocityǁ         0.0023196          9.8391          5.1342          5.1342
v  Pressure               -30.604           21.66         -6.8783         -6.8783
v  nu_tilda           4.4127e-007       0.0042695       0.0016641       0.0016641
v  TempC                       21          73.049          22.017          22.017
v  TurbVisc           3.3344e-014       0.0050321       0.0019554       0.0019554
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2090:        0.21270E+01

===============================================================


 INSTANT    0.209100000E+04   TIME STEP NUMBER            2091
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54447E-02 0.89468E+00
   Friction velocity        uk    :  0.54447E-02 0.89468E+00
   Dimensionless distance   yplus :  0.43834E-01 0.72027E+01
   Friction thermal sca.    tstar : -0.25748E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32705E-01 0.53741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10262E-01      33   0.25488E-03   0.48856E+01 0.18580E+03 
c  Velocity[X]                                      0.17131E+01 
c  Velocity[Y]                                      0.31724E+01 
c  Velocity[Z]                                      0.86091E-30 
c  Pressure     0.10402E-06     522   0.95740E-08   0.10210E+00 0.12032E+04 
c  nu_tilda     0.73872E-05      33   0.49260E-05   0.65095E-06 0.21055E+03 
c  TempC        0.41275E+02      27   0.31629E-03   0.52487E+01 0.24004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.27          9.8372          4.5729          4.5729
v  Velocity[Y]            -3.0398          7.2502         0.15909         0.15909
v  Velocity[Z]       -8.1143e-015     9.0797e-015    -1.6307e-017    -1.6307e-017
v  ǁVelocityǁ         0.0024302          9.8381          5.1342          5.1342
v  Pressure               -30.433          21.784         -6.8147         -6.8147
v  nu_tilda           4.4123e-007       0.0042695       0.0016645       0.0016645
v  TempC                       21           73.05          22.017          22.017
v  TurbVisc           3.3358e-014       0.0050321       0.0019558       0.0019558
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2091:        0.21730E+01

===============================================================


 INSTANT    0.209200000E+04   TIME STEP NUMBER            2092
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13740E-01 0.89413E+00
   Friction velocity        uk    :  0.13740E-01 0.89413E+00
   Dimensionless distance   yplus :  0.11062E+00 0.71983E+01
   Friction thermal sca.    tstar : -0.13193E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82532E-01 0.53708E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10264E-01      33   0.26644E-03   0.49112E+01 0.18588E+03 
c  Velocity[X]                                      0.17490E+01 
c  Velocity[Y]                                      0.31622E+01 
c  Velocity[Z]                                      0.77450E-30 
c  Pressure     0.11626E-06     537   0.98612E-08   0.11375E+00 0.13572E+04 
c  nu_tilda     0.73895E-05      33   0.14727E-04   0.65146E-06 0.21061E+03 
c  TempC        0.41282E+02      27   0.28692E-03   0.68886E+01 0.28351E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2667          9.8361          4.5729          4.5729
v  Velocity[Y]              -3.04          7.2168         0.15944         0.15944
v  Velocity[Z]       -8.0036e-015     9.0997e-015    -1.6291e-017    -1.6291e-017
v  ǁVelocityǁ         0.0021136          9.8371          5.1342          5.1342
v  Pressure                -30.59          21.594         -6.8465         -6.8465
v  nu_tilda           4.4129e-007       0.0042695       0.0016648       0.0016648
v  TempC                       21          73.049          22.018          22.018
v  TurbVisc           3.3346e-014       0.0050321       0.0019563       0.0019563
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2092:        0.22320E+01

===============================================================


 INSTANT    0.209300000E+04   TIME STEP NUMBER            2093
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11382E-01 0.89296E+00
   Friction velocity        uk    :  0.11382E-01 0.89296E+00
   Dimensionless distance   yplus :  0.91631E-01 0.71889E+01
   Friction thermal sca.    tstar : -0.18236E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68367E-01 0.53637E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10266E-01      33   0.28667E-03   0.48995E+01 0.18589E+03 
c  Velocity[X]                                      0.17474E+01 
c  Velocity[Y]                                      0.31520E+01 
c  Velocity[Z]                                      0.88020E-30 
c  Pressure     0.10648E-06     600   0.96762E-08   0.10429E+00 0.17715E+04 
c  nu_tilda     0.73917E-05      33   0.49437E-05   0.65189E-06 0.21066E+03 
c  TempC        0.41289E+02      27   0.36142E-03   0.55744E+01 0.26750E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2634          9.8351          4.5729          4.5729
v  Velocity[Y]            -3.0405            7.24         0.15978         0.15978
v  Velocity[Z]       -8.5087e-015     9.1001e-015    -1.6285e-017    -1.6285e-017
v  ǁVelocityǁ         0.0023789           9.836          5.1341          5.1341
v  Pressure               -30.428          21.832         -6.7601         -6.7601
v  nu_tilda           4.4126e-007       0.0042695       0.0016653       0.0016653
v  TempC                       21           73.05          22.018          22.018
v  TurbVisc           3.3361e-014       0.0050321       0.0019567       0.0019567
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2093:        0.23710E+01

===============================================================


 INSTANT    0.209400000E+04   TIME STEP NUMBER            2094
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12968E-01 0.89389E+00
   Friction velocity        uk    :  0.12968E-01 0.89389E+00
   Dimensionless distance   yplus :  0.10440E+00 0.71965E+01
   Friction thermal sca.    tstar : -0.14313E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77895E-01 0.53694E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10268E-01      33   0.27167E-03   0.49196E+01 0.18599E+03 
c  Velocity[X]                                      0.17515E+01 
c  Velocity[Y]                                      0.31681E+01 
c  Velocity[Z]                                      0.72485E-30 
c  Pressure     0.11186E-06     522   0.96825E-08   0.11147E+00 0.12015E+04 
c  nu_tilda     0.73940E-05      33   0.14717E-04   0.65236E-06 0.21072E+03 
c  TempC        0.41297E+02      27   0.28098E-03   0.63889E+01 0.29140E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2602          9.8341          4.5729          4.5729
v  Velocity[Y]             -3.041          7.2159         0.16013         0.16013
v  Velocity[Z]       -8.8448e-015     9.0027e-015    -1.6266e-017    -1.6266e-017
v  ǁVelocityǁ         0.0021758           9.835          5.1341          5.1341
v  Pressure               -30.432          21.673         -6.7819         -6.7819
v  nu_tilda           4.4124e-007       0.0042695       0.0016656       0.0016656
v  TempC                       21          73.048          22.018          22.018
v  TurbVisc           3.3354e-014       0.0050321       0.0019572       0.0019572
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2094:        0.21860E+01

===============================================================


 INSTANT    0.209500000E+04   TIME STEP NUMBER            2095
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.83070E-02 0.89304E+00
   Friction velocity        uk    :  0.83070E-02 0.89304E+00
   Dimensionless distance   yplus :  0.66877E-01 0.71896E+01
   Friction thermal sca.    tstar : -0.16765E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49898E-01 0.53642E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10270E-01      33   0.25284E-03   0.49019E+01 0.18590E+03 
c  Velocity[X]                                      0.17462E+01 
c  Velocity[Y]                                      0.31557E+01 
c  Velocity[Z]                                      0.74329E-30 
c  Pressure     0.12122E-06     554   0.97605E-08   0.11613E+00 0.15231E+04 
c  nu_tilda     0.73962E-05      33   0.49434E-05   0.65279E-06 0.21077E+03 
c  TempC        0.41304E+02      27   0.25034E-03   0.57654E+01 0.27737E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.257           9.833          4.5729          4.5729
v  Velocity[Y]            -3.0415           7.237         0.16047         0.16047
v  Velocity[Z]       -8.5341e-015     8.7695e-015    -1.6252e-017    -1.6252e-017
v  ǁVelocityǁ         0.0023412           9.834           5.134           5.134
v  Pressure               -30.383          21.866         -6.7066         -6.7066
v  nu_tilda           4.4123e-007       0.0042695        0.001666        0.001666
v  TempC                       21          73.048          22.018          22.018
v  TurbVisc           3.3346e-014       0.0050321       0.0019576       0.0019576
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2095:        0.22630E+01

===============================================================


 INSTANT    0.209600000E+04   TIME STEP NUMBER            2096
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.86052E-02 0.89440E+00
   Friction velocity        uk    :  0.86052E-02 0.89440E+00
   Dimensionless distance   yplus :  0.69278E-01 0.72005E+01
   Friction thermal sca.    tstar : -0.17973E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51689E-01 0.53724E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10272E-01      33   0.26286E-03   0.48865E+01 0.18584E+03 
c  Velocity[X]                                      0.17399E+01 
c  Velocity[Y]                                      0.31466E+01 
c  Velocity[Z]                                      0.74571E-30 
c  Pressure     0.99783E-07     424   0.97083E-08   0.97480E-01 0.70905E+03 
c  nu_tilda     0.73985E-05      33   0.14719E-04   0.65327E-06 0.21083E+03 
c  TempC        0.41311E+02      27   0.34055E-03   0.39710E+01 0.23949E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2537           9.832          4.5729          4.5729
v  Velocity[Y]            -3.0419          7.2456         0.16081         0.16081
v  Velocity[Z]       -8.7778e-015     8.5869e-015    -1.6239e-017    -1.6239e-017
v  ǁVelocityǁ         0.0024195           9.833           5.134           5.134
v  Pressure               -30.458          21.829         -6.7053         -6.7053
v  nu_tilda           4.4122e-007       0.0042695       0.0016664       0.0016664
v  TempC                       21          73.048          22.018          22.018
v  TurbVisc           3.3343e-014       0.0050321       0.0019581       0.0019581
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2096:        0.19660E+01

===============================================================


 INSTANT    0.209700000E+04   TIME STEP NUMBER            2097
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13529E-01 0.89401E+00
   Friction velocity        uk    :  0.13529E-01 0.89401E+00
   Dimensionless distance   yplus :  0.10891E+00 0.71974E+01
   Friction thermal sca.    tstar : -0.22193E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81262E-01 0.53701E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10273E-01      33   0.24983E-03   0.49060E+01 0.18600E+03 
c  Velocity[X]                                      0.17367E+01 
c  Velocity[Y]                                      0.31692E+01 
c  Velocity[Z]                                      0.75518E-30 
c  Pressure     0.12118E-06     506   0.97085E-08   0.12153E+00 0.85250E+03 
c  nu_tilda     0.74007E-05      33   0.49569E-05   0.65370E-06 0.21089E+03 
c  TempC        0.41318E+02      27   0.32198E-03   0.60272E+01 0.28301E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2504           9.831          4.5729          4.5729
v  Velocity[Y]            -3.0422          7.2186         0.16116         0.16116
v  Velocity[Z]       -8.7134e-015     8.3781e-015    -1.6222e-017    -1.6222e-017
v  ǁVelocityǁ         0.0022703           9.832          5.1339          5.1339
v  Pressure               -30.227           21.86         -6.6592         -6.6592
v  nu_tilda           4.4122e-007       0.0042695       0.0016668       0.0016668
v  TempC                       21          73.049          22.018          22.018
v  TurbVisc           3.3342e-014       0.0050321       0.0019585       0.0019585
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2097:        0.21540E+01

===============================================================


 INSTANT    0.209800000E+04   TIME STEP NUMBER            2098
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11867E-01 0.89246E+00
   Friction velocity        uk    :  0.11867E-01 0.89246E+00
   Dimensionless distance   yplus :  0.95534E-01 0.71849E+01
   Friction thermal sca.    tstar : -0.16000E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71279E-01 0.53608E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10275E-01      33   0.26184E-03   0.48821E+01 0.18586E+03 
c  Velocity[X]                                      0.17306E+01 
c  Velocity[Y]                                      0.31515E+01 
c  Velocity[Z]                                      0.78086E-30 
c  Pressure     0.11640E-06     377   0.97150E-08   0.11211E+00 0.63254E+03 
c  nu_tilda     0.74030E-05      33   0.14709E-04   0.65417E-06 0.21094E+03 
c  TempC        0.41326E+02      27   0.30493E-03   0.75745E+01 0.29021E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2472            9.83          4.5729          4.5729
v  Velocity[Y]            -3.0424          7.2333          0.1615          0.1615
v  Velocity[Z]       -8.8036e-015     8.1738e-015    -1.6204e-017    -1.6204e-017
v  ǁVelocityǁ         0.0023073          9.8309          5.1339          5.1339
v  Pressure               -30.404          21.863         -6.6488         -6.6488
v  nu_tilda           4.4122e-007       0.0042695       0.0016671       0.0016671
v  TempC                       21          73.049          22.019          22.019
v  TurbVisc           3.3342e-014       0.0050321        0.001959        0.001959
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2098:        0.18600E+01

===============================================================


 INSTANT    0.209900000E+04   TIME STEP NUMBER            2099
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13008E-01 0.89380E+00
   Friction velocity        uk    :  0.13008E-01 0.89380E+00
   Dimensionless distance   yplus :  0.10473E+00 0.71957E+01
   Friction thermal sca.    tstar : -0.18499E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78137E-01 0.53688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10277E-01      33   0.29350E-03   0.49069E+01 0.18605E+03 
c  Velocity[X]                                      0.17538E+01 
c  Velocity[Y]                                      0.31532E+01 
c  Velocity[Z]                                      0.72110E-30 
c  Pressure     0.12026E-06     490   0.93151E-08   0.11886E+00 0.78035E+03 
c  nu_tilda     0.74052E-05      33   0.49598E-05   0.65460E-06 0.21099E+03 
c  TempC        0.41333E+02      27   0.28469E-03   0.45327E+01 0.25550E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.244          9.8289          4.5729          4.5729
v  Velocity[Y]            -3.0428          7.2145         0.16184         0.16184
v  Velocity[Z]       -8.6009e-015     7.9646e-015    -1.6191e-017    -1.6191e-017
v  ǁVelocityǁ         0.0021388          9.8299          5.1338          5.1338
v  Pressure               -30.211          21.892         -6.6083         -6.6083
v  nu_tilda           4.4124e-007       0.0042695       0.0016676       0.0016676
v  TempC                       21          73.049          22.019          22.019
v  TurbVisc           3.3342e-014       0.0050321       0.0019594       0.0019594
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2099:        0.20960E+01

===============================================================


 INSTANT    0.210000000E+04   TIME STEP NUMBER            2100
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99597E-03 0.89298E+00
   Friction velocity        uk    :  0.99597E-03 0.89298E+00
   Dimensionless distance   yplus :  0.80183E-02 0.71891E+01
   Friction thermal sca.    tstar : -0.55257E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59825E-02 0.53639E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10279E-01      33   0.21720E-03   0.49171E+01 0.18612E+03 
c  Velocity[X]                                      0.17502E+01 
c  Velocity[Y]                                      0.31668E+01 
c  Velocity[Z]                                      0.79401E-30 
c  Pressure     0.11239E-06     488   0.94605E-08   0.11031E+00 0.64994E+03 
c  nu_tilda     0.74075E-05      33   0.14709E-04   0.65507E-06 0.21105E+03 
c  TempC        0.41340E+02      27   0.31189E-03   0.44480E+01 0.24342E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2407          9.8279          4.5729          4.5729
v  Velocity[Y]            -3.0433          7.2382         0.16218         0.16218
v  Velocity[Z]        -8.789e-015     7.7742e-015    -1.6174e-017    -1.6174e-017
v  ǁVelocityǁ          0.002288          9.8289          5.1338          5.1338
v  Pressure               -30.243          21.959         -6.5825         -6.5825
v  nu_tilda           4.4124e-007       0.0042695       0.0016679       0.0016679
v  TempC                       21          73.048          22.019          22.019
v  TurbVisc           3.3348e-014       0.0050321       0.0019599       0.0019599
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2100:        0.21040E+01

===============================================================


 INSTANT    0.210100000E+04   TIME STEP NUMBER            2101
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94537E-02 0.89454E+00
   Friction velocity        uk    :  0.94537E-02 0.89454E+00
   Dimensionless distance   yplus :  0.76109E-01 0.72017E+01
   Friction thermal sca.    tstar : -0.15044E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56786E-01 0.53733E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10281E-01      33   0.25607E-03   0.48741E+01 0.18592E+03 
c  Velocity[X]                                      0.17204E+01 
c  Velocity[Y]                                      0.31537E+01 
c  Velocity[Z]                                      0.83814E-30 
c  Pressure     0.11052E-06     490   0.97931E-08   0.10698E+00 0.92421E+03 
c  nu_tilda     0.74097E-05      33   0.49695E-05   0.65548E-06 0.21110E+03 
c  TempC        0.41347E+02      27   0.28676E-03   0.47603E+01 0.25009E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2373          9.8269          4.5729          4.5729
v  Velocity[Y]            -3.0437          7.2452         0.16252         0.16252
v  Velocity[Z]       -8.7699e-015     7.0395e-015    -1.6156e-017    -1.6156e-017
v  ǁVelocityǁ         0.0023485          9.8279          5.1337          5.1337
v  Pressure               -30.233          22.031         -6.5342         -6.5342
v  nu_tilda           4.4117e-007       0.0042695       0.0016683       0.0016683
v  TempC                       21          73.049          22.019          22.019
v  TurbVisc           3.3347e-014       0.0050321       0.0019603       0.0019603
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2101:        0.21050E+01

===============================================================


 INSTANT    0.210200000E+04   TIME STEP NUMBER            2102
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89115E-02 0.89419E+00
   Friction velocity        uk    :  0.89115E-02 0.89419E+00
   Dimensionless distance   yplus :  0.71744E-01 0.71988E+01
   Friction thermal sca.    tstar : -0.15690E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53529E-01 0.53711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10283E-01      33   0.25647E-03   0.49115E+01 0.18606E+03 
c  Velocity[X]                                      0.17655E+01 
c  Velocity[Y]                                      0.31460E+01 
c  Velocity[Z]                                      0.70981E-30 
c  Pressure     0.10655E-06     473   0.91907E-08   0.10600E+00 0.10023E+04 
c  nu_tilda     0.74119E-05      33   0.14700E-04   0.65596E-06 0.21116E+03 
c  TempC        0.41355E+02      27   0.40244E-03   0.52508E+01 0.26646E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2341          9.8258          4.5729          4.5729
v  Velocity[Y]            -3.0441          7.2178         0.16286         0.16286
v  Velocity[Z]       -8.8597e-015     7.2395e-015    -1.6146e-017    -1.6146e-017
v  ǁVelocityǁ         0.0021352          9.8268          5.1337          5.1337
v  Pressure               -30.233           21.91         -6.5462         -6.5462
v  nu_tilda           4.4119e-007       0.0042695       0.0016686       0.0016686
v  TempC                       21          73.048          22.019          22.019
v  TurbVisc           3.3326e-014       0.0050321       0.0019608       0.0019608
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2102:        0.20840E+01

===============================================================


 INSTANT    0.210300000E+04   TIME STEP NUMBER            2103
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12070E-01 0.89279E+00
   Friction velocity        uk    :  0.12070E-01 0.89279E+00
   Dimensionless distance   yplus :  0.97169E-01 0.71876E+01
   Friction thermal sca.    tstar : -0.19327E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72499E-01 0.53627E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10284E-01      33   0.25276E-03   0.48913E+01 0.18607E+03 
c  Velocity[X]                                      0.17241E+01 
c  Velocity[Y]                                      0.31672E+01 
c  Velocity[Z]                                      0.73963E-30 
c  Pressure     0.10207E-06     568   0.99510E-08   0.99828E-01 0.16257E+04 
c  nu_tilda     0.74142E-05      33   0.49804E-05   0.65636E-06 0.21121E+03 
c  TempC        0.41362E+02      27   0.31433E-03   0.76675E+01 0.31403E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2309          9.8248          4.5729          4.5729
v  Velocity[Y]            -3.0444          7.2379          0.1632          0.1632
v  Velocity[Z]       -8.7531e-015      7.177e-015    -1.6129e-017    -1.6129e-017
v  ǁVelocityǁ         0.0023569          9.8258          5.1336          5.1336
v  Pressure               -30.034          22.123         -6.4674         -6.4674
v  nu_tilda            4.412e-007       0.0042695       0.0016691       0.0016691
v  TempC                       21          73.049          22.019          22.019
v  TurbVisc           3.3333e-014       0.0050321       0.0019612       0.0019612
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2103:        0.22720E+01

===============================================================


 INSTANT    0.210400000E+04   TIME STEP NUMBER            2104
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13222E-01 0.89363E+00
   Friction velocity        uk    :  0.13222E-01 0.89363E+00
   Dimensionless distance   yplus :  0.10645E+00 0.71944E+01
   Friction thermal sca.    tstar : -0.13182E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79423E-01 0.53678E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10286E-01      33   0.27193E-03   0.48858E+01 0.18600E+03 
c  Velocity[X]                                      0.17360E+01 
c  Velocity[Y]                                      0.31497E+01 
c  Velocity[Z]                                      0.73916E-30 
c  Pressure     0.11015E-06     505   0.95255E-08   0.10749E+00 0.13684E+04 
c  nu_tilda     0.74164E-05      33   0.14695E-04   0.65683E-06 0.21126E+03 
c  TempC        0.41369E+02      27   0.24965E-03   0.45181E+01 0.25262E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2276          9.8237          4.5729          4.5729
v  Velocity[Y]            -3.0446          7.2112         0.16354         0.16354
v  Velocity[Z]       -8.9284e-015     6.4018e-015    -1.6115e-017    -1.6115e-017
v  ǁVelocityǁ         0.0020638          9.8247          5.1336          5.1336
v  Pressure               -30.194          21.932         -6.4962         -6.4962
v  nu_tilda           4.4123e-007       0.0042695       0.0016694       0.0016694
v  TempC                       21          73.048           22.02           22.02
v  TurbVisc           3.3337e-014       0.0050321       0.0019617       0.0019617
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2104:        0.21440E+01

===============================================================


 INSTANT    0.210500000E+04   TIME STEP NUMBER            2105
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10890E-01 0.89311E+00
   Friction velocity        uk    :  0.10890E-01 0.89311E+00
   Dimensionless distance   yplus :  0.87675E-01 0.71901E+01
   Friction thermal sca.    tstar : -0.18298E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65415E-01 0.53646E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10288E-01      33   0.24561E-03   0.48933E+01 0.18610E+03 
c  Velocity[X]                                      0.17478E+01 
c  Velocity[Y]                                      0.31455E+01 
c  Velocity[Z]                                      0.73915E-30 
c  Pressure     0.11076E-06     536   0.95984E-08   0.10805E+00 0.17807E+04 
c  nu_tilda     0.74187E-05      33   0.49835E-05   0.65722E-06 0.21131E+03 
c  TempC        0.41376E+02      27   0.33098E-03   0.31198E+01 0.21632E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2242          9.8227          4.5729          4.5729
v  Velocity[Y]            -3.0449          7.2385         0.16388         0.16388
v  Velocity[Z]       -9.0086e-015     6.6801e-015    -1.6095e-017    -1.6095e-017
v  ǁVelocityǁ         0.0023589          9.8237          5.1335          5.1335
v  Pressure               -30.056          22.174         -6.4109         -6.4109
v  nu_tilda           4.4122e-007       0.0042695       0.0016698       0.0016698
v  TempC                       21          73.049           22.02           22.02
v  TurbVisc           3.3345e-014       0.0050321       0.0019621       0.0019621
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2105:        0.22240E+01

===============================================================


 INSTANT    0.210600000E+04   TIME STEP NUMBER            2106
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.92446E-02 0.89431E+00
   Friction velocity        uk    :  0.92446E-02 0.89431E+00
   Dimensionless distance   yplus :  0.74426E-01 0.71998E+01
   Friction thermal sca.    tstar : -0.16987E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55530E-01 0.53719E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10290E-01      33   0.25722E-03   0.48893E+01 0.18613E+03 
c  Velocity[X]                                      0.17276E+01 
c  Velocity[Y]                                      0.31617E+01 
c  Velocity[Z]                                      0.65597E-30 
c  Pressure     0.10283E-06     346   0.94725E-08   0.10129E+00 0.68722E+03 
c  nu_tilda     0.74209E-05      33   0.14690E-04   0.65769E-06 0.21137E+03 
c  TempC        0.41383E+02      27   0.30646E-03   0.49234E+01 0.24358E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.221          9.8217          4.5729          4.5729
v  Velocity[Y]            -3.0454          7.2445         0.16421         0.16421
v  Velocity[Z]       -9.3279e-015     6.2829e-015    -1.6081e-017    -1.6081e-017
v  ǁVelocityǁ         0.0024579          9.8227          5.1335          5.1335
v  Pressure               -30.085          22.142         -6.4039         -6.4039
v  nu_tilda           4.4122e-007       0.0042695       0.0016701       0.0016701
v  TempC                       21          73.049           22.02           22.02
v  TurbVisc           3.3341e-014       0.0050321       0.0019626       0.0019626
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2106:        0.17830E+01

===============================================================


 INSTANT    0.210700000E+04   TIME STEP NUMBER            2107
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13135E-01 0.89386E+00
   Friction velocity        uk    :  0.13135E-01 0.89386E+00
   Dimensionless distance   yplus :  0.10574E+00 0.71962E+01
   Friction thermal sca.    tstar : -0.15654E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78897E-01 0.53691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10292E-01      33   0.25280E-03   0.49047E+01 0.18617E+03 
c  Velocity[X]                                      0.17483E+01 
c  Velocity[Y]                                      0.31564E+01 
c  Velocity[Z]                                      0.81276E-30 
c  Pressure     0.13086E-06     489   0.99995E-08   0.12739E+00 0.65736E+03 
c  nu_tilda     0.74231E-05      33   0.50016E-05   0.65812E-06 0.21142E+03 
c  TempC        0.41391E+02      27   0.30111E-03   0.40754E+01 0.23942E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2177          9.8207          4.5729          4.5729
v  Velocity[Y]            -3.0458          7.2134         0.16455         0.16455
v  Velocity[Z]       -9.3534e-015     6.3382e-015    -1.6069e-017    -1.6069e-017
v  ǁVelocityǁ         0.0022125          9.8217          5.1334          5.1334
v  Pressure               -30.031          22.107         -6.3761         -6.3761
v  nu_tilda           4.4128e-007       0.0042695       0.0016706       0.0016706
v  TempC                       21          73.049           22.02           22.02
v  TurbVisc           3.3343e-014       0.0050321        0.001963        0.001963
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2107:        0.21100E+01

===============================================================


 INSTANT    0.210800000E+04   TIME STEP NUMBER            2108
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10603E-01 0.89258E+00
   Friction velocity        uk    :  0.10603E-01 0.89258E+00
   Dimensionless distance   yplus :  0.85363E-01 0.71859E+01
   Friction thermal sca.    tstar : -0.24886E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63690E-01 0.53615E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10294E-01      33   0.25919E-03   0.48931E+01 0.18611E+03 
c  Velocity[X]                                      0.17498E+01 
c  Velocity[Y]                                      0.31433E+01 
c  Velocity[Z]                                      0.72844E-30 
c  Pressure     0.10196E-06     457   0.93831E-08   0.99647E-01 0.69138E+03 
c  nu_tilda     0.74254E-05      33   0.14683E-04   0.65857E-06 0.21147E+03 
c  TempC        0.41398E+02      27   0.27494E-03   0.52419E+01 0.24720E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2144          9.8197          4.5729          4.5729
v  Velocity[Y]            -3.0462          7.2348         0.16489         0.16489
v  Velocity[Z]       -9.3425e-015     6.2427e-015    -1.6057e-017    -1.6057e-017
v  ǁVelocityǁ         0.0023899          9.8206          5.1334          5.1334
v  Pressure               -30.037          22.189         -6.3472         -6.3472
v  nu_tilda           4.4127e-007       0.0042695       0.0016709       0.0016709
v  TempC                       21          73.048           22.02           22.02
v  TurbVisc           3.3361e-014       0.0050321       0.0019634       0.0019634
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2108:        0.20650E+01

===============================================================


 INSTANT    0.210900000E+04   TIME STEP NUMBER            2109
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10673E-01 0.89373E+00
   Friction velocity        uk    :  0.10673E-01 0.89373E+00
   Dimensionless distance   yplus :  0.85924E-01 0.71952E+01
   Friction thermal sca.    tstar : -0.28169E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64109E-01 0.53684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10295E-01      33   0.26150E-03   0.48915E+01 0.18619E+03 
c  Velocity[X]                                      0.17271E+01 
c  Velocity[Y]                                      0.31644E+01 
c  Velocity[Z]                                      0.79024E-30 
c  Pressure     0.10903E-06     505   0.92127E-08   0.10904E+00 0.72634E+03 
c  nu_tilda     0.74276E-05      33   0.50003E-05   0.65895E-06 0.21152E+03 
c  TempC        0.41405E+02      27   0.28845E-03   0.41664E+01 0.23332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.211          9.8187          4.5729          4.5729
v  Velocity[Y]            -3.0465          7.2149         0.16523         0.16523
v  Velocity[Z]       -9.2781e-015     6.2839e-015    -1.6046e-017    -1.6046e-017
v  ǁVelocityǁ         0.0022552          9.8196          5.1333          5.1333
v  Pressure               -29.849          22.193         -6.3107         -6.3107
v  nu_tilda           4.4124e-007       0.0042695       0.0016713       0.0016713
v  TempC                       21          73.048           22.02           22.02
v  TurbVisc           3.3356e-014       0.0050321       0.0019639       0.0019639
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2109:        0.21680E+01

===============================================================


 INSTANT    0.211000000E+04   TIME STEP NUMBER            2110
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.34218E-02 0.89283E+00
   Friction velocity        uk    :  0.34218E-02 0.89283E+00
   Dimensionless distance   yplus :  0.27548E-01 0.71879E+01
   Friction thermal sca.    tstar : -0.31536E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20554E-01 0.53630E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10297E-01      33   0.21805E-03   0.48794E+01 0.18609E+03 
c  Velocity[X]                                      0.17324E+01 
c  Velocity[Y]                                      0.31470E+01 
c  Velocity[Z]                                      0.77902E-30 
c  Pressure     0.11162E-06     426   0.98289E-08   0.10789E+00 0.61291E+03 
c  nu_tilda     0.74299E-05      33   0.14682E-04   0.65940E-06 0.21157E+03 
c  TempC        0.41412E+02      27   0.30236E-03   0.39259E+01 0.22451E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2077          9.8176          4.5729          4.5729
v  Velocity[Y]            -3.0466          7.2336         0.16556         0.16556
v  Velocity[Z]       -9.2972e-015     6.3886e-015    -1.6032e-017    -1.6032e-017
v  ǁVelocityǁ         0.0023373          9.8185          5.1333          5.1333
v  Pressure               -30.014          22.222         -6.2935         -6.2935
v  nu_tilda           4.4123e-007       0.0042695       0.0016716       0.0016716
v  TempC                       21          73.048          22.021          22.021
v  TurbVisc           3.3349e-014       0.0050321       0.0019643       0.0019643
v  total_pressure     1.0129e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2110:        0.22920E+01

===============================================================


 INSTANT    0.211100000E+04   TIME STEP NUMBER            2111
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13365E-01 0.89444E+00
   Friction velocity        uk    :  0.13365E-01 0.89444E+00
   Dimensionless distance   yplus :  0.10760E+00 0.72008E+01
   Friction thermal sca.    tstar : -0.17783E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80280E-01 0.53726E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10299E-01      33   0.28713E-03   0.48691E+01 0.18612E+03 
c  Velocity[X]                                      0.17270E+01 
c  Velocity[Y]                                      0.31420E+01 
c  Velocity[Z]                                      0.73538E-30 
c  Pressure     0.10952E-06     506   0.94654E-08   0.10706E+00 0.12303E+04 
c  nu_tilda     0.74321E-05      33   0.50122E-05   0.65980E-06 0.21162E+03 
c  TempC        0.41419E+02      27   0.31976E-03   0.47642E+01 0.26487E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2044          9.8166          4.5729          4.5729
v  Velocity[Y]            -3.0469           7.246          0.1659          0.1659
v  Velocity[Z]       -9.1383e-015     6.0622e-015    -1.6022e-017    -1.6022e-017
v  ǁVelocityǁ          0.002399          9.8175          5.1332          5.1332
v  Pressure               -29.861           22.35         -6.2304         -6.2304
v  nu_tilda           4.4119e-007       0.0042695       0.0016721       0.0016721
v  TempC                       21          73.049          22.021          22.021
v  TurbVisc           3.3346e-014       0.0050321       0.0019648       0.0019648
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2111:        0.22480E+01

===============================================================


 INSTANT    0.211200000E+04   TIME STEP NUMBER            2112
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.50029E-02 0.89399E+00
   Friction velocity        uk    :  0.50029E-02 0.89399E+00
   Dimensionless distance   yplus :  0.40277E-01 0.71972E+01
   Friction thermal sca.    tstar : -0.14291E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30051E-01 0.53699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10301E-01      33   0.25674E-03   0.49116E+01 0.18632E+03 
c  Velocity[X]                                      0.17514E+01 
c  Velocity[Y]                                      0.31601E+01 
c  Velocity[Z]                                      0.79933E-30 
c  Pressure     0.12114E-06     506   0.97983E-08   0.12086E+00 0.11230E+04 
c  nu_tilda     0.74343E-05      33   0.14672E-04   0.66025E-06 0.21167E+03 
c  TempC        0.41426E+02      27   0.34245E-03   0.48567E+01 0.25544E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2011          9.8156          4.5729          4.5729
v  Velocity[Y]            -3.0474          7.2171         0.16623         0.16623
v  Velocity[Z]       -8.9897e-015     6.2864e-015    -1.6005e-017    -1.6005e-017
v  ǁVelocityǁ         0.0021359          9.8165          5.1332          5.1332
v  Pressure               -29.864          22.208         -6.2484         -6.2484
v  nu_tilda           4.4119e-007       0.0042695       0.0016724       0.0016724
v  TempC                       21          73.048          22.021          22.021
v  TurbVisc           3.3332e-014       0.0050321       0.0019652       0.0019652
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2112:        0.21570E+01

===============================================================


 INSTANT    0.211300000E+04   TIME STEP NUMBER            2113
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11495E-01 0.89261E+00
   Friction velocity        uk    :  0.11495E-01 0.89261E+00
   Dimensionless distance   yplus :  0.92539E-01 0.71861E+01
   Friction thermal sca.    tstar : -0.15872E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69045E-01 0.53617E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10303E-01      33   0.25418E-03   0.48792E+01 0.18618E+03 
c  Velocity[X]                                      0.17316E+01 
c  Velocity[Y]                                      0.31476E+01 
c  Velocity[Z]                                      0.76013E-30 
c  Pressure     0.10332E-06     536   0.93424E-08   0.10001E+00 0.14554E+04 
c  nu_tilda     0.74366E-05      33   0.50160E-05   0.66064E-06 0.21172E+03 
c  TempC        0.41434E+02      27   0.29473E-03   0.70319E+01 0.28402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1977          9.8146          4.5729          4.5729
v  Velocity[Y]            -3.0478          7.2336         0.16656         0.16656
v  Velocity[Z]       -8.8281e-015     6.2572e-015    -1.5989e-017    -1.5989e-017
v  ǁVelocityǁ         0.0022839          9.8155          5.1331          5.1331
v  Pressure               -29.823          22.383         -6.1764         -6.1764
v  nu_tilda           4.4121e-007       0.0042695       0.0016728       0.0016728
v  TempC                       21          73.049          22.021          22.021
v  TurbVisc           3.3334e-014       0.0050321       0.0019656       0.0019656
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2113:        0.22160E+01

===============================================================


 INSTANT    0.211400000E+04   TIME STEP NUMBER            2114
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12191E-01 0.89368E+00
   Friction velocity        uk    :  0.12191E-01 0.89368E+00
   Dimensionless distance   yplus :  0.98145E-01 0.71947E+01
   Friction thermal sca.    tstar : -0.16320E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73227E-01 0.53681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10304E-01      33   0.26904E-03   0.48956E+01 0.18623E+03 
c  Velocity[X]                                      0.17560E+01 
c  Velocity[Y]                                      0.31397E+01 
c  Velocity[Z]                                      0.79180E-30 
c  Pressure     0.10773E-06     504   0.96883E-08   0.10686E+00 0.11096E+04 
c  nu_tilda     0.74388E-05      33   0.14672E-04   0.66107E-06 0.21177E+03 
c  TempC        0.41441E+02      27   0.30906E-03   0.59498E+01 0.26988E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1944          9.8136          4.5729          4.5729
v  Velocity[Y]            -3.0482          7.2116          0.1669          0.1669
v  Velocity[Z]       -8.6975e-015     6.2344e-015    -1.5976e-017    -1.5976e-017
v  ǁVelocityǁ         0.0021048          9.8144           5.133           5.133
v  Pressure               -29.846          22.248         -6.1924         -6.1924
v  nu_tilda           4.4131e-007       0.0042695       0.0016731       0.0016731
v  TempC                       21          73.048          22.021          22.021
v  TurbVisc           3.3338e-014       0.0050321       0.0019661       0.0019661
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2114:        0.21640E+01

===============================================================


 INSTANT    0.211500000E+04   TIME STEP NUMBER            2115
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17366E-02 0.89291E+00
   Friction velocity        uk    :  0.17366E-02 0.89291E+00
   Dimensionless distance   yplus :  0.13981E-01 0.71886E+01
   Friction thermal sca.    tstar : -0.23182E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10431E-01 0.53635E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10306E-01      33   0.24289E-03   0.48908E+01 0.18632E+03 
c  Velocity[X]                                      0.17238E+01 
c  Velocity[Y]                                      0.31670E+01 
c  Velocity[Z]                                      0.83661E-30 
c  Pressure     0.10600E-06     552   0.93615E-08   0.10370E+00 0.18565E+04 
c  nu_tilda     0.74410E-05      33   0.50237E-05   0.66147E-06 0.21182E+03 
c  TempC        0.41448E+02      27   0.28922E-03   0.47919E+01 0.25602E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1911          9.8126          4.5729          4.5729
v  Velocity[Y]            -3.0484           7.236         0.16723         0.16723
v  Velocity[Z]       -8.1912e-015     6.1823e-015    -1.5963e-017    -1.5963e-017
v  ǁVelocityǁ         0.0023855          9.8134           5.133           5.133
v  Pressure               -29.643          22.493         -6.1036         -6.1036
v  nu_tilda           4.4135e-007       0.0042695       0.0016736       0.0016736
v  TempC                       21          73.048          22.021          22.021
v  TurbVisc            3.337e-014       0.0050321       0.0019665       0.0019665
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2115:        0.22590E+01

===============================================================


 INSTANT    0.211600000E+04   TIME STEP NUMBER            2116
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85301E-02 0.89396E+00
   Friction velocity        uk    :  0.85301E-02 0.89396E+00
   Dimensionless distance   yplus :  0.68673E-01 0.71970E+01
   Friction thermal sca.    tstar : -0.14051E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51238E-01 0.53697E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10308E-01      33   0.26389E-03   0.48543E+01 0.18612E+03 
c  Velocity[X]                                      0.17093E+01 
c  Velocity[Y]                                      0.31450E+01 
c  Velocity[Z]                                      0.73004E-30 
c  Pressure     0.11523E-06     505   0.93305E-08   0.11091E+00 0.95575E+03 
c  nu_tilda     0.74433E-05      33   0.14662E-04   0.66192E-06 0.21187E+03 
c  TempC        0.41455E+02      27   0.28080E-03   0.53843E+01 0.27066E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1878          9.8116          4.5729          4.5729
v  Velocity[Y]            -3.0486          7.2394         0.16756         0.16756
v  Velocity[Z]       -8.1682e-015     6.3634e-015    -1.5945e-017    -1.5945e-017
v  ǁVelocityǁ         0.0023674          9.8124          5.1329          5.1329
v  Pressure               -29.848          22.391         -6.1163         -6.1163
v  nu_tilda           4.4133e-007       0.0042695       0.0016739       0.0016739
v  TempC                       21          73.047          22.022          22.022
v  TurbVisc           3.3382e-014       0.0050321        0.001967        0.001967
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2116:        0.21450E+01

===============================================================


 INSTANT    0.211700000E+04   TIME STEP NUMBER            2117
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13444E-01 0.89383E+00
   Friction velocity        uk    :  0.13444E-01 0.89383E+00
   Dimensionless distance   yplus :  0.10823E+00 0.71960E+01
   Friction thermal sca.    tstar : -0.18591E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80753E-01 0.53690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10310E-01      33   0.28344E-03   0.48926E+01 0.18633E+03 
c  Velocity[X]                                      0.17523E+01 
c  Velocity[Y]                                      0.31403E+01 
c  Velocity[Z]                                      0.79422E-30 
c  Pressure     0.11562E-06     521   0.95630E-08   0.11524E+00 0.80028E+03 
c  nu_tilda     0.74455E-05      33   0.50352E-05   0.66230E-06 0.21192E+03 
c  TempC        0.41462E+02      27   0.38641E-03   0.54893E+01 0.26803E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1844          9.8106          4.5729          4.5729
v  Velocity[Y]            -3.0488          7.2153         0.16789         0.16789
v  Velocity[Z]       -8.1986e-015     6.1268e-015    -1.5931e-017    -1.5931e-017
v  ǁVelocityǁ          0.002245          9.8114          5.1329          5.1329
v  Pressure               -29.672          22.419         -6.0751         -6.0751
v  nu_tilda           4.4133e-007       0.0042695       0.0016743       0.0016743
v  TempC                       21          73.048          22.022          22.022
v  TurbVisc           3.3376e-014       0.0050321       0.0019674       0.0019674
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2117:        0.21770E+01

===============================================================


 INSTANT    0.211800000E+04   TIME STEP NUMBER            2118
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99815E-02 0.89244E+00
   Friction velocity        uk    :  0.99815E-02 0.89244E+00
   Dimensionless distance   yplus :  0.80358E-01 0.71847E+01
   Friction thermal sca.    tstar : -0.17387E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59956E-01 0.53606E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10312E-01      33   0.26308E-03   0.48959E+01 0.18639E+03 
c  Velocity[X]                                      0.17395E+01 
c  Velocity[Y]                                      0.31564E+01 
c  Velocity[Z]                                      0.70787E-30 
c  Pressure     0.10338E-06     473   0.98775E-08   0.10153E+00 0.67079E+03 
c  nu_tilda     0.74477E-05      33   0.14659E-04   0.66273E-06 0.21196E+03 
c  TempC        0.41469E+02      27   0.31842E-03   0.81179E+01 0.31736E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1809          9.8096          4.5729          4.5729
v  Velocity[Y]            -3.0493          7.2336         0.16822         0.16822
v  Velocity[Z]       -8.2935e-015     6.2579e-015    -1.5915e-017    -1.5915e-017
v  ǁVelocityǁ         0.0024302          9.8104          5.1328          5.1328
v  Pressure               -29.681          22.487         -6.0482         -6.0482
v  nu_tilda           4.4132e-007       0.0042695       0.0016746       0.0016746
v  TempC                       21          73.048          22.022          22.022
v  TurbVisc           3.3375e-014       0.0050321       0.0019678       0.0019678
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2118:        0.20710E+01

===============================================================


 INSTANT    0.211900000E+04   TIME STEP NUMBER            2119
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14087E-01 0.89354E+00
   Friction velocity        uk    :  0.14087E-01 0.89354E+00
   Dimensionless distance   yplus :  0.11341E+00 0.71936E+01
   Friction thermal sca.    tstar : -0.15397E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84615E-01 0.53672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10313E-01      33   0.26194E-03   0.48826E+01 0.18629E+03 
c  Velocity[X]                                      0.17382E+01 
c  Velocity[Y]                                      0.31444E+01 
c  Velocity[Z]                                      0.78012E-30 
c  Pressure     0.12512E-06     488   0.96607E-08   0.12192E+00 0.68039E+03 
c  nu_tilda     0.74499E-05      33   0.50378E-05   0.66309E-06 0.21201E+03 
c  TempC        0.41476E+02      27   0.32661E-03   0.49324E+01 0.25588E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1777          9.8086          4.5729          4.5729
v  Velocity[Y]            -3.0497          7.2089         0.16855         0.16855
v  Velocity[Z]       -8.2614e-015     6.2216e-015    -1.5901e-017    -1.5901e-017
v  ǁVelocityǁ          0.002162          9.8094          5.1327          5.1327
v  Pressure               -29.611           22.46         -6.0172         -6.0172
v  nu_tilda           4.4132e-007       0.0042695        0.001675        0.001675
v  TempC                       21          73.049          22.022          22.022
v  TurbVisc           3.3372e-014       0.0050321       0.0019683       0.0019683
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2119:        0.21160E+01

===============================================================


 INSTANT    0.212000000E+04   TIME STEP NUMBER            2120
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11035E-01 0.89286E+00
   Friction velocity        uk    :  0.11035E-01 0.89286E+00
   Dimensionless distance   yplus :  0.88842E-01 0.71881E+01
   Friction thermal sca.    tstar : -0.17757E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66286E-01 0.53631E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10315E-01      33   0.21085E-03   0.48839E+01 0.18630E+03 
c  Velocity[X]                                      0.17485E+01 
c  Velocity[Y]                                      0.31353E+01 
c  Velocity[Z]                                      0.84277E-30 
c  Pressure     0.98552E-07     440   0.98202E-08   0.96440E-01 0.68448E+03 
c  nu_tilda     0.74522E-05      33   0.14656E-04   0.66352E-06 0.21206E+03 
c  TempC        0.41484E+02      27   0.29158E-03   0.52302E+01 0.27282E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1743          9.8076          4.5729          4.5729
v  Velocity[Y]              -3.05          7.2349         0.16888         0.16888
v  Velocity[Z]       -8.1983e-015     6.1174e-015    -1.5884e-017    -1.5884e-017
v  ǁVelocityǁ         0.0023508          9.8084          5.1327          5.1327
v  Pressure               -29.654           22.54         -5.9906         -5.9906
v  nu_tilda           4.4128e-007       0.0042695       0.0016754       0.0016754
v  TempC                       21          73.048          22.022          22.022
v  TurbVisc           3.3372e-014       0.0050321       0.0019687       0.0019687
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2120:        0.20010E+01

===============================================================


 INSTANT    0.212100000E+04   TIME STEP NUMBER            2121
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13512E-01 0.89444E+00
   Friction velocity        uk    :  0.13512E-01 0.89444E+00
   Dimensionless distance   yplus :  0.10878E+00 0.72008E+01
   Friction thermal sca.    tstar : -0.14858E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81161E-01 0.53726E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10317E-01      33   0.24744E-03   0.48593E+01 0.18629E+03 
c  Velocity[X]                                      0.17018E+01 
c  Velocity[Y]                                      0.31575E+01 
c  Velocity[Z]                                      0.80848E-30 
c  Pressure     0.10134E-06     552   0.95354E-08   0.10014E+00 0.11599E+04 
c  nu_tilda     0.74544E-05      33   0.50536E-05   0.66388E-06 0.21210E+03 
c  TempC        0.41491E+02      27   0.32994E-03   0.45824E+01 0.24712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1709          9.8065          4.5729          4.5729
v  Velocity[Y]            -3.0503          7.2458         0.16921         0.16921
v  Velocity[Z]       -8.2569e-015     6.3374e-015    -1.5864e-017    -1.5864e-017
v  ǁVelocityǁ         0.0025053          9.8074          5.1326          5.1326
v  Pressure               -29.501          22.654         -5.9308         -5.9308
v  nu_tilda           4.4119e-007       0.0042695       0.0016758       0.0016758
v  TempC                       21          73.049          22.022          22.022
v  TurbVisc           3.3361e-014       0.0050321       0.0019692       0.0019692
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2121:        0.22230E+01

===============================================================


 INSTANT    0.212200000E+04   TIME STEP NUMBER            2122
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14236E-01 0.89384E+00
   Friction velocity        uk    :  0.14236E-01 0.89384E+00
   Dimensionless distance   yplus :  0.11461E+00 0.71960E+01
   Friction thermal sca.    tstar : -0.12511E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85512E-01 0.53690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10319E-01      33   0.25823E-03   0.48753E+01 0.18631E+03 
c  Velocity[X]                                      0.17343E+01 
c  Velocity[Y]                                      0.31410E+01 
c  Velocity[Z]                                      0.73385E-30 
c  Pressure     0.11102E-06     505   0.95891E-08   0.10901E+00 0.13951E+04 
c  nu_tilda     0.74566E-05      33   0.14645E-04   0.66432E-06 0.21215E+03 
c  TempC        0.41498E+02      27   0.39194E-03   0.60861E+01 0.26247E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1675          9.8055          4.5729          4.5729
v  Velocity[Y]            -3.0504          7.2124         0.16954         0.16954
v  Velocity[Z]       -8.3757e-015     6.3246e-015    -1.5845e-017    -1.5845e-017
v  ǁVelocityǁ         0.0021669          9.8064          5.1326          5.1326
v  Pressure               -29.647          22.463          -5.959          -5.959
v  nu_tilda           4.4122e-007       0.0042695       0.0016761       0.0016761
v  TempC                       21          73.048          22.022          22.022
v  TurbVisc           3.3334e-014       0.0050321       0.0019696       0.0019696
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2122:        0.21510E+01

===============================================================


 INSTANT    0.212300000E+04   TIME STEP NUMBER            2123
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12292E-01 0.89261E+00
   Friction velocity        uk    :  0.12292E-01 0.89261E+00
   Dimensionless distance   yplus :  0.98958E-01 0.71861E+01
   Friction thermal sca.    tstar : -0.15791E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73834E-01 0.53616E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10321E-01      33   0.28676E-03   0.48774E+01 0.18641E+03 
c  Velocity[X]                                      0.17358E+01 
c  Velocity[Y]                                      0.31416E+01 
c  Velocity[Z]                                      0.88378E-30 
c  Pressure     0.11208E-06     537   0.99642E-08   0.10921E+00 0.17499E+04 
c  nu_tilda     0.74589E-05      33   0.50522E-05   0.66471E-06 0.21220E+03 
c  TempC        0.41505E+02      27   0.27567E-03   0.82945E+01 0.31967E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1642          9.8045          4.5729          4.5729
v  Velocity[Y]            -3.0506          7.2357         0.16986         0.16986
v  Velocity[Z]       -8.4037e-015     6.1528e-015    -1.5832e-017    -1.5832e-017
v  ǁVelocityǁ         0.0023889          9.8054          5.1325          5.1325
v  Pressure               -29.467          22.692         -5.8761         -5.8761
v  nu_tilda           4.4124e-007       0.0042695       0.0016765       0.0016765
v  TempC                       21          73.049          22.023          22.023
v  TurbVisc           3.3343e-014       0.0050321         0.00197         0.00197
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2123:        0.22100E+01

===============================================================


 INSTANT    0.212400000E+04   TIME STEP NUMBER            2124
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.98014E-02 0.89358E+00
   Friction velocity        uk    :  0.98014E-02 0.89358E+00
   Dimensionless distance   yplus :  0.78908E-01 0.71939E+01
   Friction thermal sca.    tstar : -0.15649E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58874E-01 0.53675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10322E-01      33   0.26761E-03   0.48979E+01 0.18651E+03 
c  Velocity[X]                                      0.17437E+01 
c  Velocity[Y]                                      0.31542E+01 
c  Velocity[Z]                                      0.81135E-30 
c  Pressure     0.11613E-06     506   0.92977E-08   0.11479E+00 0.11222E+04 
c  nu_tilda     0.74611E-05      33   0.14646E-04   0.66512E-06 0.21224E+03 
c  TempC        0.41512E+02      27   0.37574E-03   0.40751E+01 0.23727E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1608          9.8035          4.5729          4.5729
v  Velocity[Y]             -3.051          7.2112         0.17019         0.17019
v  Velocity[Z]        -8.646e-015     6.2981e-015    -1.5819e-017    -1.5819e-017
v  ǁVelocityǁ         0.0021803          9.8044          5.1324          5.1324
v  Pressure               -29.481          22.553         -5.8943         -5.8943
v  nu_tilda           4.4124e-007       0.0042695       0.0016768       0.0016768
v  TempC                       21          73.048          22.023          22.023
v  TurbVisc           3.3348e-014       0.0050321       0.0019705       0.0019705
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2124:        0.21560E+01

===============================================================


 INSTANT    0.212500000E+04   TIME STEP NUMBER            2125
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11772E-01 0.89272E+00
   Friction velocity        uk    :  0.11772E-01 0.89272E+00
   Dimensionless distance   yplus :  0.94772E-01 0.71870E+01
   Friction thermal sca.    tstar : -0.19969E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70711E-01 0.53623E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10324E-01      33   0.20171E-03   0.48775E+01 0.18638E+03 
c  Velocity[X]                                      0.17326E+01 
c  Velocity[Y]                                      0.31449E+01 
c  Velocity[Z]                                      0.79679E-30 
c  Pressure     0.11681E-06     552   0.92338E-08   0.11323E+00 0.16219E+04 
c  nu_tilda     0.74633E-05      33   0.50630E-05   0.66547E-06 0.21229E+03 
c  TempC        0.41519E+02      27   0.33381E-03   0.57758E+01 0.28325E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1574          9.8025          4.5729          4.5729
v  Velocity[Y]            -3.0514          7.2324         0.17052         0.17052
v  Velocity[Z]       -8.6855e-015     6.2349e-015    -1.5801e-017    -1.5801e-017
v  ǁVelocityǁ         0.0023943          9.8034          5.1324          5.1324
v  Pressure               -29.433          22.752         -5.8154         -5.8154
v  nu_tilda           4.4123e-007       0.0042695       0.0016772       0.0016772
v  TempC                       21          73.049          22.023          22.023
v  TurbVisc           3.3348e-014       0.0050321       0.0019709       0.0019709
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2125:        0.22520E+01

===============================================================


 INSTANT    0.212600000E+04   TIME STEP NUMBER            2126
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13146E-01 0.89408E+00
   Friction velocity        uk    :  0.13146E-01 0.89408E+00
   Dimensionless distance   yplus :  0.10583E+00 0.71980E+01
   Friction thermal sca.    tstar : -0.12614E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78964E-01 0.53705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10326E-01      33   0.26103E-03   0.48623E+01 0.18632E+03 
c  Velocity[X]                                      0.17278E+01 
c  Velocity[Y]                                      0.31344E+01 
c  Velocity[Z]                                      0.78943E-30 
c  Pressure     0.92542E-07     424   0.96206E-08   0.90809E-01 0.73476E+03 
c  nu_tilda     0.74655E-05      33   0.14635E-04   0.66589E-06 0.21233E+03 
c  TempC        0.41526E+02      27   0.29451E-03   0.55996E+01 0.27902E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1539          9.8015          4.5729          4.5729
v  Velocity[Y]            -3.0518          7.2411         0.17084         0.17084
v  Velocity[Z]       -8.8085e-015     6.2077e-015    -1.5783e-017    -1.5783e-017
v  ǁVelocityǁ         0.0024916          9.8024          5.1323          5.1323
v  Pressure               -29.504          22.711         -5.8152         -5.8152
v  nu_tilda           4.4123e-007       0.0042695       0.0016776       0.0016776
v  TempC                       21          73.049          22.023          22.023
v  TurbVisc           3.3344e-014       0.0050321       0.0019713       0.0019713
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2126:        0.20000E+01

===============================================================


 INSTANT    0.212700000E+04   TIME STEP NUMBER            2127
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14300E-01 0.89370E+00
   Friction velocity        uk    :  0.14300E-01 0.89370E+00
   Dimensionless distance   yplus :  0.11513E+00 0.71949E+01
   Friction thermal sca.    tstar : -0.12942E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85898E-01 0.53682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10328E-01      33   0.24513E-03   0.48784E+01 0.18648E+03 
c  Velocity[X]                                      0.17260E+01 
c  Velocity[Y]                                      0.31524E+01 
c  Velocity[Z]                                      0.93396E-30 
c  Pressure     0.11633E-06     522   0.95070E-08   0.11522E+00 0.82278E+03 
c  nu_tilda     0.74677E-05      33   0.50674E-05   0.66626E-06 0.21238E+03 
c  TempC        0.41533E+02      27   0.31668E-03   0.45335E+01 0.25199E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1505          9.8005          4.5729          4.5729
v  Velocity[Y]             -3.052          7.2137         0.17117         0.17117
v  Velocity[Z]       -9.1546e-015     6.0661e-015    -1.5772e-017    -1.5772e-017
v  ǁVelocityǁ         0.0023098          9.8014          5.1322          5.1322
v  Pressure               -29.279          22.733         -5.7722         -5.7722
v  nu_tilda           4.4122e-007       0.0042695        0.001678        0.001678
v  TempC                       21          73.049          22.023          22.023
v  TurbVisc           3.3344e-014       0.0050321       0.0019718       0.0019718
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2127:        0.21770E+01

===============================================================


 INSTANT    0.212800000E+04   TIME STEP NUMBER            2128
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12161E-01 0.89213E+00
   Friction velocity        uk    :  0.12161E-01 0.89213E+00
   Dimensionless distance   yplus :  0.97903E-01 0.71822E+01
   Friction thermal sca.    tstar : -0.12522E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73046E-01 0.53588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10329E-01      33   0.26455E-03   0.48581E+01 0.18635E+03 
c  Velocity[X]                                      0.17216E+01 
c  Velocity[Y]                                      0.31365E+01 
c  Velocity[Z]                                      0.92989E-30 
c  Pressure     0.10984E-06     424   0.93086E-08   0.10661E+00 0.64628E+03 
c  nu_tilda     0.74700E-05      33   0.14636E-04   0.66667E-06 0.21242E+03 
c  TempC        0.41540E+02      27   0.27955E-03   0.65907E+01 0.26750E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1471          9.7994          4.5729          4.5729
v  Velocity[Y]            -3.0521          7.2285         0.17149         0.17149
v  Velocity[Z]       -9.0016e-015     6.3644e-015    -1.5752e-017    -1.5752e-017
v  ǁVelocityǁ         0.0023924          9.8003          5.1322          5.1322
v  Pressure               -29.441          22.743         -5.7589         -5.7589
v  nu_tilda            4.412e-007       0.0042695       0.0016783       0.0016783
v  TempC                       21          73.048          22.023          22.023
v  TurbVisc           3.3341e-014       0.0050321       0.0019722       0.0019722
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2128:        0.19630E+01

===============================================================


 INSTANT    0.212900000E+04   TIME STEP NUMBER            2129
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.95970E-02 0.89348E+00
   Friction velocity        uk    :  0.95970E-02 0.89348E+00
   Dimensionless distance   yplus :  0.77262E-01 0.71931E+01
   Friction thermal sca.    tstar : -0.12373E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57646E-01 0.53669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10331E-01      33   0.28783E-03   0.48774E+01 0.18649E+03 
c  Velocity[X]                                      0.17441E+01 
c  Velocity[Y]                                      0.31333E+01 
c  Velocity[Z]                                      0.87343E-30 
c  Pressure     0.11927E-06     521   0.98513E-08   0.11876E+00 0.81664E+03 
c  nu_tilda     0.74722E-05      33   0.50729E-05   0.66700E-06 0.21246E+03 
c  TempC        0.41547E+02      27   0.35496E-03   0.47111E+01 0.24561E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1437          9.7984          4.5729          4.5729
v  Velocity[Y]            -3.0522          7.2104         0.17181         0.17181
v  Velocity[Z]       -8.7921e-015      6.175e-015    -1.5738e-017    -1.5738e-017
v  ǁVelocityǁ         0.0022665          9.7993          5.1321          5.1321
v  Pressure               -29.268           22.77         -5.7163         -5.7163
v  nu_tilda           4.4119e-007       0.0042695       0.0016787       0.0016787
v  TempC                       21          73.049          22.024          22.024
v  TurbVisc           3.3335e-014       0.0050321       0.0019726       0.0019726
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2129:        0.22180E+01

===============================================================


 INSTANT    0.213000000E+04   TIME STEP NUMBER            2130
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11937E-01 0.89270E+00
   Friction velocity        uk    :  0.11937E-01 0.89270E+00
   Dimensionless distance   yplus :  0.96102E-01 0.71869E+01
   Friction thermal sca.    tstar : -0.12759E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71703E-01 0.53622E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10333E-01      33   0.21170E-03   0.48829E+01 0.18654E+03 
c  Velocity[X]                                      0.17354E+01 
c  Velocity[Y]                                      0.31476E+01 
c  Velocity[Z]                                      0.73172E-30 
c  Pressure     0.10376E-06     472   0.96501E-08   0.10140E+00 0.66226E+03 
c  nu_tilda     0.74744E-05      33   0.14627E-04   0.66740E-06 0.21250E+03 
c  TempC        0.41554E+02      27   0.30812E-03   0.62994E+01 0.29624E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1402          9.7974          4.5729          4.5729
v  Velocity[Y]            -3.0527          7.2335         0.17213         0.17213
v  Velocity[Z]       -8.8311e-015      6.315e-015    -1.5722e-017    -1.5722e-017
v  ǁVelocityǁ         0.0024671          9.7983           5.132           5.132
v  Pressure                 -29.3          22.834         -5.6931         -5.6931
v  nu_tilda           4.4115e-007       0.0042695        0.001679        0.001679
v  TempC                       21          73.048          22.024          22.024
v  TurbVisc           3.3334e-014       0.0050321       0.0019731       0.0019731
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2130:        0.20720E+01

===============================================================


 INSTANT    0.213100000E+04   TIME STEP NUMBER            2131
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14287E-01 0.89417E+00
   Friction velocity        uk    :  0.14287E-01 0.89417E+00
   Dimensionless distance   yplus :  0.11502E+00 0.71987E+01
   Friction thermal sca.    tstar : -0.13604E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85817E-01 0.53710E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10335E-01      33   0.25847E-03   0.48549E+01 0.18642E+03 
c  Velocity[X]                                      0.17099E+01 
c  Velocity[Y]                                      0.31449E+01 
c  Velocity[Z]                                      0.74478E-30 
c  Pressure     0.12164E-06     506   0.99143E-08   0.11801E+00 0.10751E+04 
c  nu_tilda     0.74766E-05      33   0.50865E-05   0.66778E-06 0.21255E+03 
c  TempC        0.41561E+02      27   0.33704E-03   0.52699E+01 0.25763E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1368          9.7964          4.5729          4.5729
v  Velocity[Y]            -3.0531          7.2406         0.17246         0.17246
v  Velocity[Z]       -8.7012e-015     6.2474e-015    -1.5715e-017    -1.5715e-017
v  ǁVelocityǁ         0.0024398          9.7973           5.132           5.132
v  Pressure               -29.255          22.922         -5.6376         -5.6376
v  nu_tilda           4.4113e-007       0.0042695       0.0016794       0.0016794
v  TempC                       21          73.049          22.024          22.024
v  TurbVisc           3.3321e-014       0.0050321       0.0019735       0.0019735
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2131:        0.21530E+01

===============================================================


 INSTANT    0.213200000E+04   TIME STEP NUMBER            2132
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13611E-01 0.89388E+00
   Friction velocity        uk    :  0.13611E-01 0.89388E+00
   Dimensionless distance   yplus :  0.10958E+00 0.71963E+01
   Friction thermal sca.    tstar : -0.11569E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81760E-01 0.53693E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10336E-01      33   0.25765E-03   0.48893E+01 0.18655E+03 
c  Velocity[X]                                      0.17575E+01 
c  Velocity[Y]                                      0.31319E+01 
c  Velocity[Z]                                      0.85668E-30 
c  Pressure     0.11447E-06     490   0.92879E-08   0.11355E+00 0.11306E+04 
c  nu_tilda     0.74788E-05      33   0.14621E-04   0.66820E-06 0.21260E+03 
c  TempC        0.41568E+02      27   0.37972E-03   0.52350E+01 0.26904E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1334          9.7953          4.5729          4.5729
v  Velocity[Y]            -3.0534          7.2129         0.17278         0.17278
v  Velocity[Z]       -8.5488e-015     6.2714e-015    -1.5709e-017    -1.5709e-017
v  ǁVelocityǁ         0.0021752          9.7963          5.1319          5.1319
v  Pressure               -29.286          22.786         -5.6547         -5.6547
v  nu_tilda           4.4122e-007       0.0042695       0.0016797       0.0016797
v  TempC                       21          73.048          22.024          22.024
v  TurbVisc           3.3313e-014       0.0050321       0.0019739       0.0019739
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2132:        0.21100E+01

===============================================================


 INSTANT    0.213300000E+04   TIME STEP NUMBER            2133
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11913E-01 0.89252E+00
   Friction velocity        uk    :  0.11913E-01 0.89252E+00
   Dimensionless distance   yplus :  0.95906E-01 0.71854E+01
   Friction thermal sca.    tstar : -0.13800E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71556E-01 0.53611E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10338E-01      33   0.25189E-03   0.48605E+01 0.18652E+03 
c  Velocity[X]                                      0.17122E+01 
c  Velocity[Y]                                      0.31483E+01 
c  Velocity[Z]                                      0.89761E-30 
c  Pressure     0.89660E-07     568   0.95113E-08   0.88020E-01 0.16290E+04 
c  nu_tilda     0.74810E-05      33   0.50862E-05   0.66854E-06 0.21264E+03 
c  TempC        0.41575E+02      27   0.23925E-03   0.66542E+01 0.28398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.13          9.7943          4.5729          4.5729
v  Velocity[Y]            -3.0536          7.2339          0.1731          0.1731
v  Velocity[Z]       -8.3196e-015     6.1841e-015    -1.5704e-017    -1.5704e-017
v  ǁVelocityǁ         0.0024033          9.7953          5.1318          5.1318
v  Pressure               -29.102          22.994         -5.5781         -5.5781
v  nu_tilda           4.4126e-007       0.0042695       0.0016802       0.0016802
v  TempC                       21          73.049          22.024          22.024
v  TurbVisc           3.3341e-014       0.0050321       0.0019743       0.0019743
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2133:        0.23020E+01

===============================================================


 INSTANT    0.213400000E+04   TIME STEP NUMBER            2134
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59015E-02 0.89337E+00
   Friction velocity        uk    :  0.59015E-02 0.89337E+00
   Dimensionless distance   yplus :  0.47511E-01 0.71922E+01
   Friction thermal sca.    tstar : -0.12580E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35448E-01 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10340E-01      33   0.26945E-03   0.48584E+01 0.18646E+03 
c  Velocity[X]                                      0.17250E+01 
c  Velocity[Y]                                      0.31334E+01 
c  Velocity[Z]                                      0.80257E-30 
c  Pressure     0.11320E-06     506   0.92364E-08   0.11140E+00 0.12926E+04 
c  nu_tilda     0.74833E-05      33   0.14619E-04   0.66892E-06 0.21268E+03 
c  TempC        0.41582E+02      27   0.31558E-03   0.46228E+01 0.23749E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1265          9.7933          4.5729          4.5729
v  Velocity[Y]            -3.0537          7.2067         0.17342         0.17342
v  Velocity[Z]       -8.1823e-015     6.3252e-015    -1.5698e-017    -1.5698e-017
v  ǁVelocityǁ         0.0021529          9.7942          5.1318          5.1318
v  Pressure               -29.251          22.822         -5.6015         -5.6015
v  nu_tilda            4.413e-007       0.0042695       0.0016805       0.0016805
v  TempC                       21          73.048          22.024          22.024
v  TurbVisc           3.3354e-014       0.0050321       0.0019748       0.0019748
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2134:        0.21430E+01

===============================================================


 INSTANT    0.213500000E+04   TIME STEP NUMBER            2135
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11700E-01 0.89277E+00
   Friction velocity        uk    :  0.11700E-01 0.89277E+00
   Dimensionless distance   yplus :  0.94191E-01 0.71874E+01
   Friction thermal sca.    tstar : -0.13826E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70277E-01 0.53626E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10342E-01      33   0.28346E-03   0.48674E+01 0.18655E+03 
c  Velocity[X]                                      0.17380E+01 
c  Velocity[Y]                                      0.31294E+01 
c  Velocity[Z]                                      0.82215E-30 
c  Pressure     0.10577E-06     584   0.95073E-08   0.10308E+00 0.17931E+04 
c  nu_tilda     0.74855E-05      33   0.51010E-05   0.66925E-06 0.21272E+03 
c  TempC        0.41589E+02      27   0.30030E-03   0.43555E+01 0.24123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1229          9.7923          4.5729          4.5729
v  Velocity[Y]            -3.0538          7.2341         0.17374         0.17374
v  Velocity[Z]       -7.9791e-015     6.2621e-015    -1.5694e-017    -1.5694e-017
v  ǁVelocityǁ         0.0024074          9.7932          5.1317          5.1317
v  Pressure               -29.076          23.054         -5.5164         -5.5164
v  nu_tilda           4.4126e-007       0.0042695       0.0016809       0.0016809
v  TempC                       21          73.049          22.025          22.025
v  TurbVisc           3.3366e-014       0.0050321       0.0019752       0.0019752
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2135:        0.23180E+01

===============================================================


 INSTANT    0.213600000E+04   TIME STEP NUMBER            2136
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13233E-01 0.89397E+00
   Friction velocity        uk    :  0.13233E-01 0.89397E+00
   Dimensionless distance   yplus :  0.10654E+00 0.71970E+01
   Friction thermal sca.    tstar : -0.22302E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79487E-01 0.53698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10343E-01      33   0.25748E-03   0.48625E+01 0.18658E+03 
c  Velocity[X]                                      0.17191E+01 
c  Velocity[Y]                                      0.31434E+01 
c  Velocity[Z]                                      0.83849E-30 
c  Pressure     0.11196E-06     280   0.94168E-08   0.10922E+00 0.69981E+03 
c  nu_tilda     0.74877E-05      33   0.14608E-04   0.66965E-06 0.21276E+03 
c  TempC        0.41596E+02      27   0.30249E-03   0.53440E+01 0.26395E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1196          9.7912          4.5729          4.5729
v  Velocity[Y]            -3.0542          7.2391         0.17406         0.17406
v  Velocity[Z]       -7.8001e-015      6.163e-015    -1.5691e-017    -1.5691e-017
v  ǁVelocityǁ         0.0025405          9.7922          5.1316          5.1316
v  Pressure               -29.128          23.026         -5.5093         -5.5093
v  nu_tilda           4.4114e-007       0.0042695       0.0016812       0.0016812
v  TempC                       21          73.049          22.025          22.025
v  TurbVisc           3.3355e-014       0.0050321       0.0019756       0.0019756
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2136:        0.16960E+01

===============================================================


 INSTANT    0.213700000E+04   TIME STEP NUMBER            2137
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45004E-02 0.89347E+00
   Friction velocity        uk    :  0.45004E-02 0.89347E+00
   Dimensionless distance   yplus :  0.36231E-01 0.71930E+01
   Friction thermal sca.    tstar : -0.27461E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27032E-01 0.53668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10345E-01      33   0.24697E-03   0.48721E+01 0.18658E+03 
c  Velocity[X]                                      0.17355E+01 
c  Velocity[Y]                                      0.31366E+01 
c  Velocity[Z]                                      0.69619E-30 
c  Pressure     0.11818E-06     488   0.97441E-08   0.11691E+00 0.63621E+03 
c  nu_tilda     0.74899E-05      33   0.50999E-05   0.67000E-06 0.21280E+03 
c  TempC        0.41603E+02      27   0.36610E-03   0.51664E+01 0.26786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1161          9.7902          4.5729          4.5729
v  Velocity[Y]            -3.0546          7.2091         0.17437         0.17437
v  Velocity[Z]       -7.5836e-015     6.2275e-015    -1.5685e-017    -1.5685e-017
v  ǁVelocityǁ         0.0022694          9.7912          5.1316          5.1316
v  Pressure               -29.068          22.977         -5.4855         -5.4855
v  nu_tilda           4.4113e-007       0.0042695       0.0016816       0.0016816
v  TempC                       21          73.049          22.025          22.025
v  TurbVisc           3.3318e-014       0.0050321       0.0019761       0.0019761
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2137:        0.23130E+01

===============================================================


 INSTANT    0.213800000E+04   TIME STEP NUMBER            2138
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44831E-02 0.89224E+00
   Friction velocity        uk    :  0.44831E-02 0.89224E+00
   Dimensionless distance   yplus :  0.36092E-01 0.71831E+01
   Friction thermal sca.    tstar : -0.14455E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26929E-01 0.53594E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10347E-01      33   0.25736E-03   0.48644E+01 0.18654E+03 
c  Velocity[X]                                      0.17375E+01 
c  Velocity[Y]                                      0.31269E+01 
c  Velocity[Z]                                      0.75151E-30 
c  Pressure     0.91209E-07     505   0.93717E-08   0.89453E-01 0.72376E+03 
c  nu_tilda     0.74921E-05      33   0.14612E-04   0.67039E-06 0.21284E+03 
c  TempC        0.41610E+02      27   0.28525E-03   0.74435E+01 0.30377E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1126          9.7892          4.5729          4.5729
v  Velocity[Y]            -3.0549          7.2299         0.17469         0.17469
v  Velocity[Z]       -7.4132e-015     6.3644e-015     -1.568e-017     -1.568e-017
v  ǁVelocityǁ         0.0024688          9.7902          5.1315          5.1315
v  Pressure               -29.086          23.059         -5.4561         -5.4561
v  nu_tilda           4.4115e-007       0.0042695       0.0016819       0.0016819
v  TempC                       21          73.048          22.025          22.025
v  TurbVisc           3.3314e-014       0.0050321       0.0019765       0.0019765
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2138:        0.23310E+01

===============================================================


 INSTANT    0.213900000E+04   TIME STEP NUMBER            2139
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82543E-02 0.89340E+00
   Friction velocity        uk    :  0.82543E-02 0.89340E+00
   Dimensionless distance   yplus :  0.66453E-01 0.71925E+01
   Friction thermal sca.    tstar : -0.11795E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49581E-01 0.53664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10349E-01      33   0.25320E-03   0.48683E+01 0.18668E+03 
c  Velocity[X]                                      0.17172E+01 
c  Velocity[Y]                                      0.31511E+01 
c  Velocity[Z]                                      0.11441E-29 
c  Pressure     0.11945E-06     520   0.96262E-08   0.11794E+00 0.77999E+03 
c  nu_tilda     0.74943E-05      33   0.51099E-05   0.67073E-06 0.21288E+03 
c  TempC        0.41617E+02      27   0.33788E-03   0.56517E+01 0.27652E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.109          9.7882          4.5729          4.5729
v  Velocity[Y]            -3.0551          7.2091         0.17501         0.17501
v  Velocity[Z]       -7.2324e-015     6.2011e-015    -1.5684e-017    -1.5684e-017
v  ǁVelocityǁ         0.0022803          9.7891          5.1314          5.1314
v  Pressure               -28.892          23.074         -5.4162         -5.4162
v  nu_tilda            4.412e-007       0.0042695       0.0016823       0.0016823
v  TempC                       21          73.049          22.025          22.025
v  TurbVisc           3.3322e-014       0.0050321       0.0019769       0.0019769
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2139:        0.24850E+01

===============================================================


 INSTANT    0.214000000E+04   TIME STEP NUMBER            2140
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12322E-01 0.89245E+00
   Friction velocity        uk    :  0.12322E-01 0.89245E+00
   Dimensionless distance   yplus :  0.99204E-01 0.71848E+01
   Friction thermal sca.    tstar : -0.11891E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74017E-01 0.53607E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10350E-01      33   0.21592E-03   0.48517E+01 0.18655E+03 
c  Velocity[X]                                      0.17214E+01 
c  Velocity[Y]                                      0.31303E+01 
c  Velocity[Z]                                      0.86007E-30 
c  Pressure     0.11454E-06     410   0.94865E-08   0.11070E+00 0.63587E+03 
c  nu_tilda     0.74965E-05      33   0.14599E-04   0.67111E-06 0.21292E+03 
c  TempC        0.41624E+02      27   0.26771E-03   0.57049E+01 0.27548E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1056          9.7871          4.5729          4.5729
v  Velocity[Y]            -3.0552          7.2287         0.17532         0.17532
v  Velocity[Z]       -7.0589e-015     6.3101e-015    -1.5688e-017    -1.5688e-017
v  ǁVelocityǁ         0.0023256          9.7881          5.1313          5.1313
v  Pressure               -29.055          23.087         -5.4034         -5.4034
v  nu_tilda           4.4127e-007       0.0042695       0.0016826       0.0016826
v  TempC                       21          73.048          22.025          22.025
v  TurbVisc           3.3336e-014       0.0050321       0.0019773       0.0019773
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2140:        0.21180E+01

===============================================================


 INSTANT    0.214100000E+04   TIME STEP NUMBER            2141
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.59372E-02 0.89415E+00
   Friction velocity        uk    :  0.59372E-02 0.89415E+00
   Dimensionless distance   yplus :  0.47799E-01 0.71985E+01
   Friction thermal sca.    tstar : -0.12670E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35663E-01 0.53709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10352E-01      33   0.27955E-03   0.48438E+01 0.18656E+03 
c  Velocity[X]                                      0.17149E+01 
c  Velocity[Y]                                      0.31289E+01 
c  Velocity[Z]                                      0.95868E-30 
c  Pressure     0.10420E-06     538   0.95204E-08   0.10306E+00 0.13060E+04 
c  nu_tilda     0.74987E-05      33   0.51128E-05   0.67144E-06 0.21296E+03 
c  TempC        0.41631E+02      27   0.22525E-03   0.42027E+01 0.24317E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1021          9.7861          4.5729          4.5729
v  Velocity[Y]            -3.0553          7.2416         0.17564         0.17564
v  Velocity[Z]       -6.9287e-015     6.2343e-015    -1.5692e-017    -1.5692e-017
v  ǁVelocityǁ         0.0024531          9.7871          5.1313          5.1313
v  Pressure               -28.921          23.223         -5.3387         -5.3387
v  nu_tilda           4.4127e-007       0.0042695       0.0016831       0.0016831
v  TempC                       21          73.049          22.025          22.025
v  TurbVisc           3.3356e-014       0.0050321       0.0019778       0.0019778
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2141:        0.22190E+01

===============================================================


 INSTANT    0.214200000E+04   TIME STEP NUMBER            2142
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13606E-01 0.89374E+00
   Friction velocity        uk    :  0.13606E-01 0.89374E+00
   Dimensionless distance   yplus :  0.10954E+00 0.71952E+01
   Friction thermal sca.    tstar : -0.98040E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81726E-01 0.53684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10354E-01      33   0.25211E-03   0.48820E+01 0.18675E+03 
c  Velocity[X]                                      0.17396E+01 
c  Velocity[Y]                                      0.31423E+01 
c  Velocity[Z]                                      0.85688E-30 
c  Pressure     0.11543E-06     474   0.99936E-08   0.11482E+00 0.11784E+04 
c  nu_tilda     0.75009E-05      33   0.14598E-04   0.67183E-06 0.21300E+03 
c  TempC        0.41638E+02      27   0.37434E-03   0.38572E+01 0.22944E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0986          9.7851          4.5729          4.5729
v  Velocity[Y]            -3.0557          7.2124         0.17595         0.17595
v  Velocity[Z]       -6.9287e-015     6.1986e-015    -1.5698e-017    -1.5698e-017
v  ǁVelocityǁ         0.0022549          9.7861          5.1312          5.1312
v  Pressure               -28.925          23.082         -5.3571         -5.3571
v  nu_tilda           4.4125e-007       0.0042695       0.0016834       0.0016834
v  TempC                       21          73.049          22.026          22.026
v  TurbVisc           3.3356e-014       0.0050321       0.0019782       0.0019782
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2142:        0.20670E+01

===============================================================


 INSTANT    0.214300000E+04   TIME STEP NUMBER            2143
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12057E-01 0.89230E+00
   Friction velocity        uk    :  0.12057E-01 0.89230E+00
   Dimensionless distance   yplus :  0.97071E-01 0.71836E+01
   Friction thermal sca.    tstar : -0.10347E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72426E-01 0.53598E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10356E-01      33   0.25395E-03   0.48500E+01 0.18660E+03 
c  Velocity[X]                                      0.17212E+01 
c  Velocity[Y]                                      0.31288E+01 
c  Velocity[Z]                                      0.72879E-30 
c  Pressure     0.11148E-06     537   0.96647E-08   0.10710E+00 0.14998E+04 
c  nu_tilda     0.75032E-05      33   0.51190E-05   0.67216E-06 0.21304E+03 
c  TempC        0.41645E+02      27   0.38059E-03   0.72207E+01 0.30226E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.095          9.7841          4.5729          4.5729
v  Velocity[Y]             -3.056           7.229         0.17626         0.17626
v  Velocity[Z]       -6.9287e-015     6.0606e-015    -1.5708e-017    -1.5708e-017
v  ǁVelocityǁ         0.0023919          9.7851          5.1311          5.1311
v  Pressure               -28.862          23.256          -5.285          -5.285
v  nu_tilda           4.4122e-007       0.0042695       0.0016838       0.0016838
v  TempC                       21           73.05          22.026          22.026
v  TurbVisc           3.3351e-014       0.0050321       0.0019786       0.0019786
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2143:        0.22240E+01

===============================================================


 INSTANT    0.214400000E+04   TIME STEP NUMBER            2144
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13062E-01 0.89342E+00
   Friction velocity        uk    :  0.13062E-01 0.89342E+00
   Dimensionless distance   yplus :  0.10516E+00 0.71927E+01
   Friction thermal sca.    tstar : -0.10251E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78460E-01 0.53665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10357E-01      33   0.27099E-03   0.48694E+01 0.18667E+03 
c  Velocity[X]                                      0.17473E+01 
c  Velocity[Y]                                      0.31221E+01 
c  Velocity[Z]                                      0.93445E-30 
c  Pressure     0.10782E-06     457   0.99755E-08   0.10775E+00 0.10730E+04 
c  nu_tilda     0.75054E-05      33   0.14591E-04   0.67252E-06 0.21308E+03 
c  TempC        0.41652E+02      27   0.34041E-03   0.54180E+01 0.27168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0915           9.783          4.5729          4.5729
v  Velocity[Y]            -3.0563          7.2065         0.17658         0.17658
v  Velocity[Z]       -6.9287e-015     6.3599e-015     -1.571e-017     -1.571e-017
v  ǁVelocityǁ         0.0022463           9.784           5.131           5.131
v  Pressure               -28.893          23.136         -5.2969         -5.2969
v  nu_tilda           4.4123e-007       0.0042695       0.0016841       0.0016841
v  TempC                       21          73.049          22.026          22.026
v  TurbVisc           3.3343e-014       0.0050321        0.001979        0.001979
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2144:        0.20320E+01

===============================================================


 INSTANT    0.214500000E+04   TIME STEP NUMBER            2145
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11002E-01 0.89258E+00
   Friction velocity        uk    :  0.11002E-01 0.89258E+00
   Dimensionless distance   yplus :  0.88577E-01 0.71859E+01
   Friction thermal sca.    tstar : -0.10468E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66088E-01 0.53615E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10359E-01      33   0.20185E-03   0.48557E+01 0.18672E+03 
c  Velocity[X]                                      0.17148E+01 
c  Velocity[Y]                                      0.31410E+01 
c  Velocity[Z]                                      0.83193E-30 
c  Pressure     0.90999E-07     521   0.99060E-08   0.89241E-01 0.16347E+04 
c  nu_tilda     0.75076E-05      33   0.51293E-05   0.67282E-06 0.21312E+03 
c  TempC        0.41659E+02      27   0.30616E-03   0.52169E+01 0.26265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.088           9.782          4.5729          4.5729
v  Velocity[Y]            -3.0565          7.2324         0.17689         0.17689
v  Velocity[Z]       -6.9287e-015     6.1684e-015    -1.5714e-017    -1.5714e-017
v  ǁVelocityǁ         0.0025138           9.783           5.131           5.131
v  Pressure               -28.719          23.339         -5.2195         -5.2195
v  nu_tilda           4.4119e-007       0.0042695       0.0016845       0.0016845
v  TempC                       21          73.049          22.026          22.026
v  TurbVisc           3.3343e-014       0.0050321       0.0019795       0.0019795
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2145:        0.21750E+01

===============================================================


 INSTANT    0.214600000E+04   TIME STEP NUMBER            2146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91100E-02 0.89374E+00
   Friction velocity        uk    :  0.91100E-02 0.89374E+00
   Dimensionless distance   yplus :  0.73341E-01 0.71952E+01
   Friction thermal sca.    tstar : -0.97414E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54721E-01 0.53684E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10361E-01      33   0.26219E-03   0.48233E+01 0.18653E+03 
c  Velocity[X]                                      0.16997E+01 
c  Velocity[Y]                                      0.31237E+01 
c  Velocity[Z]                                      0.74705E-30 
c  Pressure     0.11172E-06     442   0.96243E-08   0.10773E+00 0.83129E+03 
c  nu_tilda     0.75098E-05      33   0.14583E-04   0.67320E-06 0.21315E+03 
c  TempC        0.41666E+02      27   0.35492E-03   0.50877E+01 0.26818E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0845          9.7809          4.5729          4.5729
v  Velocity[Y]            -3.0566          7.2346          0.1772          0.1772
v  Velocity[Z]       -6.9287e-015     6.3084e-015    -1.5717e-017    -1.5717e-017
v  ǁVelocityǁ         0.0025529           9.782          5.1309          5.1309
v  Pressure               -28.919          23.279         -5.2212         -5.2212
v  nu_tilda           4.4114e-007       0.0042695       0.0016848       0.0016848
v  TempC                       21          73.048          22.026          22.026
v  TurbVisc           3.3334e-014       0.0050321       0.0019799       0.0019799
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2146:        0.20110E+01

===============================================================


 INSTANT    0.214700000E+04   TIME STEP NUMBER            2147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14865E-01 0.89346E+00
   Friction velocity        uk    :  0.14865E-01 0.89346E+00
   Dimensionless distance   yplus :  0.11967E+00 0.71930E+01
   Friction thermal sca.    tstar : -0.10787E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89289E-01 0.53668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10362E-01      33   0.27784E-03   0.48688E+01 0.18680E+03 
c  Velocity[X]                                      0.17415E+01 
c  Velocity[Y]                                      0.31273E+01 
c  Velocity[Z]                                      0.91891E-30 
c  Pressure     0.12234E-06     506   0.93989E-08   0.12135E+00 0.76652E+03 
c  nu_tilda     0.75120E-05      33   0.51289E-05   0.67355E-06 0.21320E+03 
c  TempC        0.41673E+02      27   0.32730E-03   0.72228E+01 0.30674E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0809          9.7799          4.5729          4.5729
v  Velocity[Y]            -3.0566          7.2108         0.17751         0.17751
v  Velocity[Z]       -6.9287e-015     6.1871e-015    -1.5723e-017    -1.5723e-017
v  ǁVelocityǁ         0.0022706           9.781          5.1308          5.1308
v  Pressure               -28.713          23.287         -5.1826         -5.1826
v  nu_tilda           4.4118e-007       0.0042695       0.0016852       0.0016852
v  TempC                       21          73.048          22.026          22.026
v  TurbVisc           3.3318e-014       0.0050321       0.0019803       0.0019803
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2147:        0.21470E+01

===============================================================


 INSTANT    0.214800000E+04   TIME STEP NUMBER            2148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.41554E-02 0.89213E+00
   Friction velocity        uk    :  0.41554E-02 0.89213E+00
   Dimensionless distance   yplus :  0.33454E-01 0.71823E+01
   Friction thermal sca.    tstar : -0.10853E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24960E-01 0.53588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10364E-01      33   0.25595E-03   0.48672E+01 0.18682E+03 
c  Velocity[X]                                      0.17273E+01 
c  Velocity[Y]                                      0.31399E+01 
c  Velocity[Z]                                      0.77056E-30 
c  Pressure     0.10748E-06     472   0.98695E-08   0.10560E+00 0.69930E+03 
c  nu_tilda     0.75142E-05      33   0.14584E-04   0.67393E-06 0.21324E+03 
c  TempC        0.41680E+02      27   0.28873E-03   0.59398E+01 0.27244E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0773          9.7789          4.5729          4.5729
v  Velocity[Y]             -3.057          7.2293         0.17782         0.17782
v  Velocity[Z]       -6.9287e-015     6.2265e-015    -1.5729e-017    -1.5729e-017
v  ǁVelocityǁ          0.002438          9.7799          5.1307          5.1307
v  Pressure                -28.73          23.362         -5.1557         -5.1557
v  nu_tilda           4.4123e-007       0.0042695       0.0016855       0.0016855
v  TempC                       21          73.048          22.026          22.026
v  TurbVisc           3.3331e-014       0.0050321       0.0019807       0.0019807
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2148:        0.20750E+01

===============================================================


 INSTANT    0.214900000E+04   TIME STEP NUMBER            2149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13898E-01 0.89325E+00
   Friction velocity        uk    :  0.13898E-01 0.89325E+00
   Dimensionless distance   yplus :  0.11188E+00 0.71913E+01
   Friction thermal sca.    tstar : -0.94846E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83478E-01 0.53655E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10366E-01      33   0.25492E-03   0.48526E+01 0.18671E+03 
c  Velocity[X]                                      0.17263E+01 
c  Velocity[Y]                                      0.31263E+01 
c  Velocity[Z]                                      0.66670E-30 
c  Pressure     0.11695E-06     488   0.98860E-08   0.11486E+00 0.70043E+03 
c  nu_tilda     0.75164E-05      33   0.51432E-05   0.67423E-06 0.21327E+03 
c  TempC        0.41687E+02      27   0.29550E-03   0.39083E+01 0.23947E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0738          9.7779          4.5729          4.5729
v  Velocity[Y]            -3.0573          7.2044         0.17813         0.17813
v  Velocity[Z]       -6.9287e-015     6.2034e-015    -1.5733e-017    -1.5733e-017
v  ǁVelocityǁ          0.002216          9.7789          5.1307          5.1307
v  Pressure               -28.676          23.332         -5.1245         -5.1245
v  nu_tilda           4.4124e-007       0.0042695       0.0016859       0.0016859
v  TempC                       21          73.049          22.027          22.027
v  TurbVisc           3.3345e-014       0.0050321       0.0019811       0.0019811
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2149:        0.22380E+01

===============================================================


 INSTANT    0.215000000E+04   TIME STEP NUMBER            2150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11477E-01 0.89251E+00
   Friction velocity        uk    :  0.11477E-01 0.89251E+00
   Dimensionless distance   yplus :  0.92396E-01 0.71853E+01
   Friction thermal sca.    tstar : -0.97104E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68938E-01 0.53610E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10368E-01      33   0.20897E-03   0.48553E+01 0.18672E+03 
c  Velocity[X]                                      0.17376E+01 
c  Velocity[Y]                                      0.31177E+01 
c  Velocity[Z]                                      0.76359E-30 
c  Pressure     0.10016E-06     441   0.96261E-08   0.98207E-01 0.65354E+03 
c  nu_tilda     0.75186E-05      33   0.14573E-04   0.67458E-06 0.21330E+03 
c  TempC        0.41694E+02      27   0.29585E-03   0.42648E+01 0.24920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0703          9.7768          4.5729          4.5729
v  Velocity[Y]            -3.0576          7.2303         0.17844         0.17844
v  Velocity[Z]       -6.9287e-015       6.33e-015    -1.5735e-017    -1.5735e-017
v  ǁVelocityǁ         0.0024415          9.7778          5.1306          5.1306
v  Pressure               -28.718          23.394         -5.1032         -5.1032
v  nu_tilda           4.4127e-007       0.0042695       0.0016862       0.0016862
v  TempC                       21          73.049          22.027          22.027
v  TurbVisc           3.3349e-014       0.0050321       0.0019816       0.0019816
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2150:        0.22190E+01

===============================================================


 INSTANT    0.215100000E+04   TIME STEP NUMBER            2151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14130E-01 0.89408E+00
   Friction velocity        uk    :  0.14130E-01 0.89408E+00
   Dimensionless distance   yplus :  0.11376E+00 0.71980E+01
   Friction thermal sca.    tstar : -0.10282E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84878E-01 0.53705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10369E-01      33   0.25091E-03   0.48284E+01 0.18670E+03 
c  Velocity[X]                                      0.16924E+01 
c  Velocity[Y]                                      0.31360E+01 
c  Velocity[Z]                                      0.73602E-30 
c  Pressure     0.96555E-07     552   0.93782E-08   0.94371E-01 0.13622E+04 
c  nu_tilda     0.75208E-05      33   0.51403E-05   0.67488E-06 0.21334E+03 
c  TempC        0.41701E+02      27   0.31899E-03   0.42571E+01 0.23575E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0666          9.7758          4.5729          4.5729
v  Velocity[Y]            -3.0577          7.2406         0.17874         0.17874
v  Velocity[Z]       -6.9287e-015     6.2053e-015     -1.574e-017     -1.574e-017
v  ǁVelocityǁ         0.0026226          9.7768          5.1305          5.1305
v  Pressure               -28.541          23.535         -5.0347         -5.0347
v  nu_tilda           4.4125e-007       0.0042695       0.0016866       0.0016866
v  TempC                       21          73.049          22.027          22.027
v  TurbVisc           3.3356e-014       0.0050321        0.001982        0.001982
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2151:        0.25000E+01

===============================================================


 INSTANT    0.215200000E+04   TIME STEP NUMBER            2152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14919E-01 0.89349E+00
   Friction velocity        uk    :  0.14919E-01 0.89349E+00
   Dimensionless distance   yplus :  0.12011E+00 0.71932E+01
   Friction thermal sca.    tstar : -0.92113E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89615E-01 0.53670E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10371E-01      33   0.26264E-03   0.48511E+01 0.18675E+03 
c  Velocity[X]                                      0.17288E+01 
c  Velocity[Y]                                      0.31223E+01 
c  Velocity[Z]                                      0.75508E-30 
c  Pressure     0.11327E-06     505   0.91904E-08   0.11177E+00 0.14230E+04 
c  nu_tilda     0.75230E-05      33   0.14574E-04   0.67525E-06 0.21338E+03 
c  TempC        0.41708E+02      27   0.25841E-03   0.50591E+01 0.25299E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.063          9.7747          4.5729          4.5729
v  Velocity[Y]            -3.0578          7.2073         0.17905         0.17905
v  Velocity[Z]       -6.9287e-015     6.3381e-015    -1.5742e-017    -1.5742e-017
v  ǁVelocityǁ          0.002257          9.7758          5.1304          5.1304
v  Pressure               -28.684          23.343         -5.0642         -5.0642
v  nu_tilda           4.4122e-007       0.0042695       0.0016869       0.0016869
v  TempC                       21          73.048          22.027          22.027
v  TurbVisc            3.335e-014       0.0050321       0.0019824       0.0019824
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2152:        0.23480E+01

===============================================================


 INSTANT    0.215300000E+04   TIME STEP NUMBER            2153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.99637E-03 0.89233E+00
   Friction velocity        uk    :  0.99637E-03 0.89233E+00
   Dimensionless distance   yplus :  0.80214E-02 0.71838E+01
   Friction thermal sca.    tstar : -0.92329E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59849E-02 0.53599E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10373E-01      33   0.28150E-03   0.48452E+01 0.18678E+03 
c  Velocity[X]                                      0.17281E+01 
c  Velocity[Y]                                      0.31171E+01 
c  Velocity[Z]                                      0.82610E-30 
c  Pressure     0.10571E-06     522   0.94445E-08   0.10385E+00 0.18717E+04 
c  nu_tilda     0.75252E-05      33   0.51490E-05   0.67556E-06 0.21342E+03 
c  TempC        0.41714E+02      27   0.34263E-03   0.51084E+01 0.25849E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0595          9.7737          4.5729          4.5729
v  Velocity[Y]            -3.0579          7.2308         0.17936         0.17936
v  Velocity[Z]       -6.9287e-015     6.1503e-015    -1.5745e-017    -1.5745e-017
v  ǁVelocityǁ          0.002515          9.7748          5.1303          5.1303
v  Pressure               -28.526          23.581         -4.9757         -4.9757
v  nu_tilda           4.4116e-007       0.0042695       0.0016873       0.0016873
v  TempC                       21          73.049          22.027          22.027
v  TurbVisc           3.3343e-014       0.0050321       0.0019828       0.0019828
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2153:        0.24500E+01

===============================================================


 INSTANT    0.215400000E+04   TIME STEP NUMBER            2154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13762E-01 0.89331E+00
   Friction velocity        uk    :  0.13762E-01 0.89331E+00
   Dimensionless distance   yplus :  0.11079E+00 0.71918E+01
   Friction thermal sca.    tstar : -0.86257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82665E-01 0.53659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10374E-01      33   0.26777E-03   0.48632E+01 0.18689E+03 
c  Velocity[X]                                      0.17311E+01 
c  Velocity[Y]                                      0.31321E+01 
c  Velocity[Z]                                      0.69503E-30 
c  Pressure     0.10643E-06     490   0.98124E-08   0.10568E+00 0.12227E+04 
c  nu_tilda     0.75274E-05      33   0.14563E-04   0.67591E-06 0.21345E+03 
c  TempC        0.41721E+02      27   0.32307E-03   0.63282E+01 0.29630E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0559          9.7726          4.5729          4.5729
v  Velocity[Y]            -3.0582          7.2067         0.17966         0.17966
v  Velocity[Z]       -6.9287e-015     6.2274e-015    -1.5747e-017    -1.5747e-017
v  ǁVelocityǁ         0.0022977          9.7737          5.1302          5.1302
v  Pressure               -28.528           23.43         -4.9978         -4.9978
v  nu_tilda           4.4119e-007       0.0042695       0.0016876       0.0016876
v  TempC                       21          73.049          22.027          22.027
v  TurbVisc           3.3324e-014       0.0050321       0.0019832       0.0019832
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2154:        0.21870E+01

===============================================================


 INSTANT    0.215500000E+04   TIME STEP NUMBER            2155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13006E-01 0.89246E+00
   Friction velocity        uk    :  0.13006E-01 0.89246E+00
   Dimensionless distance   yplus :  0.10471E+00 0.71849E+01
   Friction thermal sca.    tstar : -0.89749E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78125E-01 0.53608E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10376E-01      33   0.25010E-03   0.48489E+01 0.18679E+03 
c  Velocity[X]                                      0.17253E+01 
c  Velocity[Y]                                      0.31236E+01 
c  Velocity[Z]                                      0.61083E-30 
c  Pressure     0.11832E-06     537   0.99642E-08   0.11417E+00 0.16224E+04 
c  nu_tilda     0.75295E-05      33   0.51497E-05   0.67620E-06 0.21348E+03 
c  TempC        0.41728E+02      27   0.26397E-03   0.62920E+01 0.27804E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0523          9.7716          4.5729          4.5729
v  Velocity[Y]            -3.0585          7.2274         0.17996         0.17996
v  Velocity[Z]       -6.9287e-015     6.2769e-015    -1.5746e-017    -1.5746e-017
v  ǁVelocityǁ         0.0024636          9.7727          5.1302          5.1302
v  Pressure               -28.478          23.623         -4.9196         -4.9196
v  nu_tilda           4.4122e-007       0.0042695        0.001688        0.001688
v  TempC                       21           73.05          22.028          22.028
v  TurbVisc           3.3333e-014       0.0050321       0.0019837       0.0019837
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2155:        0.23060E+01

===============================================================


 INSTANT    0.215600000E+04   TIME STEP NUMBER            2156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13647E-01 0.89376E+00
   Friction velocity        uk    :  0.13647E-01 0.89376E+00
   Dimensionless distance   yplus :  0.10987E+00 0.71954E+01
   Friction thermal sca.    tstar : -0.84526E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81975E-01 0.53686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10378E-01      33   0.25815E-03   0.48404E+01 0.18680E+03 
c  Velocity[X]                                      0.17198E+01 
c  Velocity[Y]                                      0.31206E+01 
c  Velocity[Z]                                      0.76805E-30 
c  Pressure     0.96485E-07     424   0.98293E-08   0.94734E-01 0.73355E+03 
c  nu_tilda     0.75317E-05      33   0.14562E-04   0.67657E-06 0.21352E+03 
c  TempC        0.41735E+02      27   0.31626E-03   0.46840E+01 0.24542E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0486          9.7705          4.5729          4.5729
v  Velocity[Y]            -3.0587          7.2364         0.18027         0.18027
v  Velocity[Z]       -6.9287e-015     6.3811e-015    -1.5747e-017    -1.5747e-017
v  ǁVelocityǁ          0.002572          9.7716          5.1301          5.1301
v  Pressure               -28.547          23.587         -4.9177         -4.9177
v  nu_tilda           4.4121e-007       0.0042695       0.0016883       0.0016883
v  TempC                       21          73.049          22.028          22.028
v  TurbVisc           3.3342e-014       0.0050321       0.0019841       0.0019841
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2156:        0.19630E+01

===============================================================


 INSTANT    0.215700000E+04   TIME STEP NUMBER            2157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14828E-01 0.89342E+00
   Friction velocity        uk    :  0.14828E-01 0.89342E+00
   Dimensionless distance   yplus :  0.11938E+00 0.71927E+01
   Friction thermal sca.    tstar : -0.85324E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89068E-01 0.53665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10379E-01      33   0.24504E-03   0.48493E+01 0.18691E+03 
c  Velocity[X]                                      0.17159E+01 
c  Velocity[Y]                                      0.31334E+01 
c  Velocity[Z]                                      0.75654E-30 
c  Pressure     0.11697E-06     489   0.97550E-08   0.11633E+00 0.74398E+03 
c  nu_tilda     0.75339E-05      33   0.51557E-05   0.67687E-06 0.21355E+03 
c  TempC        0.41742E+02      27   0.33697E-03   0.48997E+01 0.26024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0451          9.7695          4.5729          4.5729
v  Velocity[Y]            -3.0589          7.2092         0.18057         0.18057
v  Velocity[Z]       -6.9287e-015     6.3288e-015    -1.5747e-017    -1.5747e-017
v  ǁVelocityǁ         0.0023903          9.7706            5.13            5.13
v  Pressure                -28.36          23.585         -4.8817         -4.8817
v  nu_tilda           4.4123e-007       0.0042695       0.0016887       0.0016887
v  TempC                       21          73.049          22.028          22.028
v  TurbVisc           3.3338e-014       0.0050321       0.0019845       0.0019845
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2157:        0.21130E+01

===============================================================


 INSTANT    0.215800000E+04   TIME STEP NUMBER            2158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12202E-01 0.89184E+00
   Friction velocity        uk    :  0.12202E-01 0.89184E+00
   Dimensionless distance   yplus :  0.98236E-01 0.71799E+01
   Friction thermal sca.    tstar : -0.92103E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73295E-01 0.53570E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10381E-01      33   0.25751E-03   0.48245E+01 0.18675E+03 
c  Velocity[X]                                      0.17093E+01 
c  Velocity[Y]                                      0.31152E+01 
c  Velocity[Z]                                      0.70894E-30 
c  Pressure     0.10943E-06     408   0.97355E-08   0.10607E+00 0.61328E+03 
c  nu_tilda     0.75361E-05      33   0.14556E-04   0.67724E-06 0.21359E+03 
c  TempC        0.41749E+02      27   0.33781E-03   0.56205E+01 0.26946E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0415          9.7685          4.5729          4.5729
v  Velocity[Y]             -3.059           7.224         0.18087         0.18087
v  Velocity[Z]       -6.9287e-015     6.1876e-015     -1.575e-017     -1.575e-017
v  ǁVelocityǁ         0.0024867          9.7696          5.1299          5.1299
v  Pressure               -28.505          23.609         -4.8675         -4.8675
v  nu_tilda           4.4128e-007       0.0042695        0.001689        0.001689
v  TempC                       21          73.049          22.028          22.028
v  TurbVisc           3.3346e-014       0.0050321       0.0019849       0.0019849
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2158:        0.19360E+01

===============================================================


 INSTANT    0.215900000E+04   TIME STEP NUMBER            2159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14490E-01 0.89319E+00
   Friction velocity        uk    :  0.14490E-01 0.89319E+00
   Dimensionless distance   yplus :  0.11666E+00 0.71908E+01
   Friction thermal sca.    tstar : -0.89815E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87039E-01 0.53652E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10383E-01      33   0.28868E-03   0.48465E+01 0.18689E+03 
c  Velocity[X]                                      0.17337E+01 
c  Velocity[Y]                                      0.31128E+01 
c  Velocity[Z]                                      0.90051E-30 
c  Pressure     0.12019E-06     490   0.96313E-08   0.11854E+00 0.83403E+03 
c  nu_tilda     0.75383E-05      33   0.51616E-05   0.67751E-06 0.21362E+03 
c  TempC        0.41756E+02      27   0.26977E-03   0.54215E+01 0.25790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0378          9.7674          4.5729          4.5729
v  Velocity[Y]             -3.059           7.205         0.18117         0.18117
v  Velocity[Z]       -6.9287e-015     6.1736e-015    -1.5748e-017    -1.5748e-017
v  ǁVelocityǁ         0.0022982          9.7685          5.1298          5.1298
v  Pressure               -28.327          23.636         -4.8248         -4.8248
v  nu_tilda            4.413e-007       0.0042695       0.0016894       0.0016894
v  TempC                       21           73.05          22.028          22.028
v  TurbVisc           3.3359e-014       0.0050321       0.0019853       0.0019853
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2159:        0.21160E+01

===============================================================


 INSTANT    0.216000000E+04   TIME STEP NUMBER            2160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12532E-01 0.89233E+00
   Friction velocity        uk    :  0.12532E-01 0.89233E+00
   Dimensionless distance   yplus :  0.10089E+00 0.71838E+01
   Friction thermal sca.    tstar : -0.98724E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75278E-01 0.53599E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10384E-01      33   0.21232E-03   0.48591E+01 0.18699E+03 
c  Velocity[X]                                      0.17302E+01 
c  Velocity[Y]                                      0.31289E+01 
c  Velocity[Z]                                      0.69682E-30 
c  Pressure     0.10230E-06     441   0.99009E-08   0.10038E+00 0.66531E+03 
c  nu_tilda     0.75405E-05      33   0.14550E-04   0.67784E-06 0.21365E+03 
c  TempC        0.41762E+02      27   0.30384E-03   0.31113E+01 0.22355E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0341          9.7664          4.5729          4.5729
v  Velocity[Y]            -3.0593          7.2289         0.18147         0.18147
v  Velocity[Z]       -6.9287e-015     6.2284e-015    -1.5754e-017    -1.5754e-017
v  ǁVelocityǁ         0.0024558          9.7675          5.1297          5.1297
v  Pressure               -28.351          23.693          -4.802          -4.802
v  nu_tilda           4.4122e-007       0.0042695       0.0016897       0.0016897
v  TempC                       21           73.05          22.028          22.028
v  TurbVisc           3.3367e-014       0.0050321       0.0019857       0.0019857
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2160:        0.20050E+01

===============================================================


 INSTANT    0.216100000E+04   TIME STEP NUMBER            2161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12275E-01 0.89392E+00
   Friction velocity        uk    :  0.12275E-01 0.89392E+00
   Dimensionless distance   yplus :  0.98821E-01 0.71967E+01
   Friction thermal sca.    tstar : -0.88878E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73732E-01 0.53695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10386E-01      33   0.25106E-03   0.48199E+01 0.18678E+03 
c  Velocity[X]                                      0.17020E+01 
c  Velocity[Y]                                      0.31179E+01 
c  Velocity[Z]                                      0.63080E-30 
c  Pressure     0.11467E-06     505   0.94940E-08   0.11158E+00 0.11776E+04 
c  nu_tilda     0.75427E-05      33   0.51639E-05   0.67811E-06 0.21368E+03 
c  TempC        0.41769E+02      27   0.34219E-03   0.64877E+01 0.27343E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0305          9.7653          4.5729          4.5729
v  Velocity[Y]            -3.0596          7.2362         0.18177         0.18177
v  Velocity[Z]       -6.9287e-015     6.3421e-015    -1.5749e-017    -1.5749e-017
v  ǁVelocityǁ         0.0025153          9.7664          5.1297          5.1297
v  Pressure               -28.322          23.794         -4.7413         -4.7413
v  nu_tilda           4.4112e-007       0.0042695       0.0016901       0.0016901
v  TempC                       21           73.05          22.028          22.028
v  TurbVisc           3.3342e-014       0.0050321       0.0019861       0.0019861
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2161:        0.21480E+01

===============================================================


 INSTANT    0.216200000E+04   TIME STEP NUMBER            2162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97391E-02 0.89361E+00
   Friction velocity        uk    :  0.97391E-02 0.89361E+00
   Dimensionless distance   yplus :  0.78407E-01 0.71942E+01
   Friction thermal sca.    tstar : -0.11066E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58500E-01 0.53677E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10388E-01      33   0.25112E-03   0.48540E+01 0.18692E+03 
c  Velocity[X]                                      0.17447E+01 
c  Velocity[Y]                                      0.31093E+01 
c  Velocity[Z]                                      0.80075E-30 
c  Pressure     0.98490E-07     488   0.98673E-08   0.98439E-01 0.12066E+04 
c  nu_tilda     0.75449E-05      33   0.14546E-04   0.67847E-06 0.21372E+03 
c  TempC        0.41776E+02      27   0.32594E-03   0.72214E+01 0.28966E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0269          9.7642          4.5729          4.5729
v  Velocity[Y]            -3.0598          7.2088         0.18207         0.18207
v  Velocity[Z]       -6.9287e-015     6.3543e-015    -1.5747e-017    -1.5747e-017
v  ǁVelocityǁ         0.0022959          9.7654          5.1296          5.1296
v  Pressure               -28.339          23.649         -4.7641         -4.7641
v  nu_tilda           4.4115e-007       0.0042695       0.0016904       0.0016904
v  TempC                       21          73.048          22.029          22.029
v  TurbVisc           3.3313e-014       0.0050321       0.0019866       0.0019866
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2162:        0.21040E+01

===============================================================


 INSTANT    0.216300000E+04   TIME STEP NUMBER            2163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11638E-01 0.89221E+00
   Friction velocity        uk    :  0.11638E-01 0.89221E+00
   Dimensionless distance   yplus :  0.93694E-01 0.71829E+01
   Friction thermal sca.    tstar : -0.13639E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69906E-01 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10389E-01      33   0.25232E-03   0.48298E+01 0.18692E+03 
c  Velocity[X]                                      0.17029E+01 
c  Velocity[Y]                                      0.31269E+01 
c  Velocity[Z]                                      0.78380E-30 
c  Pressure     0.89697E-07     553   0.93044E-08   0.87395E-01 0.16768E+04 
c  nu_tilda     0.75471E-05      33   0.51758E-05   0.67876E-06 0.21376E+03 
c  TempC        0.41783E+02      27   0.30743E-03   0.51513E+01 0.28010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0232          9.7632          4.5729          4.5729
v  Velocity[Y]              -3.06           7.229         0.18237         0.18237
v  Velocity[Z]       -6.9287e-015     6.2693e-015    -1.5742e-017    -1.5742e-017
v  ǁVelocityǁ         0.0025134          9.7644          5.1295          5.1295
v  Pressure               -28.157          23.854         -4.6842         -4.6842
v  nu_tilda           4.4119e-007       0.0042695       0.0016908       0.0016908
v  TempC                       21          73.049          22.029          22.029
v  TurbVisc            3.332e-014       0.0050321        0.001987        0.001987
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2163:        0.22640E+01

===============================================================


 INSTANT    0.216400000E+04   TIME STEP NUMBER            2164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13424E-01 0.89307E+00
   Friction velocity        uk    :  0.13424E-01 0.89307E+00
   Dimensionless distance   yplus :  0.10807E+00 0.71898E+01
   Friction thermal sca.    tstar : -0.23984E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80633E-01 0.53644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10391E-01      33   0.27084E-03   0.48358E+01 0.18693E+03 
c  Velocity[X]                                      0.17185E+01 
c  Velocity[Y]                                      0.31173E+01 
c  Velocity[Z]                                      0.80067E-30 
c  Pressure     0.11488E-06     474   0.98811E-08   0.11243E+00 0.12383E+04 
c  nu_tilda     0.75493E-05      33   0.14536E-04   0.67913E-06 0.21379E+03 
c  TempC        0.41790E+02      27   0.33362E-03   0.49417E+01 0.26536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0194          9.7622          4.5729          4.5729
v  Velocity[Y]              -3.06          7.2021         0.18267         0.18267
v  Velocity[Z]       -6.9287e-015     6.3069e-015    -1.5744e-017    -1.5744e-017
v  ǁVelocityǁ         0.0022353          9.7633          5.1294          5.1294
v  Pressure               -28.291          23.694          -4.705          -4.705
v  nu_tilda           4.4125e-007       0.0042695       0.0016911       0.0016911
v  TempC                       21          73.048          22.029          22.029
v  TurbVisc           3.3333e-014       0.0050321       0.0019874       0.0019874
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2164:        0.20740E+01

===============================================================


 INSTANT    0.216500000E+04   TIME STEP NUMBER            2165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12200E-01 0.89251E+00
   Friction velocity        uk    :  0.12200E-01 0.89251E+00
   Dimensionless distance   yplus :  0.98218E-01 0.71853E+01
   Friction thermal sca.    tstar : -0.26942E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73281E-01 0.53611E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10393E-01      33   0.23240E-03   0.48405E+01 0.18696E+03 
c  Velocity[X]                                      0.17278E+01 
c  Velocity[Y]                                      0.31127E+01 
c  Velocity[Z]                                      0.93502E-30 
c  Pressure     0.11227E-06     552   0.98802E-08   0.11058E+00 0.18842E+04 
c  nu_tilda     0.75514E-05      33   0.51712E-05   0.67939E-06 0.21382E+03 
c  TempC        0.41796E+02      27   0.31919E-03   0.61979E+01 0.29386E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0158          9.7611          4.5729          4.5729
v  Velocity[Y]            -3.0601          7.2293         0.18296         0.18296
v  Velocity[Z]       -6.9287e-015     6.3136e-015     -1.574e-017     -1.574e-017
v  ǁVelocityǁ         0.0025384          9.7622          5.1293          5.1293
v  Pressure               -28.148          23.935         -4.6185         -4.6185
v  nu_tilda           4.4122e-007       0.0042695       0.0016915       0.0016915
v  TempC                       21          73.049          22.029          22.029
v  TurbVisc           3.3352e-014       0.0050321       0.0019878       0.0019878
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2165:        0.22440E+01

===============================================================


 INSTANT    0.216600000E+04   TIME STEP NUMBER            2166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.87835E-02 0.89369E+00
   Friction velocity        uk    :  0.87835E-02 0.89369E+00
   Dimensionless distance   yplus :  0.70713E-01 0.71949E+01
   Friction thermal sca.    tstar : -0.14185E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52760E-01 0.53682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10394E-01      33   0.25037E-03   0.48290E+01 0.18695E+03 
c  Velocity[X]                                      0.17050E+01 
c  Velocity[Y]                                      0.31240E+01 
c  Velocity[Z]                                      0.77319E-30 
c  Pressure     0.96241E-07     473   0.94051E-08   0.94451E-01 0.85607E+03 
c  nu_tilda     0.75536E-05      33   0.14536E-04   0.67970E-06 0.21385E+03 
c  TempC        0.41803E+02      27   0.29474E-03   0.54378E+01 0.26842E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0122            9.76          4.5729          4.5729
v  Velocity[Y]            -3.0602          7.2352         0.18326         0.18326
v  Velocity[Z]       -6.9287e-015     6.2564e-015    -1.5735e-017    -1.5735e-017
v  ǁVelocityǁ         0.0026142          9.7612          5.1292          5.1292
v  Pressure                -28.21          23.871         -4.6261         -4.6261
v  nu_tilda           4.4117e-007       0.0042695       0.0016918       0.0016918
v  TempC                       21          73.049          22.029          22.029
v  TurbVisc            3.334e-014       0.0050321       0.0019882       0.0019882
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2166:        0.20740E+01

===============================================================


 INSTANT    0.216700000E+04   TIME STEP NUMBER            2167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76638E-02 0.89322E+00
   Friction velocity        uk    :  0.76638E-02 0.89322E+00
   Dimensionless distance   yplus :  0.61699E-01 0.71910E+01
   Friction thermal sca.    tstar : -0.10766E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46034E-01 0.53653E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10396E-01      33   0.25294E-03   0.48413E+01 0.18697E+03 
c  Velocity[X]                                      0.17287E+01 
c  Velocity[Y]                                      0.31126E+01 
c  Velocity[Z]                                      0.52831E-30 
c  Pressure     0.12521E-06     490   0.98753E-08   0.12243E+00 0.73454E+03 
c  nu_tilda     0.75558E-05      33   0.51822E-05   0.67997E-06 0.21388E+03 
c  TempC        0.41810E+02      27   0.30255E-03   0.49666E+01 0.24599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0084           9.759          4.5729          4.5729
v  Velocity[Y]            -3.0605          7.2048         0.18356         0.18356
v  Velocity[Z]       -6.9287e-015     6.4214e-015    -1.5733e-017    -1.5733e-017
v  ǁVelocityǁ         0.0022901          9.7602          5.1291          5.1291
v  Pressure               -28.125          23.849         -4.5913         -4.5913
v  nu_tilda            4.412e-007       0.0042695       0.0016922       0.0016922
v  TempC                       21          73.049          22.029          22.029
v  TurbVisc           3.3326e-014       0.0050321       0.0019886       0.0019886
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2167:        0.21220E+01

===============================================================


 INSTANT    0.216800000E+04   TIME STEP NUMBER            2168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11921E-01 0.89203E+00
   Friction velocity        uk    :  0.11921E-01 0.89203E+00
   Dimensionless distance   yplus :  0.95973E-01 0.71815E+01
   Friction thermal sca.    tstar : -0.95414E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71607E-01 0.53582E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10398E-01      33   0.25911E-03   0.48377E+01 0.18695E+03 
c  Velocity[X]                                      0.17323E+01 
c  Velocity[Y]                                      0.31054E+01 
c  Velocity[Z]                                      0.72034E-30 
c  Pressure     0.97957E-07     458   0.97343E-08   0.96708E-01 0.71961E+03 
c  nu_tilda     0.75580E-05      33   0.14528E-04   0.68032E-06 0.21391E+03 
c  TempC        0.41817E+02      27   0.28766E-03   0.52328E+01 0.26753E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0101          9.7579          4.5729          4.5729
v  Velocity[Y]            -3.0608          7.2257         0.18385         0.18385
v  Velocity[Z]       -6.9287e-015     6.5837e-015    -1.5721e-017    -1.5721e-017
v  ǁVelocityǁ         0.0025254          9.7591           5.129           5.129
v  Pressure                -28.16          23.936         -4.5643         -4.5643
v  nu_tilda           4.4114e-007       0.0042695       0.0016925       0.0016925
v  TempC                       21          73.049          22.029          22.029
v  TurbVisc           3.3335e-014       0.0050321        0.001989        0.001989
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2168:        0.22850E+01

===============================================================


 INSTANT    0.216900000E+04   TIME STEP NUMBER            2169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14469E-01 0.89314E+00
   Friction velocity        uk    :  0.14469E-01 0.89314E+00
   Dimensionless distance   yplus :  0.11648E+00 0.71904E+01
   Friction thermal sca.    tstar : -0.81197E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86910E-01 0.53648E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10399E-01      33   0.25453E-03   0.48339E+01 0.18703E+03 
c  Velocity[X]                                      0.17105E+01 
c  Velocity[Y]                                      0.31234E+01 
c  Velocity[Z]                                      0.79041E-30 
c  Pressure     0.10470E-06     474   0.92412E-08   0.10446E+00 0.77688E+03 
c  nu_tilda     0.75602E-05      33   0.51783E-05   0.68060E-06 0.21395E+03 
c  TempC        0.41824E+02      27   0.33674E-03   0.41798E+01 0.24047E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0152          9.7569          4.5729          4.5729
v  Velocity[Y]            -3.0609          7.2058         0.18414         0.18414
v  Velocity[Z]       -6.9287e-015      6.644e-015    -1.5718e-017    -1.5718e-017
v  ǁVelocityǁ         0.0023578          9.7581          5.1289          5.1289
v  Pressure               -28.009          23.934         -4.5259         -4.5259
v  nu_tilda           4.4111e-007       0.0042695       0.0016929       0.0016929
v  TempC                       21          73.049           22.03           22.03
v  TurbVisc           3.3318e-014       0.0050321       0.0019894       0.0019894
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2169:        0.23170E+01

===============================================================


 INSTANT    0.217000000E+04   TIME STEP NUMBER            2170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.35603E-02 0.89223E+00
   Friction velocity        uk    :  0.35603E-02 0.89223E+00
   Dimensionless distance   yplus :  0.28663E-01 0.71831E+01
   Friction thermal sca.    tstar : -0.71986E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21386E-01 0.53594E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10401E-01      33   0.20966E-03   0.48175E+01 0.18692E+03 
c  Velocity[X]                                      0.17115E+01 
c  Velocity[Y]                                      0.31061E+01 
c  Velocity[Z]                                      0.72191E-30 
c  Pressure     0.11502E-06     329   0.96993E-08   0.11132E+00 0.64140E+03 
c  nu_tilda     0.75623E-05      33   0.14527E-04   0.68090E-06 0.21397E+03 
c  TempC        0.41830E+02      27   0.24423E-03   0.50058E+01 0.24791E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0203          9.7558          4.5729          4.5729
v  Velocity[Y]             -3.061          7.2244         0.18444         0.18444
v  Velocity[Z]       -6.9287e-015     6.5135e-015    -1.5705e-017    -1.5705e-017
v  ǁVelocityǁ         0.0024649           9.757          5.1288          5.1288
v  Pressure               -28.147          23.944         -4.5175         -4.5175
v  nu_tilda           4.4114e-007       0.0042695       0.0016932       0.0016932
v  TempC                       21          73.048           22.03           22.03
v  TurbVisc           3.3308e-014       0.0050321       0.0019898       0.0019898
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2170:        0.17390E+01

===============================================================


 INSTANT    0.217100000E+04   TIME STEP NUMBER            2171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.44796E-02 0.89381E+00
   Friction velocity        uk    :  0.44796E-02 0.89381E+00
   Dimensionless distance   yplus :  0.36064E-01 0.71958E+01
   Friction thermal sca.    tstar : -0.73431E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26907E-01 0.53689E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10403E-01      33   0.28143E-03   0.48103E+01 0.18695E+03 
c  Velocity[X]                                      0.17081E+01 
c  Velocity[Y]                                      0.31022E+01 
c  Velocity[Z]                                      0.76294E-30 
c  Pressure     0.10381E-06     490   0.95730E-08   0.10177E+00 0.13513E+04 
c  nu_tilda     0.75645E-05      33   0.51858E-05   0.68114E-06 0.21400E+03 
c  TempC        0.41837E+02      27   0.31092E-03   0.30263E+01 0.21389E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0253          9.7548          4.5729          4.5729
v  Velocity[Y]             -3.061          7.2369         0.18473         0.18473
v  Velocity[Z]       -6.9287e-015     6.6127e-015      -1.57e-017      -1.57e-017
v  ǁVelocityǁ         0.0025416          9.7559          5.1288          5.1288
v  Pressure               -27.983          24.079         -4.4504         -4.4504
v  nu_tilda           4.4116e-007       0.0042695       0.0016936       0.0016936
v  TempC                       21           73.05           22.03           22.03
v  TurbVisc           3.3317e-014       0.0050321       0.0019902       0.0019902
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2171:        0.21160E+01

===============================================================


 INSTANT    0.217200000E+04   TIME STEP NUMBER            2172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.94234E-02 0.89337E+00
   Friction velocity        uk    :  0.94234E-02 0.89337E+00
   Dimensionless distance   yplus :  0.75864E-01 0.71922E+01
   Friction thermal sca.    tstar : -0.73034E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56603E-01 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10404E-01      33   0.25088E-03   0.48552E+01 0.18716E+03 
c  Velocity[X]                                      0.17349E+01 
c  Velocity[Y]                                      0.31203E+01 
c  Velocity[Z]                                      0.68182E-30 
c  Pressure     0.11214E-06     488   0.96844E-08   0.11130E+00 0.12147E+04 
c  nu_tilda     0.75667E-05      33   0.14517E-04   0.68147E-06 0.21403E+03 
c  TempC        0.41844E+02      27   0.30520E-03   0.58378E+01 0.25911E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0303          9.7537          4.5729          4.5729
v  Velocity[Y]            -3.0611          7.2082         0.18502         0.18502
v  Velocity[Z]       -6.9287e-015     6.6554e-015    -1.5691e-017    -1.5691e-017
v  ǁVelocityǁ         0.0022677          9.7549          5.1287          5.1287
v  Pressure               -27.991          23.931         -4.4703         -4.4703
v  nu_tilda           4.4122e-007       0.0042695       0.0016939       0.0016939
v  TempC                       21          73.049           22.03           22.03
v  TurbVisc           3.3322e-014       0.0050321       0.0019907       0.0019907
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2172:        0.21120E+01

===============================================================


 INSTANT    0.217300000E+04   TIME STEP NUMBER            2173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12912E-01 0.89204E+00
   Friction velocity        uk    :  0.12912E-01 0.89204E+00
   Dimensionless distance   yplus :  0.10395E+00 0.71816E+01
   Friction thermal sca.    tstar : -0.76750E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77559E-01 0.53583E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10406E-01      33   0.24711E-03   0.48264E+01 0.18705E+03 
c  Velocity[X]                                      0.17122E+01 
c  Velocity[Y]                                      0.31142E+01 
c  Velocity[Z]                                      0.85174E-30 
c  Pressure     0.10603E-06     537   0.93116E-08   0.10277E+00 0.16084E+04 
c  nu_tilda     0.75689E-05      33   0.51859E-05   0.68179E-06 0.21407E+03 
c  TempC        0.41851E+02      27   0.22253E-03   0.66978E+01 0.26046E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0351          9.7526          4.5729          4.5729
v  Velocity[Y]            -3.0614          7.2244         0.18531         0.18531
v  Velocity[Z]       -6.9287e-015     6.5901e-015    -1.5687e-017    -1.5687e-017
v  ǁVelocityǁ         0.0024635          9.7538          5.1286          5.1286
v  Pressure               -27.944           24.12          -4.394          -4.394
v  nu_tilda           4.4125e-007       0.0042695       0.0016943       0.0016943
v  TempC                       21           73.05           22.03           22.03
v  TurbVisc           3.3341e-014       0.0050321       0.0019911       0.0019911
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2173:        0.22190E+01

===============================================================


 INSTANT    0.217400000E+04   TIME STEP NUMBER            2174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.74809E-02 0.89307E+00
   Friction velocity        uk    :  0.74809E-02 0.89307E+00
   Dimensionless distance   yplus :  0.60226E-01 0.71898E+01
   Friction thermal sca.    tstar : -0.71643E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44936E-01 0.53644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10407E-01      33   0.26345E-03   0.48368E+01 0.18707E+03 
c  Velocity[X]                                      0.17362E+01 
c  Velocity[Y]                                      0.31006E+01 
c  Velocity[Z]                                      0.69575E-30 
c  Pressure     0.10175E-06     521   0.92765E-08   0.10110E+00 0.11962E+04 
c  nu_tilda     0.75710E-05      33   0.14516E-04   0.68212E-06 0.21410E+03 
c  TempC        0.41857E+02      27   0.31907E-03   0.37703E+01 0.21569E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.04          9.7516          4.5729          4.5729
v  Velocity[Y]            -3.0616          7.2025          0.1856          0.1856
v  Velocity[Z]       -6.9287e-015     6.5094e-015    -1.5679e-017    -1.5679e-017
v  ǁVelocityǁ         0.0022846          9.7528          5.1285          5.1285
v  Pressure               -27.969          23.977         -4.4167         -4.4167
v  nu_tilda           4.4131e-007       0.0042695       0.0016946       0.0016946
v  TempC                       21          73.049           22.03           22.03
v  TurbVisc            3.335e-014       0.0050321       0.0019915       0.0019915
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2174:        0.21880E+01

===============================================================


 INSTANT    0.217500000E+04   TIME STEP NUMBER            2175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85852E-02 0.89230E+00
   Friction velocity        uk    :  0.85852E-02 0.89230E+00
   Dimensionless distance   yplus :  0.69117E-01 0.71836E+01
   Friction thermal sca.    tstar : -0.72217E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51569E-01 0.53598E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10409E-01      33   0.24943E-03   0.48244E+01 0.18709E+03 
c  Velocity[X]                                      0.17064E+01 
c  Velocity[Y]                                      0.31180E+01 
c  Velocity[Z]                                      0.68101E-30 
c  Pressure     0.96697E-07     537   0.98766E-08   0.94176E-01 0.18388E+04 
c  nu_tilda     0.75732E-05      33   0.51898E-05   0.68235E-06 0.21412E+03 
c  TempC        0.41864E+02      27   0.30053E-03   0.50973E+01 0.25580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0447          9.7505          4.5729          4.5729
v  Velocity[Y]            -3.0617          7.2274         0.18589         0.18589
v  Velocity[Z]       -6.9287e-015     6.5348e-015    -1.5676e-017    -1.5676e-017
v  ǁVelocityǁ         0.0025652          9.7517          5.1284          5.1284
v  Pressure               -27.878          24.204          -4.331          -4.331
v  nu_tilda           4.4129e-007       0.0042695        0.001695        0.001695
v  TempC                       21           73.05           22.03           22.03
v  TurbVisc           3.3368e-014       0.0050321       0.0019919       0.0019919
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2175:        0.22570E+01

===============================================================


 INSTANT    0.217600000E+04   TIME STEP NUMBER            2176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.10711E-01 0.89341E+00
   Friction velocity        uk    :  0.10711E-01 0.89341E+00
   Dimensionless distance   yplus :  0.86228E-01 0.71926E+01
   Friction thermal sca.    tstar : -0.69859E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64336E-01 0.53665E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10411E-01      33   0.26462E-03   0.47946E+01 0.18693E+03 
c  Velocity[X]                                      0.16929E+01 
c  Velocity[Y]                                      0.31017E+01 
c  Velocity[Z]                                      0.73921E-30 
c  Pressure     0.10626E-06     488   0.97334E-08   0.10260E+00 0.94386E+03 
c  nu_tilda     0.75754E-05      33   0.14507E-04   0.68263E-06 0.21415E+03 
c  TempC        0.41871E+02      27   0.33052E-03   0.61634E+01 0.26567E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0496          9.7494          4.5729          4.5729
v  Velocity[Y]            -3.0618          7.2305         0.18618         0.18618
v  Velocity[Z]       -6.9287e-015     6.5977e-015    -1.5661e-017    -1.5661e-017
v  ǁVelocityǁ         0.0025564          9.7506          5.1283          5.1283
v  Pressure               -27.984          24.117         -4.3414         -4.3414
v  nu_tilda           4.4116e-007       0.0042695       0.0016953       0.0016953
v  TempC                       21           73.05          22.031          22.031
v  TurbVisc           3.3363e-014       0.0050321       0.0019923       0.0019923
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2176:        0.21010E+01

===============================================================


 INSTANT    0.217700000E+04   TIME STEP NUMBER            2177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.72192E-03 0.89326E+00
   Friction velocity        uk    :  0.72192E-03 0.89326E+00
   Dimensionless distance   yplus :  0.58119E-02 0.71914E+01
   Friction thermal sca.    tstar : -0.67644E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43363E-02 0.53656E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10412E-01      33   0.27529E-03   0.48346E+01 0.18714E+03 
c  Velocity[X]                                      0.17358E+01 
c  Velocity[Y]                                      0.30988E+01 
c  Velocity[Z]                                      0.98627E-30 
c  Pressure     0.11680E-06     506   0.96136E-08   0.11655E+00 0.94724E+03 
c  nu_tilda     0.75776E-05      33   0.51955E-05   0.68288E-06 0.21417E+03 
c  TempC        0.41877E+02      27   0.27667E-03   0.55724E+01 0.25652E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0547          9.7484          4.5729          4.5729
v  Velocity[Y]            -3.0618          7.2064         0.18646         0.18646
v  Velocity[Z]       -6.9287e-015     6.5258e-015     -1.566e-017     -1.566e-017
v  ǁVelocityǁ         0.0023744          9.7496          5.1282          5.1282
v  Pressure               -27.827          24.154          -4.292          -4.292
v  nu_tilda            4.411e-007       0.0042695       0.0016957       0.0016957
v  TempC                       21           73.05          22.031          22.031
v  TurbVisc           3.3323e-014       0.0050321       0.0019927       0.0019927
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2177:        0.21570E+01

===============================================================


 INSTANT    0.217800000E+04   TIME STEP NUMBER            2178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.97720E-02 0.89187E+00
   Friction velocity        uk    :  0.97720E-02 0.89187E+00
   Dimensionless distance   yplus :  0.78671E-01 0.71802E+01
   Friction thermal sca.    tstar : -0.66460E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58698E-01 0.53572E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10414E-01      33   0.25600E-03   0.48311E+01 0.18716E+03 
c  Velocity[X]                                      0.17181E+01 
c  Velocity[Y]                                      0.31130E+01 
c  Velocity[Z]                                      0.76236E-30 
c  Pressure     0.10225E-06     440   0.97418E-08   0.99969E-01 0.63155E+03 
c  nu_tilda     0.75797E-05      33   0.14504E-04   0.68321E-06 0.21421E+03 
c  TempC        0.41884E+02      27   0.23067E-03   0.39351E+01 0.22205E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0598          9.7473          4.5729          4.5729
v  Velocity[Y]            -3.0619          7.2248         0.18675         0.18675
v  Velocity[Z]       -6.9287e-015     6.5354e-015    -1.5646e-017    -1.5646e-017
v  ǁVelocityǁ         0.0025968          9.7485          5.1281          5.1281
v  Pressure               -27.837          24.204         -4.2767         -4.2767
v  nu_tilda           4.4112e-007       0.0042695        0.001696        0.001696
v  TempC                       21          73.049          22.031          22.031
v  TurbVisc           3.3306e-014       0.0050321       0.0019931       0.0019931
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2178:        0.20100E+01

===============================================================


 INSTANT    0.217900000E+04   TIME STEP NUMBER            2179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.12609E-01 0.89292E+00
   Friction velocity        uk    :  0.12609E-01 0.89292E+00
   Dimensionless distance   yplus :  0.10151E+00 0.71886E+01
   Friction thermal sca.    tstar : -0.65992E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75739E-01 0.53635E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10416E-01      33   0.25724E-03   0.48257E+01 0.18709E+03 
c  Velocity[X]                                      0.17198E+01 
c  Velocity[Y]                                      0.31059E+01 
c  Velocity[Z]                                      0.57885E-30 
c  Pressure     0.13488E-06     520   0.97604E-08   0.13254E+00 0.81740E+03 
c  nu_tilda     0.75819E-05      33   0.51951E-05   0.68348E-06 0.21424E+03 
c  TempC        0.41891E+02      27   0.32736E-03   0.41864E+01 0.24208E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0648          9.7462          4.5729          4.5729
v  Velocity[Y]            -3.0622          7.2001         0.18703         0.18703
v  Velocity[Z]       -6.9287e-015     6.5712e-015    -1.5643e-017    -1.5643e-017
v  ǁVelocityǁ         0.0023129          9.7475           5.128           5.128
v  Pressure               -27.783          24.196         -4.2355         -4.2355
v  nu_tilda           4.4121e-007       0.0042695       0.0016964       0.0016964
v  TempC                       21          73.049          22.031          22.031
v  TurbVisc           3.3311e-014       0.0050321       0.0019935       0.0019935
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2179:        0.21930E+01

===============================================================


 INSTANT    0.218000000E+04   TIME STEP NUMBER            2180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54037E-02 0.89227E+00
   Friction velocity        uk    :  0.54037E-02 0.89227E+00
   Dimensionless distance   yplus :  0.43503E-01 0.71834E+01
   Friction thermal sca.    tstar : -0.61702E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32458E-01 0.53596E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10417E-01      33   0.20579E-03   0.48278E+01 0.18711E+03 
c  Velocity[X]                                      0.17323E+01 
c  Velocity[Y]                                      0.30956E+01 
c  Velocity[Z]                                      0.75564E-30 
c  Pressure     0.94981E-07     442   0.92858E-08   0.93313E-01 0.65304E+03 
c  nu_tilda     0.75841E-05      33   0.14499E-04   0.68377E-06 0.21426E+03 
c  TempC        0.41898E+02      27   0.32259E-03   0.57297E+01 0.29040E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0698          9.7452          4.5729          4.5729
v  Velocity[Y]            -3.0624          7.2253         0.18732         0.18732
v  Velocity[Z]       -6.9287e-015     6.8355e-015    -1.5632e-017    -1.5632e-017
v  ǁVelocityǁ          0.002537          9.7464          5.1279          5.1279
v  Pressure               -27.799          24.256         -4.2181         -4.2181
v  nu_tilda           4.4122e-007       0.0042695       0.0016966       0.0016966
v  TempC                       21          73.049          22.031          22.031
v  TurbVisc           3.3338e-014       0.0050321       0.0019939       0.0019939
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2180:        0.20070E+01

===============================================================


 INSTANT    0.218100000E+04   TIME STEP NUMBER            2181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.91823E-02 0.89377E+00
   Friction velocity        uk    :  0.91823E-02 0.89377E+00
   Dimensionless distance   yplus :  0.73924E-01 0.71955E+01
   Friction thermal sca.    tstar : -0.61203E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55156E-01 0.53686E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10419E-01      33   0.24290E-03   0.47972E+01 0.18708E+03 
c  Velocity[X]                                      0.16848E+01 
c  Velocity[Y]                                      0.31123E+01 
c  Velocity[Z]                                      0.74481E-30 
c  Pressure     0.89232E-07     520   0.98072E-08   0.87954E-01 0.13274E+04 
c  nu_tilda     0.75862E-05      33   0.52063E-05   0.68398E-06 0.21428E+03 
c  TempC        0.41904E+02      27   0.31259E-03   0.65038E+01 0.28731E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0747          9.7441          4.5729          4.5729
v  Velocity[Y]            -3.0625          7.2368          0.1876          0.1876
v  Velocity[Z]       -6.9287e-015     7.3451e-015    -1.5625e-017    -1.5625e-017
v  ǁVelocityǁ         0.0026673          9.7453          5.1278          5.1278
v  Pressure               -27.737          24.379         -4.1509         -4.1509
v  nu_tilda           4.4114e-007       0.0042695        0.001697        0.001697
v  TempC                       21          73.051          22.031          22.031
v  TurbVisc           3.3341e-014       0.0050321       0.0019943       0.0019943
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2181:        0.21770E+01

===============================================================


 INSTANT    0.218200000E+04   TIME STEP NUMBER            2182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13405E-01 0.89325E+00
   Friction velocity        uk    :  0.13405E-01 0.89325E+00
   Dimensionless distance   yplus :  0.10792E+00 0.71913E+01
   Friction thermal sca.    tstar : -0.59719E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80519E-01 0.53655E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10420E-01      33   0.25385E-03   0.48223E+01 0.18717E+03 
c  Velocity[X]                                      0.17171E+01 
c  Velocity[Y]                                      0.31052E+01 
c  Velocity[Z]                                      0.90286E-30 
c  Pressure     0.11468E-06     505   0.91873E-08   0.11286E+00 0.14922E+04 
c  nu_tilda     0.75884E-05      33   0.14489E-04   0.68430E-06 0.21431E+03 
c  TempC        0.41911E+02      27   0.26847E-03   0.56666E+01 0.26560E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0795           9.743          4.5729          4.5729
v  Velocity[Y]            -3.0626          7.2034         0.18789         0.18789
v  Velocity[Z]       -6.9287e-015     7.2637e-015     -1.563e-017     -1.563e-017
v  ǁVelocityǁ         0.0023081          9.7443          5.1277          5.1277
v  Pressure                -27.78          24.185         -4.1858         -4.1858
v  nu_tilda           4.4119e-007       0.0042695       0.0016973       0.0016973
v  TempC                       21           73.05          22.031          22.031
v  TurbVisc           3.3318e-014       0.0050321       0.0019947       0.0019947
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2182:        0.21510E+01

===============================================================


 INSTANT    0.218300000E+04   TIME STEP NUMBER            2183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.54169E-02 0.89203E+00
   Friction velocity        uk    :  0.54169E-02 0.89203E+00
   Dimensionless distance   yplus :  0.43610E-01 0.71815E+01
   Friction thermal sca.    tstar : -0.61680E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32538E-01 0.53582E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10422E-01      33   0.28072E-03   0.48201E+01 0.18718E+03 
c  Velocity[X]                                      0.17209E+01 
c  Velocity[Y]                                      0.30991E+01 
c  Velocity[Z]                                      0.84894E-30 
c  Pressure     0.11058E-06     585   0.94261E-08   0.10882E+00 0.19290E+04 
c  nu_tilda     0.75906E-05      33   0.52000E-05   0.68456E-06 0.21434E+03 
c  TempC        0.41918E+02      27   0.36829E-03   0.38090E+01 0.23762E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0843          9.7419          4.5729          4.5729
v  Velocity[Y]            -3.0625          7.2264         0.18817         0.18817
v  Velocity[Z]       -6.9287e-015     7.6931e-015    -1.5634e-017    -1.5634e-017
v  ǁVelocityǁ          0.002534          9.7432          5.1276          5.1276
v  Pressure               -27.696          24.425         -4.0972         -4.0972
v  nu_tilda           4.4122e-007       0.0042695       0.0016977       0.0016977
v  TempC                       21           73.05          22.032          22.032
v  TurbVisc           3.3334e-014       0.0050321       0.0019951       0.0019951
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2183:        0.23410E+01

===============================================================


 INSTANT    0.218400000E+04   TIME STEP NUMBER            2184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14417E-01 0.89297E+00
   Friction velocity        uk    :  0.14417E-01 0.89297E+00
   Dimensionless distance   yplus :  0.11607E+00 0.71890E+01
   Friction thermal sca.    tstar : -0.60241E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86600E-01 0.53638E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10424E-01      33   0.26302E-03   0.48403E+01 0.18731E+03 
c  Velocity[X]                                      0.17288E+01 
c  Velocity[Y]                                      0.31115E+01 
c  Velocity[Z]                                      0.65605E-30 
c  Pressure     0.10942E-06     521   0.94685E-08   0.10849E+00 0.12713E+04 
c  nu_tilda     0.75927E-05      33   0.14490E-04   0.68487E-06 0.21437E+03 
c  TempC        0.41924E+02      27   0.36251E-03   0.65141E+01 0.28363E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0891          9.7409          4.5729          4.5729
v  Velocity[Y]            -3.0626          7.2021         0.18845         0.18845
v  Velocity[Z]       -6.9287e-015     7.9265e-015    -1.5639e-017    -1.5639e-017
v  ǁVelocityǁ         0.0022981          9.7422          5.1275          5.1275
v  Pressure               -27.699          24.272         -4.1221         -4.1221
v  nu_tilda           4.4118e-007       0.0042695        0.001698        0.001698
v  TempC                       21          73.049          22.032          22.032
v  TurbVisc           3.3342e-014       0.0050321       0.0019955       0.0019955
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2184:        0.22170E+01

===============================================================


 INSTANT    0.218500000E+04   TIME STEP NUMBER            2185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13164E-01 0.89213E+00
   Friction velocity        uk    :  0.13164E-01 0.89213E+00
   Dimensionless distance   yplus :  0.10598E+00 0.71823E+01
   Friction thermal sca.    tstar : -0.61490E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79074E-01 0.53588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10425E-01      33   0.19772E-03   0.48136E+01 0.18716E+03 
c  Velocity[X]                                      0.17161E+01 
c  Velocity[Y]                                      0.30975E+01 
c  Velocity[Z]                                      0.66165E-30 
c  Pressure     0.11153E-06     538   0.97231E-08   0.10779E+00 0.15210E+04 
c  nu_tilda     0.75949E-05      33   0.52096E-05   0.68509E-06 0.21439E+03 
c  TempC        0.41931E+02      27   0.32330E-03   0.56005E+01 0.27626E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0938          9.7398          4.5729          4.5729
v  Velocity[Y]            -3.0628          7.2238         0.18873         0.18873
v  Velocity[Z]       -6.9287e-015     8.0589e-015    -1.5639e-017    -1.5639e-017
v  ǁVelocityǁ         0.0024814          9.7411          5.1274          5.1274
v  Pressure               -27.649          24.444         -4.0494         -4.0494
v  nu_tilda           4.4112e-007       0.0042695       0.0016984       0.0016984
v  TempC                       21           73.05          22.032          22.032
v  TurbVisc           3.3331e-014       0.0050321       0.0019959       0.0019959
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2185:        0.22520E+01

===============================================================


 INSTANT    0.218600000E+04   TIME STEP NUMBER            2186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.89580E-02 0.89355E+00
   Friction velocity        uk    :  0.89580E-02 0.89355E+00
   Dimensionless distance   yplus :  0.72118E-01 0.71937E+01
   Friction thermal sca.    tstar : -0.61609E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53808E-01 0.53673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10427E-01      33   0.25726E-03   0.48022E+01 0.18711E+03 
c  Velocity[X]                                      0.17121E+01 
c  Velocity[Y]                                      0.30902E+01 
c  Velocity[Z]                                      0.70476E-30 
c  Pressure     0.91486E-07     360   0.93019E-08   0.90015E-01 0.66637E+03 
c  nu_tilda     0.75971E-05      33   0.14478E-04   0.68535E-06 0.21441E+03 
c  TempC        0.41937E+02      27   0.28592E-03   0.47757E+01 0.25941E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0987          9.7387          4.5729          4.5729
v  Velocity[Y]             -3.063           7.232         0.18901         0.18901
v  Velocity[Z]       -6.9287e-015     8.0255e-015     -1.565e-017     -1.565e-017
v  ǁVelocityǁ         0.0026706            9.74          5.1273          5.1273
v  Pressure               -27.658           24.43         -4.0452         -4.0452
v  nu_tilda           4.4105e-007       0.0042695       0.0016987       0.0016987
v  TempC                       21          73.049          22.032          22.032
v  TurbVisc            3.331e-014       0.0050321       0.0019963       0.0019963
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2186:        0.18270E+01

===============================================================


 INSTANT    0.218700000E+04   TIME STEP NUMBER            2187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11885E-01 0.89309E+00
   Friction velocity        uk    :  0.11885E-01 0.89309E+00
   Dimensionless distance   yplus :  0.95679E-01 0.71900E+01
   Friction thermal sca.    tstar : -0.65472E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71387E-01 0.53645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10428E-01      33   0.23995E-03   0.48194E+01 0.18726E+03 
c  Velocity[X]                                      0.17106E+01 
c  Velocity[Y]                                      0.31088E+01 
c  Velocity[Z]                                      0.84831E-30 
c  Pressure     0.11372E-06     489   0.92440E-08   0.11265E+00 0.75880E+03 
c  nu_tilda     0.75992E-05      33   0.52043E-05   0.68557E-06 0.21443E+03 
c  TempC        0.41944E+02      27   0.29697E-03   0.49197E+01 0.25311E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1036          9.7376          4.5729          4.5729
v  Velocity[Y]            -3.0631          7.2054         0.18929         0.18929
v  Velocity[Z]       -6.9287e-015     8.1879e-015    -1.5647e-017    -1.5647e-017
v  ǁVelocityǁ         0.0024026          9.7389          5.1272          5.1272
v  Pressure               -27.605          24.418         -4.0087         -4.0087
v  nu_tilda           4.4108e-007       0.0042695       0.0016991       0.0016991
v  TempC                       21           73.05          22.032          22.032
v  TurbVisc            3.329e-014       0.0050321       0.0019967       0.0019967
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2187:        0.21060E+01

===============================================================


 INSTANT    0.218800000E+04   TIME STEP NUMBER            2188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13206E-01 0.89163E+00
   Friction velocity        uk    :  0.13206E-01 0.89163E+00
   Dimensionless distance   yplus :  0.10631E+00 0.71783E+01
   Friction thermal sca.    tstar : -0.71560E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79322E-01 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10430E-01      33   0.25918E-03   0.47964E+01 0.18714E+03 
c  Velocity[X]                                      0.17051E+01 
c  Velocity[Y]                                      0.30913E+01 
c  Velocity[Z]                                      0.82593E-30 
c  Pressure     0.10289E-06     409   0.99923E-08   0.99530E-01 0.62645E+03 
c  nu_tilda     0.76014E-05      33   0.14482E-04   0.68587E-06 0.21446E+03 
c  TempC        0.41951E+02      27   0.38768E-03   0.41842E+01 0.23852E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1086          9.7365          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.2195         0.18957         0.18957
v  Velocity[Z]       -6.9287e-015     8.3017e-015    -1.5661e-017    -1.5661e-017
v  ǁVelocityǁ         0.0025967          9.7379          5.1271          5.1271
v  Pressure               -27.614          24.458          -3.993          -3.993
v  nu_tilda           4.4113e-007       0.0042695       0.0016993       0.0016993
v  TempC                       21          73.049          22.032          22.032
v  TurbVisc             3.33e-014       0.0050321       0.0019971       0.0019971
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2188:        0.19340E+01

===============================================================


 INSTANT    0.218900000E+04   TIME STEP NUMBER            2189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11940E-01 0.89288E+00
   Friction velocity        uk    :  0.11940E-01 0.89288E+00
   Dimensionless distance   yplus :  0.96127E-01 0.71883E+01
   Friction thermal sca.    tstar : -0.78371E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71721E-01 0.53633E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10432E-01      33   0.27949E-03   0.48149E+01 0.18725E+03 
c  Velocity[X]                                      0.17265E+01 
c  Velocity[Y]                                      0.30884E+01 
c  Velocity[Z]                                      0.80703E-30 
c  Pressure     0.10588E-06     505   0.95955E-08   0.10541E+00 0.82557E+03 
c  nu_tilda     0.76035E-05      33   0.52103E-05   0.68610E-06 0.21449E+03 
c  TempC        0.41957E+02      27   0.26221E-03   0.59838E+01 0.28758E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1133          9.7355          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.2017         0.18985         0.18985
v  Velocity[Z]       -6.9287e-015     8.3125e-015    -1.5672e-017    -1.5672e-017
v  ǁVelocityǁ         0.0024189          9.7368          5.1269          5.1269
v  Pressure               -27.557          24.464         -3.9515         -3.9515
v  nu_tilda            4.412e-007       0.0042695       0.0016997       0.0016997
v  TempC                       21           73.05          22.032          22.032
v  TurbVisc           3.3314e-014       0.0050321       0.0019975       0.0019975
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2189:        0.21460E+01

===============================================================


 INSTANT    0.219000000E+04   TIME STEP NUMBER            2190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11746E-01 0.89212E+00
   Friction velocity        uk    :  0.11746E-01 0.89212E+00
   Dimensionless distance   yplus :  0.94562E-01 0.71822E+01
   Friction thermal sca.    tstar : -0.89142E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70554E-01 0.53587E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10433E-01      33   0.20430E-03   0.48238E+01 0.18732E+03 
c  Velocity[X]                                      0.17196E+01 
c  Velocity[Y]                                      0.31042E+01 
c  Velocity[Z]                                      0.67080E-30 
c  Pressure     0.96182E-07     442   0.92471E-08   0.94500E-01 0.68110E+03 
c  nu_tilda     0.76057E-05      33   0.14469E-04   0.68639E-06 0.21451E+03 
c  TempC        0.41964E+02      27   0.37108E-03   0.47079E+01 0.23982E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1182          9.7344          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.2247         0.19012         0.19012
v  Velocity[Z]       -6.9287e-015     8.2962e-015    -1.5686e-017    -1.5686e-017
v  ǁVelocityǁ         0.0027084          9.7357          5.1268          5.1268
v  Pressure               -27.569          24.542         -3.9287         -3.9287
v  nu_tilda           4.4122e-007       0.0042695          0.0017          0.0017
v  TempC                       21          73.049          22.032          22.032
v  TurbVisc           3.3336e-014       0.0050321       0.0019979       0.0019979
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2190:        0.20030E+01

===============================================================


 INSTANT    0.219100000E+04   TIME STEP NUMBER            2191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.76402E-02 0.89358E+00
   Friction velocity        uk    :  0.76402E-02 0.89358E+00
   Dimensionless distance   yplus :  0.61509E-01 0.71939E+01
   Friction thermal sca.    tstar : -0.10306E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45893E-01 0.53675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10435E-01      33   0.25382E-03   0.47946E+01 0.18722E+03 
c  Velocity[X]                                      0.16955E+01 
c  Velocity[Y]                                      0.30991E+01 
c  Velocity[Z]                                      0.11656E-29 
c  Pressure     0.11596E-06     506   0.95526E-08   0.11179E+00 0.10331E+04 
c  nu_tilda     0.76078E-05      33   0.52088E-05   0.68661E-06 0.21453E+03 
c  TempC        0.41971E+02      27   0.35040E-03   0.60456E+01 0.28703E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.123          9.7333          4.5729          4.5729
v  Velocity[Y]            -3.0634          7.2319          0.1904          0.1904
v  Velocity[Z]       -7.1024e-015     8.3553e-015    -1.5709e-017    -1.5709e-017
v  ǁVelocityǁ         0.0026355          9.7346          5.1267          5.1267
v  Pressure               -27.516          24.612          -3.876          -3.876
v  nu_tilda           4.4116e-007       0.0042695       0.0017004       0.0017004
v  TempC                       21          73.051          22.033          22.033
v  TurbVisc           3.3341e-014       0.0050321       0.0019983       0.0019983
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2191:        0.21480E+01

===============================================================


 INSTANT    0.219200000E+04   TIME STEP NUMBER            2192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30167E-02 0.89331E+00
   Friction velocity        uk    :  0.30167E-02 0.89331E+00
   Dimensionless distance   yplus :  0.24287E-01 0.71918E+01
   Friction thermal sca.    tstar : -0.13011E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18121E-01 0.53659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10436E-01      33   0.25776E-03   0.48283E+01 0.18733E+03 
c  Velocity[X]                                      0.17422E+01 
c  Velocity[Y]                                      0.30860E+01 
c  Velocity[Z]                                      0.84775E-30 
c  Pressure     0.10544E-06     490   0.94838E-08   0.10505E+00 0.11123E+04 
c  nu_tilda     0.76100E-05      33   0.14470E-04   0.68687E-06 0.21455E+03 
c  TempC        0.41977E+02      27   0.31590E-03   0.60678E+01 0.28450E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1278          9.7322          4.5729          4.5729
v  Velocity[Y]            -3.0636           7.204         0.19068         0.19068
v  Velocity[Z]       -6.9287e-015     8.4375e-015    -1.5723e-017    -1.5723e-017
v  ǁVelocityǁ         0.0023788          9.7336          5.1266          5.1266
v  Pressure               -27.524          24.487         -3.8957         -3.8957
v  nu_tilda           4.4111e-007       0.0042695       0.0017007       0.0017007
v  TempC                       21           73.05          22.033          22.033
v  TurbVisc           3.3324e-014       0.0050321       0.0019987       0.0019987
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2192:        0.21210E+01

===============================================================


 INSTANT    0.219300000E+04   TIME STEP NUMBER            2193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.82484E-02 0.89193E+00
   Friction velocity        uk    :  0.82484E-02 0.89193E+00
   Dimensionless distance   yplus :  0.66405E-01 0.71806E+01
   Friction thermal sca.    tstar : -0.20175E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49546E-01 0.53576E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10438E-01      33   0.24719E-03   0.48020E+01 0.18730E+03 
c  Velocity[X]                                      0.16995E+01 
c  Velocity[Y]                                      0.31025E+01 
c  Velocity[Z]                                      0.84527E-30 
c  Pressure     0.89042E-07     537   0.94533E-08   0.87416E-01 0.17075E+04 
c  nu_tilda     0.76122E-05      33   0.52114E-05   0.68708E-06 0.21457E+03 
c  TempC        0.41984E+02      27   0.33062E-03   0.56086E+01 0.26912E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1324          9.7312          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.2254         0.19095         0.19095
v  Velocity[Z]       -7.3075e-015     8.3938e-015    -1.5747e-017    -1.5747e-017
v  ǁVelocityǁ         0.0026024          9.7325          5.1265          5.1265
v  Pressure               -27.472          24.688         -3.8152         -3.8152
v  nu_tilda           4.4105e-007       0.0042695       0.0017011       0.0017011
v  TempC                       21           73.05          22.033          22.033
v  TurbVisc           3.3308e-014       0.0050321       0.0019991       0.0019991
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2193:        0.22210E+01

===============================================================


 INSTANT    0.219400000E+04   TIME STEP NUMBER            2194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.51829E-02 0.89284E+00
   Friction velocity        uk    :  0.51829E-02 0.89284E+00
   Dimensionless distance   yplus :  0.41726E-01 0.71879E+01
   Friction thermal sca.    tstar : -0.30423E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31132E-01 0.53630E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10439E-01      33   0.26592E-03   0.47979E+01 0.18723E+03 
c  Velocity[X]                                      0.17109E+01 
c  Velocity[Y]                                      0.30870E+01 
c  Velocity[Z]                                      0.83929E-30 
c  Pressure     0.11148E-06     506   0.95040E-08   0.10935E+00 0.13660E+04 
c  nu_tilda     0.76143E-05      33   0.14459E-04   0.68737E-06 0.21460E+03 
c  TempC        0.41990E+02      27   0.21692E-03   0.52527E+01 0.26335E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1371          9.7301          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.1978         0.19122         0.19122
v  Velocity[Z]        -7.519e-015     8.3954e-015    -1.5775e-017    -1.5775e-017
v  ǁVelocityǁ         0.0023356          9.7314          5.1264          5.1264
v  Pressure               -27.479          24.515         -3.8453         -3.8453
v  nu_tilda           4.4109e-007       0.0042695       0.0017014       0.0017014
v  TempC                       21          73.048          22.033          22.033
v  TurbVisc           3.3289e-014       0.0050321       0.0019995       0.0019995
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2194:        0.21390E+01

===============================================================


 INSTANT    0.219500000E+04   TIME STEP NUMBER            2195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.45603E-02 0.89218E+00
   Friction velocity        uk    :  0.45603E-02 0.89218E+00
   Dimensionless distance   yplus :  0.36714E-01 0.71827E+01
   Friction thermal sca.    tstar : -0.14985E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27392E-01 0.53591E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10441E-01      33   0.27402E-03   0.48117E+01 0.18733E+03 
c  Velocity[X]                                      0.17254E+01 
c  Velocity[Y]                                      0.30863E+01 
c  Velocity[Z]                                      0.98594E-30 
c  Pressure     0.11569E-06     552   0.92233E-08   0.11359E+00 0.19687E+04 
c  nu_tilda     0.76165E-05      33   0.52138E-05   0.68759E-06 0.21462E+03 
c  TempC        0.41997E+02      27   0.37301E-03   0.38165E+01 0.24178E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1417          9.7291          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.2252          0.1915          0.1915
v  Velocity[Z]       -7.9619e-015     8.4049e-015    -1.5809e-017    -1.5809e-017
v  ǁVelocityǁ         0.0026071          9.7303          5.1263          5.1263
v  Pressure               -27.431          24.756         -3.7547         -3.7547
v  nu_tilda           4.4114e-007       0.0042695       0.0017017       0.0017017
v  TempC                       21           73.05          22.033          22.033
v  TurbVisc           3.3304e-014       0.0050321       0.0019999       0.0019999
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2195:        0.22580E+01

===============================================================


 INSTANT    0.219600000E+04   TIME STEP NUMBER            2196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89052E-02 0.89337E+00
   Friction velocity        uk    :  0.89052E-02 0.89337E+00
   Dimensionless distance   yplus :  0.71693E-01 0.71922E+01
   Friction thermal sca.    tstar : -0.11374E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53491E-01 0.53662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10442E-01      33   0.24805E-03   0.48029E+01 0.18735E+03 
c  Velocity[X]                                      0.17033E+01 
c  Velocity[Y]                                      0.30996E+01 
c  Velocity[Z]                                      0.82065E-30 
c  Pressure     0.95570E-07     426   0.96973E-08   0.93666E-01 0.83131E+03 
c  nu_tilda     0.76186E-05      33   0.14455E-04   0.68783E-06 0.21464E+03 
c  TempC        0.42003E+02      27   0.33210E-03   0.78994E+01 0.31660E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1466           9.728          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.2306         0.19177         0.19177
v  Velocity[Z]        -8.511e-015     8.4759e-015    -1.5831e-017    -1.5831e-017
v  ǁVelocityǁ         0.0027129          9.7292          5.1262          5.1262
v  Pressure                -27.44          24.701         -3.7621         -3.7621
v  nu_tilda           4.4111e-007       0.0042695        0.001702        0.001702
v  TempC                       21           73.05          22.033          22.033
v  TurbVisc           3.3317e-014       0.0050321       0.0020003       0.0020003
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2196:        0.20600E+01

===============================================================


 INSTANT    0.219700000E+04   TIME STEP NUMBER            2197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18049E-02 0.89290E+00
   Friction velocity        uk    :  0.18049E-02 0.89290E+00
   Dimensionless distance   yplus :  0.14531E-01 0.71885E+01
   Friction thermal sca.    tstar : -0.31952E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10841E-01 0.53634E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10444E-01      33   0.24348E-03   0.48090E+01 0.18734E+03 
c  Velocity[X]                                      0.17214E+01 
c  Velocity[Y]                                      0.30876E+01 
c  Velocity[Z]                                      0.69244E-30 
c  Pressure     0.11903E-06     474   0.96448E-08   0.11738E+00 0.74983E+03 
c  nu_tilda     0.76208E-05      33   0.52135E-05   0.68802E-06 0.21466E+03 
c  TempC        0.42010E+02      27   0.32753E-03   0.51792E+01 0.26678E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1514           9.727          4.5729          4.5729
v  Velocity[Y]            -3.0639          7.2003         0.19204         0.19204
v  Velocity[Z]       -8.9677e-015     8.4259e-015    -1.5866e-017    -1.5866e-017
v  ǁVelocityǁ         0.0023862          9.7282          5.1261          5.1261
v  Pressure               -27.384          24.669          -3.728          -3.728
v  nu_tilda           4.4115e-007       0.0042695       0.0017024       0.0017024
v  TempC                       21           73.05          22.033          22.033
v  TurbVisc           3.3309e-014       0.0050321       0.0020006       0.0020006
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2197:        0.20720E+01

===============================================================


 INSTANT    0.219800000E+04   TIME STEP NUMBER            2198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.45370E-02 0.89166E+00
   Friction velocity        uk    :  0.45370E-02 0.89166E+00
   Dimensionless distance   yplus :  0.36526E-01 0.71785E+01
   Friction thermal sca.    tstar : -0.12611E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27253E-01 0.53559E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10446E-01      33   0.25118E-03   0.48044E+01 0.18731E+03 
c  Velocity[X]                                      0.17245E+01 
c  Velocity[Y]                                      0.30800E+01 
c  Velocity[Z]                                      0.76081E-30 
c  Pressure     0.93985E-07     440   0.97301E-08   0.92269E-01 0.65244E+03 
c  nu_tilda     0.76229E-05      33   0.14452E-04   0.68828E-06 0.21468E+03 
c  TempC        0.42017E+02      27   0.30339E-03   0.52981E+01 0.27567E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1563          9.7259          4.5729          4.5729
v  Velocity[Y]            -3.0641          7.2207         0.19231         0.19231
v  Velocity[Z]       -8.9776e-015     8.3421e-015     -1.589e-017     -1.589e-017
v  ǁVelocityǁ         0.0026291          9.7271           5.126           5.126
v  Pressure               -27.395          24.738         -3.7094         -3.7094
v  nu_tilda           4.4119e-007       0.0042695       0.0017027       0.0017027
v  TempC                       21           73.05          22.033          22.033
v  TurbVisc           3.3319e-014       0.0050321        0.002001        0.002001
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2198:        0.22600E+01

===============================================================


 INSTANT    0.219900000E+04   TIME STEP NUMBER            2199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57285E-02 0.89276E+00
   Friction velocity        uk    :  0.57285E-02 0.89276E+00
   Dimensionless distance   yplus :  0.46119E-01 0.71873E+01
   Friction thermal sca.    tstar : -0.10089E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34410E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10447E-01      33   0.25507E-03   0.48030E+01 0.18739E+03 
c  Velocity[X]                                      0.17044E+01 
c  Velocity[Y]                                      0.30985E+01 
c  Velocity[Z]                                      0.87712E-30 
c  Pressure     0.10602E-06     489   0.98412E-08   0.10502E+00 0.84352E+03 
c  nu_tilda     0.76251E-05      33   0.52217E-05   0.68850E-06 0.21470E+03 
c  TempC        0.42023E+02      27   0.28527E-03   0.63278E+01 0.28448E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1609          9.7249          4.5729          4.5729
v  Velocity[Y]            -3.0641          7.2008         0.19258         0.19258
v  Velocity[Z]       -9.5658e-015     8.2228e-015     -1.591e-017     -1.591e-017
v  ǁVelocityǁ         0.0023979           9.726          5.1259          5.1259
v  Pressure               -27.341          24.746         -3.6667         -3.6667
v  nu_tilda           4.4124e-007       0.0042695       0.0017031       0.0017031
v  TempC                       21           73.05          22.034          22.034
v  TurbVisc           3.3333e-014       0.0050321       0.0020014       0.0020014
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2199:        0.22690E+01

===============================================================


 INSTANT    0.220000000E+04   TIME STEP NUMBER            2200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10447E-02 0.89194E+00
   Friction velocity        uk    :  0.10447E-02 0.89194E+00
   Dimensionless distance   yplus :  0.84104E-02 0.71807E+01
   Friction thermal sca.    tstar : -0.54962E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62751E-02 0.53576E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10449E-01      33   0.21210E-03   0.47899E+01 0.18730E+03 
c  Velocity[X]                                      0.17082E+01 
c  Velocity[Y]                                      0.30818E+01 
c  Velocity[Z]                                      0.75766E-30 
c  Pressure     0.10628E-06     360   0.92337E-08   0.10273E+00 0.63258E+03 
c  nu_tilda     0.76272E-05      33   0.14442E-04   0.68878E-06 0.21473E+03 
c  TempC        0.42030E+02      27   0.31262E-03   0.45679E+01 0.23837E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1656          9.7238          4.5729          4.5729
v  Velocity[Y]            -3.0642          7.2197         0.19285         0.19285
v  Velocity[Z]       -9.7412e-015     8.1398e-015    -1.5935e-017    -1.5935e-017
v  ǁVelocityǁ         0.0025541          9.7249          5.1258          5.1258
v  Pressure                -27.35           24.77         -3.6563         -3.6563
v  nu_tilda           4.4116e-007       0.0042695       0.0017033       0.0017033
v  TempC                       21          73.049          22.034          22.034
v  TurbVisc           3.3348e-014       0.0050321       0.0020018       0.0020018
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2200:        0.18180E+01

===============================================================


 INSTANT    0.220100000E+04   TIME STEP NUMBER            2201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.35444E-02 0.89355E+00
   Friction velocity        uk    :  0.35444E-02 0.89355E+00
   Dimensionless distance   yplus :  0.28535E-01 0.71937E+01
   Friction thermal sca.    tstar : -0.16371E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21290E-01 0.53673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10450E-01      33   0.27939E-03   0.47894E+01 0.18739E+03 
c  Velocity[X]                                      0.17041E+01 
c  Velocity[Y]                                      0.30853E+01 
c  Velocity[Z]                                      0.10035E-29 
c  Pressure     0.96488E-07     521   0.98443E-08   0.95207E-01 0.13845E+04 
c  nu_tilda     0.76293E-05      33   0.52158E-05   0.68900E-06 0.21475E+03 
c  TempC        0.42036E+02      27   0.29374E-03   0.44811E+01 0.26137E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1703          9.7227          4.5729          4.5729
v  Velocity[Y]            -3.0641          7.2329         0.19312         0.19312
v  Velocity[Z]       -1.0047e-014      7.965e-015     -1.596e-017     -1.596e-017
v  ǁVelocityǁ         0.0026896          9.7238          5.1256          5.1256
v  Pressure               -27.298          24.902         -3.5881         -3.5881
v  nu_tilda           4.4101e-007       0.0042695       0.0017037       0.0017037
v  TempC                       21           73.05          22.034          22.034
v  TurbVisc           3.3323e-014       0.0050321       0.0020022       0.0020022
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2201:        0.21960E+01

===============================================================


 INSTANT    0.220200000E+04   TIME STEP NUMBER            2202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10210E-01 0.89316E+00
   Friction velocity        uk    :  0.10210E-01 0.89316E+00
   Dimensionless distance   yplus :  0.82198E-01 0.71905E+01
   Friction thermal sca.    tstar : -0.59915E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61329E-01 0.53649E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10452E-01      33   0.25167E-03   0.48233E+01 0.18754E+03 
c  Velocity[X]                                      0.17269E+01 
c  Velocity[Y]                                      0.30964E+01 
c  Velocity[Z]                                      0.76471E-30 
c  Pressure     0.10845E-06     521   0.95090E-08   0.10792E+00 0.13275E+04 
c  nu_tilda     0.76315E-05      33   0.14442E-04   0.68923E-06 0.21476E+03 
c  TempC        0.42043E+02      27   0.33622E-03   0.50926E+01 0.27215E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.175          9.7217          4.5729          4.5729
v  Velocity[Y]            -3.0641           7.204         0.19338         0.19338
v  Velocity[Z]       -9.6746e-015     7.7755e-015    -1.5972e-017    -1.5972e-017
v  ǁVelocityǁ         0.0024409          9.7228          5.1255          5.1255
v  Pressure               -27.306          24.744         -3.6176         -3.6176
v  nu_tilda           4.4103e-007       0.0042695        0.001704        0.001704
v  TempC                       21          73.049          22.034          22.034
v  TurbVisc           3.3278e-014       0.0050321       0.0020026       0.0020026
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2202:        0.21830E+01

===============================================================


 INSTANT    0.220300000E+04   TIME STEP NUMBER            2203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11609E-01 0.89177E+00
   Friction velocity        uk    :  0.11609E-01 0.89177E+00
   Dimensionless distance   yplus :  0.93463E-01 0.71793E+01
   Friction thermal sca.    tstar : -0.60413E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69734E-01 0.53566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10453E-01      33   0.24872E-03   0.47910E+01 0.18736E+03 
c  Velocity[X]                                      0.17092E+01 
c  Velocity[Y]                                      0.30818E+01 
c  Velocity[Z]                                      0.74416E-30 
c  Pressure     0.10983E-06     553   0.99561E-08   0.10589E+00 0.16660E+04 
c  nu_tilda     0.76336E-05      33   0.52252E-05   0.68941E-06 0.21478E+03 
c  TempC        0.42049E+02      27   0.28599E-03   0.46620E+01 0.25380E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1795          9.7206          4.5729          4.5729
v  Velocity[Y]            -3.0643          7.2203         0.19365         0.19365
v  Velocity[Z]       -1.0064e-014     7.5564e-015    -1.5995e-017    -1.5995e-017
v  ǁVelocityǁ         0.0025561          9.7218          5.1254          5.1254
v  Pressure               -27.258          24.932         -3.5396         -3.5396
v  nu_tilda           4.4109e-007       0.0042695       0.0017044       0.0017044
v  TempC                       21           73.05          22.034          22.034
v  TurbVisc           3.3283e-014       0.0050321        0.002003        0.002003
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2203:        0.22630E+01

===============================================================


 INSTANT    0.220400000E+04   TIME STEP NUMBER            2204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11345E-01 0.89285E+00
   Friction velocity        uk    :  0.11345E-01 0.89285E+00
   Dimensionless distance   yplus :  0.91338E-01 0.71881E+01
   Friction thermal sca.    tstar : -0.59904E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68148E-01 0.53631E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10455E-01      33   0.26182E-03   0.48077E+01 0.18743E+03 
c  Velocity[X]                                      0.17342E+01 
c  Velocity[Y]                                      0.30735E+01 
c  Velocity[Z]                                      0.74298E-30 
c  Pressure     0.98265E-07     505   0.94238E-08   0.97498E-01 0.12227E+04 
c  nu_tilda     0.76358E-05      33   0.14431E-04   0.68968E-06 0.21480E+03 
c  TempC        0.42056E+02      27   0.25331E-03   0.35300E+01 0.22331E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1841          9.7196          4.5729          4.5729
v  Velocity[Y]            -3.0644          7.1984         0.19392         0.19392
v  Velocity[Z]       -9.8854e-015     7.3742e-015    -1.6012e-017    -1.6012e-017
v  ǁVelocityǁ         0.0023235          9.7207          5.1253          5.1253
v  Pressure               -27.263           24.79         -3.5635         -3.5635
v  nu_tilda           4.4119e-007       0.0042695       0.0017047       0.0017047
v  TempC                       21          73.049          22.034          22.034
v  TurbVisc           3.3304e-014       0.0050321       0.0020034       0.0020034
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2204:        0.21550E+01

===============================================================


 INSTANT    0.220500000E+04   TIME STEP NUMBER            2205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12639E-01 0.89209E+00
   Friction velocity        uk    :  0.12639E-01 0.89209E+00
   Dimensionless distance   yplus :  0.10175E+00 0.71820E+01
   Friction thermal sca.    tstar : -0.60852E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75917E-01 0.53585E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10456E-01      33   0.24335E-03   0.47945E+01 0.18746E+03 
c  Velocity[X]                                      0.17020E+01 
c  Velocity[Y]                                      0.30925E+01 
c  Velocity[Z]                                      0.73093E-30 
c  Pressure     0.90891E-07     568   0.97250E-08   0.89218E-01 0.19320E+04 
c  nu_tilda     0.76379E-05      33   0.52175E-05   0.68990E-06 0.21483E+03 
c  TempC        0.42062E+02      27   0.35299E-03   0.57301E+01 0.27381E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1886          9.7185          4.5729          4.5729
v  Velocity[Y]            -3.0645          7.2234         0.19418         0.19418
v  Velocity[Z]       -9.8961e-015     7.1268e-015    -1.6029e-017    -1.6029e-017
v  ǁVelocityǁ          0.002636          9.7196          5.1252          5.1252
v  Pressure               -27.214          25.025         -3.4745         -3.4745
v  nu_tilda           4.4119e-007       0.0042695        0.001705        0.001705
v  TempC                       21           73.05          22.034          22.034
v  TurbVisc           3.3332e-014       0.0050321       0.0020038       0.0020038
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2205:        0.22900E+01

===============================================================


 INSTANT    0.220600000E+04   TIME STEP NUMBER            2206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12448E-01 0.89314E+00
   Friction velocity        uk    :  0.12448E-01 0.89314E+00
   Dimensionless distance   yplus :  0.10021E+00 0.71904E+01
   Friction thermal sca.    tstar : -0.59382E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74770E-01 0.53648E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10458E-01      33   0.25752E-03   0.47638E+01 0.18729E+03 
c  Velocity[X]                                      0.16875E+01 
c  Velocity[Y]                                      0.30763E+01 
c  Velocity[Z]                                      0.77941E-30 
c  Pressure     0.10531E-06     505   0.92429E-08   0.10194E+00 0.10377E+04 
c  nu_tilda     0.76400E-05      33   0.14431E-04   0.69015E-06 0.21484E+03 
c  TempC        0.42069E+02      27   0.25203E-03   0.69365E+01 0.30241E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1934          9.7174          4.5729          4.5729
v  Velocity[Y]            -3.0645          7.2265         0.19445         0.19445
v  Velocity[Z]        -9.704e-015      6.972e-015    -1.6036e-017    -1.6036e-017
v  ǁVelocityǁ         0.0026466          9.7186          5.1251          5.1251
v  Pressure               -27.223          24.922         -3.4925         -3.4925
v  nu_tilda           4.4117e-007       0.0042695       0.0017053       0.0017053
v  TempC                       21           73.05          22.035          22.035
v  TurbVisc           3.3333e-014       0.0050321       0.0020041       0.0020041
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2206:        0.21560E+01

===============================================================


 INSTANT    0.220700000E+04   TIME STEP NUMBER            2207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11608E-01 0.89296E+00
   Friction velocity        uk    :  0.11608E-01 0.89296E+00
   Dimensionless distance   yplus :  0.93455E-01 0.71890E+01
   Friction thermal sca.    tstar : -0.59692E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69728E-01 0.53638E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10459E-01      33   0.27691E-03   0.48048E+01 0.18750E+03 
c  Velocity[X]                                      0.17312E+01 
c  Velocity[Y]                                      0.30736E+01 
c  Velocity[Z]                                      0.86818E-30 
c  Pressure     0.11680E-06     552   0.94523E-08   0.11616E+00 0.96672E+03 
c  nu_tilda     0.76422E-05      33   0.52233E-05   0.69031E-06 0.21486E+03 
c  TempC        0.42075E+02      27   0.33093E-03   0.35413E+01 0.23309E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1982          9.7164          4.5729          4.5729
v  Velocity[Y]            -3.0645          7.2019         0.19471         0.19471
v  Velocity[Z]       -9.7876e-015     7.3047e-015    -1.6047e-017    -1.6047e-017
v  ǁVelocityǁ         0.0024631          9.7175          5.1249          5.1249
v  Pressure               -27.169          24.965         -3.4429         -3.4429
v  nu_tilda           4.4121e-007       0.0042695       0.0017057       0.0017057
v  TempC                       21           73.05          22.035          22.035
v  TurbVisc           3.3328e-014       0.0050321       0.0020045       0.0020045
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2207:        0.22590E+01

===============================================================


 INSTANT    0.220800000E+04   TIME STEP NUMBER            2208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13679E-01 0.89153E+00
   Friction velocity        uk    :  0.13679E-01 0.89153E+00
   Dimensionless distance   yplus :  0.11012E+00 0.71774E+01
   Friction thermal sca.    tstar : -0.60549E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82164E-01 0.53551E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10461E-01      33   0.25240E-03   0.48066E+01 0.18757E+03 
c  Velocity[X]                                      0.17183E+01 
c  Velocity[Y]                                      0.30883E+01 
c  Velocity[Z]                                      0.73201E-30 
c  Pressure     0.10134E-06     425   0.96294E-08   0.98688E-01 0.62357E+03 
c  nu_tilda     0.76443E-05      33   0.14422E-04   0.69055E-06 0.21487E+03 
c  TempC        0.42082E+02      27   0.33683E-03   0.67629E+01 0.29781E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2029          9.7153          4.5729          4.5729
v  Velocity[Y]            -3.0644          7.2206         0.19497         0.19497
v  Velocity[Z]       -9.8486e-015     7.2218e-015    -1.6057e-017    -1.6057e-017
v  ǁVelocityǁ         0.0026743          9.7165          5.1248          5.1248
v  Pressure               -27.181          25.002         -3.4309         -3.4309
v  nu_tilda           4.4116e-007       0.0042695        0.001706        0.001706
v  TempC                       21           73.05          22.035          22.035
v  TurbVisc           3.3339e-014       0.0050321       0.0020049       0.0020049
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2208:        0.19790E+01

===============================================================


 INSTANT    0.220900000E+04   TIME STEP NUMBER            2209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.77331E-02 0.89265E+00
   Friction velocity        uk    :  0.77331E-02 0.89265E+00
   Dimensionless distance   yplus :  0.62257E-01 0.71864E+01
   Friction thermal sca.    tstar : -0.60018E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46451E-01 0.53619E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10462E-01      33   0.25129E-03   0.47928E+01 0.18746E+03 
c  Velocity[X]                                      0.17162E+01 
c  Velocity[Y]                                      0.30766E+01 
c  Velocity[Z]                                      0.74185E-30 
c  Pressure     0.11700E-06     520   0.92050E-08   0.11448E+00 0.77600E+03 
c  nu_tilda     0.76465E-05      33   0.52181E-05   0.69075E-06 0.21490E+03 
c  TempC        0.42088E+02      27   0.30852E-03   0.55092E+01 0.27783E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2074          9.7143          4.5729          4.5729
v  Velocity[Y]            -3.0646          7.1961         0.19523         0.19523
v  Velocity[Z]        -9.641e-015     7.2847e-015    -1.6061e-017    -1.6061e-017
v  ǁVelocityǁ         0.0024071          9.7154          5.1247          5.1247
v  Pressure               -27.126          24.984          -3.394          -3.394
v  nu_tilda           4.4112e-007       0.0042695       0.0017063       0.0017063
v  TempC                       21           73.05          22.035          22.035
v  TurbVisc           3.3323e-014       0.0050321       0.0020053       0.0020053
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2209:        0.21770E+01

===============================================================


 INSTANT    0.221000000E+04   TIME STEP NUMBER            2210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13007E-01 0.89199E+00
   Friction velocity        uk    :  0.13007E-01 0.89199E+00
   Dimensionless distance   yplus :  0.10471E+00 0.71811E+01
   Friction thermal sca.    tstar : -0.60886E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78126E-01 0.53579E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10464E-01      33   0.20367E-03   0.47973E+01 0.18747E+03 
c  Velocity[X]                                      0.17275E+01 
c  Velocity[Y]                                      0.30698E+01 
c  Velocity[Z]                                      0.67906E-30 
c  Pressure     0.95453E-07     474   0.94584E-08   0.94294E-01 0.70501E+03 
c  nu_tilda     0.76486E-05      33   0.14422E-04   0.69102E-06 0.21492E+03 
c  TempC        0.42095E+02      27   0.30151E-03   0.43497E+01 0.26430E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2121          9.7132          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.2213         0.19549         0.19549
v  Velocity[Z]       -9.5904e-015      7.254e-015    -1.6068e-017    -1.6068e-017
v  ǁVelocityǁ         0.0026806          9.7143          5.1246          5.1246
v  Pressure               -27.138          25.069         -3.3701         -3.3701
v  nu_tilda           4.4109e-007       0.0042695       0.0017066       0.0017066
v  TempC                       21          73.049          22.035          22.035
v  TurbVisc            3.331e-014       0.0050321       0.0020057       0.0020057
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2210:        0.20750E+01

===============================================================


 INSTANT    0.221100000E+04   TIME STEP NUMBER            2211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.75307E-02 0.89348E+00
   Friction velocity        uk    :  0.75307E-02 0.89348E+00
   Dimensionless distance   yplus :  0.60627E-01 0.71931E+01
   Friction thermal sca.    tstar : -0.59744E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45235E-01 0.53669E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10465E-01      33   0.24570E-03   0.47757E+01 0.18753E+03 
c  Velocity[X]                                      0.16813E+01 
c  Velocity[Y]                                      0.30943E+01 
c  Velocity[Z]                                      0.68065E-30 
c  Pressure     0.95058E-07     552   0.98922E-08   0.93249E-01 0.11686E+04 
c  nu_tilda     0.76507E-05      33   0.52218E-05   0.69125E-06 0.21494E+03 
c  TempC        0.42101E+02      27   0.27032E-03   0.72686E+01 0.30149E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2167          9.7121          4.5729          4.5729
v  Velocity[Y]            -3.0648          7.2321         0.19575         0.19575
v  Velocity[Z]       -9.5609e-015     7.1763e-015    -1.6072e-017    -1.6072e-017
v  ǁVelocityǁ         0.0027496          9.7133          5.1245          5.1245
v  Pressure               -27.087           25.17         -3.3122         -3.3122
v  nu_tilda           4.4103e-007       0.0042695        0.001707        0.001707
v  TempC                       21           73.05          22.035          22.035
v  TurbVisc           3.3302e-014       0.0050321       0.0020061       0.0020061
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2211:        0.22620E+01

===============================================================


 INSTANT    0.221200000E+04   TIME STEP NUMBER            2212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14174E-01 0.89296E+00
   Friction velocity        uk    :  0.14174E-01 0.89296E+00
   Dimensionless distance   yplus :  0.11411E+00 0.71889E+01
   Friction thermal sca.    tstar : -0.58977E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85139E-01 0.53637E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10467E-01      33   0.25896E-03   0.47919E+01 0.18752E+03 
c  Velocity[X]                                      0.17178E+01 
c  Velocity[Y]                                      0.30740E+01 
c  Velocity[Z]                                      0.71368E-30 
c  Pressure     0.11308E-06     537   0.99038E-08   0.11083E+00 0.14127E+04 
c  nu_tilda     0.76529E-05      33   0.14411E-04   0.69147E-06 0.21496E+03 
c  TempC        0.42107E+02      27   0.35187E-03   0.56324E+01 0.26985E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2212          9.7111          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.1989         0.19601         0.19601
v  Velocity[Z]       -9.5295e-015     7.1455e-015    -1.6073e-017    -1.6073e-017
v  ǁVelocityǁ         0.0021262          9.7122          5.1244          5.1244
v  Pressure               -27.094          24.989         -3.3441         -3.3441
v  nu_tilda           4.4106e-007       0.0042695       0.0017073       0.0017073
v  TempC                       21          73.049          22.035          22.035
v  TurbVisc           3.3285e-014       0.0050321       0.0020065       0.0020065
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2212:        0.22380E+01

===============================================================


 INSTANT    0.221300000E+04   TIME STEP NUMBER            2213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.19337E-02 0.89178E+00
   Friction velocity        uk    :  0.19337E-02 0.89178E+00
   Dimensionless distance   yplus :  0.15568E-01 0.71795E+01
   Friction thermal sca.    tstar : -0.60724E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11615E-01 0.53567E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10468E-01      33   0.27268E-03   0.47880E+01 0.18752E+03 
c  Velocity[X]                                      0.17174E+01 
c  Velocity[Y]                                      0.30706E+01 
c  Velocity[Z]                                      0.71434E-30 
c  Pressure     0.98153E-07     553   0.96335E-08   0.96919E-01 0.18989E+04 
c  nu_tilda     0.76550E-05      33   0.52183E-05   0.69163E-06 0.21497E+03 
c  TempC        0.42114E+02      27   0.28741E-03   0.59558E+01 0.29496E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2257            9.71          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.2224         0.19627         0.19627
v  Velocity[Z]       -9.3722e-015     7.0481e-015     -1.607e-017     -1.607e-017
v  ǁVelocityǁ         0.0022439          9.7112          5.1242          5.1242
v  Pressure               -27.046          25.219         -3.2576         -3.2576
v  nu_tilda           4.4112e-007       0.0042695       0.0017076       0.0017076
v  TempC                       21           73.05          22.035          22.035
v  TurbVisc           3.3293e-014       0.0050321       0.0020068       0.0020068
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2213:        0.22700E+01

===============================================================


 INSTANT    0.221400000E+04   TIME STEP NUMBER            2214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11012E-01 0.89274E+00
   Friction velocity        uk    :  0.11012E-01 0.89274E+00
   Dimensionless distance   yplus :  0.88653E-01 0.71871E+01
   Friction thermal sca.    tstar : -0.59899E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66145E-01 0.53624E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10470E-01      33   0.25941E-03   0.48045E+01 0.18764E+03 
c  Velocity[X]                                      0.17204E+01 
c  Velocity[Y]                                      0.30841E+01 
c  Velocity[Z]                                      0.65765E-30 
c  Pressure     0.10654E-06     536   0.91806E-08   0.10553E+00 0.13162E+04 
c  nu_tilda     0.76571E-05      33   0.14409E-04   0.69188E-06 0.21499E+03 
c  TempC        0.42120E+02      27   0.31945E-03   0.79039E+01 0.29730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2302          9.7089          4.5729          4.5729
v  Velocity[Y]            -3.0646          7.1979         0.19653         0.19653
v  Velocity[Z]        -9.175e-015     6.9865e-015    -1.6074e-017    -1.6074e-017
v  ǁVelocityǁ         0.0021254          9.7101          5.1241          5.1241
v  Pressure               -27.056          25.063         -3.2878         -3.2878
v  nu_tilda           4.4122e-007       0.0042695       0.0017079       0.0017079
v  TempC                       21          73.049          22.036          22.036
v  TurbVisc           3.3311e-014       0.0050321       0.0020072       0.0020072
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2214:        0.22170E+01

===============================================================


 INSTANT    0.221500000E+04   TIME STEP NUMBER            2215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.66624E-02 0.89187E+00
   Friction velocity        uk    :  0.66624E-02 0.89187E+00
   Dimensionless distance   yplus :  0.53637E-01 0.71801E+01
   Friction thermal sca.    tstar : -0.61424E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40019E-01 0.53572E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10471E-01      33   0.24705E-03   0.47846E+01 0.18753E+03 
c  Velocity[X]                                      0.17144E+01 
c  Velocity[Y]                                      0.30701E+01 
c  Velocity[Z]                                      0.72515E-30 
c  Pressure     0.12089E-06     538   0.97442E-08   0.11543E+00 0.15368E+04 
c  nu_tilda     0.76592E-05      33   0.52196E-05   0.69208E-06 0.21501E+03 
c  TempC        0.42127E+02      27   0.25404E-03   0.60708E+01 0.27905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2346          9.7079          4.5729          4.5729
v  Velocity[Y]            -3.0648          7.2192         0.19679         0.19679
v  Velocity[Z]       -8.9739e-015      6.879e-015    -1.6073e-017    -1.6073e-017
v  ǁVelocityǁ         0.0025577           9.709           5.124           5.124
v  Pressure               -27.005          25.232         -3.2147         -3.2147
v  nu_tilda           4.4126e-007       0.0042695       0.0017083       0.0017083
v  TempC                       21           73.05          22.036          22.036
v  TurbVisc           3.3342e-014       0.0050321       0.0020076       0.0020076
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2215:        0.22310E+01

===============================================================


 INSTANT    0.221600000E+04   TIME STEP NUMBER            2216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14285E-01 0.89323E+00
   Friction velocity        uk    :  0.14285E-01 0.89323E+00
   Dimensionless distance   yplus :  0.11501E+00 0.71911E+01
   Friction thermal sca.    tstar : -0.62638E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85809E-01 0.53654E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10473E-01      33   0.25997E-03   0.47731E+01 0.18749E+03 
c  Velocity[X]                                      0.17111E+01 
c  Velocity[Y]                                      0.30620E+01 
c  Velocity[Z]                                      0.82080E-30 
c  Pressure     0.86659E-07     376   0.93657E-08   0.84997E-01 0.65636E+03 
c  nu_tilda     0.76614E-05      33   0.14401E-04   0.69234E-06 0.21503E+03 
c  TempC        0.42133E+02      27   0.31835E-03   0.45685E+01 0.24149E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2394          9.7068          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2274         0.19704         0.19704
v  Velocity[Z]       -8.8886e-015     7.4004e-015    -1.6068e-017    -1.6068e-017
v  ǁVelocityǁ         0.0026801           9.708          5.1239          5.1239
v  Pressure               -27.017          25.219         -3.2117         -3.2117
v  nu_tilda           4.4117e-007       0.0042695       0.0017085       0.0017085
v  TempC                       21           73.05          22.036          22.036
v  TurbVisc           3.3355e-014       0.0050321        0.002008        0.002008
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2216:        0.18600E+01

===============================================================


 INSTANT    0.221700000E+04   TIME STEP NUMBER            2217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15427E-01 0.89282E+00
   Friction velocity        uk    :  0.15427E-01 0.89282E+00
   Dimensionless distance   yplus :  0.12420E+00 0.71878E+01
   Friction thermal sca.    tstar : -0.65467E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92665E-01 0.53629E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10474E-01      33   0.24216E-03   0.47920E+01 0.18765E+03 
c  Velocity[X]                                      0.17099E+01 
c  Velocity[Y]                                      0.30821E+01 
c  Velocity[Z]                                      0.77916E-30 
c  Pressure     0.10953E-06     504   0.92553E-08   0.10883E+00 0.75441E+03 
c  nu_tilda     0.76635E-05      33   0.52208E-05   0.69250E-06 0.21504E+03 
c  TempC        0.42140E+02      27   0.34080E-03   0.77780E+01 0.30905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2439          9.7057          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2009          0.1973          0.1973
v  Velocity[Z]       -8.8836e-015     6.9641e-015    -1.6075e-017    -1.6075e-017
v  ǁVelocityǁ          0.002434          9.7069          5.1237          5.1237
v  Pressure                -26.96          25.203         -3.1766         -3.1766
v  nu_tilda            4.411e-007       0.0042695       0.0017089       0.0017089
v  TempC                       21          73.051          22.036          22.036
v  TurbVisc           3.3327e-014       0.0050321       0.0020083       0.0020083
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2217:        0.21500E+01

===============================================================


 INSTANT    0.221800000E+04   TIME STEP NUMBER            2218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93664E-02 0.89132E+00
   Friction velocity        uk    :  0.93664E-02 0.89132E+00
   Dimensionless distance   yplus :  0.75406E-01 0.71758E+01
   Friction thermal sca.    tstar : -0.70936E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56261E-01 0.53539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10476E-01      33   0.25336E-03   0.47658E+01 0.18750E+03 
c  Velocity[X]                                      0.17012E+01 
c  Velocity[Y]                                      0.30646E+01 
c  Velocity[Z]                                      0.78474E-30 
c  Pressure     0.10308E-06     378   0.96111E-08   0.99724E-01 0.60385E+03 
c  nu_tilda     0.76656E-05      33   0.14399E-04   0.69272E-06 0.21506E+03 
c  TempC        0.42146E+02      27   0.30423E-03   0.60209E+01 0.29043E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2485          9.7046          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2157         0.19755         0.19755
v  Velocity[Z]       -9.0503e-015      6.867e-015     -1.608e-017     -1.608e-017
v  ǁVelocityǁ          0.002568          9.7058          5.1236          5.1236
v  Pressure               -26.974          25.228         -3.1665         -3.1665
v  nu_tilda           4.4108e-007       0.0042695       0.0017092       0.0017092
v  TempC                       21          73.049          22.036          22.036
v  TurbVisc           3.3305e-014       0.0050321       0.0020087       0.0020087
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2218:        0.18570E+01

===============================================================


 INSTANT    0.221900000E+04   TIME STEP NUMBER            2219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.79376E-02 0.89267E+00
   Friction velocity        uk    :  0.79376E-02 0.89267E+00
   Dimensionless distance   yplus :  0.63903E-01 0.71866E+01
   Friction thermal sca.    tstar : -0.76571E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47679E-01 0.53620E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10477E-01      33   0.28091E-03   0.47876E+01 0.18763E+03 
c  Velocity[X]                                      0.17259E+01 
c  Velocity[Y]                                      0.30617E+01 
c  Velocity[Z]                                      0.64335E-30 
c  Pressure     0.11388E-06     490   0.97998E-08   0.11199E+00 0.88280E+03 
c  nu_tilda     0.76677E-05      33   0.52176E-05   0.69290E-06 0.21508E+03 
c  TempC        0.42152E+02      27   0.29894E-03   0.45194E+01 0.26071E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.253          9.7036          4.5729          4.5729
v  Velocity[Y]            -3.0648          7.1967          0.1978          0.1978
v  Velocity[Z]       -8.9325e-015     6.9893e-015    -1.6078e-017    -1.6078e-017
v  ǁVelocityǁ         0.0024127          9.7048          5.1235          5.1235
v  Pressure               -26.919          25.257         -3.1219         -3.1219
v  nu_tilda            4.411e-007       0.0042695       0.0017096       0.0017096
v  TempC                       21           73.05          22.036          22.036
v  TurbVisc           3.3298e-014       0.0050321       0.0020091       0.0020091
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2219:        0.21210E+01

===============================================================


 INSTANT    0.222000000E+04   TIME STEP NUMBER            2220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13258E-01 0.89181E+00
   Friction velocity        uk    :  0.13258E-01 0.89181E+00
   Dimensionless distance   yplus :  0.10674E+00 0.71797E+01
   Friction thermal sca.    tstar : -0.86366E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79638E-01 0.53569E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10479E-01      33   0.20484E-03   0.47979E+01 0.18772E+03 
c  Velocity[X]                                      0.17204E+01 
c  Velocity[Y]                                      0.30775E+01 
c  Velocity[Z]                                      0.61820E-30 
c  Pressure     0.99706E-07     456   0.91808E-08   0.97692E-01 0.64085E+03 
c  nu_tilda     0.76699E-05      33   0.14392E-04   0.69316E-06 0.21510E+03 
c  TempC        0.42159E+02      27   0.30771E-03   0.58679E+01 0.26899E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2575          9.7025          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.2204         0.19806         0.19806
v  Velocity[Z]        -9.834e-015     7.0607e-015    -1.6085e-017    -1.6085e-017
v  ǁVelocityǁ         0.0026303          9.7037          5.1234          5.1234
v  Pressure               -26.933          25.313          -3.104          -3.104
v  nu_tilda           4.4108e-007       0.0042695       0.0017098       0.0017098
v  TempC                       21          73.049          22.036          22.036
v  TurbVisc           3.3307e-014       0.0050321       0.0020095       0.0020095
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2220:        0.20390E+01

===============================================================


 INSTANT    0.222100000E+04   TIME STEP NUMBER            2221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15137E-01 0.89336E+00
   Friction velocity        uk    :  0.15137E-01 0.89336E+00
   Dimensionless distance   yplus :  0.12186E+00 0.71921E+01
   Friction thermal sca.    tstar : -0.97642E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90924E-01 0.53661E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10480E-01      33   0.24761E-03   0.47679E+01 0.18760E+03 
c  Velocity[X]                                      0.16939E+01 
c  Velocity[Y]                                      0.30739E+01 
c  Velocity[Z]                                      0.76192E-30 
c  Pressure     0.11746E-06     521   0.97932E-08   0.11420E+00 0.11386E+04 
c  nu_tilda     0.76720E-05      33   0.52245E-05   0.69338E-06 0.21512E+03 
c  TempC        0.42165E+02      27   0.34616E-03   0.61199E+01 0.27496E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.262          9.7014          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2277         0.19831         0.19831
v  Velocity[Z]       -9.2186e-015     7.0393e-015    -1.6084e-017    -1.6084e-017
v  ǁVelocityǁ         0.0026551          9.7026          5.1232          5.1232
v  Pressure               -26.878          25.397         -3.0462         -3.0462
v  nu_tilda           4.4103e-007       0.0042695       0.0017102       0.0017102
v  TempC                       21           73.05          22.036          22.036
v  TurbVisc             3.33e-014       0.0050321       0.0020099       0.0020099
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2221:        0.21940E+01

===============================================================


 INSTANT    0.222200000E+04   TIME STEP NUMBER            2222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14880E-01 0.89308E+00
   Friction velocity        uk    :  0.14880E-01 0.89308E+00
   Dimensionless distance   yplus :  0.11980E+00 0.71899E+01
   Friction thermal sca.    tstar : -0.12438E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89382E-01 0.53645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10482E-01      33   0.24672E-03   0.47969E+01 0.18769E+03 
c  Velocity[X]                                      0.17370E+01 
c  Velocity[Y]                                      0.30598E+01 
c  Velocity[Z]                                      0.67918E-30 
c  Pressure     0.10663E-06     521   0.93703E-08   0.10698E+00 0.12418E+04 
c  nu_tilda     0.76741E-05      33   0.14384E-04   0.69361E-06 0.21514E+03 
c  TempC        0.42171E+02      27   0.31214E-03   0.59727E+01 0.27974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2665          9.7003          4.5729          4.5729
v  Velocity[Y]             -3.065          7.1999         0.19856         0.19856
v  Velocity[Z]       -8.8736e-015     7.0044e-015    -1.6082e-017    -1.6082e-017
v  ǁVelocityǁ         0.0024472          9.7015          5.1231          5.1231
v  Pressure               -26.892          25.255          -3.075          -3.075
v  nu_tilda            4.411e-007       0.0042695       0.0017105       0.0017105
v  TempC                       21          73.049          22.037          22.037
v  TurbVisc           3.3284e-014       0.0050321       0.0020102       0.0020102
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2222:        0.22020E+01

===============================================================


 INSTANT    0.222300000E+04   TIME STEP NUMBER            2223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15383E-02 0.89163E+00
   Friction velocity        uk    :  0.15383E-02 0.89163E+00
   Dimensionless distance   yplus :  0.12384E-01 0.71782E+01
   Friction thermal sca.    tstar : -0.15917E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92398E-02 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10483E-01      33   0.24787E-03   0.47716E+01 0.18766E+03 
c  Velocity[X]                                      0.16961E+01 
c  Velocity[Y]                                      0.30755E+01 
c  Velocity[Z]                                      0.62153E-30 
c  Pressure     0.93877E-07     552   0.97578E-08   0.91163E-01 0.17073E+04 
c  nu_tilda     0.76762E-05      33   0.52174E-05   0.69376E-06 0.21515E+03 
c  TempC        0.42178E+02      27   0.25528E-03   0.47510E+01 0.26346E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2708          9.6992          4.5729          4.5729
v  Velocity[Y]             -3.065          7.2203         0.19881         0.19881
v  Velocity[Z]       -8.8022e-015     7.0549e-015    -1.6082e-017    -1.6082e-017
v  ǁVelocityǁ         0.0026567          9.7005           5.123           5.123
v  Pressure               -26.841          25.453         -2.9957         -2.9957
v  nu_tilda           4.4118e-007       0.0042695       0.0017108       0.0017108
v  TempC                       21           73.05          22.037          22.037
v  TurbVisc           3.3305e-014       0.0050321       0.0020106       0.0020106
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2223:        0.22410E+01

===============================================================


 INSTANT    0.222400000E+04   TIME STEP NUMBER            2224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.79057E-02 0.89250E+00
   Friction velocity        uk    :  0.79057E-02 0.89250E+00
   Dimensionless distance   yplus :  0.63646E-01 0.71852E+01
   Friction thermal sca.    tstar : -0.39650E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47487E-01 0.53610E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10485E-01      33   0.26694E-03   0.47703E+01 0.18762E+03 
c  Velocity[X]                                      0.17113E+01 
c  Velocity[Y]                                      0.30590E+01 
c  Velocity[Z]                                      0.61805E-30 
c  Pressure     0.11016E-06     520   0.95329E-08   0.10752E+00 0.14087E+04 
c  nu_tilda     0.76783E-05      33   0.14382E-04   0.69398E-06 0.21516E+03 
c  TempC        0.42184E+02      27   0.25171E-03   0.41818E+01 0.24642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2752          9.6981          4.5729          4.5729
v  Velocity[Y]             -3.065          7.1936         0.19906         0.19906
v  Velocity[Z]        -9.016e-015     7.1429e-015    -1.6085e-017    -1.6085e-017
v  ǁVelocityǁ         0.0023501          9.6994          5.1229          5.1229
v  Pressure               -26.851          25.276         -3.0282         -3.0282
v  nu_tilda           4.4122e-007       0.0042695       0.0017111       0.0017111
v  TempC                       21          73.049          22.037          22.037
v  TurbVisc           3.3329e-014       0.0050321        0.002011        0.002011
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2224:        0.21780E+01

===============================================================


 INSTANT    0.222500000E+04   TIME STEP NUMBER            2225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13242E-01 0.89195E+00
   Friction velocity        uk    :  0.13242E-01 0.89195E+00
   Dimensionless distance   yplus :  0.10660E+00 0.71808E+01
   Friction thermal sca.    tstar : -0.20122E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79539E-01 0.53577E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10486E-01      33   0.23462E-03   0.47794E+01 0.18770E+03 
c  Velocity[X]                                      0.17232E+01 
c  Velocity[Y]                                      0.30562E+01 
c  Velocity[Z]                                      0.67601E-30 
c  Pressure     0.10034E-06     584   0.95456E-08   0.98039E-01 0.19815E+04 
c  nu_tilda     0.76805E-05      33   0.52237E-05   0.69416E-06 0.21518E+03 
c  TempC        0.42190E+02      27   0.38314E-03   0.59630E+01 0.25643E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2797          9.6971          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2212         0.19931         0.19931
v  Velocity[Z]       -9.4954e-015     7.1212e-015    -1.6089e-017    -1.6089e-017
v  ǁVelocityǁ         0.0026529          9.6983          5.1227          5.1227
v  Pressure                 -26.8          25.517         -2.9381         -2.9381
v  nu_tilda           4.4117e-007       0.0042695       0.0017115       0.0017115
v  TempC                       21           73.05          22.037          22.037
v  TurbVisc           3.3343e-014       0.0050321       0.0020114       0.0020114
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2225:        0.23230E+01

===============================================================


 INSTANT    0.222600000E+04   TIME STEP NUMBER            2226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14858E-01 0.89317E+00
   Friction velocity        uk    :  0.14858E-01 0.89317E+00
   Dimensionless distance   yplus :  0.11962E+00 0.71907E+01
   Friction thermal sca.    tstar : -0.13311E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89251E-01 0.53650E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10487E-01      33   0.25036E-03   0.47698E+01 0.18770E+03 
c  Velocity[X]                                      0.16994E+01 
c  Velocity[Y]                                      0.30703E+01 
c  Velocity[Z]                                      0.66518E-30 
c  Pressure     0.89520E-07     488   0.93266E-08   0.87567E-01 0.81196E+03 
c  nu_tilda     0.76826E-05      33   0.14370E-04   0.69442E-06 0.21520E+03 
c  TempC        0.42197E+02      27   0.26646E-03   0.71125E+01 0.31372E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2842           9.696          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.2267         0.19956         0.19956
v  Velocity[Z]       -8.8225e-015     7.1432e-015    -1.6086e-017    -1.6086e-017
v  ǁVelocityǁ         0.0027929          9.6972          5.1226          5.1226
v  Pressure               -26.815          25.465         -2.9474         -2.9474
v  nu_tilda           4.4109e-007       0.0042695       0.0017117       0.0017117
v  TempC                       21           73.05          22.037          22.037
v  TurbVisc           3.3325e-014       0.0050321       0.0020117       0.0020117
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2226:        0.21100E+01

===============================================================


 INSTANT    0.222700000E+04   TIME STEP NUMBER            2227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.41607E-02 0.89268E+00
   Friction velocity        uk    :  0.41607E-02 0.89268E+00
   Dimensionless distance   yplus :  0.33497E-01 0.71867E+01
   Friction thermal sca.    tstar : -0.10707E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24992E-01 0.53621E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10489E-01      33   0.24853E-03   0.47861E+01 0.18771E+03 
c  Velocity[X]                                      0.17231E+01 
c  Velocity[Y]                                      0.30630E+01 
c  Velocity[Z]                                      0.65174E-30 
c  Pressure     0.12999E-06     521   0.94690E-08   0.12767E+00 0.78755E+03 
c  nu_tilda     0.76847E-05      33   0.52159E-05   0.69460E-06 0.21522E+03 
c  TempC        0.42203E+02      27   0.28366E-03   0.43249E+01 0.24523E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2887          9.6949          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.1964         0.19981         0.19981
v  Velocity[Z]       -8.7212e-015     7.4034e-015    -1.6088e-017    -1.6088e-017
v  ǁVelocityǁ         0.0024347          9.6962          5.1225          5.1225
v  Pressure                -26.76          25.445         -2.9098         -2.9098
v  nu_tilda           4.4111e-007       0.0042695       0.0017121       0.0017121
v  TempC                       21          73.051          22.037          22.037
v  TurbVisc           3.3302e-014       0.0050321       0.0020121       0.0020121
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2227:        0.24560E+01

===============================================================


 INSTANT    0.222800000E+04   TIME STEP NUMBER            2228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13388E-01 0.89149E+00
   Friction velocity        uk    :  0.13388E-01 0.89149E+00
   Dimensionless distance   yplus :  0.10778E+00 0.71771E+01
   Friction thermal sca.    tstar : -0.91039E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80419E-01 0.53549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10490E-01      33   0.24993E-03   0.47779E+01 0.18770E+03 
c  Velocity[X]                                      0.17253E+01 
c  Velocity[Y]                                      0.30526E+01 
c  Velocity[Z]                                      0.62986E-30 
c  Pressure     0.89255E-07     490   0.98365E-08   0.87490E-01 0.64152E+03 
c  nu_tilda     0.76868E-05      33   0.14375E-04   0.69480E-06 0.21523E+03 
c  TempC        0.42209E+02      27   0.34784E-03   0.56946E+01 0.25476E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2932          9.6938          4.5729          4.5729
v  Velocity[Y]             -3.065          7.2172         0.20005         0.20005
v  Velocity[Z]       -8.9861e-015     7.3598e-015    -1.6088e-017    -1.6088e-017
v  ǁVelocityǁ         0.0026705          9.6951          5.1224          5.1224
v  Pressure               -26.774          25.511         -2.8937         -2.8937
v  nu_tilda            4.411e-007       0.0042695       0.0017124       0.0017124
v  TempC                       21           73.05          22.037          22.037
v  TurbVisc           3.3308e-014       0.0050321       0.0020125       0.0020125
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2228:        0.23590E+01

===============================================================


 INSTANT    0.222900000E+04   TIME STEP NUMBER            2229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15358E-01 0.89260E+00
   Friction velocity        uk    :  0.15358E-01 0.89260E+00
   Dimensionless distance   yplus :  0.12364E+00 0.71860E+01
   Friction thermal sca.    tstar : -0.81585E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92250E-01 0.53616E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10492E-01      33   0.24895E-03   0.47718E+01 0.18776E+03 
c  Velocity[X]                                      0.17028E+01 
c  Velocity[Y]                                      0.30690E+01 
c  Velocity[Z]                                      0.72210E-30 
c  Pressure     0.10465E-06     537   0.98619E-08   0.10356E+00 0.77934E+03 
c  nu_tilda     0.76889E-05      33   0.52194E-05   0.69495E-06 0.21524E+03 
c  TempC        0.42216E+02      27   0.26313E-03   0.64818E+01 0.28170E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2976          9.6927          4.5729          4.5729
v  Velocity[Y]             -3.065          7.1972          0.2003          0.2003
v  Velocity[Z]       -8.8199e-015     7.2944e-015     -1.609e-017     -1.609e-017
v  ǁVelocityǁ         0.0024676           9.694          5.1222          5.1222
v  Pressure               -26.716          25.502         -2.8566         -2.8566
v  nu_tilda           4.4111e-007       0.0042695       0.0017127       0.0017127
v  TempC                       21           73.05          22.037          22.037
v  TurbVisc           3.3306e-014       0.0050321       0.0020128       0.0020128
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2229:        0.22360E+01

===============================================================


 INSTANT    0.223000000E+04   TIME STEP NUMBER            2230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13609E-01 0.89167E+00
   Friction velocity        uk    :  0.13609E-01 0.89167E+00
   Dimensionless distance   yplus :  0.10956E+00 0.71786E+01
   Friction thermal sca.    tstar : -0.73111E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81745E-01 0.53560E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10493E-01      33   0.20647E-03   0.47597E+01 0.18766E+03 
c  Velocity[X]                                      0.17064E+01 
c  Velocity[Y]                                      0.30533E+01 
c  Velocity[Z]                                      0.89348E-30 
c  Pressure     0.10489E-06     440   0.92671E-08   0.10172E+00 0.60643E+03 
c  nu_tilda     0.76910E-05      33   0.14361E-04   0.69519E-06 0.21526E+03 
c  TempC        0.42222E+02      27   0.32201E-03   0.40386E+01 0.24210E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.302          9.6916          4.5729          4.5729
v  Velocity[Y]             -3.065          7.2165         0.20054         0.20054
v  Velocity[Z]       -9.4771e-015     7.4568e-015    -1.6086e-017    -1.6086e-017
v  ǁVelocityǁ         0.0022709          9.6929          5.1221          5.1221
v  Pressure               -26.732          25.526         -2.8461         -2.8461
v  nu_tilda           4.4112e-007       0.0042695        0.001713        0.001713
v  TempC                       21          73.049          22.038          22.038
v  TurbVisc           3.3308e-014       0.0050321       0.0020132       0.0020132
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2230:        0.19990E+01

===============================================================


 INSTANT    0.223100000E+04   TIME STEP NUMBER            2231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.38911E-02 0.89333E+00
   Friction velocity        uk    :  0.38911E-02 0.89333E+00
   Dimensionless distance   yplus :  0.31326E-01 0.71919E+01
   Friction thermal sca.    tstar : -0.68192E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23373E-01 0.53660E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10495E-01      33   0.28080E-03   0.47562E+01 0.18769E+03 
c  Velocity[X]                                      0.17041E+01 
c  Velocity[Y]                                      0.30521E+01 
c  Velocity[Z]                                      0.72125E-30 
c  Pressure     0.10230E-06     584   0.95606E-08   0.10059E+00 0.14091E+04 
c  nu_tilda     0.76931E-05      33   0.52120E-05   0.69538E-06 0.21528E+03 
c  TempC        0.42228E+02      27   0.34993E-03   0.58224E+01 0.27947E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3063          9.6905          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2282         0.20078         0.20078
v  Velocity[Z]       -8.9697e-015     7.2698e-015    -1.6087e-017    -1.6087e-017
v  ǁVelocityǁ         0.0027514          9.6918           5.122           5.122
v  Pressure               -26.679          25.667         -2.7775         -2.7775
v  nu_tilda           4.4109e-007       0.0042695       0.0017134       0.0017134
v  TempC                       21           73.05          22.038          22.038
v  TurbVisc           3.3313e-014       0.0050321       0.0020136       0.0020136
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2231:        0.23340E+01

===============================================================


 INSTANT    0.223200000E+04   TIME STEP NUMBER            2232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.36618E-02 0.89281E+00
   Friction velocity        uk    :  0.36618E-02 0.89281E+00
   Dimensionless distance   yplus :  0.29480E-01 0.71877E+01
   Friction thermal sca.    tstar : -0.63459E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21995E-01 0.53629E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10496E-01      33   0.24717E-03   0.48058E+01 0.18800E+03 
c  Velocity[X]                                      0.17316E+01 
c  Velocity[Y]                                      0.30743E+01 
c  Velocity[Z]                                      0.59987E-30 
c  Pressure     0.11364E-06     552   0.92600E-08   0.11362E+00 0.13346E+04 
c  nu_tilda     0.76952E-05      33   0.14363E-04   0.69566E-06 0.21530E+03 
c  TempC        0.42235E+02      27   0.32705E-03   0.56862E+01 0.27887E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3107          9.6894          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.1996         0.20103         0.20103
v  Velocity[Z]       -9.1378e-015     7.2916e-015    -1.6088e-017    -1.6088e-017
v  ǁVelocityǁ         0.0024738          9.6907          5.1218          5.1218
v  Pressure               -26.689          25.505         -2.8078         -2.8078
v  nu_tilda           4.4108e-007       0.0042695       0.0017136       0.0017136
v  TempC                       21           73.05          22.038          22.038
v  TurbVisc           3.3302e-014       0.0050321        0.002014        0.002014
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2232:        0.22670E+01

===============================================================


 INSTANT    0.223300000E+04   TIME STEP NUMBER            2233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51568E-02 0.89145E+00
   Friction velocity        uk    :  0.51568E-02 0.89145E+00
   Dimensionless distance   yplus :  0.41516E-01 0.71768E+01
   Friction thermal sca.    tstar : -0.60253E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30975E-01 0.53547E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10497E-01      33   0.24286E-03   0.47638E+01 0.18777E+03 
c  Velocity[X]                                      0.17086E+01 
c  Velocity[Y]                                      0.30552E+01 
c  Velocity[Z]                                      0.56642E-30 
c  Pressure     0.11259E-06     538   0.93471E-08   0.10846E+00 0.15099E+04 
c  nu_tilda     0.76973E-05      33   0.52145E-05   0.69580E-06 0.21531E+03 
c  TempC        0.42241E+02      27   0.29164E-03   0.63352E+01 0.27455E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3149          9.6883          4.5729          4.5729
v  Velocity[Y]            -3.0648          7.2163         0.20127         0.20127
v  Velocity[Z]       -9.0223e-015     7.1322e-015    -1.6086e-017    -1.6086e-017
v  ǁVelocityǁ           0.00261          9.6896          5.1217          5.1217
v  Pressure               -26.638          25.668         -2.7368         -2.7368
v  nu_tilda           4.4108e-007       0.0042695        0.001714        0.001714
v  TempC                       21           73.05          22.038          22.038
v  TurbVisc           3.3299e-014       0.0050321       0.0020143       0.0020143
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2233:        0.22260E+01

===============================================================


 INSTANT    0.223400000E+04   TIME STEP NUMBER            2234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52066E-02 0.89258E+00
   Friction velocity        uk    :  0.52066E-02 0.89258E+00
   Dimensionless distance   yplus :  0.41916E-01 0.71858E+01
   Friction thermal sca.    tstar : -0.60383E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31274E-01 0.53614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10499E-01      33   0.25929E-03   0.47778E+01 0.18780E+03 
c  Velocity[X]                                      0.17328E+01 
c  Velocity[Y]                                      0.30451E+01 
c  Velocity[Z]                                      0.63718E-30 
c  Pressure     0.10166E-06     505   0.97628E-08   0.10091E+00 0.11056E+04 
c  nu_tilda     0.76994E-05      33   0.14351E-04   0.69599E-06 0.21532E+03 
c  TempC        0.42247E+02      27   0.27340E-03   0.61957E+01 0.28332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3192          9.6872          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.1939         0.20151         0.20151
v  Velocity[Z]       -9.3403e-015     6.9973e-015    -1.6088e-017    -1.6088e-017
v  ǁVelocityǁ         0.0024553          9.6885          5.1216          5.1216
v  Pressure               -26.651          25.548         -2.7584         -2.7584
v  nu_tilda           4.4117e-007       0.0042695       0.0017142       0.0017142
v  TempC                       21          73.049          22.038          22.038
v  TurbVisc             3.33e-014       0.0050321       0.0020147       0.0020147
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2234:        0.21500E+01

===============================================================


 INSTANT    0.223500000E+04   TIME STEP NUMBER            2235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95212E-02 0.89173E+00
   Friction velocity        uk    :  0.95212E-02 0.89173E+00
   Dimensionless distance   yplus :  0.76652E-01 0.71791E+01
   Friction thermal sca.    tstar : -0.60054E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57191E-01 0.53564E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10500E-01      33   0.24563E-03   0.47671E+01 0.18784E+03 
c  Velocity[X]                                      0.17029E+01 
c  Velocity[Y]                                      0.30643E+01 
c  Velocity[Z]                                      0.81129E-30 
c  Pressure     0.93418E-07     538   0.99300E-08   0.90727E-01 0.17832E+04 
c  nu_tilda     0.77015E-05      33   0.52080E-05   0.69616E-06 0.21534E+03 
c  TempC        0.42253E+02      27   0.37237E-03   0.57008E+01 0.27362E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3234          9.6861          4.5729          4.5729
v  Velocity[Y]            -3.0649           7.219         0.20175         0.20175
v  Velocity[Z]       -9.7325e-015     7.3559e-015    -1.6084e-017    -1.6084e-017
v  ǁVelocityǁ         0.0027072          9.6874          5.1214          5.1214
v  Pressure               -26.602          25.757         -2.6767         -2.6767
v  nu_tilda           4.4119e-007       0.0042695       0.0017146       0.0017146
v  TempC                       21           73.05          22.038          22.038
v  TurbVisc           3.3326e-014       0.0050321       0.0020151       0.0020151
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2235:        0.22470E+01

===============================================================


 INSTANT    0.223600000E+04   TIME STEP NUMBER            2236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14966E-01 0.89287E+00
   Friction velocity        uk    :  0.14966E-01 0.89287E+00
   Dimensionless distance   yplus :  0.12049E+00 0.71882E+01
   Friction thermal sca.    tstar : -0.59476E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89896E-01 0.53632E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10502E-01      33   0.25976E-03   0.47372E+01 0.18769E+03 
c  Velocity[X]                                      0.16896E+01 
c  Velocity[Y]                                      0.30477E+01 
c  Velocity[Z]                                      0.78612E-30 
c  Pressure     0.10207E-06     473   0.95190E-08   0.98575E-01 0.93723E+03 
c  nu_tilda     0.77036E-05      33   0.14351E-04   0.69639E-06 0.21536E+03 
c  TempC        0.42260E+02      27   0.26788E-03   0.73392E+01 0.31141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3279           9.685          4.5729          4.5729
v  Velocity[Y]            -3.0649          7.2222         0.20199         0.20199
v  Velocity[Z]       -9.7168e-015     6.7148e-015    -1.6084e-017    -1.6084e-017
v  ǁVelocityǁ         0.0026945          9.6863          5.1213          5.1213
v  Pressure               -26.614          25.673         -2.6913         -2.6913
v  nu_tilda           4.4114e-007       0.0042695       0.0017149       0.0017149
v  TempC                       21           73.05          22.038          22.038
v  TurbVisc           3.3333e-014       0.0050321       0.0020154       0.0020154
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2236:        0.20700E+01

===============================================================


 INSTANT    0.223700000E+04   TIME STEP NUMBER            2237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95935E-02 0.89271E+00
   Friction velocity        uk    :  0.95935E-02 0.89271E+00
   Dimensionless distance   yplus :  0.77234E-01 0.71869E+01
   Friction thermal sca.    tstar : -0.59325E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57625E-01 0.53623E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10503E-01      33   0.26734E-03   0.47755E+01 0.18787E+03 
c  Velocity[X]                                      0.17311E+01 
c  Velocity[Y]                                      0.30444E+01 
c  Velocity[Z]                                      0.85454E-30 
c  Pressure     0.11030E-06     506   0.95767E-08   0.10990E+00 0.89833E+03 
c  nu_tilda     0.77057E-05      33   0.52086E-05   0.69657E-06 0.21537E+03 
c  TempC        0.42266E+02      27   0.30529E-03   0.41821E+01 0.24296E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3323          9.6839          4.5729          4.5729
v  Velocity[Y]            -3.0648          7.1983         0.20223         0.20223
v  Velocity[Z]       -9.4863e-015      6.511e-015    -1.6085e-017    -1.6085e-017
v  ǁVelocityǁ         0.0024752          9.6853          5.1212          5.1212
v  Pressure               -26.559          25.696         -2.6458         -2.6458
v  nu_tilda           4.4113e-007       0.0042695       0.0017152       0.0017152
v  TempC                       21          73.051          22.038          22.038
v  TurbVisc           3.3318e-014       0.0050321       0.0020158       0.0020158
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2237:        0.21470E+01

===============================================================


 INSTANT    0.223800000E+04   TIME STEP NUMBER            2238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13481E-01 0.89132E+00
   Friction velocity        uk    :  0.13481E-01 0.89132E+00
   Dimensionless distance   yplus :  0.10853E+00 0.71757E+01
   Friction thermal sca.    tstar : -0.59977E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80979E-01 0.53539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10505E-01      33   0.24849E-03   0.47733E+01 0.18791E+03 
c  Velocity[X]                                      0.17139E+01 
c  Velocity[Y]                                      0.30594E+01 
c  Velocity[Z]                                      0.64378E-30 
c  Pressure     0.97797E-07     456   0.90959E-08   0.95713E-01 0.61552E+03 
c  nu_tilda     0.77078E-05      33   0.14342E-04   0.69679E-06 0.21539E+03 
c  TempC        0.42272E+02      27   0.33397E-03   0.46951E+01 0.26754E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3367          9.6828          4.5729          4.5729
v  Velocity[Y]            -3.0646          7.2164         0.20247         0.20247
v  Velocity[Z]       -9.3745e-015     6.4233e-015    -1.6084e-017    -1.6084e-017
v  ǁVelocityǁ         0.0027478          9.6842           5.121           5.121
v  Pressure               -26.577          25.752         -2.6328         -2.6328
v  nu_tilda           4.4113e-007       0.0042695       0.0017155       0.0017155
v  TempC                       21           73.05          22.038          22.038
v  TurbVisc           3.3314e-014       0.0050321       0.0020162       0.0020162
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2238:        0.20270E+01

===============================================================


 INSTANT    0.223900000E+04   TIME STEP NUMBER            2239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11191E-01 0.89238E+00
   Friction velocity        uk    :  0.11191E-01 0.89238E+00
   Dimensionless distance   yplus :  0.90097E-01 0.71843E+01
   Friction thermal sca.    tstar : -0.58960E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67222E-01 0.53603E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10506E-01      33   0.24973E-03   0.47671E+01 0.18784E+03 
c  Velocity[X]                                      0.17172E+01 
c  Velocity[Y]                                      0.30499E+01 
c  Velocity[Z]                                      0.68408E-30 
c  Pressure     0.12463E-06     521   0.99840E-08   0.12227E+00 0.76592E+03 
c  nu_tilda     0.77099E-05      33   0.52039E-05   0.69693E-06 0.21540E+03 
c  TempC        0.42278E+02      27   0.25478E-03   0.75217E+01 0.30536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.341          9.6817          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.1916         0.20271         0.20271
v  Velocity[Z]       -9.2725e-015     7.4546e-015    -1.6079e-017    -1.6079e-017
v  ǁVelocityǁ         0.0024299          9.6831          5.1209          5.1209
v  Pressure               -26.521          25.727         -2.5972         -2.5972
v  nu_tilda           4.4117e-007       0.0042695       0.0017158       0.0017158
v  TempC                       21           73.05          22.039          22.039
v  TurbVisc           3.3315e-014       0.0050321       0.0020165       0.0020165
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2239:        0.21840E+01

===============================================================


 INSTANT    0.224000000E+04   TIME STEP NUMBER            2240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13375E-01 0.89168E+00
   Friction velocity        uk    :  0.13375E-01 0.89168E+00
   Dimensionless distance   yplus :  0.10768E+00 0.71787E+01
   Friction thermal sca.    tstar : -0.60295E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80341E-01 0.53561E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10507E-01      33   0.20762E-03   0.47702E+01 0.18786E+03 
c  Velocity[X]                                      0.17299E+01 
c  Velocity[Y]                                      0.30403E+01 
c  Velocity[Z]                                      0.87260E-30 
c  Pressure     0.90725E-07     456   0.98782E-08   0.88929E-01 0.64762E+03 
c  nu_tilda     0.77120E-05      33   0.14340E-04   0.69714E-06 0.21541E+03 
c  TempC        0.42284E+02      27   0.36266E-03   0.52630E+01 0.27191E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3453          9.6806          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.2171         0.20294         0.20294
v  Velocity[Z]       -9.6525e-015     6.7293e-015    -1.6075e-017    -1.6075e-017
v  ǁVelocityǁ         0.0026691           9.682          5.1207          5.1207
v  Pressure               -26.537          25.792         -2.5812         -2.5812
v  nu_tilda            4.411e-007       0.0042695       0.0017161       0.0017161
v  TempC                       21          73.049          22.039          22.039
v  TurbVisc           3.3326e-014       0.0050321       0.0020169       0.0020169
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2240:        0.20440E+01

===============================================================


 INSTANT    0.224100000E+04   TIME STEP NUMBER            2241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11119E-01 0.89325E+00
   Friction velocity        uk    :  0.11119E-01 0.89325E+00
   Dimensionless distance   yplus :  0.89515E-01 0.71913E+01
   Friction thermal sca.    tstar : -0.59686E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66788E-01 0.53655E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10509E-01      33   0.23951E-03   0.47407E+01 0.18784E+03 
c  Velocity[X]                                      0.16844E+01 
c  Velocity[Y]                                      0.30563E+01 
c  Velocity[Z]                                      0.66723E-30 
c  Pressure     0.91170E-07     553   0.97230E-08   0.89249E-01 0.11963E+04 
c  nu_tilda     0.77141E-05      33   0.52038E-05   0.69730E-06 0.21543E+03 
c  TempC        0.42291E+02      27   0.31163E-03   0.70674E+01 0.30954E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3495          9.6795          4.5729          4.5729
v  Velocity[Y]            -3.0647          7.2284         0.20318         0.20318
v  Velocity[Z]       -9.3648e-015     6.5001e-015    -1.6076e-017    -1.6076e-017
v  ǁVelocityǁ         0.0027919          9.6808          5.1206          5.1206
v  Pressure               -26.482          25.896         -2.5219         -2.5219
v  nu_tilda           4.4094e-007       0.0042695       0.0017165       0.0017165
v  TempC                       21           73.05          22.039          22.039
v  TurbVisc           3.3304e-014       0.0050321       0.0020173       0.0020173
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2241:        0.22680E+01

===============================================================


 INSTANT    0.224200000E+04   TIME STEP NUMBER            2242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15690E-01 0.89273E+00
   Friction velocity        uk    :  0.15690E-01 0.89273E+00
   Dimensionless distance   yplus :  0.12632E+00 0.71871E+01
   Friction thermal sca.    tstar : -0.58693E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94248E-01 0.53624E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10510E-01      33   0.24953E-03   0.47584E+01 0.18786E+03 
c  Velocity[X]                                      0.17163E+01 
c  Velocity[Y]                                      0.30421E+01 
c  Velocity[Z]                                      0.63870E-30 
c  Pressure     0.10854E-06     536   0.98328E-08   0.10685E+00 0.13872E+04 
c  nu_tilda     0.77162E-05      33   0.14331E-04   0.69754E-06 0.21545E+03 
c  TempC        0.42297E+02      27   0.26281E-03   0.59785E+01 0.27909E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3538          9.6784          4.5729          4.5729
v  Velocity[Y]            -3.0647           7.195         0.20341         0.20341
v  Velocity[Z]       -9.6258e-015     6.3861e-015    -1.6081e-017    -1.6081e-017
v  ǁVelocityǁ         0.0024581          9.6798          5.1205          5.1205
v  Pressure               -26.494          25.719         -2.5536         -2.5536
v  nu_tilda           4.4096e-007       0.0042695       0.0017167       0.0017167
v  TempC                       21          73.049          22.039          22.039
v  TurbVisc           3.3257e-014       0.0050321       0.0020176       0.0020176
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2242:        0.22170E+01

===============================================================


 INSTANT    0.224300000E+04   TIME STEP NUMBER            2243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12527E-01 0.89148E+00
   Friction velocity        uk    :  0.12527E-01 0.89148E+00
   Dimensionless distance   yplus :  0.10085E+00 0.71771E+01
   Friction thermal sca.    tstar : -0.60182E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75244E-01 0.53549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10511E-01      33   0.27276E-03   0.47647E+01 0.18798E+03 
c  Velocity[X]                                      0.17190E+01 
c  Velocity[Y]                                      0.30457E+01 
c  Velocity[Z]                                      0.83296E-30 
c  Pressure     0.10030E-06     553   0.95015E-08   0.97595E-01 0.18518E+04 
c  nu_tilda     0.77183E-05      33   0.52002E-05   0.69773E-06 0.21546E+03 
c  TempC        0.42303E+02      27   0.31347E-03   0.45358E+01 0.24356E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.358          9.6773          4.5729          4.5729
v  Velocity[Y]            -3.0646          7.2181         0.20365         0.20365
v  Velocity[Z]        -9.386e-015     6.4826e-015    -1.6079e-017    -1.6079e-017
v  ǁVelocityǁ           0.00271          9.6787          5.1203          5.1203
v  Pressure               -26.444          25.942         -2.4699         -2.4699
v  nu_tilda           4.4102e-007       0.0042695       0.0017171       0.0017171
v  TempC                       21           73.05          22.039          22.039
v  TurbVisc           3.3263e-014       0.0050321        0.002018        0.002018
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2243:        0.22550E+01

===============================================================


 INSTANT    0.224400000E+04   TIME STEP NUMBER            2244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15249E-01 0.89243E+00
   Friction velocity        uk    :  0.15249E-01 0.89243E+00
   Dimensionless distance   yplus :  0.12277E+00 0.71847E+01
   Friction thermal sca.    tstar : -0.59303E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91598E-01 0.53606E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10513E-01      33   0.25922E-03   0.47820E+01 0.18808E+03 
c  Velocity[X]                                      0.17260E+01 
c  Velocity[Y]                                      0.30561E+01 
c  Velocity[Z]                                      0.80899E-30 
c  Pressure     0.11026E-06     506   0.98652E-08   0.10948E+00 0.12658E+04 
c  nu_tilda     0.77204E-05      33   0.14328E-04   0.69793E-06 0.21548E+03 
c  TempC        0.42309E+02      27   0.31899E-03   0.53523E+01 0.26350E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3622          9.6762          4.5729          4.5729
v  Velocity[Y]            -3.0644          7.1947         0.20388         0.20388
v  Velocity[Z]       -9.3501e-015      7.354e-015     -1.607e-017     -1.607e-017
v  ǁVelocityǁ         0.0024906          9.6776          5.1202          5.1202
v  Pressure               -26.457          25.792         -2.4987         -2.4987
v  nu_tilda           4.4105e-007       0.0042695       0.0017173       0.0017173
v  TempC                       21          73.049          22.039          22.039
v  TurbVisc           3.3281e-014       0.0050321       0.0020183       0.0020183
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2244:        0.21560E+01

===============================================================


 INSTANT    0.224500000E+04   TIME STEP NUMBER            2245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14257E-01 0.89162E+00
   Friction velocity        uk    :  0.14257E-01 0.89162E+00
   Dimensionless distance   yplus :  0.11478E+00 0.71782E+01
   Friction thermal sca.    tstar : -0.59977E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85637E-01 0.53557E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10514E-01      33   0.19354E-03   0.47580E+01 0.18791E+03 
c  Velocity[X]                                      0.17159E+01 
c  Velocity[Y]                                      0.30421E+01 
c  Velocity[Z]                                      0.71475E-30 
c  Pressure     0.11377E-06     490   0.97900E-08   0.10942E+00 0.15825E+04 
c  nu_tilda     0.77225E-05      33   0.51980E-05   0.69806E-06 0.21549E+03 
c  TempC        0.42315E+02      27   0.35661E-03   0.51086E+01 0.26029E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3663          9.6751          4.5729          4.5729
v  Velocity[Y]            -3.0644          7.2155         0.20411         0.20411
v  Velocity[Z]       -9.4738e-015     6.7137e-015    -1.6069e-017    -1.6069e-017
v  ǁVelocityǁ         0.0026722          9.6764            5.12            5.12
v  Pressure               -26.404          25.966         -2.4244         -2.4244
v  nu_tilda           4.4106e-007       0.0042695       0.0017177       0.0017177
v  TempC                       21           73.05          22.039          22.039
v  TurbVisc           3.3289e-014       0.0050321       0.0020187       0.0020187
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2245:        0.21170E+01

===============================================================


 INSTANT    0.224600000E+04   TIME STEP NUMBER            2246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10511E-01 0.89297E+00
   Friction velocity        uk    :  0.10511E-01 0.89297E+00
   Dimensionless distance   yplus :  0.84623E-01 0.71890E+01
   Friction thermal sca.    tstar : -0.59333E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63138E-01 0.53638E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10516E-01      33   0.25275E-03   0.47446E+01 0.18787E+03 
c  Velocity[X]                                      0.17115E+01 
c  Velocity[Y]                                      0.30331E+01 
c  Velocity[Z]                                      0.64905E-30 
c  Pressure     0.87035E-07     457   0.97627E-08   0.85613E-01 0.70274E+03 
c  nu_tilda     0.77246E-05      33   0.14320E-04   0.69827E-06 0.21550E+03 
c  TempC        0.42321E+02      27   0.27654E-03   0.62890E+01 0.27598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3707          9.6739          4.5729          4.5729
v  Velocity[Y]            -3.0645          7.2232         0.20435         0.20435
v  Velocity[Z]       -9.3288e-015     6.6151e-015    -1.6074e-017    -1.6074e-017
v  ǁVelocityǁ         0.0028234          9.6753          5.1199          5.1199
v  Pressure               -26.424          25.936         -2.4301         -2.4301
v  nu_tilda           4.4104e-007       0.0042695       0.0017179       0.0017179
v  TempC                       21           73.05          22.039          22.039
v  TurbVisc           3.3292e-014       0.0050321       0.0020191       0.0020191
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2246:        0.20760E+01

===============================================================


 INSTANT    0.224700000E+04   TIME STEP NUMBER            2247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13731E-01 0.89253E+00
   Friction velocity        uk    :  0.13731E-01 0.89253E+00
   Dimensionless distance   yplus :  0.11054E+00 0.71855E+01
   Friction thermal sca.    tstar : -0.59534E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82477E-01 0.53612E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10517E-01      33   0.23597E-03   0.47625E+01 0.18801E+03 
c  Velocity[X]                                      0.17108E+01 
c  Velocity[Y]                                      0.30518E+01 
c  Velocity[Z]                                      0.59841E-30 
c  Pressure     0.11250E-06     488   0.96779E-08   0.11103E+00 0.80264E+03 
c  nu_tilda     0.77266E-05      33   0.51988E-05   0.69844E-06 0.21552E+03 
c  TempC        0.42328E+02      27   0.35995E-03   0.48525E+01 0.24830E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.375          9.6728          4.5729          4.5729
v  Velocity[Y]            -3.0645          7.1962         0.20458         0.20458
v  Velocity[Z]        -9.372e-015     6.7363e-015    -1.6077e-017    -1.6077e-017
v  ǁVelocityǁ         0.0025378          9.6742          5.1198          5.1198
v  Pressure               -26.367          25.933         -2.3911         -2.3911
v  nu_tilda           4.4106e-007       0.0042695       0.0017183       0.0017183
v  TempC                       21           73.05          22.039          22.039
v  TurbVisc           3.3288e-014       0.0050321       0.0020194       0.0020194
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2247:        0.21150E+01

===============================================================


 INSTANT    0.224800000E+04   TIME STEP NUMBER            2248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14160E-01 0.89102E+00
   Friction velocity        uk    :  0.14160E-01 0.89102E+00
   Dimensionless distance   yplus :  0.11400E+00 0.71733E+01
   Friction thermal sca.    tstar : -0.63562E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85054E-01 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10518E-01      33   0.25683E-03   0.47403E+01 0.18790E+03 
c  Velocity[X]                                      0.17054E+01 
c  Velocity[Y]                                      0.30349E+01 
c  Velocity[Z]                                      0.81529E-30 
c  Pressure     0.10281E-06     280   0.96692E-08   0.99484E-01 0.60080E+03 
c  nu_tilda     0.77287E-05      33   0.14316E-04   0.69866E-06 0.21553E+03 
c  TempC        0.42334E+02      27   0.32386E-03   0.60619E+01 0.28179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3792          9.6717          4.5729          4.5729
v  Velocity[Y]            -3.0644          7.2113         0.20481         0.20481
v  Velocity[Z]       -9.4874e-015      7.409e-015    -1.6067e-017    -1.6067e-017
v  ǁVelocityǁ         0.0020893          9.6731          5.1196          5.1196
v  Pressure               -26.386          25.953         -2.3856         -2.3856
v  nu_tilda           4.4108e-007       0.0042695       0.0017185       0.0017185
v  TempC                       21          73.049           22.04           22.04
v  TurbVisc           3.3293e-014       0.0050321       0.0020198       0.0020198
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2248:        0.16320E+01

===============================================================


 INSTANT    0.224900000E+04   TIME STEP NUMBER            2249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.76421E-02 0.89237E+00
   Friction velocity        uk    :  0.76421E-02 0.89237E+00
   Dimensionless distance   yplus :  0.61524E-01 0.71842E+01
   Friction thermal sca.    tstar : -0.67741E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45904E-01 0.53602E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10520E-01      33   0.27850E-03   0.47618E+01 0.18802E+03 
c  Velocity[X]                                      0.17294E+01 
c  Velocity[Y]                                      0.30324E+01 
c  Velocity[Z]                                      0.86377E-30 
c  Pressure     0.10801E-06     520   0.98821E-08   0.10721E+00 0.88652E+03 
c  nu_tilda     0.77308E-05      33   0.51924E-05   0.69880E-06 0.21554E+03 
c  TempC        0.42340E+02      27   0.32976E-03   0.57005E+01 0.28331E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3834          9.6706          4.5729          4.5729
v  Velocity[Y]            -3.0643          7.1939         0.20504         0.20504
v  Velocity[Z]       -9.8817e-015     6.7964e-015    -1.6072e-017    -1.6072e-017
v  ǁVelocityǁ         0.0024942           9.672          5.1195          5.1195
v  Pressure               -26.328          25.974         -2.3408         -2.3408
v  nu_tilda           4.4117e-007       0.0042695       0.0017189       0.0017189
v  TempC                       21          73.049           22.04           22.04
v  TurbVisc             3.33e-014       0.0050321       0.0020201       0.0020201
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2249:        0.21940E+01

===============================================================


 INSTANT    0.225000000E+04   TIME STEP NUMBER            2250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96693E-02 0.89159E+00
   Friction velocity        uk    :  0.96693E-02 0.89159E+00
   Dimensionless distance   yplus :  0.77844E-01 0.71779E+01
   Friction thermal sca.    tstar : -0.73724E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58081E-01 0.53555E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200


 Write intermediate restart files
   checkpoint at iteration       2250, Physical time    0.22500E+04


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.32700E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10521E-01      33   0.20411E-03   0.47674E+01 0.18809E+03 
c  Velocity[X]                                      0.17203E+01 
c  Velocity[Y]                                      0.30471E+01 
c  Velocity[Z]                                      0.64617E-30 
c  Pressure     0.93769E-07     408   0.97168E-08   0.92094E-01 0.59788E+03 
c  nu_tilda     0.77329E-05      33   0.14311E-04   0.69899E-06 0.21555E+03 
c  TempC        0.42346E+02      27   0.27962E-03   0.67590E+01 0.29027E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3876          9.6695          4.5729          4.5729
v  Velocity[Y]            -3.0641           7.217         0.20526         0.20526
v  Velocity[Z]        -9.719e-015     6.7682e-015    -1.6075e-017    -1.6075e-017
v  ǁVelocityǁ         0.0027571          9.6709          5.1193          5.1193
v  Pressure                -26.35          26.023         -2.3304         -2.3304
v  nu_tilda           4.4124e-007       0.0042695       0.0017191       0.0017191
v  TempC                       21          73.049           22.04           22.04
v  TurbVisc           3.3327e-014       0.0050321       0.0020205       0.0020205
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2250:        0.22460E+01

===============================================================


 INSTANT    0.225100000E+04   TIME STEP NUMBER            2251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14419E-01 0.89309E+00
   Friction velocity        uk    :  0.14419E-01 0.89309E+00
   Dimensionless distance   yplus :  0.11608E+00 0.71900E+01
   Friction thermal sca.    tstar : -0.79745E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86609E-01 0.53645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10522E-01      33   0.25036E-03   0.47320E+01 0.18791E+03 
c  Velocity[X]                                      0.16973E+01 
c  Velocity[Y]                                      0.30346E+01 
c  Velocity[Z]                                      0.59603E-30 
c  Pressure     0.11031E-06     522   0.96295E-08   0.10587E+00 0.11122E+04 
c  nu_tilda     0.77350E-05      33   0.51971E-05   0.69913E-06 0.21557E+03 
c  TempC        0.42352E+02      27   0.32511E-03   0.53010E+01 0.26137E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3917          9.6683          4.5729          4.5729
v  Velocity[Y]            -3.0641          7.2228         0.20549         0.20549
v  Velocity[Z]       -9.7205e-015     6.8323e-015    -1.6072e-017    -1.6072e-017
v  ǁVelocityǁ         0.0027553          9.6698          5.1192          5.1192
v  Pressure               -26.293          26.103         -2.2741         -2.2741
v  nu_tilda            4.412e-007       0.0042695       0.0017195       0.0017195
v  TempC                       21          73.051           22.04           22.04
v  TurbVisc           3.3347e-014       0.0050321       0.0020209       0.0020209
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2251:        0.21970E+01

===============================================================


 INSTANT    0.225200000E+04   TIME STEP NUMBER            2252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15517E-01 0.89273E+00
   Friction velocity        uk    :  0.15517E-01 0.89273E+00
   Dimensionless distance   yplus :  0.12492E+00 0.71871E+01
   Friction thermal sca.    tstar : -0.89699E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93206E-01 0.53624E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10524E-01      33   0.24992E-03   0.47719E+01 0.18807E+03 
c  Velocity[X]                                      0.17440E+01 
c  Velocity[Y]                                      0.30278E+01 
c  Velocity[Z]                                      0.69878E-30 
c  Pressure     0.10108E-06     505   0.96817E-08   0.10078E+00 0.11523E+04 
c  nu_tilda     0.77370E-05      33   0.14303E-04   0.69934E-06 0.21558E+03 
c  TempC        0.42358E+02      27   0.32796E-03   0.54635E+01 0.27213E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3959          9.6672          4.5729          4.5729
v  Velocity[Y]            -3.0642          7.1965         0.20572         0.20572
v  Velocity[Z]        -9.824e-015     7.4241e-015    -1.6067e-017    -1.6067e-017
v  ǁVelocityǁ          0.002509          9.6687          5.1191          5.1191
v  Pressure               -26.305          25.972         -2.2969         -2.2969
v  nu_tilda           4.4122e-007       0.0042695       0.0017197       0.0017197
v  TempC                       21           73.05           22.04           22.04
v  TurbVisc           3.3336e-014       0.0050321       0.0020212       0.0020212
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2252:        0.21530E+01

===============================================================


 INSTANT    0.225300000E+04   TIME STEP NUMBER            2253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14385E-01 0.89147E+00
   Friction velocity        uk    :  0.14385E-01 0.89147E+00
   Dimensionless distance   yplus :  0.11581E+00 0.71769E+01
   Friction thermal sca.    tstar : -0.10217E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86404E-01 0.53548E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10525E-01      33   0.24221E-03   0.47457E+01 0.18805E+03 
c  Velocity[X]                                      0.16999E+01 
c  Velocity[Y]                                      0.30458E+01 
c  Velocity[Z]                                      0.72099E-30 
c  Pressure     0.84700E-07     553   0.99231E-08   0.82859E-01 0.17603E+04 
c  nu_tilda     0.77391E-05      33   0.51865E-05   0.69951E-06 0.21560E+03 
c  TempC        0.42364E+02      27   0.30608E-03   0.56429E+01 0.27932E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -4.4          9.6661          4.5729          4.5729
v  Velocity[Y]            -3.0641           7.217         0.20594         0.20594
v  Velocity[Z]       -9.9147e-015     7.0047e-015    -1.6062e-017    -1.6062e-017
v  ǁVelocityǁ         0.0027903          9.6676          5.1189          5.1189
v  Pressure               -26.256          26.181         -2.2166         -2.2166
v  nu_tilda            4.412e-007       0.0042695       0.0017201       0.0017201
v  TempC                       21           73.05           22.04           22.04
v  TurbVisc           3.3342e-014       0.0050321       0.0020216       0.0020216
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2253:        0.22790E+01

===============================================================


 INSTANT    0.225400000E+04   TIME STEP NUMBER            2254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15683E-01 0.89226E+00
   Friction velocity        uk    :  0.15683E-01 0.89226E+00
   Dimensionless distance   yplus :  0.12626E+00 0.71833E+01
   Friction thermal sca.    tstar : -0.12532E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94203E-01 0.53595E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10526E-01      33   0.26089E-03   0.47496E+01 0.18807E+03 
c  Velocity[X]                                      0.17127E+01 
c  Velocity[Y]                                      0.30370E+01 
c  Velocity[Z]                                      0.72225E-30 
c  Pressure     0.11172E-06     520   0.97602E-08   0.10965E+00 0.14654E+04 
c  nu_tilda     0.77412E-05      33   0.14301E-04   0.69975E-06 0.21561E+03 
c  TempC        0.42370E+02      27   0.27744E-03   0.53239E+01 0.25735E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4041           9.665          4.5729          4.5729
v  Velocity[Y]             -3.064          7.1894         0.20617         0.20617
v  Velocity[Z]       -1.0142e-014     6.9244e-015    -1.6066e-017    -1.6066e-017
v  ǁVelocityǁ         0.0024735          9.6664          5.1188          5.1188
v  Pressure               -26.267          25.993         -2.2517         -2.2517
v  nu_tilda           4.4118e-007       0.0042695       0.0017203       0.0017203
v  TempC                       21           73.05           22.04           22.04
v  TurbVisc           3.3335e-014       0.0050321       0.0020219       0.0020219
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2254:        0.21850E+01

===============================================================


 INSTANT    0.225500000E+04   TIME STEP NUMBER            2255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47219E-02 0.89164E+00
   Friction velocity        uk    :  0.47219E-02 0.89164E+00
   Dimensionless distance   yplus :  0.38014E-01 0.71783E+01
   Friction thermal sca.    tstar : -0.16681E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28363E-01 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10528E-01      33   0.27397E-03   0.47540E+01 0.18811E+03 
c  Velocity[X]                                      0.17269E+01 
c  Velocity[Y]                                      0.30272E+01 
c  Velocity[Z]                                      0.77024E-30 
c  Pressure     0.10555E-06     569   0.96042E-08   0.10247E+00 0.18361E+04 
c  nu_tilda     0.77433E-05      33   0.51900E-05   0.69987E-06 0.21562E+03 
c  TempC        0.42376E+02      27   0.30105E-03   0.49312E+01 0.25174E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4081          9.6639          4.5729          4.5729
v  Velocity[Y]            -3.0639          7.2169          0.2064          0.2064
v  Velocity[Z]       -9.6153e-015     6.9241e-015    -1.6063e-017    -1.6063e-017
v  ǁVelocityǁ         0.0027363          9.6653          5.1186          5.1186
v  Pressure               -26.221          26.214         -2.1701         -2.1701
v  nu_tilda           4.4109e-007       0.0042695       0.0017207       0.0017207
v  TempC                       21           73.05           22.04           22.04
v  TurbVisc           3.3328e-014       0.0050321       0.0020223       0.0020223
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2255:        0.23060E+01

===============================================================


 INSTANT    0.225600000E+04   TIME STEP NUMBER            2256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57052E-02 0.89286E+00
   Friction velocity        uk    :  0.57052E-02 0.89286E+00
   Dimensionless distance   yplus :  0.45930E-01 0.71881E+01
   Friction thermal sca.    tstar : -0.54357E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34269E-01 0.53631E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10529E-01      33   0.24619E-03   0.47486E+01 0.18813E+03 
c  Velocity[X]                                      0.17080E+01 
c  Velocity[Y]                                      0.30406E+01 
c  Velocity[Z]                                      0.73911E-30 
c  Pressure     0.98752E-07     440   0.90648E-08   0.96774E-01 0.74491E+03 
c  nu_tilda     0.77453E-05      33   0.14289E-04   0.70005E-06 0.21563E+03 
c  TempC        0.42383E+02      27   0.29524E-03   0.48206E+01 0.25475E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4124          9.6627          4.5729          4.5729
v  Velocity[Y]            -3.0637           7.223         0.20662         0.20662
v  Velocity[Z]       -9.7144e-015     7.5017e-015    -1.6056e-017    -1.6056e-017
v  ǁVelocityǁ         0.0028673          9.6642          5.1185          5.1185
v  Pressure               -26.235          26.177         -2.1754         -2.1754
v  nu_tilda           4.4097e-007       0.0042695       0.0017209       0.0017209
v  TempC                       21           73.05          22.041          22.041
v  TurbVisc           3.3301e-014       0.0050321       0.0020226       0.0020226
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2256:        0.21310E+01

===============================================================


 INSTANT    0.225700000E+04   TIME STEP NUMBER            2257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93709E-02 0.89240E+00
   Friction velocity        uk    :  0.93709E-02 0.89240E+00
   Dimensionless distance   yplus :  0.75442E-01 0.71845E+01
   Friction thermal sca.    tstar : -0.20819E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56288E-01 0.53604E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10530E-01      33   0.23895E-03   0.47551E+01 0.18810E+03 
c  Velocity[X]                                      0.17253E+01 
c  Velocity[Y]                                      0.30298E+01 
c  Velocity[Z]                                      0.67118E-30 
c  Pressure     0.11932E-06     441   0.95101E-08   0.11692E+00 0.70269E+03 
c  nu_tilda     0.77474E-05      33   0.51788E-05   0.70020E-06 0.21564E+03 
c  TempC        0.42389E+02      27   0.33943E-03   0.50307E+01 0.26808E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4165          9.6616          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.1927         0.20684         0.20684
v  Velocity[Z]       -9.9569e-015     6.9464e-015    -1.6056e-017    -1.6056e-017
v  ǁVelocityǁ         0.0024937          9.6631          5.1183          5.1183
v  Pressure                -26.18          26.127          -2.148          -2.148
v  nu_tilda           4.4095e-007       0.0042695       0.0017213       0.0017213
v  TempC                       21           73.05          22.041          22.041
v  TurbVisc           3.3265e-014       0.0050321        0.002023        0.002023
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2257:        0.22890E+01

===============================================================


 INSTANT    0.225800000E+04   TIME STEP NUMBER            2258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13803E-01 0.89115E+00
   Friction velocity        uk    :  0.13803E-01 0.89115E+00
   Dimensionless distance   yplus :  0.11112E+00 0.71743E+01
   Friction thermal sca.    tstar : -0.13096E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82910E-01 0.53529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10532E-01      33   0.24759E-03   0.47481E+01 0.18808E+03 
c  Velocity[X]                                      0.17274E+01 
c  Velocity[Y]                                      0.30207E+01 
c  Velocity[Z]                                      0.72035E-30 
c  Pressure     0.91441E-07     440   0.95541E-08   0.89976E-01 0.68175E+03 
c  nu_tilda     0.77495E-05      33   0.14293E-04   0.70042E-06 0.21566E+03 
c  TempC        0.42395E+02      27   0.27102E-03   0.60822E+01 0.28787E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4208          9.6605          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.2132         0.20706         0.20706
v  Velocity[Z]       -9.7941e-015     6.9246e-015    -1.6053e-017    -1.6053e-017
v  ǁVelocityǁ         0.0027827          9.6619          5.1182          5.1182
v  Pressure               -26.199           26.21         -2.1285         -2.1285
v  nu_tilda           4.4097e-007       0.0042695       0.0017215       0.0017215
v  TempC                       21          73.049          22.041          22.041
v  TurbVisc           3.3261e-014       0.0050321       0.0020233       0.0020233
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2258:        0.20120E+01

===============================================================


 INSTANT    0.225900000E+04   TIME STEP NUMBER            2259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13648E-01 0.89226E+00
   Friction velocity        uk    :  0.13648E-01 0.89226E+00
   Dimensionless distance   yplus :  0.10987E+00 0.71833E+01
   Friction thermal sca.    tstar : -0.10963E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81979E-01 0.53596E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10533E-01      33   0.25152E-03   0.47483E+01 0.18816E+03 
c  Velocity[X]                                      0.17089E+01 
c  Velocity[Y]                                      0.30394E+01 
c  Velocity[Z]                                      0.66475E-30 
c  Pressure     0.10576E-06     473   0.93716E-08   0.10411E+00 0.76464E+03 
c  nu_tilda     0.77516E-05      33   0.51819E-05   0.70055E-06 0.21567E+03 
c  TempC        0.42401E+02      27   0.27259E-03   0.44940E+01 0.24984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4248          9.6593          4.5729          4.5729
v  Velocity[Y]            -3.0637          7.1917         0.20729         0.20729
v  Velocity[Z]       -9.8761e-015     6.7585e-015    -1.6051e-017    -1.6051e-017
v  ǁVelocityǁ         0.0025487          9.6608           5.118           5.118
v  Pressure               -26.143          26.202         -2.0927         -2.0927
v  nu_tilda           4.4102e-007       0.0042695       0.0017219       0.0017219
v  TempC                       21          73.049          22.041          22.041
v  TurbVisc           3.3265e-014       0.0050321       0.0020237       0.0020237
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2259:        0.20840E+01

===============================================================


 INSTANT    0.226000000E+04   TIME STEP NUMBER            2260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14249E-01 0.89133E+00
   Friction velocity        uk    :  0.14249E-01 0.89133E+00
   Dimensionless distance   yplus :  0.11471E+00 0.71758E+01
   Friction thermal sca.    tstar : -0.91737E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85589E-01 0.53540E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10534E-01      33   0.20932E-03   0.47362E+01 0.18808E+03 
c  Velocity[X]                                      0.17128E+01 
c  Velocity[Y]                                      0.30234E+01 
c  Velocity[Z]                                      0.80195E-30 
c  Pressure     0.10268E-06     329   0.97847E-08   0.99598E-01 0.60109E+03 
c  nu_tilda     0.77536E-05      33   0.14280E-04   0.70074E-06 0.21568E+03 
c  TempC        0.42407E+02      27   0.32572E-03   0.48409E+01 0.24863E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.429          9.6582          4.5729          4.5729
v  Velocity[Y]            -3.0636          7.2118         0.20751         0.20751
v  Velocity[Z]       -9.9644e-015     7.3781e-015    -1.6043e-017    -1.6043e-017
v  ǁVelocityǁ         0.0026707          9.6597          5.1179          5.1179
v  Pressure               -26.161          26.222         -2.0854         -2.0854
v  nu_tilda           4.4106e-007       0.0042695       0.0017221       0.0017221
v  TempC                       21          73.049          22.041          22.041
v  TurbVisc           3.3282e-014       0.0050321        0.002024        0.002024
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2260:        0.17490E+01

===============================================================


 INSTANT    0.226100000E+04   TIME STEP NUMBER            2261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.70738E-02 0.89307E+00
   Friction velocity        uk    :  0.70738E-02 0.89307E+00
   Dimensionless distance   yplus :  0.56949E-01 0.71898E+01
   Friction thermal sca.    tstar : -0.83203E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42490E-01 0.53644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10536E-01      33   0.27176E-03   0.47286E+01 0.18808E+03 
c  Velocity[X]                                      0.17082E+01 
c  Velocity[Y]                                      0.30204E+01 
c  Velocity[Z]                                      0.79706E-30 
c  Pressure     0.98164E-07     521   0.97087E-08   0.97119E-01 0.14115E+04 
c  nu_tilda     0.77557E-05      33   0.51696E-05   0.70087E-06 0.21569E+03 
c  TempC        0.42413E+02      27   0.28608E-03   0.51808E+01 0.25724E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.433           9.657          4.5729          4.5729
v  Velocity[Y]            -3.0634           7.225         0.20772         0.20772
v  Velocity[Z]       -1.0108e-014     6.7642e-015    -1.6046e-017    -1.6046e-017
v  ǁVelocityǁ         0.0028456          9.6585          5.1177          5.1177
v  Pressure                -26.11          26.362         -2.0177         -2.0177
v  nu_tilda           4.4099e-007       0.0042695       0.0017225       0.0017225
v  TempC                       21           73.05          22.041          22.041
v  TurbVisc           3.3294e-014       0.0050321       0.0020244       0.0020244
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2261:        0.21860E+01

===============================================================


 INSTANT    0.226200000E+04   TIME STEP NUMBER            2262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15984E-01 0.89258E+00
   Friction velocity        uk    :  0.15984E-01 0.89258E+00
   Dimensionless distance   yplus :  0.12868E+00 0.71859E+01
   Friction thermal sca.    tstar : -0.76182E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96012E-01 0.53615E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10537E-01      33   0.24374E-03   0.47675E+01 0.18829E+03 
c  Velocity[X]                                      0.17314E+01 
c  Velocity[Y]                                      0.30361E+01 
c  Velocity[Z]                                      0.63463E-30 
c  Pressure     0.10449E-06     505   0.93485E-08   0.10425E+00 0.14078E+04 
c  nu_tilda     0.77577E-05      33   0.14281E-04   0.70106E-06 0.21570E+03 
c  TempC        0.42419E+02      27   0.28053E-03   0.45502E+01 0.22675E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4371          9.6559          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.1954         0.20794         0.20794
v  Velocity[Z]       -9.8343e-015     6.5286e-015    -1.6046e-017    -1.6046e-017
v  ǁVelocityǁ          0.002577          9.6574          5.1176          5.1176
v  Pressure               -26.124          26.192         -2.0524         -2.0524
v  nu_tilda           4.4098e-007       0.0042695       0.0017227       0.0017227
v  TempC                       21           73.05          22.041          22.041
v  TurbVisc           3.3273e-014       0.0050321       0.0020247       0.0020247
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2262:        0.21690E+01

===============================================================


 INSTANT    0.226300000E+04   TIME STEP NUMBER            2263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14855E-01 0.89118E+00
   Friction velocity        uk    :  0.14855E-01 0.89118E+00
   Dimensionless distance   yplus :  0.11959E+00 0.71746E+01
   Friction thermal sca.    tstar : -0.70383E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89231E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10538E-01      33   0.24449E-03   0.47366E+01 0.18813E+03 
c  Velocity[X]                                      0.17144E+01 
c  Velocity[Y]                                      0.30223E+01 
c  Velocity[Z]                                      0.57230E-30 
c  Pressure     0.10987E-06     552   0.91468E-08   0.10541E+00 0.15639E+04 
c  nu_tilda     0.77598E-05      33   0.51723E-05   0.70121E-06 0.21571E+03 
c  TempC        0.42425E+02      27   0.32275E-03   0.40531E+01 0.23049E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4411          9.6548          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.2116         0.20816         0.20816
v  Velocity[Z]        -9.978e-015     6.5355e-015     -1.604e-017     -1.604e-017
v  ǁVelocityǁ         0.0027164          9.6563          5.1174          5.1174
v  Pressure               -26.071          26.363         -1.9789         -1.9789
v  nu_tilda           4.4102e-007       0.0042695       0.0017231       0.0017231
v  TempC                       21           73.05          22.041          22.041
v  TurbVisc            3.327e-014       0.0050321       0.0020251       0.0020251
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2263:        0.22610E+01

===============================================================


 INSTANT    0.226400000E+04   TIME STEP NUMBER            2264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.81359E-02 0.89224E+00
   Friction velocity        uk    :  0.81359E-02 0.89224E+00
   Dimensionless distance   yplus :  0.65499E-01 0.71831E+01
   Friction thermal sca.    tstar : -0.65037E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48870E-01 0.53594E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10540E-01      33   0.26251E-03   0.47537E+01 0.18821E+03 
c  Velocity[X]                                      0.17399E+01 
c  Velocity[Y]                                      0.30138E+01 
c  Velocity[Z]                                      0.74322E-30 
c  Pressure     0.96178E-07     474   0.93559E-08   0.95407E-01 0.11379E+04 
c  nu_tilda     0.77619E-05      33   0.14270E-04   0.70141E-06 0.21573E+03 
c  TempC        0.42431E+02      27   0.30790E-03   0.49965E+01 0.26030E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.445          9.6536          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.1907         0.20838         0.20838
v  Velocity[Z]       -9.8354e-015     7.4071e-015    -1.6032e-017    -1.6032e-017
v  ǁVelocityǁ         0.0025016          9.6551          5.1173          5.1173
v  Pressure               -26.084          26.235         -2.0014         -2.0014
v  nu_tilda           4.4109e-007       0.0042695       0.0017233       0.0017233
v  TempC                       21          73.049          22.041          22.041
v  TurbVisc           3.3283e-014       0.0050321       0.0020254       0.0020254
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2264:        0.20870E+01

===============================================================


 INSTANT    0.226500000E+04   TIME STEP NUMBER            2265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14347E-01 0.89155E+00
   Friction velocity        uk    :  0.14347E-01 0.89155E+00
   Dimensionless distance   yplus :  0.11551E+00 0.71776E+01
   Friction thermal sca.    tstar : -0.61527E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86180E-01 0.53553E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10541E-01      33   0.23974E-03   0.47412E+01 0.18823E+03 
c  Velocity[X]                                      0.17086E+01 
c  Velocity[Y]                                      0.30326E+01 
c  Velocity[Z]                                      0.71728E-30 
c  Pressure     0.87980E-07     522   0.99623E-08   0.86115E-01 0.18071E+04 
c  nu_tilda     0.77639E-05      33   0.51606E-05   0.70155E-06 0.21574E+03 
c  TempC        0.42437E+02      27   0.32802E-03   0.48742E+01 0.26238E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4489          9.6525          4.5729          4.5729
v  Velocity[Y]            -3.0632          7.2159         0.20859         0.20859
v  Velocity[Z]       -9.9373e-015     6.6623e-015    -1.6035e-017    -1.6035e-017
v  ǁVelocityǁ         0.0027945           9.654          5.1171          5.1171
v  Pressure               -26.035          26.447         -1.9196         -1.9196
v  nu_tilda           4.4106e-007       0.0042695       0.0017237       0.0017237
v  TempC                       21           73.05          22.041          22.041
v  TurbVisc           3.3303e-014       0.0050321       0.0020258       0.0020258
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2265:        0.21830E+01

===============================================================


 INSTANT    0.226600000E+04   TIME STEP NUMBER            2266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15713E-01 0.89264E+00
   Friction velocity        uk    :  0.15713E-01 0.89264E+00
   Dimensionless distance   yplus :  0.12650E+00 0.71864E+01
   Friction thermal sca.    tstar : -0.58735E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94383E-01 0.53619E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10542E-01      33   0.25372E-03   0.47174E+01 0.18816E+03 
c  Velocity[X]                                      0.16935E+01 
c  Velocity[Y]                                      0.30239E+01 
c  Velocity[Z]                                      0.68043E-30 
c  Pressure     0.10494E-06     472   0.96776E-08   0.10147E+00 0.91730E+03 
c  nu_tilda     0.77660E-05      33   0.14269E-04   0.70176E-06 0.21575E+03 
c  TempC        0.42443E+02      27   0.26263E-03   0.52448E+01 0.26447E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4531          9.6513          4.5729          4.5729
v  Velocity[Y]            -3.0631          7.2177         0.20881         0.20881
v  Velocity[Z]       -9.8305e-015     6.5739e-015    -1.6036e-017    -1.6036e-017
v  ǁVelocityǁ         0.0028408          9.6529           5.117           5.117
v  Pressure               -26.051          26.368         -1.9353         -1.9353
v  nu_tilda           4.4102e-007       0.0042695       0.0017239       0.0017239
v  TempC                       21           73.05          22.042          22.042
v  TurbVisc           3.3292e-014       0.0050321       0.0020261       0.0020261
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2266:        0.20890E+01

===============================================================


 INSTANT    0.226700000E+04   TIME STEP NUMBER            2267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15885E-01 0.89239E+00
   Friction velocity        uk    :  0.15885E-01 0.89239E+00
   Dimensionless distance   yplus :  0.12788E+00 0.71844E+01
   Friction thermal sca.    tstar : -0.59113E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95415E-01 0.53603E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10543E-01      33   0.27367E-03   0.47527E+01 0.18831E+03 
c  Velocity[X]                                      0.17382E+01 
c  Velocity[Y]                                      0.30145E+01 
c  Velocity[Z]                                      0.72952E-30 
c  Pressure     0.11844E-06     504   0.96222E-08   0.11702E+00 0.80722E+03 
c  nu_tilda     0.77680E-05      33   0.51615E-05   0.70188E-06 0.21576E+03 
c  TempC        0.42449E+02      27   0.29797E-03   0.39956E+01 0.24198E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4571          9.6502          4.5729          4.5729
v  Velocity[Y]            -3.0629          7.1939         0.20902         0.20902
v  Velocity[Z]       -9.8705e-015     6.4542e-015     -1.604e-017     -1.604e-017
v  ǁVelocityǁ         0.0017744          9.6517          5.1168          5.1168
v  Pressure               -25.996          26.372          -1.896          -1.896
v  nu_tilda           4.4112e-007       0.0042695       0.0017242       0.0017242
v  TempC                       21           73.05          22.042          22.042
v  TurbVisc            3.328e-014       0.0050321       0.0020265       0.0020265
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2267:        0.21530E+01

===============================================================


 INSTANT    0.226800000E+04   TIME STEP NUMBER            2268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10494E-01 0.89105E+00
   Friction velocity        uk    :  0.10494E-01 0.89105E+00
   Dimensionless distance   yplus :  0.84487E-01 0.71736E+01
   Friction thermal sca.    tstar : -0.59640E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63037E-01 0.53523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10545E-01      33   0.24864E-03   0.47540E+01 0.18836E+03 
c  Velocity[X]                                      0.17255E+01 
c  Velocity[Y]                                      0.30286E+01 
c  Velocity[Z]                                      0.82132E-30 
c  Pressure     0.10061E-06     424   0.90307E-08   0.98561E-01 0.63928E+03 
c  nu_tilda     0.77701E-05      33   0.14261E-04   0.70206E-06 0.21577E+03 
c  TempC        0.42455E+02      27   0.27994E-03   0.51289E+01 0.26348E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4613           9.649          4.5729          4.5729
v  Velocity[Y]            -3.0627          7.2126         0.20924         0.20924
v  Velocity[Z]       -9.8335e-015     7.5112e-015    -1.6038e-017    -1.6038e-017
v  ǁVelocityǁ         0.0016717          9.6506          5.1167          5.1167
v  Pressure               -26.016          26.442         -1.8801         -1.8801
v  nu_tilda           4.4121e-007       0.0042695       0.0017245       0.0017245
v  TempC                       21          73.049          22.042          22.042
v  TurbVisc           3.3312e-014       0.0050321       0.0020268       0.0020268
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2268:        0.19600E+01

===============================================================


 INSTANT    0.226900000E+04   TIME STEP NUMBER            2269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13094E-01 0.89216E+00
   Friction velocity        uk    :  0.13094E-01 0.89216E+00
   Dimensionless distance   yplus :  0.10542E+00 0.71825E+01
   Friction thermal sca.    tstar : -0.58512E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78653E-01 0.53590E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10546E-01      33   0.24683E-03   0.47396E+01 0.18825E+03 
c  Velocity[X]                                      0.17238E+01 
c  Velocity[Y]                                      0.30158E+01 
c  Velocity[Z]                                      0.69207E-30 
c  Pressure     0.11607E-06     472   0.93423E-08   0.11339E+00 0.69247E+03 
c  nu_tilda     0.77721E-05      33   0.51518E-05   0.70220E-06 0.21578E+03 
c  TempC        0.42461E+02      27   0.32206E-03   0.50770E+01 0.25420E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4652          9.6479          4.5729          4.5729
v  Velocity[Y]            -3.0627          7.1889         0.20945         0.20945
v  Velocity[Z]       -9.8944e-015      6.628e-015    -1.6037e-017    -1.6037e-017
v  ǁVelocityǁ         0.0025009          9.6495          5.1165          5.1165
v  Pressure               -25.962          26.392         -1.8541         -1.8541
v  nu_tilda           4.4125e-007       0.0042695       0.0017248       0.0017248
v  TempC                       21           73.05          22.042          22.042
v  TurbVisc            3.334e-014       0.0050321       0.0020272       0.0020272
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2269:        0.20820E+01

===============================================================


 INSTANT    0.227000000E+04   TIME STEP NUMBER            2270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13869E-01 0.89151E+00
   Friction velocity        uk    :  0.13869E-01 0.89151E+00
   Dimensionless distance   yplus :  0.11165E+00 0.71773E+01
   Friction thermal sca.    tstar : -0.59835E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83304E-01 0.53550E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10547E-01      33   0.20024E-03   0.47433E+01 0.18826E+03 
c  Velocity[X]                                      0.17351E+01 
c  Velocity[Y]                                      0.30082E+01 
c  Velocity[Z]                                      0.66067E-30 
c  Pressure     0.93464E-07     440   0.96236E-08   0.92120E-01 0.68289E+03 
c  nu_tilda     0.77742E-05      33   0.14260E-04   0.70239E-06 0.21579E+03 
c  TempC        0.42466E+02      27   0.26395E-03   0.55781E+01 0.26874E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4693          9.6467          4.5729          4.5729
v  Velocity[Y]            -3.0626          7.2138         0.20966         0.20966
v  Velocity[Z]       -1.0057e-014     6.4934e-015    -1.6043e-017    -1.6043e-017
v  ǁVelocityǁ         0.0028267          9.6483          5.1163          5.1163
v  Pressure               -25.982          26.477         -1.8352         -1.8352
v  nu_tilda           4.4122e-007       0.0042695        0.001725        0.001725
v  TempC                       21           73.05          22.042          22.042
v  TurbVisc            3.335e-014       0.0050321       0.0020275       0.0020275
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2270:        0.20090E+01

===============================================================


 INSTANT    0.227100000E+04   TIME STEP NUMBER            2271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16035E-01 0.89297E+00
   Friction velocity        uk    :  0.16035E-01 0.89297E+00
   Dimensionless distance   yplus :  0.12909E+00 0.71890E+01
   Friction thermal sca.    tstar : -0.59175E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96315E-01 0.53638E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10548E-01      33   0.24251E-03   0.47168E+01 0.18824E+03 
c  Velocity[X]                                      0.16905E+01 
c  Velocity[Y]                                      0.30264E+01 
c  Velocity[Z]                                      0.60445E-30 
c  Pressure     0.92032E-07     537   0.98155E-08   0.89755E-01 0.11325E+04 
c  nu_tilda     0.77762E-05      33   0.51511E-05   0.70251E-06 0.21580E+03 
c  TempC        0.42472E+02      27   0.25499E-03   0.52290E+01 0.26589E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4732          9.6456          4.5729          4.5729
v  Velocity[Y]            -3.0626          7.2238         0.20988         0.20988
v  Velocity[Z]       -9.9487e-015     6.3565e-015    -1.6045e-017    -1.6045e-017
v  ǁVelocityǁ          0.002879          9.6472          5.1162          5.1162
v  Pressure               -25.929          26.566         -1.7795         -1.7795
v  nu_tilda           4.4113e-007       0.0042695       0.0017254       0.0017254
v  TempC                       21          73.051          22.042          22.042
v  TurbVisc           3.3343e-014       0.0050321       0.0020278       0.0020278
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2271:        0.22340E+01

===============================================================


 INSTANT    0.227200000E+04   TIME STEP NUMBER            2272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.36432E-02 0.89244E+00
   Friction velocity        uk    :  0.36432E-02 0.89244E+00
   Dimensionless distance   yplus :  0.29330E-01 0.71848E+01
   Friction thermal sca.    tstar : -0.58429E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21884E-01 0.53606E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10550E-01      33   0.25429E-03   0.47379E+01 0.18829E+03 
c  Velocity[X]                                      0.17268E+01 
c  Velocity[Y]                                      0.30111E+01 
c  Velocity[Z]                                      0.72258E-30 
c  Pressure     0.10829E-06     520   0.98754E-08   0.10647E+00 0.13958E+04 
c  nu_tilda     0.77783E-05      33   0.14249E-04   0.70268E-06 0.21581E+03 
c  TempC        0.42478E+02      27   0.34288E-03   0.48129E+01 0.26177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4772          9.6444          4.5729          4.5729
v  Velocity[Y]            -3.0624           7.191         0.21009         0.21009
v  Velocity[Z]        -1.001e-014     7.4236e-015    -1.6042e-017    -1.6042e-017
v  ǁVelocityǁ         0.0025411           9.646           5.116           5.116
v  Pressure               -25.942          26.395         -1.8128         -1.8128
v  nu_tilda           4.4111e-007       0.0042695       0.0017256       0.0017256
v  TempC                       21           73.05          22.042          22.042
v  TurbVisc           3.3315e-014       0.0050321       0.0020282       0.0020282
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2272:        0.21970E+01

===============================================================


 INSTANT    0.227300000E+04   TIME STEP NUMBER            2273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54334E-02 0.89126E+00
   Friction velocity        uk    :  0.54334E-02 0.89126E+00
   Dimensionless distance   yplus :  0.43743E-01 0.71753E+01
   Friction thermal sca.    tstar : -0.59447E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32637E-01 0.53536E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10551E-01      33   0.26750E-03   0.47317E+01 0.18831E+03 
c  Velocity[X]                                      0.17260E+01 
c  Velocity[Y]                                      0.30056E+01 
c  Velocity[Z]                                      0.93618E-30 
c  Pressure     0.94994E-07     584   0.92039E-08   0.92950E-01 0.18506E+04 
c  nu_tilda     0.77803E-05      33   0.51417E-05   0.70280E-06 0.21582E+03 
c  TempC        0.42484E+02      27   0.27901E-03   0.62786E+01 0.29732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4811          9.6433          4.5729          4.5729
v  Velocity[Y]            -3.0623          7.2147          0.2103          0.2103
v  Velocity[Z]        -9.774e-015      6.791e-015    -1.6046e-017    -1.6046e-017
v  ǁVelocityǁ         0.0027984          9.6449          5.1159          5.1159
v  Pressure               -25.893          26.611         -1.7295         -1.7295
v  nu_tilda           4.4108e-007       0.0042695        0.001726        0.001726
v  TempC                       21          73.051          22.042          22.042
v  TurbVisc            3.331e-014       0.0050321       0.0020285       0.0020285
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2273:        0.23300E+01

===============================================================


 INSTANT    0.227400000E+04   TIME STEP NUMBER            2274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15732E-01 0.89225E+00
   Friction velocity        uk    :  0.15732E-01 0.89225E+00
   Dimensionless distance   yplus :  0.12665E+00 0.71832E+01
   Friction thermal sca.    tstar : -0.58703E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94497E-01 0.53595E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10552E-01      33   0.25684E-03   0.47524E+01 0.18844E+03 
c  Velocity[X]                                      0.17305E+01 
c  Velocity[Y]                                      0.30219E+01 
c  Velocity[Z]                                      0.72978E-30 
c  Pressure     0.10207E-06     504   0.95977E-08   0.10153E+00 0.12701E+04 
c  nu_tilda     0.77824E-05      33   0.14248E-04   0.70299E-06 0.21583E+03 
c  TempC        0.42490E+02      27   0.30099E-03   0.55680E+01 0.25732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.485          9.6422          4.5729          4.5729
v  Velocity[Y]             -3.062          7.1895          0.2105          0.2105
v  Velocity[Z]       -9.6518e-015     6.3769e-015    -1.6047e-017    -1.6047e-017
v  ǁVelocityǁ         0.0026353          9.6437          5.1157          5.1157
v  Pressure               -25.909          26.468         -1.7592         -1.7592
v  nu_tilda           4.4106e-007       0.0042695       0.0017262       0.0017262
v  TempC                       21           73.05          22.042          22.042
v  TurbVisc           3.3301e-014       0.0050321       0.0020289       0.0020289
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2274:        0.21400E+01

===============================================================


 INSTANT    0.227500000E+04   TIME STEP NUMBER            2275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15203E-01 0.89128E+00
   Friction velocity        uk    :  0.15203E-01 0.89128E+00
   Dimensionless distance   yplus :  0.12239E+00 0.71754E+01
   Friction thermal sca.    tstar : -0.59664E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91320E-01 0.53537E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10553E-01      33   0.24258E-03   0.47344E+01 0.18832E+03 
c  Velocity[X]                                      0.17247E+01 
c  Velocity[Y]                                      0.30097E+01 
c  Velocity[Z]                                      0.48124E-30 
c  Pressure     0.11224E-06     552   0.99445E-08   0.10751E+00 0.15175E+04 
c  nu_tilda     0.77844E-05      33   0.51398E-05   0.70312E-06 0.21584E+03 
c  TempC        0.42496E+02      27   0.24556E-03   0.47218E+01 0.25576E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4888           9.641          4.5729          4.5729
v  Velocity[Y]             -3.062          7.2109         0.21071         0.21071
v  Velocity[Z]       -9.8364e-015     6.3713e-015     -1.605e-017     -1.605e-017
v  ǁVelocityǁ         0.0027521          9.6426          5.1156          5.1156
v  Pressure               -25.857          26.627          -1.688          -1.688
v  nu_tilda           4.4105e-007       0.0042695       0.0017266       0.0017266
v  TempC                       21          73.051          22.043          22.043
v  TurbVisc           3.3295e-014       0.0050321       0.0020292       0.0020292
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2275:        0.22580E+01

===============================================================


 INSTANT    0.227600000E+04   TIME STEP NUMBER            2276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15507E-01 0.89266E+00
   Friction velocity        uk    :  0.15507E-01 0.89266E+00
   Dimensionless distance   yplus :  0.12484E+00 0.71865E+01
   Friction thermal sca.    tstar : -0.58874E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93144E-01 0.53620E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10555E-01      33   0.25519E-03   0.47219E+01 0.18829E+03 
c  Velocity[X]                                      0.17208E+01 
c  Velocity[Y]                                      0.30011E+01 
c  Velocity[Z]                                      0.73537E-30 
c  Pressure     0.85842E-07     456   0.97238E-08   0.84361E-01 0.70324E+03 
c  nu_tilda     0.77865E-05      33   0.14238E-04   0.70330E-06 0.21585E+03 
c  TempC        0.42502E+02      27   0.25475E-03   0.35797E+01 0.23855E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4928          9.6399          4.5729          4.5729
v  Velocity[Y]             -3.062          7.2197         0.21092         0.21092
v  Velocity[Z]       -9.7017e-015      7.398e-015    -1.6048e-017    -1.6048e-017
v  ǁVelocityǁ         0.0028769          9.6414          5.1154          5.1154
v  Pressure               -25.875            26.6         -1.6928         -1.6928
v  nu_tilda           4.4094e-007       0.0042695       0.0017268       0.0017268
v  TempC                       21           73.05          22.043          22.043
v  TurbVisc            3.329e-014       0.0050321       0.0020295       0.0020295
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2276:        0.20280E+01

===============================================================


 INSTANT    0.227700000E+04   TIME STEP NUMBER            2277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13294E-01 0.89234E+00
   Friction velocity        uk    :  0.13294E-01 0.89234E+00
   Dimensionless distance   yplus :  0.10703E+00 0.71839E+01
   Friction thermal sca.    tstar : -0.58409E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79856E-01 0.53600E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10556E-01      33   0.23757E-03   0.47404E+01 0.18844E+03 
c  Velocity[X]                                      0.17206E+01 
c  Velocity[Y]                                      0.30198E+01 
c  Velocity[Z]                                      0.77500E-30 
c  Pressure     0.10695E-06     506   0.95806E-08   0.10629E+00 0.80306E+03 
c  nu_tilda     0.77885E-05      33   0.51320E-05   0.70342E-06 0.21586E+03 
c  TempC        0.42508E+02      27   0.37516E-03   0.38385E+01 0.24141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4967          9.6388          4.5729          4.5729
v  Velocity[Y]            -3.0619          7.1927         0.21113         0.21113
v  Velocity[Z]        -9.596e-015      6.688e-015    -1.6052e-017    -1.6052e-017
v  ǁVelocityǁ         0.0026366          9.6403          5.1152          5.1152
v  Pressure                -25.82          26.603         -1.6536         -1.6536
v  nu_tilda           4.4087e-007       0.0042695       0.0017271       0.0017271
v  TempC                       21          73.051          22.043          22.043
v  TurbVisc           3.3258e-014       0.0050321       0.0020299       0.0020299
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2277:        0.21400E+01

===============================================================


 INSTANT    0.227800000E+04   TIME STEP NUMBER            2278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96648E-02 0.89079E+00
   Friction velocity        uk    :  0.96648E-02 0.89079E+00
   Dimensionless distance   yplus :  0.77808E-01 0.71714E+01
   Friction thermal sca.    tstar : -0.59137E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58054E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10557E-01      33   0.25001E-03   0.47145E+01 0.18830E+03 
c  Velocity[X]                                      0.17119E+01 
c  Velocity[Y]                                      0.30026E+01 
c  Velocity[Z]                                      0.63331E-30 
c  Pressure     0.10304E-06     425   0.95632E-08   0.99605E-01 0.61265E+03 
c  nu_tilda     0.77905E-05      33   0.14239E-04   0.70359E-06 0.21587E+03 
c  TempC        0.42514E+02      27   0.29128E-03   0.71003E+01 0.30477E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5007          9.6377          4.5729          4.5729
v  Velocity[Y]            -3.0618          7.2077         0.21133         0.21133
v  Velocity[Z]       -9.6261e-015     6.5652e-015    -1.6054e-017    -1.6054e-017
v  ǁVelocityǁ         0.0027851          9.6391          5.1151          5.1151
v  Pressure                -25.84          26.611         -1.6518         -1.6518
v  nu_tilda           4.4087e-007       0.0042695       0.0017273       0.0017273
v  TempC                       21          73.049          22.043          22.043
v  TurbVisc           3.3237e-014       0.0050321       0.0020302       0.0020302
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2278:        0.19840E+01

===============================================================


 INSTANT    0.227900000E+04   TIME STEP NUMBER            2279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15926E-01 0.89212E+00
   Friction velocity        uk    :  0.15926E-01 0.89212E+00
   Dimensionless distance   yplus :  0.12821E+00 0.71822E+01
   Friction thermal sca.    tstar : -0.62702E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95660E-01 0.53587E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10558E-01      33   0.27662E-03   0.47457E+01 0.18852E+03 
c  Velocity[X]                                      0.17375E+01 
c  Velocity[Y]                                      0.30081E+01 
c  Velocity[Z]                                      0.69078E-30 
c  Pressure     0.11641E-06     505   0.94436E-08   0.11498E+00 0.87947E+03 
c  nu_tilda     0.77926E-05      33   0.51279E-05   0.70375E-06 0.21588E+03 
c  TempC        0.42519E+02      27   0.24532E-03   0.44534E+01 0.25828E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5046          9.6366          4.5729          4.5729
v  Velocity[Y]            -3.0616          7.1895         0.21154         0.21154
v  Velocity[Z]       -9.5592e-015     6.4318e-015    -1.6064e-017    -1.6064e-017
v  ǁVelocityǁ         0.0025532           9.638          5.1149          5.1149
v  Pressure               -25.783           26.63         -1.6078         -1.6078
v  nu_tilda           4.4097e-007       0.0042695       0.0017277       0.0017277
v  TempC                       21          73.049          22.043          22.043
v  TurbVisc           3.3237e-014       0.0050321       0.0020306       0.0020306
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2279:        0.21540E+01

===============================================================


 INSTANT    0.228000000E+04   TIME STEP NUMBER            2280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14284E-01 0.89138E+00
   Friction velocity        uk    :  0.14284E-01 0.89138E+00
   Dimensionless distance   yplus :  0.11500E+00 0.71762E+01
   Friction thermal sca.    tstar : -0.61003E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85801E-01 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10560E-01      33   0.20012E-03   0.47495E+01 0.18857E+03 
c  Velocity[X]                                      0.17315E+01 
c  Velocity[Y]                                      0.30180E+01 
c  Velocity[Z]                                      0.63870E-30 
c  Pressure     0.10160E-06     408   0.97741E-08   0.99414E-01 0.59770E+03 
c  nu_tilda     0.77946E-05      33   0.14228E-04   0.70393E-06 0.21589E+03 
c  TempC        0.42525E+02      27   0.34018E-03   0.34163E+01 0.22777E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5085          9.6354          4.5729          4.5729
v  Velocity[Y]            -3.0613          7.2125         0.21174         0.21174
v  Velocity[Z]       -9.7937e-015     6.3734e-015    -1.6065e-017    -1.6065e-017
v  ǁVelocityǁ         0.0028598          9.6368          5.1148          5.1148
v  Pressure               -25.809          26.695         -1.5975         -1.5975
v  nu_tilda           4.4102e-007       0.0042697       0.0017279       0.0017279
v  TempC                       21          73.049          22.043          22.043
v  TurbVisc           3.3265e-014       0.0050321       0.0020309       0.0020309
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2280:        0.19370E+01

===============================================================


 INSTANT    0.228100000E+04   TIME STEP NUMBER            2281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16384E-01 0.89283E+00
   Friction velocity        uk    :  0.16384E-01 0.89283E+00
   Dimensionless distance   yplus :  0.13190E+00 0.71879E+01
   Friction thermal sca.    tstar : -0.63678E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98412E-01 0.53630E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10561E-01      33   0.24335E-03   0.47082E+01 0.18834E+03 
c  Velocity[X]                                      0.17055E+01 
c  Velocity[Y]                                      0.30026E+01 
c  Velocity[Z]                                      0.60587E-30 
c  Pressure     0.10977E-06     538   0.95159E-08   0.10594E+00 0.95227E+03 
c  nu_tilda     0.77966E-05      33   0.51230E-05   0.70404E-06 0.21590E+03 
c  TempC        0.42531E+02      27   0.27796E-03   0.58648E+01 0.28103E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5124          9.6343          4.5729          4.5729
v  Velocity[Y]            -3.0613          7.2202         0.21195         0.21195
v  Velocity[Z]       -9.5027e-015      6.352e-015    -1.6069e-017    -1.6069e-017
v  ǁVelocityǁ         0.0028217          9.6356          5.1146          5.1146
v  Pressure               -25.755          26.744         -1.5501         -1.5501
v  nu_tilda           4.4097e-007       0.0042704       0.0017283       0.0017283
v  TempC                       21          73.051          22.043          22.043
v  TurbVisc            3.328e-014       0.0050322       0.0020312       0.0020312
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2281:        0.22370E+01

===============================================================


 INSTANT    0.228200000E+04   TIME STEP NUMBER            2282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.99233E-02 0.89258E+00
   Friction velocity        uk    :  0.99233E-02 0.89258E+00
   Dimensionless distance   yplus :  0.79889E-01 0.71859E+01
   Friction thermal sca.    tstar : -0.68471E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59607E-01 0.53615E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10562E-01      33   0.24347E-03   0.47448E+01 0.18848E+03 
c  Velocity[X]                                      0.17489E+01 
c  Velocity[Y]                                      0.29959E+01 
c  Velocity[Z]                                      0.79058E-30 
c  Pressure     0.10097E-06     504   0.92432E-08   0.10103E+00 0.10973E+04 
c  nu_tilda     0.77987E-05      33   0.14226E-04   0.70422E-06 0.21591E+03 
c  TempC        0.42537E+02      27   0.31261E-03   0.47281E+01 0.25216E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5162          9.6332          4.5729          4.5729
v  Velocity[Y]            -3.0612          7.1921         0.21215         0.21215
v  Velocity[Z]       -9.4513e-015     7.3238e-015    -1.6072e-017    -1.6072e-017
v  ǁVelocityǁ         0.0026469          9.6345          5.1144          5.1144
v  Pressure               -25.774          26.628         -1.5746         -1.5746
v  nu_tilda           4.4102e-007       0.0042712       0.0017285       0.0017285
v  TempC                       21           73.05          22.043          22.043
v  TurbVisc           3.3267e-014       0.0050331       0.0020316       0.0020316
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2282:        0.22480E+01

===============================================================


 INSTANT    0.228300000E+04   TIME STEP NUMBER            2283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15276E-01 0.89107E+00
   Friction velocity        uk    :  0.15276E-01 0.89107E+00
   Dimensionless distance   yplus :  0.12298E+00 0.71737E+01
   Friction thermal sca.    tstar : -0.73127E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91756E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10563E-01      33   0.24380E-03   0.47222E+01 0.18847E+03 
c  Velocity[X]                                      0.17093E+01 
c  Velocity[Y]                                      0.30129E+01 
c  Velocity[Z]                                      0.68122E-30 
c  Pressure     0.86666E-07     585   0.96879E-08   0.84285E-01 0.16636E+04 
c  nu_tilda     0.78007E-05      33   0.51166E-05   0.70432E-06 0.21591E+03 
c  TempC        0.42543E+02      27   0.26557E-03   0.46681E+01 0.25538E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.52          9.6321          4.5729          4.5729
v  Velocity[Y]            -3.0612          7.2127         0.21235         0.21235
v  Velocity[Z]       -9.3703e-015     6.7443e-015    -1.6079e-017    -1.6079e-017
v  ǁVelocityǁ         0.0028334          9.6334          5.1143          5.1143
v  Pressure               -25.723          26.812         -1.4984         -1.4984
v  nu_tilda           4.4102e-007       0.0042719       0.0017288       0.0017288
v  TempC                       21          73.051          22.043          22.043
v  TurbVisc           3.3282e-014        0.005034       0.0020319       0.0020319
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2283:        0.24960E+01

===============================================================


 INSTANT    0.228400000E+04   TIME STEP NUMBER            2284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15960E-01 0.89199E+00
   Friction velocity        uk    :  0.15960E-01 0.89199E+00
   Dimensionless distance   yplus :  0.12849E+00 0.71811E+01
   Friction thermal sca.    tstar : -0.80350E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95870E-01 0.53579E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10565E-01      33   0.26360E-03   0.47209E+01 0.18844E+03 
c  Velocity[X]                                      0.17239E+01 
c  Velocity[Y]                                      0.29969E+01 
c  Velocity[Z]                                      0.61264E-30 
c  Pressure     0.10436E-06     536   0.92874E-08   0.10210E+00 0.14561E+04 
c  nu_tilda     0.78027E-05      33   0.14218E-04   0.70448E-06 0.21592E+03 
c  TempC        0.42549E+02      27   0.28886E-03   0.40381E+01 0.24525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5238          9.6309          4.5729          4.5729
v  Velocity[Y]             -3.061          7.1858         0.21255         0.21255
v  Velocity[Z]       -9.6759e-015     6.5126e-015    -1.6082e-017    -1.6082e-017
v  ǁVelocityǁ          0.002534          9.6322          5.1141          5.1141
v  Pressure               -25.741          26.635         -1.5372         -1.5372
v  nu_tilda           4.4102e-007       0.0042726        0.001729        0.001729
v  TempC                       21          73.049          22.043          22.043
v  TurbVisc            3.328e-014       0.0050349       0.0020322       0.0020322
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2284:        0.22240E+01

===============================================================


 INSTANT    0.228500000E+04   TIME STEP NUMBER            2285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14552E-01 0.89142E+00
   Friction velocity        uk    :  0.14552E-01 0.89142E+00
   Dimensionless distance   yplus :  0.11715E+00 0.71765E+01
   Friction thermal sca.    tstar : -0.88582E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87410E-01 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10566E-01      33   0.22906E-03   0.47300E+01 0.18851E+03 
c  Velocity[X]                                      0.17368E+01 
c  Velocity[Y]                                      0.29932E+01 
c  Velocity[Z]                                      0.64871E-30 
c  Pressure     0.97448E-07     570   0.96352E-08   0.95339E-01 0.19014E+04 
c  nu_tilda     0.78048E-05      33   0.51135E-05   0.70459E-06 0.21593E+03 
c  TempC        0.42554E+02      27   0.30255E-03   0.42510E+01 0.25797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5276          9.6298          4.5729          4.5729
v  Velocity[Y]            -3.0608          7.2134         0.21275         0.21275
v  Velocity[Z]       -9.4128e-015      6.491e-015    -1.6088e-017    -1.6088e-017
v  ǁVelocityǁ         0.0028359          9.6311           5.114           5.114
v  Pressure               -25.692           26.86         -1.4525         -1.4525
v  nu_tilda           4.4099e-007       0.0042733       0.0017294       0.0017294
v  TempC                       21           73.05          22.043          22.043
v  TurbVisc           3.3282e-014       0.0050357       0.0020326       0.0020326
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2285:        0.22980E+01

===============================================================


 INSTANT    0.228600000E+04   TIME STEP NUMBER            2286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.97657E-02 0.89264E+00
   Friction velocity        uk    :  0.97657E-02 0.89264E+00
   Dimensionless distance   yplus :  0.78620E-01 0.71864E+01
   Friction thermal sca.    tstar : -0.10176E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58659E-01 0.53618E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10567E-01      33   0.24608E-03   0.47203E+01 0.18853E+03 
c  Velocity[X]                                      0.17126E+01 
c  Velocity[Y]                                      0.30077E+01 
c  Velocity[Z]                                      0.64397E-30 
c  Pressure     0.92797E-07     490   0.96885E-08   0.90833E-01 0.77078E+03 
c  nu_tilda     0.78068E-05      33   0.14212E-04   0.70477E-06 0.21594E+03 
c  TempC        0.42560E+02      27   0.35552E-03   0.44373E+01 0.26445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5313          9.6286          4.5729          4.5729
v  Velocity[Y]            -3.0605          7.2186         0.21295         0.21295
v  Velocity[Z]       -9.3923e-015     6.2918e-015    -1.6091e-017    -1.6091e-017
v  ǁVelocityǁ         0.0030187            9.63          5.1138          5.1138
v  Pressure               -25.712          26.816         -1.4638         -1.4638
v  nu_tilda           4.4092e-007       0.0042741       0.0017296       0.0017296
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc           3.3271e-014       0.0050365       0.0020329       0.0020329
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2286:        0.23760E+01

===============================================================


 INSTANT    0.228700000E+04   TIME STEP NUMBER            2287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14546E-01 0.89212E+00
   Friction velocity        uk    :  0.14546E-01 0.89212E+00
   Dimensionless distance   yplus :  0.11710E+00 0.71822E+01
   Friction thermal sca.    tstar : -0.11841E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87373E-01 0.53587E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10568E-01      33   0.24462E-03   0.47327E+01 0.18853E+03 
c  Velocity[X]                                      0.17363E+01 
c  Velocity[Y]                                      0.29964E+01 
c  Velocity[Z]                                      0.65291E-30 
c  Pressure     0.12330E-06     472   0.99494E-08   0.12014E+00 0.72367E+03 
c  nu_tilda     0.78088E-05      33   0.51055E-05   0.70489E-06 0.21595E+03 
c  TempC        0.42566E+02      27   0.30706E-03   0.48255E+01 0.26728E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5351          9.6275          4.5729          4.5729
v  Velocity[Y]            -3.0605          7.1885         0.21315         0.21315
v  Velocity[Z]       -9.3442e-015     6.4683e-015    -1.6096e-017    -1.6096e-017
v  ǁVelocityǁ         0.0025875          9.6289          5.1136          5.1136
v  Pressure               -25.654          26.763          -1.436          -1.436
v  nu_tilda           4.4098e-007       0.0042749         0.00173         0.00173
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc            3.325e-014       0.0050375       0.0020332       0.0020332
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2287:        0.22200E+01

===============================================================


 INSTANT    0.228800000E+04   TIME STEP NUMBER            2288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.88379E-02 0.89095E+00
   Friction velocity        uk    :  0.88379E-02 0.89095E+00
   Dimensionless distance   yplus :  0.71151E-01 0.71727E+01
   Friction thermal sca.    tstar : -0.16703E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53087E-01 0.53517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10569E-01      33   0.24709E-03   0.47276E+01 0.18852E+03 
c  Velocity[X]                                      0.17391E+01 
c  Velocity[Y]                                      0.29885E+01 
c  Velocity[Z]                                      0.74643E-30 
c  Pressure     0.92255E-07     426   0.99537E-08   0.90685E-01 0.65051E+03 
c  nu_tilda     0.78108E-05      33   0.14210E-04   0.70506E-06 0.21595E+03 
c  TempC        0.42572E+02      27   0.23002E-03   0.39227E+01 0.24612E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5391          9.6264          4.5729          4.5729
v  Velocity[Y]            -3.0604          7.2094         0.21335         0.21335
v  Velocity[Z]       -9.3324e-015     7.2827e-015    -1.6092e-017    -1.6092e-017
v  ǁVelocityǁ         0.0023772          9.6277          5.1135          5.1135
v  Pressure               -25.679          26.842         -1.4207         -1.4207
v  nu_tilda           4.4106e-007       0.0042756       0.0017302       0.0017302
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc           3.3271e-014       0.0050384       0.0020336       0.0020336
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2288:        0.19850E+01

===============================================================


 INSTANT    0.228900000E+04   TIME STEP NUMBER            2289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.34179E-02 0.89209E+00
   Friction velocity        uk    :  0.34179E-02 0.89209E+00
   Dimensionless distance   yplus :  0.27516E-01 0.71819E+01
   Friction thermal sca.    tstar : -0.28986E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20530E-01 0.53585E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10570E-01      33   0.24501E-03   0.47244E+01 0.18858E+03 
c  Velocity[X]                                      0.17184E+01 
c  Velocity[Y]                                      0.30060E+01 
c  Velocity[Z]                                      0.77035E-30 
c  Pressure     0.10161E-06     505   0.93849E-08   0.10079E+00 0.80389E+03 
c  nu_tilda     0.78128E-05      33   0.51050E-05   0.70515E-06 0.21596E+03 
c  TempC        0.42578E+02      27   0.32896E-03   0.31159E+01 0.21931E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5428          9.6252          4.5729          4.5729
v  Velocity[Y]            -3.0603          7.1895         0.21355         0.21355
v  Velocity[Z]        -9.253e-015     6.8063e-015    -1.6098e-017    -1.6098e-017
v  ǁVelocityǁ         0.0018672          9.6266          5.1133          5.1133
v  Pressure               -25.622          26.839         -1.3818         -1.3818
v  nu_tilda           4.4114e-007       0.0042764       0.0017305       0.0017305
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc           3.3294e-014       0.0050393       0.0020339       0.0020339
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2289:        0.22970E+01

===============================================================


 INSTANT    0.229000000E+04   TIME STEP NUMBER            2290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.31821E-02 0.89118E+00
   Friction velocity        uk    :  0.31821E-02 0.89118E+00
   Dimensionless distance   yplus :  0.25618E-01 0.71746E+01
   Friction thermal sca.    tstar : -0.21891E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19114E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10572E-01      33   0.20204E-03   0.47098E+01 0.18849E+03 
c  Velocity[X]                                      0.17206E+01 
c  Velocity[Y]                                      0.29893E+01 
c  Velocity[Z]                                      0.68670E-30 
c  Pressure     0.10421E-06     392   0.91494E-08   0.10097E+00 0.59388E+03 
c  nu_tilda     0.78149E-05      33   0.14200E-04   0.70531E-06 0.21597E+03 
c  TempC        0.42583E+02      27   0.28130E-03   0.59776E+01 0.28603E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5467          9.6241          4.5729          4.5729
v  Velocity[Y]            -3.0601          7.2083         0.21374         0.21374
v  Velocity[Z]       -9.2708e-015     6.5015e-015      -1.61e-017      -1.61e-017
v  ǁVelocityǁ         0.0028239          9.6255          5.1131          5.1131
v  Pressure               -25.645          26.853         -1.3811         -1.3811
v  nu_tilda            4.412e-007       0.0042771       0.0017307       0.0017307
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc           3.3316e-014       0.0050401       0.0020342       0.0020342
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2290:        0.19550E+01

===============================================================


 INSTANT    0.229100000E+04   TIME STEP NUMBER            2291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.75338E-02 0.89276E+00
   Friction velocity        uk    :  0.75338E-02 0.89276E+00
   Dimensionless distance   yplus :  0.60652E-01 0.71873E+01
   Friction thermal sca.    tstar : -0.14789E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45253E-01 0.53626E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10573E-01      33   0.27671E-03   0.47056E+01 0.18852E+03 
c  Velocity[X]                                      0.17195E+01 
c  Velocity[Y]                                      0.29861E+01 
c  Velocity[Z]                                      0.76967E-30 
c  Pressure     0.99859E-07     570   0.95989E-08   0.97683E-01 0.13456E+04 
c  nu_tilda     0.78169E-05      33   0.50939E-05   0.70543E-06 0.21597E+03 
c  TempC        0.42589E+02      27   0.31118E-03   0.71878E+01 0.28928E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5504          9.6229          4.5729          4.5729
v  Velocity[Y]            -3.0599          7.2207         0.21394         0.21394
v  Velocity[Z]       -9.1733e-015     7.4456e-015    -1.6095e-017    -1.6095e-017
v  ǁVelocityǁ         0.0026198          9.6243           5.113           5.113
v  Pressure               -25.591          26.976         -1.3159         -1.3159
v  nu_tilda           4.4116e-007       0.0042778       0.0017311       0.0017311
v  TempC                       21          73.051          22.044          22.044
v  TurbVisc           3.3335e-014        0.005041       0.0020345       0.0020345
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2291:        0.22890E+01

===============================================================


 INSTANT    0.229200000E+04   TIME STEP NUMBER            2292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94087E-02 0.89233E+00
   Friction velocity        uk    :  0.94087E-02 0.89233E+00
   Dimensionless distance   yplus :  0.75747E-01 0.71838E+01
   Friction thermal sca.    tstar : -0.11438E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56516E-01 0.53600E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10574E-01      33   0.24355E-03   0.47583E+01 0.18885E+03 
c  Velocity[X]                                      0.17470E+01 
c  Velocity[Y]                                      0.30113E+01 
c  Velocity[Z]                                      0.68603E-30 
c  Pressure     0.10979E-06     536   0.90524E-08   0.10919E+00 0.13708E+04 
c  nu_tilda     0.78189E-05      33   0.14199E-04   0.70564E-06 0.21599E+03 
c  TempC        0.42595E+02      27   0.24651E-03   0.62108E+01 0.29078E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5541          9.6218          4.5729          4.5729
v  Velocity[Y]            -3.0596          7.1922         0.21414         0.21414
v  Velocity[Z]       -9.1729e-015     6.6346e-015    -1.6092e-017    -1.6092e-017
v  ǁVelocityǁ         0.0026388          9.6232          5.1128          5.1128
v  Pressure               -25.612          26.814         -1.3528         -1.3528
v  nu_tilda           4.4111e-007       0.0042786       0.0017313       0.0017313
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc           3.3324e-014       0.0050419       0.0020349       0.0020349
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2292:        0.22180E+01

===============================================================


 INSTANT    0.229300000E+04   TIME STEP NUMBER            2293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85361E-02 0.89099E+00
   Friction velocity        uk    :  0.85361E-02 0.89099E+00
   Dimensionless distance   yplus :  0.68721E-01 0.71731E+01
   Friction thermal sca.    tstar : -0.98240E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51274E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10575E-01      33   0.23978E-03   0.47158E+01 0.18860E+03 
c  Velocity[X]                                      0.17249E+01 
c  Velocity[Y]                                      0.29909E+01 
c  Velocity[Z]                                      0.65953E-30 
c  Pressure     0.11068E-06     568   0.98384E-08   0.10675E+00 0.16649E+04 
c  nu_tilda     0.78209E-05      33   0.50950E-05   0.70575E-06 0.21599E+03 
c  TempC        0.42600E+02      27   0.34152E-03   0.34787E+01 0.23300E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5578          9.6207          4.5729          4.5729
v  Velocity[Y]            -3.0596          7.2083         0.21433         0.21433
v  Velocity[Z]       -9.0035e-015     6.6007e-015     -1.609e-017     -1.609e-017
v  ǁVelocityǁ         0.0028239          9.6221          5.1126          5.1126
v  Pressure                -25.56          26.997         -1.2761         -1.2761
v  nu_tilda           4.4104e-007       0.0042794       0.0017316       0.0017316
v  TempC                       21          73.051          22.044          22.044
v  TurbVisc            3.331e-014       0.0050428       0.0020352       0.0020352
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2293:        0.24940E+01

===============================================================


 INSTANT    0.229400000E+04   TIME STEP NUMBER            2294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96760E-02 0.89202E+00
   Friction velocity        uk    :  0.96760E-02 0.89202E+00
   Dimensionless distance   yplus :  0.77898E-01 0.71814E+01
   Friction thermal sca.    tstar : -0.86486E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58121E-01 0.53581E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10576E-01      33   0.25604E-03   0.47309E+01 0.18864E+03 
c  Velocity[X]                                      0.17486E+01 
c  Velocity[Y]                                      0.29822E+01 
c  Velocity[Z]                                      0.78630E-30 
c  Pressure     0.99884E-07     538   0.99779E-08   0.99744E-01 0.12979E+04 
c  nu_tilda     0.78229E-05      33   0.14188E-04   0.70589E-06 0.21600E+03 
c  TempC        0.42606E+02      27   0.31496E-03   0.57192E+01 0.27505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5615          9.6195          4.5729          4.5729
v  Velocity[Y]            -3.0595          7.1863         0.21452         0.21452
v  Velocity[Z]       -8.8958e-015     7.5016e-015    -1.6084e-017    -1.6084e-017
v  ǁVelocityǁ         0.0026269          9.6209          5.1125          5.1125
v  Pressure                -25.58          26.848         -1.3097         -1.3097
v  nu_tilda           4.4106e-007       0.0042801       0.0017318       0.0017318
v  TempC                       21           73.05          22.044          22.044
v  TurbVisc           3.3287e-014       0.0050437       0.0020355       0.0020355
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2294:        0.24150E+01

===============================================================


 INSTANT    0.229500000E+04   TIME STEP NUMBER            2295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10537E-01 0.89124E+00
   Friction velocity        uk    :  0.10537E-01 0.89124E+00
   Dimensionless distance   yplus :  0.84834E-01 0.71751E+01
   Friction thermal sca.    tstar : -0.78905E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63295E-01 0.53534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10577E-01      33   0.24162E-03   0.47197E+01 0.18868E+03 
c  Velocity[X]                                      0.17202E+01 
c  Velocity[Y]                                      0.29995E+01 
c  Velocity[Z]                                      0.74841E-30 
c  Pressure     0.92926E-07     552   0.96370E-08   0.90209E-01 0.17912E+04 
c  nu_tilda     0.78249E-05      33   0.50820E-05   0.70598E-06 0.21600E+03 
c  TempC        0.42612E+02      27   0.31028E-03   0.52564E+01 0.27615E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5651          9.6184          4.5729          4.5729
v  Velocity[Y]            -3.0594          7.2115         0.21472         0.21472
v  Velocity[Z]       -8.8351e-015     6.7026e-015    -1.6082e-017    -1.6082e-017
v  ǁVelocityǁ         0.0028854          9.6198          5.1123          5.1123
v  Pressure               -25.533          27.057         -1.2299         -1.2299
v  nu_tilda           4.4103e-007       0.0042808       0.0017322       0.0017322
v  TempC                       21          73.051          22.044          22.044
v  TurbVisc           3.3293e-014       0.0050445       0.0020358       0.0020358
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2295:        0.24320E+01

===============================================================


 INSTANT    0.229600000E+04   TIME STEP NUMBER            2296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14483E-01 0.89240E+00
   Friction velocity        uk    :  0.14483E-01 0.89240E+00
   Dimensionless distance   yplus :  0.11660E+00 0.71845E+01
   Friction thermal sca.    tstar : -0.72367E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86996E-01 0.53604E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10579E-01      33   0.25298E-03   0.46895E+01 0.18853E+03 
c  Velocity[X]                                      0.17065E+01 
c  Velocity[Y]                                      0.29830E+01 
c  Velocity[Z]                                      0.62896E-30 
c  Pressure     0.10366E-06     489   0.98134E-08   0.10008E+00 0.97174E+03 
c  nu_tilda     0.78269E-05      33   0.14187E-04   0.70613E-06 0.21601E+03 
c  TempC        0.42618E+02      27   0.28024E-03   0.56109E+01 0.28117E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5688          9.6172          4.5729          4.5729
v  Velocity[Y]            -3.0592          7.2143         0.21491         0.21491
v  Velocity[Z]       -8.8512e-015     6.5674e-015    -1.6077e-017    -1.6077e-017
v  ǁVelocityǁ         0.0029029          9.6186          5.1121          5.1121
v  Pressure               -25.554          26.971         -1.2511         -1.2511
v  nu_tilda           4.4091e-007       0.0042816       0.0017324       0.0017324
v  TempC                       21           73.05          22.045          22.045
v  TurbVisc           3.3283e-014       0.0050454       0.0020362       0.0020362
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2296:        0.22150E+01

===============================================================


 INSTANT    0.229700000E+04   TIME STEP NUMBER            2297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14422E-01 0.89220E+00
   Friction velocity        uk    :  0.14422E-01 0.89220E+00
   Dimensionless distance   yplus :  0.11611E+00 0.71828E+01
   Friction thermal sca.    tstar : -0.68291E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86628E-01 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10580E-01      33   0.26355E-03   0.47291E+01 0.18871E+03 
c  Velocity[X]                                      0.17489E+01 
c  Velocity[Y]                                      0.29802E+01 
c  Velocity[Z]                                      0.80642E-30 
c  Pressure     0.11048E-06     522   0.95158E-08   0.11019E+00 0.86041E+03 
c  nu_tilda     0.78289E-05      33   0.50814E-05   0.70624E-06 0.21602E+03 
c  TempC        0.42623E+02      27   0.27427E-03   0.43236E+01 0.25660E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5724          9.6161          4.5729          4.5729
v  Velocity[Y]             -3.059          7.1905          0.2151          0.2151
v  Velocity[Z]       -8.7524e-015     7.4592e-015    -1.6069e-017    -1.6069e-017
v  ǁVelocityǁ         0.0026439          9.6175           5.112           5.112
v  Pressure               -25.499          26.986         -1.2081         -1.2081
v  nu_tilda           4.4088e-007       0.0042823       0.0017327       0.0017327
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc           3.3248e-014       0.0050463       0.0020365       0.0020365
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2297:        0.22830E+01

===============================================================


 INSTANT    0.229800000E+04   TIME STEP NUMBER            2298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13849E-01 0.89082E+00
   Friction velocity        uk    :  0.13849E-01 0.89082E+00
   Dimensionless distance   yplus :  0.11150E+00 0.71717E+01
   Friction thermal sca.    tstar : -0.63731E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83188E-01 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10581E-01      33   0.24483E-03   0.47266E+01 0.18876E+03 
c  Velocity[X]                                      0.17320E+01 
c  Velocity[Y]                                      0.29945E+01 
c  Velocity[Z]                                      0.71436E-30 
c  Pressure     0.93404E-07     281   0.96058E-08   0.91461E-01 0.58551E+03 
c  nu_tilda     0.78309E-05      33   0.14179E-04   0.70641E-06 0.21603E+03 
c  TempC        0.42629E+02      27   0.31124E-03   0.37952E+01 0.24150E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5762          9.6149          4.5729          4.5729
v  Velocity[Y]            -3.0587          7.2088         0.21529         0.21529
v  Velocity[Z]        -8.734e-015     6.7887e-015    -1.6065e-017    -1.6065e-017
v  ǁVelocityǁ         0.0029353          9.6163          5.1118          5.1118
v  Pressure               -25.524          27.031         -1.2032         -1.2032
v  nu_tilda           4.4089e-007       0.0042831       0.0017329       0.0017329
v  TempC                       21           73.05          22.045          22.045
v  TurbVisc           3.3239e-014       0.0050471       0.0020368       0.0020368
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2298:        0.16330E+01

===============================================================


 INSTANT    0.229900000E+04   TIME STEP NUMBER            2299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13074E-01 0.89190E+00
   Friction velocity        uk    :  0.13074E-01 0.89190E+00
   Dimensionless distance   yplus :  0.10526E+00 0.71804E+01
   Friction thermal sca.    tstar : -0.60616E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78533E-01 0.53574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10582E-01      33   0.24599E-03   0.47174E+01 0.18869E+03 
c  Velocity[X]                                      0.17355E+01 
c  Velocity[Y]                                      0.29820E+01 
c  Velocity[Z]                                      0.61707E-30 
c  Pressure     0.11804E-06     474   0.99171E-08   0.11471E+00 0.70296E+03 
c  nu_tilda     0.78329E-05      33   0.50683E-05   0.70651E-06 0.21603E+03 
c  TempC        0.42635E+02      27   0.31088E-03   0.49229E+01 0.26314E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5799          9.6138          4.5729          4.5729
v  Velocity[Y]            -3.0586          7.1839         0.21548         0.21548
v  Velocity[Z]       -8.7765e-015     6.4472e-015    -1.6057e-017    -1.6057e-017
v  ǁVelocityǁ         0.0025761          9.6152          5.1116          5.1116
v  Pressure               -25.469          26.991          -1.174          -1.174
v  nu_tilda           4.4093e-007       0.0042838       0.0017333       0.0017333
v  TempC                       21          73.049          22.045          22.045
v  TurbVisc           3.3242e-014        0.005048       0.0020371       0.0020371
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2299:        0.20730E+01

===============================================================


 INSTANT    0.230000000E+04   TIME STEP NUMBER            2300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13780E-01 0.89120E+00
   Friction velocity        uk    :  0.13780E-01 0.89120E+00
   Dimensionless distance   yplus :  0.11093E+00 0.71747E+01
   Friction thermal sca.    tstar : -0.59364E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82770E-01 0.53532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10583E-01      33   0.20466E-03   0.47228E+01 0.18872E+03 
c  Velocity[X]                                      0.17480E+01 
c  Velocity[Y]                                      0.29748E+01 
c  Velocity[Z]                                      0.67883E-30 
c  Pressure     0.92159E-07     456   0.95093E-08   0.90723E-01 0.66018E+03 
c  nu_tilda     0.78349E-05      33   0.14178E-04   0.70665E-06 0.21603E+03 
c  TempC        0.42640E+02      27   0.31741E-03   0.48905E+01 0.27231E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5837          9.6126          4.5729          4.5729
v  Velocity[Y]            -3.0585          7.2095         0.21567         0.21567
v  Velocity[Z]       -8.7621e-015     6.3513e-015    -1.6055e-017    -1.6055e-017
v  ǁVelocityǁ         0.0028738           9.614          5.1115          5.1115
v  Pressure               -25.493          27.073         -1.1577         -1.1577
v  nu_tilda           4.4092e-007       0.0042845       0.0017335       0.0017335
v  TempC                       21          73.049          22.045          22.045
v  TurbVisc           3.3253e-014       0.0050489       0.0020375       0.0020375
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2300:        0.20400E+01

===============================================================


 INSTANT    0.230100000E+04   TIME STEP NUMBER            2301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15623E-01 0.89276E+00
   Friction velocity        uk    :  0.15623E-01 0.89276E+00
   Dimensionless distance   yplus :  0.12578E+00 0.71873E+01
   Friction thermal sca.    tstar : -0.58739E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93842E-01 0.53625E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10584E-01      33   0.23489E-03   0.46936E+01 0.18868E+03 
c  Velocity[X]                                      0.17017E+01 
c  Velocity[Y]                                      0.29919E+01 
c  Velocity[Z]                                      0.72979E-30 
c  Pressure     0.84551E-07     522   0.99353E-08   0.83031E-01 0.11332E+04 
c  nu_tilda     0.78369E-05      33   0.50675E-05   0.70673E-06 0.21604E+03 
c  TempC        0.42646E+02      27   0.31188E-03   0.55742E+01 0.27933E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5874          9.6114          4.5729          4.5729
v  Velocity[Y]            -3.0584          7.2209         0.21586         0.21586
v  Velocity[Z]       -8.6653e-015     6.4974e-015    -1.6043e-017    -1.6043e-017
v  ǁVelocityǁ          0.002976          9.6129          5.1113          5.1113
v  Pressure               -25.439          27.164         -1.1022         -1.1022
v  nu_tilda           4.4085e-007       0.0042853       0.0017338       0.0017338
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc            3.325e-014       0.0050498       0.0020378       0.0020378
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2301:        0.22020E+01

===============================================================


 INSTANT    0.230200000E+04   TIME STEP NUMBER            2302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.86228E-02 0.89226E+00
   Friction velocity        uk    :  0.86228E-02 0.89226E+00
   Dimensionless distance   yplus :  0.69420E-01 0.71833E+01
   Friction thermal sca.    tstar : -0.58011E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51795E-01 0.53595E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10586E-01      33   0.24620E-03   0.47114E+01 0.18872E+03 
c  Velocity[X]                                      0.17348E+01 
c  Velocity[Y]                                      0.29766E+01 
c  Velocity[Z]                                      0.76876E-30 
c  Pressure     0.10680E-06     506   0.97336E-08   0.10503E+00 0.14850E+04 
c  nu_tilda     0.78389E-05      33   0.14167E-04   0.70689E-06 0.21605E+03 
c  TempC        0.42652E+02      27   0.25895E-03   0.60582E+01 0.26807E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5911          9.6103          4.5729          4.5729
v  Velocity[Y]            -3.0582          7.1873         0.21605         0.21605
v  Velocity[Z]       -8.6323e-015     7.4058e-015    -1.6027e-017    -1.6027e-017
v  ǁVelocityǁ         0.0026405          9.6117          5.1111          5.1111
v  Pressure               -25.457           26.98         -1.1413         -1.1413
v  nu_tilda           4.4092e-007        0.004286        0.001734        0.001734
v  TempC                       21           73.05          22.045          22.045
v  TurbVisc           3.3231e-014       0.0050506       0.0020381       0.0020381
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2302:        0.21670E+01

===============================================================


 INSTANT    0.230300000E+04   TIME STEP NUMBER            2303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11920E-01 0.89098E+00
   Friction velocity        uk    :  0.11920E-01 0.89098E+00
   Dimensionless distance   yplus :  0.95963E-01 0.71730E+01
   Friction thermal sca.    tstar : -0.59189E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71599E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10587E-01      33   0.27350E-03   0.47116E+01 0.18876E+03 
c  Velocity[X]                                      0.17394E+01 
c  Velocity[Y]                                      0.29722E+01 
c  Velocity[Z]                                      0.72474E-30 
c  Pressure     0.97260E-07     569   0.96893E-08   0.95000E-01 0.18528E+04 
c  nu_tilda     0.78409E-05      33   0.50526E-05   0.70701E-06 0.21605E+03 
c  TempC        0.42657E+02      27   0.21362E-03   0.42729E+01 0.24606E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5947          9.6091          4.5729          4.5729
v  Velocity[Y]             -3.058          7.2103         0.21623         0.21623
v  Velocity[Z]       -8.5276e-015     6.7817e-015    -1.6018e-017    -1.6018e-017
v  ǁVelocityǁ         0.0027502          9.6106          5.1109          5.1109
v  Pressure               -25.408          27.197         -1.0589         -1.0589
v  nu_tilda           4.4099e-007       0.0042867       0.0017343       0.0017343
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc            3.325e-014       0.0050515       0.0020384       0.0020384
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2303:        0.23070E+01

===============================================================


 INSTANT    0.230400000E+04   TIME STEP NUMBER            2304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54278E-02 0.89195E+00
   Friction velocity        uk    :  0.54278E-02 0.89195E+00
   Dimensionless distance   yplus :  0.43697E-01 0.71808E+01
   Friction thermal sca.    tstar : -0.58080E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32603E-01 0.53577E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10588E-01      33   0.25584E-03   0.47367E+01 0.18893E+03 
c  Velocity[X]                                      0.17477E+01 
c  Velocity[Y]                                      0.29890E+01 
c  Velocity[Z]                                      0.60368E-30 
c  Pressure     0.10442E-06     504   0.95979E-08   0.10351E+00 0.13067E+04 
c  nu_tilda     0.78429E-05      33   0.14168E-04   0.70717E-06 0.21606E+03 
c  TempC        0.42663E+02      27   0.37313E-03   0.42655E+01 0.24679E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5983          9.6079          4.5729          4.5729
v  Velocity[Y]            -3.0577          7.1871         0.21642         0.21642
v  Velocity[Z]       -8.5219e-015     6.5114e-015    -1.6011e-017    -1.6011e-017
v  ǁVelocityǁ          0.002655          9.6094          5.1108          5.1108
v  Pressure               -25.427          27.045         -1.0917         -1.0917
v  nu_tilda           4.4104e-007       0.0042875       0.0017346       0.0017346
v  TempC                       21           73.05          22.045          22.045
v  TurbVisc           3.3272e-014       0.0050523       0.0020387       0.0020387
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2304:        0.21310E+01

===============================================================


 INSTANT    0.230500000E+04   TIME STEP NUMBER            2305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15293E-01 0.89118E+00
   Friction velocity        uk    :  0.15293E-01 0.89118E+00
   Dimensionless distance   yplus :  0.12312E+00 0.71746E+01
   Friction thermal sca.    tstar : -0.59643E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91860E-01 0.53531E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10589E-01      33   0.18998E-03   0.47119E+01 0.18878E+03 
c  Velocity[X]                                      0.17362E+01 
c  Velocity[Y]                                      0.29756E+01 
c  Velocity[Z]                                      0.67593E-30 
c  Pressure     0.11017E-06     536   0.89931E-08   0.10600E+00 0.15926E+04 
c  nu_tilda     0.78449E-05      33   0.50526E-05   0.70725E-06 0.21606E+03 
c  TempC        0.42668E+02      27   0.29698E-03   0.89279E+01 0.34238E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6018          9.6068          4.5729          4.5729
v  Velocity[Y]            -3.0576          7.2077          0.2166          0.2166
v  Velocity[Z]       -8.4974e-015     7.5558e-015    -1.5988e-017    -1.5988e-017
v  ǁVelocityǁ         0.0028714          9.6083          5.1106          5.1106
v  Pressure               -25.376          27.222         -1.0185         -1.0185
v  nu_tilda           4.4101e-007       0.0042882       0.0017349       0.0017349
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc           3.3288e-014       0.0050532       0.0020391       0.0020391
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2305:        0.22280E+01

===============================================================


 INSTANT    0.230600000E+04   TIME STEP NUMBER            2306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16138E-01 0.89249E+00
   Friction velocity        uk    :  0.16138E-01 0.89249E+00
   Dimensionless distance   yplus :  0.12992E+00 0.71852E+01
   Friction thermal sca.    tstar : -0.58408E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96935E-01 0.53609E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10590E-01      33   0.24963E-03   0.47075E+01 0.18883E+03 
c  Velocity[X]                                      0.17320E+01 
c  Velocity[Y]                                      0.29755E+01 
c  Velocity[Z]                                      0.81469E-30 
c  Pressure     0.88477E-07     473   0.99542E-08   0.87008E-01 0.72846E+03 
c  nu_tilda     0.78469E-05      33   0.14156E-04   0.70741E-06 0.21607E+03 
c  TempC        0.42674E+02      27   0.30161E-03   0.47270E+01 0.26659E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6054          9.6056          4.5729          4.5729
v  Velocity[Y]            -3.0575          7.2155         0.21679         0.21679
v  Velocity[Z]       -8.5048e-015      6.706e-015    -1.5977e-017    -1.5977e-017
v  ǁVelocityǁ         0.0030225          9.6071          5.1104          5.1104
v  Pressure               -25.399          27.182         -1.0292         -1.0292
v  nu_tilda           4.4091e-007       0.0042889       0.0017351       0.0017351
v  TempC                       21          73.051          22.046          22.046
v  TurbVisc           3.3277e-014       0.0050541       0.0020394       0.0020394
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2306:        0.20780E+01

===============================================================


 INSTANT    0.230700000E+04   TIME STEP NUMBER            2307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10152E-01 0.89205E+00
   Friction velocity        uk    :  0.10152E-01 0.89205E+00
   Dimensionless distance   yplus :  0.81733E-01 0.71816E+01
   Friction thermal sca.    tstar : -0.58002E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60982E-01 0.53583E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10591E-01      33   0.23279E-03   0.47212E+01 0.18892E+03 
c  Velocity[X]                                      0.17321E+01 
c  Velocity[Y]                                      0.29891E+01 
c  Velocity[Z]                                      0.71530E-30 
c  Pressure     0.11190E-06     504   0.93045E-08   0.11093E+00 0.75028E+03 
c  nu_tilda     0.78489E-05      33   0.50366E-05   0.70751E-06 0.21608E+03 
c  TempC        0.42680E+02      27   0.32780E-03   0.42844E+01 0.26265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6088          9.6045          4.5729          4.5729
v  Velocity[Y]            -3.0573          7.1892         0.21697         0.21697
v  Velocity[Z]       -8.4693e-015     6.4484e-015    -1.5969e-017    -1.5969e-017
v  ǁVelocityǁ         0.0027034           9.606          5.1102          5.1102
v  Pressure               -25.347          27.174        -0.99386        -0.99386
v  nu_tilda           4.4087e-007       0.0042896       0.0017354       0.0017354
v  TempC                       21          73.051          22.046          22.046
v  TurbVisc           3.3249e-014       0.0050549       0.0020397       0.0020397
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2307:        0.21570E+01

===============================================================


 INSTANT    0.230800000E+04   TIME STEP NUMBER            2308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11430E-01 0.89061E+00
   Friction velocity        uk    :  0.11430E-01 0.89061E+00
   Dimensionless distance   yplus :  0.92020E-01 0.71700E+01
   Friction thermal sca.    tstar : -0.58655E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68658E-01 0.53496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10592E-01      33   0.24819E-03   0.46969E+01 0.18878E+03 
c  Velocity[X]                                      0.17264E+01 
c  Velocity[Y]                                      0.29705E+01 
c  Velocity[Z]                                      0.64324E-30 
c  Pressure     0.10288E-06     394   0.96151E-08   0.99501E-01 0.58633E+03 
c  nu_tilda     0.78509E-05      33   0.14159E-04   0.70766E-06 0.21608E+03 
c  TempC        0.42685E+02      27   0.23247E-03   0.58464E+01 0.27420E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6125          9.6033          4.5729          4.5729
v  Velocity[Y]            -3.0571          7.2039         0.21716         0.21716
v  Velocity[Z]       -8.4936e-015     6.4625e-015    -1.5958e-017    -1.5958e-017
v  ǁVelocityǁ         0.0028569          9.6048          5.1101          5.1101
v  Pressure               -25.372           27.19        -0.99507        -0.99507
v  nu_tilda           4.4082e-007       0.0042903       0.0017356       0.0017356
v  TempC                       21           73.05          22.046          22.046
v  TurbVisc           3.3236e-014       0.0050558         0.00204         0.00204
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2308:        0.18980E+01

===============================================================


 INSTANT    0.230900000E+04   TIME STEP NUMBER            2309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14620E-01 0.89190E+00
   Friction velocity        uk    :  0.14620E-01 0.89190E+00
   Dimensionless distance   yplus :  0.11770E+00 0.71804E+01
   Friction thermal sca.    tstar : -0.58543E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87819E-01 0.53574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10593E-01      33   0.27095E-03   0.47142E+01 0.18888E+03 
c  Velocity[X]                                      0.17494E+01 
c  Velocity[Y]                                      0.29649E+01 
c  Velocity[Z]                                      0.90955E-30 
c  Pressure     0.10794E-06     520   0.96681E-08   0.10715E+00 0.82414E+03 
c  nu_tilda     0.78529E-05      33   0.50364E-05   0.70776E-06 0.21609E+03 
c  TempC        0.42691E+02      27   0.34120E-03   0.45029E+01 0.25060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6161          9.6021          4.5729          4.5729
v  Velocity[Y]            -3.0569          7.1866         0.21734         0.21734
v  Velocity[Z]       -8.4457e-015     7.3492e-015    -1.5942e-017    -1.5942e-017
v  ǁVelocityǁ         0.0026504          9.6036          5.1099          5.1099
v  Pressure               -25.318          27.202        -0.95465        -0.95465
v  nu_tilda           4.4083e-007        0.004291        0.001736        0.001736
v  TempC                       21           73.05          22.046          22.046
v  TurbVisc           3.3222e-014       0.0050566       0.0020403       0.0020403
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2309:        0.21940E+01

===============================================================


 INSTANT    0.231000000E+04   TIME STEP NUMBER            2310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14885E-01 0.89111E+00
   Friction velocity        uk    :  0.14885E-01 0.89111E+00
   Dimensionless distance   yplus :  0.11983E+00 0.71740E+01
   Friction thermal sca.    tstar : -0.59425E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89408E-01 0.53526E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10594E-01      33   0.19720E-03   0.47232E+01 0.18897E+03 
c  Velocity[X]                                      0.17417E+01 
c  Velocity[Y]                                      0.29814E+01 
c  Velocity[Z]                                      0.71664E-30 
c  Pressure     0.98756E-07     344   0.94572E-08   0.97113E-01 0.58054E+03 
c  nu_tilda     0.78548E-05      33   0.14146E-04   0.70790E-06 0.21609E+03 
c  TempC        0.42696E+02      27   0.24856E-03   0.64526E+01 0.30409E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6198          9.6009          4.5729          4.5729
v  Velocity[Y]            -3.0566          7.2094         0.21752         0.21752
v  Velocity[Z]       -8.4258e-015     6.6327e-015    -1.5936e-017    -1.5936e-017
v  ǁVelocityǁ         0.0027772          9.6024          5.1097          5.1097
v  Pressure               -25.345          27.258        -0.94652        -0.94652
v  nu_tilda           4.4081e-007       0.0042918       0.0017362       0.0017362
v  TempC                       21           73.05          22.046          22.046
v  TurbVisc           3.3223e-014       0.0050574       0.0020406       0.0020406
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2310:        0.18220E+01

===============================================================


 INSTANT    0.231100000E+04   TIME STEP NUMBER            2311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.78479E-02 0.89257E+00
   Friction velocity        uk    :  0.78479E-02 0.89257E+00
   Dimensionless distance   yplus :  0.63181E-01 0.71858E+01
   Friction thermal sca.    tstar : -0.58319E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47140E-01 0.53614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10595E-01      33   0.24322E-03   0.46882E+01 0.18879E+03 
c  Velocity[X]                                      0.17195E+01 
c  Velocity[Y]                                      0.29687E+01 
c  Velocity[Z]                                      0.57759E-30 
c  Pressure     0.11189E-06     506   0.94691E-08   0.10774E+00 0.96060E+03 
c  nu_tilda     0.78568E-05      33   0.50206E-05   0.70796E-06 0.21609E+03 
c  TempC        0.42702E+02      27   0.28354E-03   0.42513E+01 0.24197E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6234          9.5998          4.5729          4.5729
v  Velocity[Y]            -3.0565          7.2152          0.2177          0.2177
v  Velocity[Z]       -8.3889e-015     6.5645e-015    -1.5923e-017    -1.5923e-017
v  ǁVelocityǁ         0.0011183          9.6013          5.1096          5.1096
v  Pressure               -25.292          27.317        -0.89907        -0.89907
v  nu_tilda           4.4078e-007       0.0042925       0.0017365       0.0017365
v  TempC                       21          73.051          22.046          22.046
v  TurbVisc           3.3217e-014       0.0050583        0.002041        0.002041
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2311:        0.21560E+01

===============================================================


 INSTANT    0.231200000E+04   TIME STEP NUMBER            2312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11471E-01 0.89221E+00
   Friction velocity        uk    :  0.11471E-01 0.89221E+00
   Dimensionless distance   yplus :  0.92352E-01 0.71829E+01
   Friction thermal sca.    tstar : -0.57905E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68905E-01 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10597E-01      33   0.24895E-03   0.47274E+01 0.18896E+03 
c  Velocity[X]                                      0.17661E+01 
c  Velocity[Y]                                      0.29613E+01 
c  Velocity[Z]                                      0.75933E-30 
c  Pressure     0.99534E-07     506   0.94013E-08   0.99090E-01 0.11900E+04 
c  nu_tilda     0.78588E-05      33   0.14148E-04   0.70810E-06 0.21610E+03 
c  TempC        0.42707E+02      27   0.34403E-03   0.46682E+01 0.24511E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6269          9.5986          4.5729          4.5729
v  Velocity[Y]            -3.0564          7.1888         0.21788         0.21788
v  Velocity[Z]       -8.3633e-015     7.5105e-015     -1.591e-017     -1.591e-017
v  ǁVelocityǁ         0.0025576          9.6001          5.1094          5.1094
v  Pressure               -25.314          27.182        -0.92921        -0.92921
v  nu_tilda           4.4083e-007       0.0042932       0.0017367       0.0017367
v  TempC                       21           73.05          22.046          22.046
v  TurbVisc            3.321e-014       0.0050592       0.0020413       0.0020413
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2312:        0.21480E+01

===============================================================


 INSTANT    0.231300000E+04   TIME STEP NUMBER            2313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.59913E-02 0.89095E+00
   Friction velocity        uk    :  0.59913E-02 0.89095E+00
   Dimensionless distance   yplus :  0.48234E-01 0.71727E+01
   Friction thermal sca.    tstar : -0.59214E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35988E-01 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10598E-01      33   0.23904E-03   0.47033E+01 0.18894E+03 
c  Velocity[X]                                      0.17244E+01 
c  Velocity[Y]                                      0.29789E+01 
c  Velocity[Z]                                      0.69418E-30 
c  Pressure     0.88124E-07     585   0.95332E-08   0.86513E-01 0.18784E+04 
c  nu_tilda     0.78608E-05      33   0.50199E-05   0.70818E-06 0.21610E+03 
c  TempC        0.42713E+02      27   0.26202E-03   0.49568E+01 0.26180E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6305          9.5974          4.5729          4.5729
v  Velocity[Y]            -3.0562          7.2092         0.21806         0.21806
v  Velocity[Z]       -8.2245e-015     6.7952e-015    -1.5903e-017    -1.5903e-017
v  ǁVelocityǁ        0.00056317          9.5989          5.1092          5.1092
v  Pressure               -25.262            27.4        -0.84446        -0.84446
v  nu_tilda           4.4086e-007       0.0042939        0.001737        0.001737
v  TempC                       21          73.051          22.046          22.046
v  TurbVisc           3.3225e-014         0.00506       0.0020416       0.0020416
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2313:        0.23330E+01

===============================================================


 INSTANT    0.231400000E+04   TIME STEP NUMBER            2314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.79032E-02 0.89173E+00
   Friction velocity        uk    :  0.79032E-02 0.89173E+00
   Dimensionless distance   yplus :  0.63626E-01 0.71790E+01
   Friction thermal sca.    tstar : -0.77437E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47472E-01 0.53563E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10599E-01      33   0.25719E-03   0.46989E+01 0.18889E+03 
c  Velocity[X]                                      0.17356E+01 
c  Velocity[Y]                                      0.29633E+01 
c  Velocity[Z]                                      0.66395E-30 
c  Pressure     0.10501E-06     568   0.97288E-08   0.10301E+00 0.17265E+04 
c  nu_tilda     0.78628E-05      33   0.14135E-04   0.70835E-06 0.21611E+03 
c  TempC        0.42718E+02      27   0.28897E-03   0.37984E+01 0.22721E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.634          9.5962          4.5729          4.5729
v  Velocity[Y]             -3.056          7.1818         0.21824         0.21824
v  Velocity[Z]       -8.1634e-015     6.4826e-015    -1.5894e-017    -1.5894e-017
v  ǁVelocityǁ          0.002631          9.5977           5.109           5.109
v  Pressure               -25.286          27.182        -0.89672        -0.89672
v  nu_tilda           4.4091e-007       0.0042946       0.0017372       0.0017372
v  TempC                       21          73.049          22.046          22.046
v  TurbVisc           3.3234e-014       0.0050608       0.0020419       0.0020419
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2314:        0.22930E+01

===============================================================


 INSTANT    0.231500000E+04   TIME STEP NUMBER            2315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46942E-02 0.89115E+00
   Friction velocity        uk    :  0.46942E-02 0.89115E+00
   Dimensionless distance   yplus :  0.37791E-01 0.71744E+01
   Friction thermal sca.    tstar : -0.64524E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28197E-01 0.53529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10600E-01      33   0.27112E-03   0.47095E+01 0.18897E+03 
c  Velocity[X]                                      0.17509E+01 
c  Velocity[Y]                                      0.29586E+01 
c  Velocity[Z]                                      0.87525E-30 
c  Pressure     0.10049E-06     538   0.95654E-08   0.97702E-01 0.19556E+04 
c  nu_tilda     0.78647E-05      33   0.50033E-05   0.70845E-06 0.21612E+03 
c  TempC        0.42724E+02      27   0.31040E-03   0.37742E+01 0.23422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6374           9.595          4.5729          4.5729
v  Velocity[Y]            -3.0557          7.2091         0.21842         0.21842
v  Velocity[Z]       -8.0839e-015      7.514e-015    -1.5877e-017    -1.5877e-017
v  ǁVelocityǁ         0.0010017          9.5966          5.1088          5.1088
v  Pressure               -25.235          27.416        -0.80995        -0.80995
v  nu_tilda           4.4089e-007       0.0042953       0.0017375       0.0017375
v  TempC                       21          73.051          22.046          22.046
v  TurbVisc           3.3248e-014       0.0050617       0.0020422       0.0020422
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2315:        0.24550E+01

===============================================================


 INSTANT    0.231600000E+04   TIME STEP NUMBER            2316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10685E-01 0.89234E+00
   Friction velocity        uk    :  0.10685E-01 0.89234E+00
   Dimensionless distance   yplus :  0.86019E-01 0.71839E+01
   Friction thermal sca.    tstar : -0.69046E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64180E-01 0.53600E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10601E-01      33   0.24229E-03   0.47056E+01 0.18903E+03 
c  Velocity[X]                                      0.17321E+01 
c  Velocity[Y]                                      0.29736E+01 
c  Velocity[Z]                                      0.71075E-30 
c  Pressure     0.93741E-07     489   0.96200E-08   0.91794E-01 0.80634E+03 
c  nu_tilda     0.78667E-05      33   0.14136E-04   0.70857E-06 0.21612E+03 
c  TempC        0.42729E+02      27   0.26442E-03   0.50510E+01 0.24811E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6409          9.5939          4.5729          4.5729
v  Velocity[Y]            -3.0554          7.2157         0.21859         0.21859
v  Velocity[Z]       -8.0519e-015     6.7652e-015     -1.587e-017     -1.587e-017
v  ǁVelocityǁ         0.0028816          9.5954          5.1087          5.1087
v  Pressure                -25.26          27.362        -0.82574        -0.82574
v  nu_tilda           4.4081e-007       0.0042961       0.0017377       0.0017377
v  TempC                       21          73.051          22.046          22.046
v  TurbVisc           3.3243e-014       0.0050625       0.0020425       0.0020425
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2316:        0.22940E+01

===============================================================


 INSTANT    0.231700000E+04   TIME STEP NUMBER            2317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.36552E-02 0.89194E+00
   Friction velocity        uk    :  0.36552E-02 0.89194E+00
   Dimensionless distance   yplus :  0.29426E-01 0.71807E+01
   Friction thermal sca.    tstar : -0.73172E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21955E-01 0.53576E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10602E-01      33   0.23555E-03   0.47128E+01 0.18900E+03 
c  Velocity[X]                                      0.17503E+01 
c  Velocity[Y]                                      0.29625E+01 
c  Velocity[Z]                                      0.64296E-30 
c  Pressure     0.11706E-06     506   0.98729E-08   0.11507E+00 0.73131E+03 
c  nu_tilda     0.78687E-05      33   0.50027E-05   0.70863E-06 0.21612E+03 
c  TempC        0.42735E+02      27   0.26502E-03   0.35462E+01 0.22505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6443          9.5927          4.5729          4.5729
v  Velocity[Y]            -3.0553          7.1853         0.21877         0.21877
v  Velocity[Z]       -8.0619e-015     6.4709e-015    -1.5865e-017    -1.5865e-017
v  ǁVelocityǁ         0.0022336          9.5942          5.1085          5.1085
v  Pressure               -25.202          27.321        -0.79482        -0.79482
v  nu_tilda           4.4084e-007       0.0042968       0.0017381       0.0017381
v  TempC                       21          73.051          22.047          22.047
v  TurbVisc           3.3219e-014       0.0050633       0.0020428       0.0020428
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2317:        0.21540E+01

===============================================================


 INSTANT    0.231800000E+04   TIME STEP NUMBER            2318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.83862E-02 0.89067E+00
   Friction velocity        uk    :  0.83862E-02 0.89067E+00
   Dimensionless distance   yplus :  0.67515E-01 0.71705E+01
   Friction thermal sca.    tstar : -0.80527E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50373E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10603E-01      33   0.24396E-03   0.47060E+01 0.18899E+03 
c  Velocity[X]                                      0.17518E+01 
c  Velocity[Y]                                      0.29542E+01 
c  Velocity[Z]                                      0.72744E-30 
c  Pressure     0.90053E-07     408   0.91962E-08   0.88456E-01 0.59312E+03 
c  nu_tilda     0.78706E-05      33   0.14128E-04   0.70876E-06 0.21612E+03 
c  TempC        0.42740E+02      27   0.27904E-03   0.35891E+01 0.23342E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6477          9.5915          4.5729          4.5729
v  Velocity[Y]            -3.0552          7.2057         0.21895         0.21895
v  Velocity[Z]       -8.0435e-015     6.4409e-015    -1.5856e-017    -1.5856e-017
v  ǁVelocityǁ         0.0029694           9.593          5.1083          5.1083
v  Pressure               -25.231          27.388        -0.78567        -0.78567
v  nu_tilda           4.4089e-007       0.0042975       0.0017383       0.0017383
v  TempC                       21           73.05          22.047          22.047
v  TurbVisc           3.3227e-014       0.0050642       0.0020431       0.0020431
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2318:        0.19210E+01

===============================================================


 INSTANT    0.231900000E+04   TIME STEP NUMBER            2319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60392E-02 0.89180E+00
   Friction velocity        uk    :  0.60392E-02 0.89180E+00
   Dimensionless distance   yplus :  0.48620E-01 0.71796E+01
   Friction thermal sca.    tstar : -0.86989E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36276E-01 0.53568E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10604E-01      33   0.24809E-03   0.47051E+01 0.18906E+03 
c  Velocity[X]                                      0.17336E+01 
c  Velocity[Y]                                      0.29715E+01 
c  Velocity[Z]                                      0.79588E-30 
c  Pressure     0.10570E-06     505   0.97520E-08   0.10426E+00 0.78457E+03 
c  nu_tilda     0.78726E-05      33   0.49864E-05   0.70887E-06 0.21613E+03 
c  TempC        0.42746E+02      27   0.31666E-03   0.35495E+01 0.23384E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6512          9.5903          4.5729          4.5729
v  Velocity[Y]             -3.055          7.1843         0.21912         0.21912
v  Velocity[Z]       -7.9831e-015     7.3835e-015     -1.584e-017     -1.584e-017
v  ǁVelocityǁ         0.0027132          9.5918          5.1081          5.1081
v  Pressure               -25.174          27.384        -0.74805        -0.74805
v  nu_tilda           4.4095e-007       0.0042982       0.0017386       0.0017386
v  TempC                       21           73.05          22.047          22.047
v  TurbVisc           3.3241e-014        0.005065       0.0020434       0.0020434
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2319:        0.21510E+01

===============================================================


 INSTANT    0.232000000E+04   TIME STEP NUMBER            2320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15300E-01 0.89085E+00
   Friction velocity        uk    :  0.15300E-01 0.89085E+00
   Dimensionless distance   yplus :  0.12318E+00 0.71720E+01
   Friction thermal sca.    tstar : -0.10042E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91903E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10605E-01      33   0.20657E-03   0.46930E+01 0.18899E+03 
c  Velocity[X]                                      0.17374E+01 
c  Velocity[Y]                                      0.29556E+01 
c  Velocity[Z]                                      0.71114E-30 
c  Pressure     0.10414E-06     425   0.96214E-08   0.10083E+00 0.61172E+03 
c  nu_tilda     0.78746E-05      33   0.14127E-04   0.70903E-06 0.21614E+03 
c  TempC        0.42751E+02      27   0.27730E-03   0.66718E+01 0.29398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6548          9.5891          4.5729          4.5729
v  Velocity[Y]            -3.0547          7.2043         0.21929         0.21929
v  Velocity[Z]       -7.9931e-015     6.7827e-015     -1.583e-017     -1.583e-017
v  ǁVelocityǁ         0.0028477          9.5907           5.108           5.108
v  Pressure               -25.201          27.385        -0.75328        -0.75328
v  nu_tilda           4.4096e-007       0.0042989       0.0017388       0.0017388
v  TempC                       21           73.05          22.047          22.047
v  TurbVisc           3.3259e-014       0.0050658       0.0020437       0.0020437
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2320:        0.19660E+01

===============================================================


 INSTANT    0.232100000E+04   TIME STEP NUMBER            2321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16333E-01 0.89258E+00
   Friction velocity        uk    :  0.16333E-01 0.89258E+00
   Dimensionless distance   yplus :  0.13149E+00 0.71859E+01
   Friction thermal sca.    tstar : -0.11548E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98105E-01 0.53615E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10606E-01      33   0.26775E-03   0.46942E+01 0.18909E+03 
c  Velocity[X]                                      0.17340E+01 
c  Velocity[Y]                                      0.29602E+01 
c  Velocity[Z]                                      0.67733E-30 
c  Pressure     0.97999E-07     522   0.96748E-08   0.96462E-01 0.14228E+04 
c  nu_tilda     0.78765E-05      33   0.49843E-05   0.70914E-06 0.21614E+03 
c  TempC        0.42757E+02      27   0.28288E-03   0.46654E+01 0.25764E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6583          9.5879          4.5729          4.5729
v  Velocity[Y]            -3.0545          7.2182         0.21947         0.21947
v  Velocity[Z]        -7.958e-015      6.496e-015    -1.5821e-017    -1.5821e-017
v  ǁVelocityǁ         0.0029866          9.5895          5.1078          5.1078
v  Pressure               -25.148           27.52         -0.6854         -0.6854
v  nu_tilda           4.4092e-007       0.0042996       0.0017391       0.0017391
v  TempC                       21          73.051          22.047          22.047
v  TurbVisc           3.3263e-014       0.0050667        0.002044        0.002044
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2321:        0.21800E+01

===============================================================


 INSTANT    0.232200000E+04   TIME STEP NUMBER            2322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14094E-01 0.89221E+00
   Friction velocity        uk    :  0.14094E-01 0.89221E+00
   Dimensionless distance   yplus :  0.11346E+00 0.71829E+01
   Friction thermal sca.    tstar : -0.14588E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84656E-01 0.53592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10607E-01      33   0.24047E-03   0.47275E+01 0.18924E+03 
c  Velocity[X]                                      0.17573E+01 
c  Velocity[Y]                                      0.29702E+01 
c  Velocity[Z]                                      0.73465E-30 
c  Pressure     0.10549E-06     522   0.99898E-08   0.10500E+00 0.13902E+04 
c  nu_tilda     0.78785E-05      33   0.14116E-04   0.70923E-06 0.21614E+03 
c  TempC        0.42762E+02      27   0.29140E-03   0.36297E+01 0.23297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6618          9.5867          4.5729          4.5729
v  Velocity[Y]            -3.0541          7.1878         0.21964         0.21964
v  Velocity[Z]       -7.9147e-015     7.3596e-015    -1.5806e-017    -1.5806e-017
v  ǁVelocityǁ         0.0027916          9.5883          5.1076          5.1076
v  Pressure               -25.175          27.362        -0.72689        -0.72689
v  nu_tilda           4.4091e-007       0.0043003       0.0017393       0.0017393
v  TempC                       21           73.05          22.047          22.047
v  TurbVisc           3.3252e-014       0.0050675       0.0020444       0.0020444
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2322:        0.21830E+01

===============================================================


 INSTANT    0.232300000E+04   TIME STEP NUMBER            2323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95600E-02 0.89067E+00
   Friction velocity        uk    :  0.95600E-02 0.89067E+00
   Dimensionless distance   yplus :  0.76964E-01 0.71705E+01
   Friction thermal sca.    tstar : -0.21667E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57424E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10608E-01      33   0.23853E-03   0.46952E+01 0.18905E+03 
c  Velocity[X]                                      0.17411E+01 
c  Velocity[Y]                                      0.29541E+01 
c  Velocity[Z]                                      0.65573E-30 
c  Pressure     0.10833E-06     522   0.96744E-08   0.10404E+00 0.14761E+04 
c  nu_tilda     0.78804E-05      33   0.49687E-05   0.70930E-06 0.21614E+03 
c  TempC        0.42768E+02      27   0.25288E-03   0.50451E+01 0.24981E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6652          9.5855          4.5729          4.5729
v  Velocity[Y]             -3.054          7.2047         0.21981         0.21981
v  Velocity[Z]       -7.8918e-015     6.7233e-015    -1.5793e-017    -1.5793e-017
v  ǁVelocityǁ         0.0028702          9.5871          5.1074          5.1074
v  Pressure               -25.124          27.513        -0.65836        -0.65836
v  nu_tilda            4.409e-007        0.004301       0.0017396       0.0017396
v  TempC                       21           73.05          22.047          22.047
v  TurbVisc           3.3249e-014       0.0050683       0.0020447       0.0020447
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2323:        0.21880E+01

===============================================================


 INSTANT    0.232400000E+04   TIME STEP NUMBER            2324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13575E-02 0.89182E+00
   Friction velocity        uk    :  0.13575E-02 0.89182E+00
   Dimensionless distance   yplus :  0.10929E-01 0.71798E+01
   Friction thermal sca.    tstar : -0.32387E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81539E-02 0.53569E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10609E-01      33   0.25832E-03   0.47125E+01 0.18913E+03 
c  Velocity[X]                                      0.17660E+01 
c  Velocity[Y]                                      0.29466E+01 
c  Velocity[Z]                                      0.71103E-30 
c  Pressure     0.96905E-07     521   0.96436E-08   0.96296E-01 0.11769E+04 
c  nu_tilda     0.78824E-05      33   0.14117E-04   0.70943E-06 0.21614E+03 
c  TempC        0.42773E+02      26   0.34218E-03   0.46230E+01 0.26309E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6686          9.5843          4.5729          4.5729
v  Velocity[Y]            -3.0539          7.1837         0.21999         0.21999
v  Velocity[Z]       -7.8304e-015     7.5248e-015     -1.578e-017     -1.578e-017
v  ǁVelocityǁ         0.0026731          9.5859          5.1072          5.1072
v  Pressure               -25.147          27.383        -0.68917        -0.68917
v  nu_tilda           4.4095e-007       0.0043017       0.0017398       0.0017398
v  TempC                       21          73.049          22.047          22.047
v  TurbVisc           3.3245e-014       0.0050692        0.002045        0.002045
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2324:        0.21800E+01

===============================================================


 INSTANT    0.232500000E+04   TIME STEP NUMBER            2325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15394E-01 0.89112E+00
   Friction velocity        uk    :  0.15394E-01 0.89112E+00
   Dimensionless distance   yplus :  0.12393E+00 0.71741E+01
   Friction thermal sca.    tstar : -0.17198E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92465E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10610E-01      33   0.23715E-03   0.47032E+01 0.18917E+03 
c  Velocity[X]                                      0.17378E+01 
c  Velocity[Y]                                      0.29654E+01 
c  Velocity[Z]                                      0.66118E-30 
c  Pressure     0.90392E-07     553   0.92915E-08   0.88492E-01 0.18143E+04 
c  nu_tilda     0.78844E-05      33   0.49659E-05   0.70953E-06 0.21615E+03 
c  TempC        0.42778E+02      27   0.27610E-03   0.59585E+01 0.29648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6719          9.5831          4.5729          4.5729
v  Velocity[Y]            -3.0537          7.2082         0.22016         0.22016
v  Velocity[Z]        -7.775e-015     6.7717e-015    -1.5773e-017    -1.5773e-017
v  ǁVelocityǁ         0.0026598          9.5848           5.107           5.107
v  Pressure                 -25.1          27.598        -0.60909        -0.60909
v  nu_tilda           4.4094e-007       0.0043024       0.0017401       0.0017401
v  TempC                       21          73.051          22.047          22.047
v  TurbVisc            3.326e-014         0.00507       0.0020453       0.0020453
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2325:        0.22810E+01

===============================================================


 INSTANT    0.232600000E+04   TIME STEP NUMBER            2326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.67258E-02 0.89212E+00
   Friction velocity        uk    :  0.67258E-02 0.89212E+00
   Dimensionless distance   yplus :  0.54148E-01 0.71822E+01
   Friction thermal sca.    tstar : -0.12640E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40400E-01 0.53587E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10611E-01      33   0.25067E-03   0.46698E+01 0.18901E+03 
c  Velocity[X]                                      0.17210E+01 
c  Velocity[Y]                                      0.29488E+01 
c  Velocity[Z]                                      0.63141E-30 
c  Pressure     0.10148E-06     504   0.95711E-08   0.98242E-01 0.10674E+04 
c  nu_tilda     0.78863E-05      33   0.14104E-04   0.70966E-06 0.21615E+03 
c  TempC        0.42784E+02      27   0.30232E-03   0.49214E+01 0.25452E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6753          9.5819          4.5729          4.5729
v  Velocity[Y]            -3.0534          7.2104         0.22033         0.22033
v  Velocity[Z]        -7.753e-015     6.4481e-015    -1.5765e-017    -1.5765e-017
v  ǁVelocityǁ         0.0030081          9.5836          5.1069          5.1069
v  Pressure               -25.125          27.491        -0.63733        -0.63733
v  nu_tilda            4.409e-007       0.0043031       0.0017403       0.0017403
v  TempC                       21          73.051          22.047          22.047
v  TurbVisc           3.3258e-014       0.0050708       0.0020456       0.0020456
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2326:        0.21490E+01

===============================================================


 INSTANT    0.232700000E+04   TIME STEP NUMBER            2327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12318E-01 0.89192E+00
   Friction velocity        uk    :  0.12318E-01 0.89192E+00
   Dimensionless distance   yplus :  0.99168E-01 0.71806E+01
   Friction thermal sca.    tstar : -0.10767E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73990E-01 0.53575E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10612E-01      33   0.26599E-03   0.47107E+01 0.18921E+03 
c  Velocity[X]                                      0.17658E+01 
c  Velocity[Y]                                      0.29449E+01 
c  Velocity[Z]                                      0.79760E-30 
c  Pressure     0.11558E-06     488   0.94207E-08   0.11440E+00 0.81006E+03 
c  nu_tilda     0.78883E-05      33   0.49497E-05   0.70971E-06 0.21615E+03 
c  TempC        0.42789E+02      27   0.26063E-03   0.48969E+01 0.26139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6786          9.5808          4.5729          4.5729
v  Velocity[Y]            -3.0531          7.1863          0.2205          0.2205
v  Velocity[Z]       -7.7258e-015     7.4607e-015     -1.575e-017     -1.575e-017
v  ǁVelocityǁ         0.0027302          9.5824          5.1067          5.1067
v  Pressure               -25.071          27.506        -0.59776        -0.59776
v  nu_tilda           4.4091e-007       0.0043037       0.0017406       0.0017406
v  TempC                       21          73.051          22.047          22.047
v  TurbVisc           3.3245e-014       0.0050716       0.0020459       0.0020459
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2327:        0.21030E+01

===============================================================


 INSTANT    0.232800000E+04   TIME STEP NUMBER            2328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90995E-02 0.89053E+00
   Friction velocity        uk    :  0.90995E-02 0.89053E+00
   Dimensionless distance   yplus :  0.73257E-01 0.71694E+01
   Friction thermal sca.    tstar : -0.91368E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54658E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10613E-01      33   0.24494E-03   0.47117E+01 0.18928E+03 
c  Velocity[X]                                      0.17514E+01 
c  Velocity[Y]                                      0.29603E+01 
c  Velocity[Z]                                      0.69229E-30 
c  Pressure     0.96436E-07     312   0.90346E-08   0.94351E-01 0.56194E+03 
c  nu_tilda     0.78902E-05      33   0.14108E-04   0.70982E-06 0.21615E+03 
c  TempC        0.42795E+02      27   0.30468E-03   0.43189E+01 0.24987E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.682          9.5795          4.5729          4.5729
v  Velocity[Y]            -3.0528          7.2052         0.22066         0.22066
v  Velocity[Z]       -7.6905e-015     6.7318e-015    -1.5741e-017    -1.5741e-017
v  ǁVelocityǁ         0.0029798          9.5811          5.1065          5.1065
v  Pressure               -25.099          27.551        -0.59318        -0.59318
v  nu_tilda           4.4094e-007       0.0043045       0.0017408       0.0017408
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3249e-014       0.0050724       0.0020462       0.0020462
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2328:        0.17170E+01

===============================================================


 INSTANT    0.232900000E+04   TIME STEP NUMBER            2329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16974E-01 0.89167E+00
   Friction velocity        uk    :  0.16974E-01 0.89167E+00
   Dimensionless distance   yplus :  0.13665E+00 0.71786E+01
   Friction thermal sca.    tstar : -0.84105E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10196E+00 0.53560E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10614E-01      33   0.24371E-03   0.47007E+01 0.18918E+03 
c  Velocity[X]                                      0.17525E+01 
c  Velocity[Y]                                      0.29482E+01 
c  Velocity[Z]                                      0.69903E-30 
c  Pressure     0.11561E-06     488   0.99106E-08   0.11332E+00 0.71375E+03 
c  nu_tilda     0.78922E-05      33   0.49471E-05   0.70989E-06 0.21615E+03 
c  TempC        0.42800E+02      27   0.29916E-03   0.47426E+01 0.26512E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6853          9.5783          4.5729          4.5729
v  Velocity[Y]            -3.0526          7.1811         0.22083         0.22083
v  Velocity[Z]       -7.6869e-015     6.4442e-015    -1.5737e-017    -1.5737e-017
v  ǁVelocityǁ         0.0026778            9.58          5.1063          5.1063
v  Pressure               -25.045          27.523        -0.56171        -0.56171
v  nu_tilda           4.4094e-007       0.0043052       0.0017411       0.0017411
v  TempC                       21          73.051          22.048          22.048
v  TurbVisc           3.3258e-014       0.0050732       0.0020465       0.0020465
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2329:        0.21120E+01

===============================================================


 INSTANT    0.233000000E+04   TIME STEP NUMBER            2330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10661E-01 0.89097E+00
   Friction velocity        uk    :  0.10661E-01 0.89097E+00
   Dimensionless distance   yplus :  0.85832E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.76239E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64040E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10615E-01      33   0.19554E-03   0.47036E+01 0.18921E+03 
c  Velocity[X]                                      0.17630E+01 
c  Velocity[Y]                                      0.29406E+01 
c  Velocity[Z]                                      0.81291E-30 
c  Pressure     0.90501E-07     329   0.93548E-08   0.89093E-01 0.56663E+03 
c  nu_tilda     0.78941E-05      33   0.14096E-04   0.71003E-06 0.21616E+03 
c  TempC        0.42805E+02      27   0.23690E-03   0.75339E+01 0.29598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6888          9.5771          4.5729          4.5729
v  Velocity[Y]            -3.0525          7.2066           0.221           0.221
v  Velocity[Z]       -7.6608e-015     7.3565e-015    -1.5723e-017    -1.5723e-017
v  ǁVelocityǁ         0.0029753          9.5788          5.1061          5.1061
v  Pressure               -25.074          27.574        -0.55723        -0.55723
v  nu_tilda           4.4088e-007       0.0043058       0.0017413       0.0017413
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3258e-014       0.0050741       0.0020468       0.0020468
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2330:        0.17490E+01

===============================================================


 INSTANT    0.233100000E+04   TIME STEP NUMBER            2331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14668E-01 0.89250E+00
   Friction velocity        uk    :  0.14668E-01 0.89250E+00
   Dimensionless distance   yplus :  0.11809E+00 0.71853E+01
   Friction thermal sca.    tstar : -0.71668E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88107E-01 0.53610E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10616E-01      33   0.23876E-03   0.46759E+01 0.18918E+03 
c  Velocity[X]                                      0.17192E+01 
c  Velocity[Y]                                      0.29567E+01 
c  Velocity[Z]                                      0.65860E-30 
c  Pressure     0.88538E-07     536   0.91928E-08   0.86343E-01 0.11809E+04 
c  nu_tilda     0.78960E-05      33   0.49312E-05   0.71013E-06 0.21617E+03 
c  TempC        0.42811E+02      27   0.32107E-03   0.40935E+01 0.23812E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6922          9.5759          4.5729          4.5729
v  Velocity[Y]            -3.0523          7.2166         0.22116         0.22116
v  Velocity[Z]       -7.6502e-015     6.7225e-015    -1.5713e-017    -1.5713e-017
v  ǁVelocityǁ         0.0030561          9.5776          5.1059          5.1059
v  Pressure                -25.02          27.674        -0.49971        -0.49971
v  nu_tilda           4.4078e-007       0.0043065       0.0017417       0.0017417
v  TempC                       21          73.051          22.048          22.048
v  TurbVisc           3.3238e-014       0.0050749       0.0020471       0.0020471
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2331:        0.22130E+01

===============================================================


 INSTANT    0.233200000E+04   TIME STEP NUMBER            2332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17086E-01 0.89198E+00
   Friction velocity        uk    :  0.17086E-01 0.89198E+00
   Dimensionless distance   yplus :  0.13756E+00 0.71810E+01
   Friction thermal sca.    tstar : -0.66591E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10263E+00 0.53578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10617E-01      33   0.24908E-03   0.46963E+01 0.18923E+03 
c  Velocity[X]                                      0.17536E+01 
c  Velocity[Y]                                      0.29427E+01 
c  Velocity[Z]                                      0.71048E-30 
c  Pressure     0.10500E-06     521   0.95876E-08   0.10317E+00 0.15247E+04 
c  nu_tilda     0.78980E-05      33   0.14097E-04   0.71024E-06 0.21617E+03 
c  TempC        0.42816E+02      27   0.27554E-03   0.50070E+01 0.27066E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6956          9.5747          4.5729          4.5729
v  Velocity[Y]             -3.052          7.1844         0.22133         0.22133
v  Velocity[Z]       -7.6495e-015     7.5439e-015    -1.5696e-017    -1.5696e-017
v  ǁVelocityǁ         0.0026773          9.5764          5.1058          5.1058
v  Pressure               -25.043          27.485        -0.54334        -0.54334
v  nu_tilda           4.4082e-007       0.0043072       0.0017418       0.0017418
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3208e-014       0.0050757       0.0020474       0.0020474
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2332:        0.21890E+01

===============================================================


 INSTANT    0.233300000E+04   TIME STEP NUMBER            2333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15417E-01 0.89080E+00
   Friction velocity        uk    :  0.15417E-01 0.89080E+00
   Dimensionless distance   yplus :  0.12412E+00 0.71716E+01
   Friction thermal sca.    tstar : -0.63156E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92606E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10618E-01      33   0.26855E-03   0.46945E+01 0.18926E+03 
c  Velocity[X]                                      0.17566E+01 
c  Velocity[Y]                                      0.29379E+01 
c  Velocity[Z]                                      0.76369E-30 
c  Pressure     0.93842E-07     569   0.92821E-08   0.92229E-01 0.19282E+04 
c  nu_tilda     0.78999E-05      33   0.49273E-05   0.71028E-06 0.21616E+03 
c  TempC        0.42821E+02      27   0.30370E-03   0.51782E+01 0.27077E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6989          9.5735          4.5729          4.5729
v  Velocity[Y]            -3.0517          7.2072         0.22149         0.22149
v  Velocity[Z]       -7.6236e-015      6.714e-015    -1.5689e-017    -1.5689e-017
v  ǁVelocityǁ         0.0029796          9.5751          5.1056          5.1056
v  Pressure               -24.995          27.713        -0.45836        -0.45836
v  nu_tilda           4.4087e-007       0.0043079       0.0017422       0.0017422
v  TempC                       21          73.051          22.048          22.048
v  TurbVisc           3.3221e-014       0.0050765       0.0020477       0.0020477
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2333:        0.22820E+01

===============================================================


 INSTANT    0.233400000E+04   TIME STEP NUMBER            2334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16397E-01 0.89170E+00
   Friction velocity        uk    :  0.16397E-01 0.89170E+00
   Dimensionless distance   yplus :  0.13200E+00 0.71788E+01
   Friction thermal sca.    tstar : -0.59922E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98490E-01 0.53562E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10619E-01      33   0.25546E-03   0.47129E+01 0.18939E+03 
c  Velocity[X]                                      0.17597E+01 
c  Velocity[Y]                                      0.29532E+01 
c  Velocity[Z]                                      0.66817E-30 
c  Pressure     0.10266E-06     521   0.98092E-08   0.10185E+00 0.14073E+04 
c  nu_tilda     0.79019E-05      33   0.14085E-04   0.71040E-06 0.21616E+03 
c  TempC        0.42827E+02      27   0.32190E-03   0.42440E+01 0.24188E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7022          9.5723          4.5729          4.5729
v  Velocity[Y]            -3.0514          7.1828         0.22166         0.22166
v  Velocity[Z]        -7.606e-015     6.4869e-015    -1.5682e-017    -1.5682e-017
v  ǁVelocityǁ         0.0027794          9.5739          5.1054          5.1054
v  Pressure               -25.019          27.548        -0.49863        -0.49863
v  nu_tilda           4.4093e-007       0.0043086       0.0017423       0.0017423
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3237e-014       0.0050772        0.002048        0.002048
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2334:        0.22340E+01

===============================================================


 INSTANT    0.233500000E+04   TIME STEP NUMBER            2335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96259E-02 0.89086E+00
   Friction velocity        uk    :  0.96259E-02 0.89086E+00
   Dimensionless distance   yplus :  0.77495E-01 0.71720E+01
   Friction thermal sca.    tstar : -0.58675E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57820E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10620E-01      33   0.19434E-03   0.46943E+01 0.18927E+03 
c  Velocity[X]                                      0.17543E+01 
c  Velocity[Y]                                      0.29400E+01 
c  Velocity[Z]                                      0.73204E-30 
c  Pressure     0.11184E-06     522   0.99390E-08   0.10716E+00 0.15728E+04 
c  nu_tilda     0.79038E-05      33   0.49114E-05   0.71048E-06 0.21617E+03 
c  TempC        0.42832E+02      27   0.27846E-03   0.44518E+01 0.24303E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7055          9.5711          4.5729          4.5729
v  Velocity[Y]            -3.0512          7.2039         0.22182         0.22182
v  Velocity[Z]       -7.5974e-015     7.3702e-015    -1.5662e-017    -1.5662e-017
v  ǁVelocityǁ          0.001232          9.5728          5.1052          5.1052
v  Pressure               -24.967          27.718        -0.42637        -0.42637
v  nu_tilda           4.4095e-007       0.0043093       0.0017427       0.0017427
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3255e-014       0.0050781       0.0020483       0.0020483
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2335:        0.22040E+01

===============================================================


 INSTANT    0.233600000E+04   TIME STEP NUMBER            2336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14880E-02 0.89225E+00
   Friction velocity        uk    :  0.14880E-02 0.89225E+00
   Dimensionless distance   yplus :  0.11980E-01 0.71832E+01
   Friction thermal sca.    tstar : -0.57780E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89381E-02 0.53595E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10621E-01      33   0.24785E-03   0.46829E+01 0.18925E+03 
c  Velocity[X]                                      0.17510E+01 
c  Velocity[Y]                                      0.29319E+01 
c  Velocity[Z]                                      0.68866E-30 
c  Pressure     0.84902E-07     504   0.94472E-08   0.83274E-01 0.71372E+03 
c  nu_tilda     0.79057E-05      33   0.14085E-04   0.71062E-06 0.21617E+03 
c  TempC        0.42837E+02      27   0.34313E-03   0.46279E+01 0.26043E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7088          9.5699          4.5729          4.5729
v  Velocity[Y]            -3.0511          7.2127         0.22198         0.22198
v  Velocity[Z]       -7.5604e-015     6.6729e-015     -1.565e-017     -1.565e-017
v  ǁVelocityǁ         0.0030514          9.5715           5.105           5.105
v  Pressure               -24.994          27.683        -0.43879        -0.43879
v  nu_tilda           4.4091e-007       0.0043099       0.0017428       0.0017428
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3261e-014       0.0050789       0.0020486       0.0020486
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2336:        0.21640E+01

===============================================================


 INSTANT    0.233700000E+04   TIME STEP NUMBER            2337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17415E-01 0.89191E+00
   Friction velocity        uk    :  0.17415E-01 0.89191E+00
   Dimensionless distance   yplus :  0.14020E+00 0.71805E+01
   Friction thermal sca.    tstar : -0.57754E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10460E+00 0.53574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10622E-01      33   0.23747E-03   0.47115E+01 0.18949E+03 
c  Velocity[X]                                      0.17521E+01 
c  Velocity[Y]                                      0.29594E+01 
c  Velocity[Z]                                      0.74743E-30 
c  Pressure     0.11142E-06     489   0.99759E-08   0.11104E+00 0.80823E+03 
c  nu_tilda     0.79077E-05      33   0.49080E-05   0.71073E-06 0.21618E+03 
c  TempC        0.42842E+02      27   0.25627E-03   0.58879E+01 0.29283E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.712          9.5686          4.5729          4.5729
v  Velocity[Y]            -3.0509          7.1856         0.22215         0.22215
v  Velocity[Z]       -7.4881e-015     7.4501e-015    -1.5629e-017    -1.5629e-017
v  ǁVelocityǁ         0.0028221          9.5703          5.1048          5.1048
v  Pressure                -24.94          27.689         -0.3989         -0.3989
v  nu_tilda            4.409e-007       0.0043106       0.0017432       0.0017432
v  TempC                       21          73.051          22.048          22.048
v  TurbVisc           3.3248e-014       0.0050797       0.0020488       0.0020488
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2337:        0.21200E+01

===============================================================


 INSTANT    0.233800000E+04   TIME STEP NUMBER            2338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14510E-01 0.89034E+00
   Friction velocity        uk    :  0.14510E-01 0.89034E+00
   Dimensionless distance   yplus :  0.11681E+00 0.71679E+01
   Friction thermal sca.    tstar : -0.58252E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87155E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10623E-01      33   0.24621E-03   0.46799E+01 0.18931E+03 
c  Velocity[X]                                      0.17432E+01 
c  Velocity[Y]                                      0.29366E+01 
c  Velocity[Z]                                      0.69611E-30 
c  Pressure     0.10670E-06     458   0.94422E-08   0.10320E+00 0.64412E+03 
c  nu_tilda     0.79096E-05      33   0.14076E-04   0.71082E-06 0.21618E+03 
c  TempC        0.42848E+02      27   0.31032E-03   0.40309E+01 0.24165E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7153          9.5674          4.5729          4.5729
v  Velocity[Y]            -3.0506          7.2007         0.22231         0.22231
v  Velocity[Z]       -7.3772e-015     6.6697e-015    -1.5616e-017    -1.5616e-017
v  ǁVelocityǁ         0.0027913          9.5691          5.1046          5.1046
v  Pressure               -24.972           27.68        -0.41049        -0.41049
v  nu_tilda           4.4087e-007       0.0043113       0.0017433       0.0017433
v  TempC                       21           73.05          22.048          22.048
v  TurbVisc           3.3244e-014       0.0050805       0.0020491       0.0020491
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2338:        0.20470E+01

===============================================================


 INSTANT    0.233900000E+04   TIME STEP NUMBER            2339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72141E-02 0.89169E+00
   Friction velocity        uk    :  0.72141E-02 0.89169E+00
   Dimensionless distance   yplus :  0.58079E-01 0.71787E+01
   Friction thermal sca.    tstar : -0.57982E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43333E-01 0.53561E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10624E-01      33   0.27708E-03   0.46980E+01 0.18940E+03 
c  Velocity[X]                                      0.17679E+01 
c  Velocity[Y]                                      0.29301E+01 
c  Velocity[Z]                                      0.60629E-30 
c  Pressure     0.11770E-06     505   0.93741E-08   0.11621E+00 0.82622E+03 
c  nu_tilda     0.79115E-05      33   0.48903E-05   0.71086E-06 0.21617E+03 
c  TempC        0.42853E+02      27   0.28821E-03   0.52706E+01 0.25886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7184          9.5662          4.5729          4.5729
v  Velocity[Y]            -3.0503          7.1822         0.22247         0.22247
v  Velocity[Z]       -7.3489e-015     6.5586e-015    -1.5601e-017    -1.5601e-017
v  ǁVelocityǁ         0.0027392          9.5679          5.1045          5.1045
v  Pressure               -24.916          27.696        -0.36975        -0.36975
v  nu_tilda            4.409e-007        0.004312       0.0017437       0.0017437
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3236e-014       0.0050813       0.0020494       0.0020494
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2339:        0.21500E+01

===============================================================


 INSTANT    0.234000000E+04   TIME STEP NUMBER            2340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.69644E-02 0.89086E+00
   Friction velocity        uk    :  0.69644E-02 0.89086E+00
   Dimensionless distance   yplus :  0.56068E-01 0.71720E+01
   Friction thermal sca.    tstar : -0.58442E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41833E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10625E-01      33   0.19831E-03   0.47115E+01 0.18952E+03 
c  Velocity[X]                                      0.17653E+01 
c  Velocity[Y]                                      0.29462E+01 
c  Velocity[Z]                                      0.66416E-30 
c  Pressure     0.99867E-07     409   0.99933E-08   0.97831E-01 0.54790E+03 
c  nu_tilda     0.79134E-05      33   0.14076E-04   0.71097E-06 0.21617E+03 
c  TempC        0.42858E+02      27   0.35455E-03   0.44176E+01 0.24996E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7216           9.565          4.5729          4.5729
v  Velocity[Y]            -3.0499          7.2058         0.22263         0.22263
v  Velocity[Z]       -7.2792e-015     7.3406e-015    -1.5582e-017    -1.5582e-017
v  ǁVelocityǁ         0.0029917          9.5667          5.1043          5.1043
v  Pressure                -24.95          27.729        -0.37199        -0.37199
v  nu_tilda            4.409e-007       0.0043127       0.0017438       0.0017438
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3246e-014       0.0050821       0.0020497       0.0020497
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2340:        0.19330E+01

===============================================================


 INSTANT    0.234100000E+04   TIME STEP NUMBER            2341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46111E-02 0.89236E+00
   Friction velocity        uk    :  0.46111E-02 0.89236E+00
   Dimensionless distance   yplus :  0.37122E-01 0.71841E+01
   Friction thermal sca.    tstar : -0.58173E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27697E-01 0.53601E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10626E-01      33   0.24071E-03   0.46723E+01 0.18931E+03 
c  Velocity[X]                                      0.17388E+01 
c  Velocity[Y]                                      0.29336E+01 
c  Velocity[Z]                                      0.74630E-30 
c  Pressure     0.11028E-06     520   0.96475E-08   0.10682E+00 0.11159E+04 
c  nu_tilda     0.79154E-05      33   0.48884E-05   0.71104E-06 0.21618E+03 
c  TempC        0.42863E+02      27   0.32817E-03   0.53393E+01 0.27572E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.725          9.5638          4.5729          4.5729
v  Velocity[Y]            -3.0497          7.2126         0.22279         0.22279
v  Velocity[Z]       -7.2206e-015     6.6281e-015    -1.5567e-017    -1.5567e-017
v  ǁVelocityǁ         0.0030211          9.5655          5.1041          5.1041
v  Pressure               -24.896          27.811        -0.31694        -0.31694
v  nu_tilda           4.4082e-007       0.0043134       0.0017441       0.0017441
v  TempC                       21          73.051          22.049          22.049
v  TurbVisc           3.3244e-014        0.005083         0.00205         0.00205
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2341:        0.21940E+01

===============================================================


 INSTANT    0.234200000E+04   TIME STEP NUMBER            2342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15296E-01 0.89204E+00
   Friction velocity        uk    :  0.15296E-01 0.89204E+00
   Dimensionless distance   yplus :  0.12315E+00 0.71816E+01
   Friction thermal sca.    tstar : -0.58120E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91881E-01 0.53582E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10627E-01      33   0.24037E-03   0.47077E+01 0.18946E+03 
c  Velocity[X]                                      0.17811E+01 
c  Velocity[Y]                                      0.29266E+01 
c  Velocity[Z]                                      0.70472E-30 
c  Pressure     0.96828E-07     538   0.96504E-08   0.96698E-01 0.13614E+04 
c  nu_tilda     0.79173E-05      33   0.14066E-04   0.71117E-06 0.21618E+03 
c  TempC        0.42869E+02      27   0.32043E-03   0.55593E+01 0.27628E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7283          9.5625          4.5729          4.5729
v  Velocity[Y]            -3.0496          7.1854         0.22295         0.22295
v  Velocity[Z]       -7.1881e-015     6.4623e-015    -1.5557e-017    -1.5557e-017
v  ǁVelocityǁ         0.0027815          9.5642          5.1039          5.1039
v  Pressure               -24.924          27.654        -0.35815        -0.35815
v  nu_tilda           4.4083e-007       0.0043141       0.0017443       0.0017443
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3222e-014       0.0050838       0.0020503       0.0020503
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2342:        0.22050E+01

===============================================================


 INSTANT    0.234300000E+04   TIME STEP NUMBER            2343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13597E-01 0.89067E+00
   Friction velocity        uk    :  0.13597E-01 0.89067E+00
   Dimensionless distance   yplus :  0.10947E+00 0.71705E+01
   Friction thermal sca.    tstar : -0.62482E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81675E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10628E-01      33   0.24111E-03   0.46852E+01 0.18945E+03 
c  Velocity[X]                                      0.17421E+01 
c  Velocity[Y]                                      0.29431E+01 
c  Velocity[Z]                                      0.79819E-30 
c  Pressure     0.85474E-07     568   0.98524E-08   0.83163E-01 0.17902E+04 
c  nu_tilda     0.79192E-05      33   0.48695E-05   0.71123E-06 0.21618E+03 
c  TempC        0.42874E+02      27   0.27503E-03   0.60382E+01 0.28483E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7316          9.5613          4.5729          4.5729
v  Velocity[Y]            -3.0493          7.2052         0.22311         0.22311
v  Velocity[Z]       -7.1792e-015     7.3535e-015    -1.5538e-017    -1.5538e-017
v  ǁVelocityǁ         0.0030321           9.563          5.1037          5.1037
v  Pressure               -24.873          27.861        -0.27789        -0.27789
v  nu_tilda           4.4086e-007       0.0043148       0.0017446       0.0017446
v  TempC                       21          73.051          22.049          22.049
v  TurbVisc           3.3225e-014       0.0050846       0.0020506       0.0020506
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2343:        0.23060E+01

===============================================================


 INSTANT    0.234400000E+04   TIME STEP NUMBER            2344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16977E-01 0.89150E+00
   Friction velocity        uk    :  0.16977E-01 0.89150E+00
   Dimensionless distance   yplus :  0.13667E+00 0.71772E+01
   Friction thermal sca.    tstar : -0.58675E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10197E+00 0.53550E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10629E-01      33   0.25661E-03   0.46849E+01 0.18943E+03 
c  Velocity[X]                                      0.17567E+01 
c  Velocity[Y]                                      0.29282E+01 
c  Velocity[Z]                                      0.77203E-30 
c  Pressure     0.10411E-06     505   0.95226E-08   0.10198E+00 0.16339E+04 
c  nu_tilda     0.79211E-05      33   0.14066E-04   0.71131E-06 0.21618E+03 
c  TempC        0.42879E+02      27   0.34649E-03   0.49603E+01 0.26017E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7348            9.56          4.5729          4.5729
v  Velocity[Y]            -3.0491          7.1788         0.22326         0.22326
v  Velocity[Z]       -7.1111e-015      6.652e-015    -1.5526e-017    -1.5526e-017
v  ǁVelocityǁ         0.0026682          9.5618          5.1035          5.1035
v  Pressure                 -24.9          27.656        -0.32825        -0.32825
v  nu_tilda           4.4088e-007       0.0043155       0.0017448       0.0017448
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3232e-014       0.0050854       0.0020509       0.0020509
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2344:        0.22170E+01

===============================================================


 INSTANT    0.234500000E+04   TIME STEP NUMBER            2345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15371E-01 0.89098E+00
   Friction velocity        uk    :  0.15371E-01 0.89098E+00
   Dimensionless distance   yplus :  0.12375E+00 0.71730E+01
   Friction thermal sca.    tstar : -0.59287E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92330E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10630E-01      33   0.26186E-03   0.46924E+01 0.18948E+03 
c  Velocity[X]                                      0.17689E+01 
c  Velocity[Y]                                      0.29234E+01 
c  Velocity[Z]                                      0.72945E-30 
c  Pressure     0.96887E-07     553   0.97623E-08   0.94951E-01 0.19512E+04 
c  nu_tilda     0.79230E-05      33   0.48671E-05   0.71136E-06 0.21617E+03 
c  TempC        0.42884E+02      27   0.29562E-03   0.54101E+01 0.25701E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.738          9.5588          4.5729          4.5729
v  Velocity[Y]            -3.0487           7.206         0.22342         0.22342
v  Velocity[Z]        -7.097e-015     7.4466e-015     -1.551e-017     -1.551e-017
v  ǁVelocityǁ         0.0030112          9.5606          5.1033          5.1033
v  Pressure               -24.851          27.891          -0.243          -0.243
v  nu_tilda           4.4083e-007       0.0043162       0.0017451       0.0017451
v  TempC                       21          73.051          22.049          22.049
v  TurbVisc            3.324e-014       0.0050862       0.0020512       0.0020512
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2345:        0.26030E+01

===============================================================


 INSTANT    0.234600000E+04   TIME STEP NUMBER            2346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.69167E-02 0.89210E+00
   Friction velocity        uk    :  0.69167E-02 0.89210E+00
   Dimensionless distance   yplus :  0.55684E-01 0.71820E+01
   Friction thermal sca.    tstar : -0.58025E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41546E-01 0.53586E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10631E-01      33   0.23890E-03   0.46836E+01 0.18951E+03 
c  Velocity[X]                                      0.17455E+01 
c  Velocity[Y]                                      0.29381E+01 
c  Velocity[Z]                                      0.70215E-30 
c  Pressure     0.89635E-07     474   0.94814E-08   0.87847E-01 0.87140E+03 
c  nu_tilda     0.79249E-05      33   0.14055E-04   0.71148E-06 0.21618E+03 
c  TempC        0.42889E+02      27   0.34828E-03   0.42343E+01 0.25081E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7412          9.5576          4.5729          4.5729
v  Velocity[Y]            -3.0483          7.2115         0.22358         0.22358
v  Velocity[Z]        -7.103e-015     6.6446e-015    -1.5502e-017    -1.5502e-017
v  ǁVelocityǁ         0.0031567          9.5593          5.1031          5.1031
v  Pressure               -24.881          27.824        -0.26528        -0.26528
v  nu_tilda           4.4075e-007       0.0043169       0.0017453       0.0017453
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3225e-014       0.0050871       0.0020515       0.0020515
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2346:        0.21280E+01

===============================================================


 INSTANT    0.234700000E+04   TIME STEP NUMBER            2347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17793E-01 0.89164E+00
   Friction velocity        uk    :  0.17793E-01 0.89164E+00
   Dimensionless distance   yplus :  0.14325E+00 0.71783E+01
   Friction thermal sca.    tstar : -0.57569E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10688E+00 0.53559E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10631E-01      33   0.23462E-03   0.46952E+01 0.18951E+03 
c  Velocity[X]                                      0.17691E+01 
c  Velocity[Y]                                      0.29261E+01 
c  Velocity[Z]                                      0.60704E-30 
c  Pressure     0.12166E-06     488   0.92329E-08   0.11866E+00 0.72843E+03 
c  nu_tilda     0.79268E-05      33   0.48482E-05   0.71157E-06 0.21618E+03 
c  TempC        0.42895E+02      27   0.27328E-03   0.65535E+01 0.29797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7443          9.5564          4.5729          4.5729
v  Velocity[Y]            -3.0482          7.1816         0.22373         0.22373
v  Velocity[Z]       -7.1197e-015     6.5345e-015    -1.5491e-017    -1.5491e-017
v  ǁVelocityǁ         0.0027069          9.5581          5.1029          5.1029
v  Pressure               -24.821          27.781        -0.23455        -0.23455
v  nu_tilda           4.4081e-007       0.0043176       0.0017456       0.0017456
v  TempC                       21          73.051          22.049          22.049
v  TurbVisc           3.3199e-014       0.0050879       0.0020517       0.0020517
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2347:        0.21090E+01

===============================================================


 INSTANT    0.234800000E+04   TIME STEP NUMBER            2348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13383E-01 0.89046E+00
   Friction velocity        uk    :  0.13383E-01 0.89046E+00
   Dimensionless distance   yplus :  0.10775E+00 0.71688E+01
   Friction thermal sca.    tstar : -0.58589E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80391E-01 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10632E-01      33   0.24857E-03   0.46904E+01 0.18952E+03 
c  Velocity[X]                                      0.17725E+01 
c  Velocity[Y]                                      0.29178E+01 
c  Velocity[Z]                                      0.77347E-30 
c  Pressure     0.87572E-07     280   0.97327E-08   0.85820E-01 0.58225E+03 
c  nu_tilda     0.79287E-05      33   0.14057E-04   0.71168E-06 0.21618E+03 
c  TempC        0.42900E+02      27   0.29996E-03   0.47298E+01 0.25945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7475          9.5551          4.5729          4.5729
v  Velocity[Y]             -3.048           7.202         0.22389         0.22389
v  Velocity[Z]       -7.0842e-015     7.3792e-015    -1.5476e-017    -1.5476e-017
v  ǁVelocityǁ         0.0030153          9.5569          5.1027          5.1027
v  Pressure               -24.856          27.849        -0.23006        -0.23006
v  nu_tilda           4.4089e-007       0.0043183       0.0017458       0.0017458
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3218e-014       0.0050887        0.002052        0.002052
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2348:        0.16260E+01

===============================================================


 INSTANT    0.234900000E+04   TIME STEP NUMBER            2349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17137E-01 0.89159E+00
   Friction velocity        uk    :  0.17137E-01 0.89159E+00
   Dimensionless distance   yplus :  0.13797E+00 0.71779E+01
   Friction thermal sca.    tstar : -0.60426E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10294E+00 0.53555E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10633E-01      33   0.24239E-03   0.46889E+01 0.18958E+03 
c  Velocity[X]                                      0.17538E+01 
c  Velocity[Y]                                      0.29351E+01 
c  Velocity[Z]                                      0.73606E-30 
c  Pressure     0.10028E-06     506   0.96771E-08   0.99477E-01 0.78705E+03 
c  nu_tilda     0.79307E-05      33   0.48459E-05   0.71171E-06 0.21618E+03 
c  TempC        0.42905E+02      27   0.26957E-03   0.45153E+01 0.25896E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7505          9.5539          4.5729          4.5729
v  Velocity[Y]            -3.0478          7.1821         0.22404         0.22404
v  Velocity[Z]        -7.048e-015     6.6876e-015    -1.5466e-017    -1.5466e-017
v  ǁVelocityǁ         0.0027871          9.5556          5.1026          5.1026
v  Pressure                 -24.8          27.847        -0.19164        -0.19164
v  nu_tilda           4.4094e-007       0.0043189       0.0017461       0.0017461
v  TempC                       21          73.051          22.049          22.049
v  TurbVisc           3.3241e-014       0.0050895       0.0020523       0.0020523
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2349:        0.21520E+01

===============================================================


 INSTANT    0.235000000E+04   TIME STEP NUMBER            2350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15691E-01 0.89068E+00
   Friction velocity        uk    :  0.15691E-01 0.89068E+00
   Dimensionless distance   yplus :  0.12632E+00 0.71706E+01
   Friction thermal sca.    tstar : -0.64117E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94251E-01 0.53501E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10634E-01      33   0.19981E-03   0.46746E+01 0.18950E+03 
c  Velocity[X]                                      0.17552E+01 
c  Velocity[Y]                                      0.29194E+01 
c  Velocity[Z]                                      0.66980E-30 
c  Pressure     0.10314E-06     440   0.93994E-08   0.99890E-01 0.59836E+03 
c  nu_tilda     0.79326E-05      33   0.14045E-04   0.71180E-06 0.21618E+03 
c  TempC        0.42910E+02      27   0.24794E-03   0.51162E+01 0.26809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7536          9.5526          4.5729          4.5729
v  Velocity[Y]            -3.0475          7.2015         0.22419         0.22419
v  Velocity[Z]       -6.9878e-015     7.3847e-015    -1.5452e-017    -1.5452e-017
v  ǁVelocityǁ         0.0029828          9.5544          5.1024          5.1024
v  Pressure                -24.83          27.852         -0.1983         -0.1983
v  nu_tilda           4.4093e-007       0.0043196       0.0017463       0.0017463
v  TempC                       21           73.05          22.049          22.049
v  TurbVisc           3.3258e-014       0.0050903       0.0020526       0.0020526
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2350:        0.20070E+01

===============================================================


 INSTANT    0.235100000E+04   TIME STEP NUMBER            2351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17018E-01 0.89240E+00
   Friction velocity        uk    :  0.17018E-01 0.89240E+00
   Dimensionless distance   yplus :  0.13700E+00 0.71845E+01
   Friction thermal sca.    tstar : -0.67219E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10222E+00 0.53604E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10635E-01      33   0.27418E-03   0.46706E+01 0.18952E+03 
c  Velocity[X]                                      0.17550E+01 
c  Velocity[Y]                                      0.29156E+01 
c  Velocity[Z]                                      0.65310E-30 
c  Pressure     0.98233E-07     521   0.99999E-08   0.96169E-01 0.13275E+04 
c  nu_tilda     0.79345E-05      33   0.48263E-05   0.71186E-06 0.21617E+03 
c  TempC        0.42915E+02      27   0.36196E-03   0.46694E+01 0.26620E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7568          9.5514          4.5729          4.5729
v  Velocity[Y]            -3.0471          7.2141         0.22434         0.22434
v  Velocity[Z]       -7.0099e-015     6.7183e-015    -1.5441e-017    -1.5441e-017
v  ǁVelocityǁ         0.0025435          9.5532          5.1022          5.1022
v  Pressure               -24.778          27.974        -0.13466        -0.13466
v  nu_tilda           4.4087e-007       0.0043203       0.0017466       0.0017466
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3254e-014       0.0050911       0.0020529       0.0020529
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2351:        0.22010E+01

===============================================================


 INSTANT    0.235200000E+04   TIME STEP NUMBER            2352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49298E-02 0.89196E+00
   Friction velocity        uk    :  0.49298E-02 0.89196E+00
   Dimensionless distance   yplus :  0.39689E-01 0.71809E+01
   Friction thermal sca.    tstar : -0.72050E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29612E-01 0.53577E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10636E-01      33   0.24105E-03   0.47151E+01 0.18977E+03 
c  Velocity[X]                                      0.17823E+01 
c  Velocity[Y]                                      0.29327E+01 
c  Velocity[Z]                                      0.66408E-30 
c  Pressure     0.10760E-06     505   0.93332E-08   0.10702E+00 0.14122E+04 
c  nu_tilda     0.79364E-05      33   0.14046E-04   0.71198E-06 0.21618E+03 
c  TempC        0.42920E+02      27   0.25195E-03   0.71181E+01 0.31385E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.76          9.5502          4.5729          4.5729
v  Velocity[Y]            -3.0467          7.1854          0.2245          0.2245
v  Velocity[Z]       -6.9895e-015     6.4264e-015    -1.5436e-017    -1.5436e-017
v  ǁVelocityǁ         0.0028288          9.5519           5.102           5.102
v  Pressure               -24.807          27.812        -0.17817        -0.17817
v  nu_tilda           4.4084e-007        0.004321       0.0017467       0.0017467
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3236e-014       0.0050919       0.0020532       0.0020532
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2352:        0.21620E+01

===============================================================


 INSTANT    0.235300000E+04   TIME STEP NUMBER            2353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16238E-01 0.89056E+00
   Friction velocity        uk    :  0.16238E-01 0.89056E+00
   Dimensionless distance   yplus :  0.13073E+00 0.71696E+01
   Friction thermal sca.    tstar : -0.77073E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97540E-01 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10637E-01      33   0.23650E-03   0.46791E+01 0.18957E+03 
c  Velocity[X]                                      0.17612E+01 
c  Velocity[Y]                                      0.29179E+01 
c  Velocity[Z]                                      0.71030E-30 
c  Pressure     0.10488E-06     520   0.98329E-08   0.10120E+00 0.15190E+04 
c  nu_tilda     0.79383E-05      33   0.48240E-05   0.71205E-06 0.21618E+03 
c  TempC        0.42925E+02      27   0.29836E-03   0.50301E+01 0.24879E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7631           9.549          4.5729          4.5729
v  Velocity[Y]            -3.0466          7.2019         0.22465         0.22465
v  Velocity[Z]       -6.9613e-015      7.409e-015    -1.5418e-017    -1.5418e-017
v  ǁVelocityǁ         0.0029609          9.5507          5.1018          5.1018
v  Pressure               -24.754           27.97        -0.10759        -0.10759
v  nu_tilda           4.4078e-007       0.0043217        0.001747        0.001747
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3226e-014       0.0050928       0.0020534       0.0020534
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2353:        0.22300E+01

===============================================================


 INSTANT    0.235400000E+04   TIME STEP NUMBER            2354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12422E-01 0.89163E+00
   Friction velocity        uk    :  0.12422E-01 0.89163E+00
   Dimensionless distance   yplus :  0.10000E+00 0.71782E+01
   Friction thermal sca.    tstar : -0.85006E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74614E-01 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10638E-01      33   0.25257E-03   0.47034E+01 0.18975E+03 
c  Velocity[X]                                      0.17843E+01 
c  Velocity[Y]                                      0.29191E+01 
c  Velocity[Z]                                      0.65678E-30 
c  Pressure     0.97161E-07     536   0.98023E-08   0.96763E-01 0.12661E+04 
c  nu_tilda     0.79402E-05      33   0.14035E-04   0.71218E-06 0.21618E+03 
c  TempC        0.42931E+02      27   0.31701E-03   0.47856E+01 0.25995E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7663          9.5478          4.5729          4.5729
v  Velocity[Y]            -3.0464          7.1798          0.2248          0.2248
v  Velocity[Z]       -6.9469e-015     6.7011e-015    -1.5413e-017    -1.5413e-017
v  ǁVelocityǁ         0.0027904          9.5495          5.1016          5.1016
v  Pressure               -24.784          27.829        -0.14544        -0.14544
v  nu_tilda           4.4078e-007       0.0043224       0.0017472       0.0017472
v  TempC                       21           73.05           22.05           22.05
v  TurbVisc            3.321e-014       0.0050936       0.0020537       0.0020537
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2354:        0.22270E+01

===============================================================


 INSTANT    0.235500000E+04   TIME STEP NUMBER            2355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16069E-01 0.89081E+00
   Friction velocity        uk    :  0.16069E-01 0.89081E+00
   Dimensionless distance   yplus :  0.12937E+00 0.71716E+01
   Friction thermal sca.    tstar : -0.93257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96524E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10639E-01      33   0.19380E-03   0.46874E+01 0.18972E+03 
c  Velocity[X]                                      0.17568E+01 
c  Velocity[Y]                                      0.29306E+01 
c  Velocity[Z]                                      0.78768E-30 
c  Pressure     0.92539E-07     537   0.97073E-08   0.89764E-01 0.18055E+04 
c  nu_tilda     0.79420E-05      33   0.48046E-05   0.71222E-06 0.21618E+03 
c  TempC        0.42936E+02      27   0.30981E-03   0.44640E+01 0.25716E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7694          9.5466          4.5729          4.5729
v  Velocity[Y]            -3.0461          7.2049         0.22495         0.22495
v  Velocity[Z]       -6.9591e-015     7.4125e-015    -1.5397e-017    -1.5397e-017
v  ǁVelocityǁ         0.0027052          9.5482          5.1014          5.1014
v  Pressure               -24.735          28.038       -0.065501       -0.065501
v  nu_tilda           4.4076e-007        0.004323       0.0017475       0.0017475
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3208e-014       0.0050943        0.002054        0.002054
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2355:        0.22340E+01

===============================================================


 INSTANT    0.235600000E+04   TIME STEP NUMBER            2356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96407E-02 0.89201E+00
   Friction velocity        uk    :  0.96407E-02 0.89201E+00
   Dimensionless distance   yplus :  0.77614E-01 0.71813E+01
   Friction thermal sca.    tstar : -0.10691E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57909E-01 0.53580E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10640E-01      33   0.25451E-03   0.46566E+01 0.18956E+03 
c  Velocity[X]                                      0.17433E+01 
c  Velocity[Y]                                      0.29134E+01 
c  Velocity[Z]                                      0.74631E-30 
c  Pressure     0.10169E-06     489   0.94939E-08   0.98307E-01 0.10887E+04 
c  nu_tilda     0.79439E-05      33   0.14034E-04   0.71230E-06 0.21617E+03 
c  TempC        0.42941E+02      26   0.32126E-03   0.49937E+01 0.25665E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7725          9.5454          4.5729          4.5729
v  Velocity[Y]            -3.0458          7.2078          0.2251          0.2251
v  Velocity[Z]       -6.9287e-015     6.6407e-015     -1.539e-017     -1.539e-017
v  ǁVelocityǁ         0.0030646           9.547          5.1012          5.1012
v  Pressure               -24.766          27.934        -0.09845        -0.09845
v  nu_tilda           4.4074e-007       0.0043237       0.0017477       0.0017477
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3204e-014       0.0050951       0.0020543       0.0020543
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2356:        0.21140E+01

===============================================================


 INSTANT    0.235700000E+04   TIME STEP NUMBER            2357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11397E-01 0.89179E+00
   Friction velocity        uk    :  0.11397E-01 0.89179E+00
   Dimensionless distance   yplus :  0.91753E-01 0.71795E+01
   Friction thermal sca.    tstar : -0.12473E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68458E-01 0.53567E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10640E-01      33   0.26078E-03   0.46948E+01 0.18973E+03 
c  Velocity[X]                                      0.17857E+01 
c  Velocity[Y]                                      0.29091E+01 
c  Velocity[Z]                                      0.62432E-30 
c  Pressure     0.10959E-06     522   0.93893E-08   0.10943E+00 0.84137E+03 
c  nu_tilda     0.79458E-05      33   0.48006E-05   0.71234E-06 0.21617E+03 
c  TempC        0.42946E+02      27   0.25137E-03   0.58277E+01 0.27740E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7756          9.5441          4.5729          4.5729
v  Velocity[Y]            -3.0454          7.1839         0.22525         0.22525
v  Velocity[Z]       -6.9287e-015     6.5096e-015    -1.5382e-017    -1.5382e-017
v  ǁVelocityǁ         0.0028097          9.5457           5.101           5.101
v  Pressure               -24.712          27.952       -0.056565       -0.056565
v  nu_tilda           4.4078e-007       0.0043244        0.001748        0.001748
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3196e-014       0.0050959       0.0020546       0.0020546
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2357:        0.21970E+01

===============================================================


 INSTANT    0.235800000E+04   TIME STEP NUMBER            2358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.73001E-02 0.89036E+00
   Friction velocity        uk    :  0.73001E-02 0.89036E+00
   Dimensionless distance   yplus :  0.58770E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.17113E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43849E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10641E-01      33   0.24208E-03   0.46926E+01 0.18979E+03 
c  Velocity[X]                                      0.17684E+01 
c  Velocity[Y]                                      0.29241E+01 
c  Velocity[Z]                                      0.65926E-30 
c  Pressure     0.96322E-07     424   0.96512E-08   0.94362E-01 0.54568E+03 
c  nu_tilda     0.79477E-05      33   0.14026E-04   0.71245E-06 0.21617E+03 
c  TempC        0.42951E+02      27   0.34584E-03   0.50107E+01 0.25507E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7786          9.5429          4.5729          4.5729
v  Velocity[Y]             -3.045          7.2021         0.22539         0.22539
v  Velocity[Z]       -6.9287e-015     7.2605e-015    -1.5369e-017    -1.5369e-017
v  ǁVelocityǁ         0.0031139          9.5444          5.1008          5.1008
v  Pressure               -24.747          27.989       -0.059665       -0.059665
v  nu_tilda            4.408e-007       0.0043251       0.0017482       0.0017482
v  TempC                       21           73.05           22.05           22.05
v  TurbVisc           3.3208e-014       0.0050967       0.0020549       0.0020549
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2358:        0.19700E+01

===============================================================


 INSTANT    0.235900000E+04   TIME STEP NUMBER            2359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10865E-01 0.89143E+00
   Friction velocity        uk    :  0.10865E-01 0.89143E+00
   Dimensionless distance   yplus :  0.87468E-01 0.71766E+01
   Friction thermal sca.    tstar : -0.27239E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65261E-01 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10642E-01      33   0.24347E-03   0.46843E+01 0.18971E+03 
c  Velocity[X]                                      0.17730E+01 
c  Velocity[Y]                                      0.29113E+01 
c  Velocity[Z]                                      0.69032E-30 
c  Pressure     0.11864E-06     473   0.98637E-08   0.11549E+00 0.69323E+03 
c  nu_tilda     0.79496E-05      33   0.47823E-05   0.71251E-06 0.21617E+03 
c  TempC        0.42956E+02      27   0.30785E-03   0.68829E+01 0.29350E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7816          9.5417          4.5729          4.5729
v  Velocity[Y]            -3.0448          7.1772         0.22554         0.22554
v  Velocity[Z]       -6.9287e-015     6.7315e-015    -1.5361e-017    -1.5361e-017
v  ǁVelocityǁ         0.0027257          9.5432          5.1006          5.1006
v  Pressure               -24.691          27.946        -0.03135        -0.03135
v  nu_tilda           4.4088e-007       0.0043257       0.0017485       0.0017485
v  TempC                       21           73.05           22.05           22.05
v  TurbVisc           3.3216e-014       0.0050975       0.0020551       0.0020551
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2359:        0.21090E+01

===============================================================


 INSTANT    0.236000000E+04   TIME STEP NUMBER            2360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12643E-01 0.89072E+00
   Friction velocity        uk    :  0.12643E-01 0.89072E+00
   Dimensionless distance   yplus :  0.10178E+00 0.71709E+01
   Friction thermal sca.    tstar : -0.23403E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75942E-01 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10643E-01      33   0.20217E-03   0.46893E+01 0.18975E+03 
c  Velocity[X]                                      0.17859E+01 
c  Velocity[Y]                                      0.29034E+01 
c  Velocity[Z]                                      0.74511E-30 
c  Pressure     0.92525E-07     330   0.96965E-08   0.90835E-01 0.56472E+03 
c  nu_tilda     0.79515E-05      33   0.14026E-04   0.71260E-06 0.21617E+03 
c  TempC        0.42961E+02      27   0.23895E-03   0.54582E+01 0.27370E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7847          9.5405          4.5729          4.5729
v  Velocity[Y]            -3.0446          7.2029         0.22569         0.22569
v  Velocity[Z]       -6.9287e-015     7.4304e-015    -1.5338e-017    -1.5338e-017
v  ǁVelocityǁ         0.0030065           9.542          5.1004          5.1004
v  Pressure               -24.726          28.011       -0.027053       -0.027053
v  nu_tilda           4.4088e-007       0.0043264       0.0017486       0.0017486
v  TempC                       21           73.05           22.05           22.05
v  TurbVisc            3.324e-014       0.0050983       0.0020554       0.0020554
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2360:        0.17390E+01

===============================================================


 INSTANT    0.236100000E+04   TIME STEP NUMBER            2361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12699E-01 0.89231E+00
   Friction velocity        uk    :  0.12699E-01 0.89231E+00
   Dimensionless distance   yplus :  0.10223E+00 0.71837E+01
   Friction thermal sca.    tstar : -0.16350E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76278E-01 0.53599E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10644E-01      33   0.23441E-03   0.46636E+01 0.18973E+03 
c  Velocity[X]                                      0.17433E+01 
c  Velocity[Y]                                      0.29204E+01 
c  Velocity[Z]                                      0.70408E-30 
c  Pressure     0.86749E-07     506   0.95943E-08   0.85080E-01 0.11722E+04 
c  nu_tilda     0.79534E-05      33   0.47776E-05   0.71262E-06 0.21617E+03 
c  TempC        0.42966E+02      27   0.31487E-03   0.37872E+01 0.23135E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7876          9.5393          4.5729          4.5729
v  Velocity[Y]            -3.0444          7.2134         0.22583         0.22583
v  Velocity[Z]       -6.9287e-015     6.6974e-015    -1.5332e-017    -1.5332e-017
v  ǁVelocityǁ         0.0031564          9.5408          5.1002          5.1002
v  Pressure               -24.674          28.111        0.029647        0.029647
v  nu_tilda           4.4077e-007       0.0043271       0.0017489       0.0017489
v  TempC                       21          73.052           22.05           22.05
v  TurbVisc           3.3239e-014       0.0050991       0.0020557       0.0020557
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2361:        0.21640E+01

===============================================================


 INSTANT    0.236200000E+04   TIME STEP NUMBER            2362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.71634E-02 0.89171E+00
   Friction velocity        uk    :  0.71634E-02 0.89171E+00
   Dimensionless distance   yplus :  0.57670E-01 0.71789E+01
   Friction thermal sca.    tstar : -0.12249E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43029E-01 0.53562E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10645E-01      33   0.24613E-03   0.46808E+01 0.18977E+03 
c  Velocity[X]                                      0.17752E+01 
c  Velocity[Y]                                      0.29056E+01 
c  Velocity[Z]                                      0.74146E-30 
c  Pressure     0.10816E-06     568   0.93017E-08   0.10620E+00 0.16139E+04 
c  nu_tilda     0.79552E-05      33   0.14015E-04   0.71271E-06 0.21616E+03 
c  TempC        0.42971E+02      27   0.25991E-03   0.45023E+01 0.24151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7906          9.5381          4.5729          4.5729
v  Velocity[Y]             -3.044          7.1802         0.22598         0.22598
v  Velocity[Z]       -6.9287e-015     7.3699e-015     -1.532e-017     -1.532e-017
v  ǁVelocityǁ         0.0028113          9.5396             5.1             5.1
v  Pressure               -24.703          27.912       -0.021543       -0.021543
v  nu_tilda           4.4074e-007       0.0043277       0.0017491       0.0017491
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3205e-014       0.0050999        0.002056        0.002056
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2362:        0.22860E+01

===============================================================


 INSTANT    0.236300000E+04   TIME STEP NUMBER            2363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16174E-01 0.89054E+00
   Friction velocity        uk    :  0.16174E-01 0.89054E+00
   Dimensionless distance   yplus :  0.13021E+00 0.71695E+01
   Friction thermal sca.    tstar : -0.10521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97150E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10645E-01      33   0.26680E-03   0.46792E+01 0.18980E+03 
c  Velocity[X]                                      0.17786E+01 
c  Velocity[Y]                                      0.29007E+01 
c  Velocity[Z]                                      0.69364E-30 
c  Pressure     0.10063E-06     521   0.90997E-08   0.98315E-01 0.19020E+04 
c  nu_tilda     0.79571E-05      33   0.47588E-05   0.71277E-06 0.21616E+03 
c  TempC        0.42976E+02      27   0.27091E-03   0.37617E+01 0.22719E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7937          9.5369          4.5729          4.5729
v  Velocity[Y]            -3.0437          7.2036         0.22612         0.22612
v  Velocity[Z]       -6.9287e-015     6.7988e-015     -1.531e-017     -1.531e-017
v  ǁVelocityǁ         0.0030497          9.5384          5.0998          5.0998
v  Pressure               -24.653          28.134        0.062825        0.062825
v  nu_tilda           4.4078e-007       0.0043284       0.0017494       0.0017494
v  TempC                       21          73.051           22.05           22.05
v  TurbVisc           3.3198e-014       0.0051007       0.0020562       0.0020562
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2363:        0.21980E+01

===============================================================


 INSTANT    0.236400000E+04   TIME STEP NUMBER            2364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.64032E-02 0.89153E+00
   Friction velocity        uk    :  0.64032E-02 0.89153E+00
   Dimensionless distance   yplus :  0.51550E-01 0.71774E+01
   Friction thermal sca.    tstar : -0.92245E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38462E-01 0.53551E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10646E-01      33   0.25244E-03   0.47019E+01 0.18996E+03 
c  Velocity[X]                                      0.17843E+01 
c  Velocity[Y]                                      0.29176E+01 
c  Velocity[Z]                                      0.58880E-30 
c  Pressure     0.10416E-06     505   0.94733E-08   0.10334E+00 0.14943E+04 
c  nu_tilda     0.79590E-05      33   0.14015E-04   0.71288E-06 0.21617E+03 
c  TempC        0.42981E+02      26   0.35677E-03   0.51431E+01 0.26112E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7968          9.5356          4.5729          4.5729
v  Velocity[Y]            -3.0433          7.1804         0.22627         0.22627
v  Velocity[Z]       -6.9287e-015     6.3716e-015    -1.5305e-017    -1.5305e-017
v  ǁVelocityǁ         0.0028182          9.5372          5.0996          5.0996
v  Pressure               -24.683          27.959        0.014884        0.014884
v  nu_tilda           4.4083e-007       0.0043291       0.0017496       0.0017496
v  TempC                       21           73.05          22.051          22.051
v  TurbVisc           3.3209e-014       0.0051015       0.0020565       0.0020565
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2364:        0.21660E+01

===============================================================


 INSTANT    0.236500000E+04   TIME STEP NUMBER            2365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60361E-02 0.89075E+00
   Friction velocity        uk    :  0.60361E-02 0.89075E+00
   Dimensionless distance   yplus :  0.48595E-01 0.71711E+01
   Friction thermal sca.    tstar : -0.84144E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36257E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10647E-01      33   0.23389E-03   0.46799E+01 0.18982E+03 
c  Velocity[X]                                      0.17763E+01 
c  Velocity[Y]                                      0.29036E+01 
c  Velocity[Z]                                      0.78450E-30 
c  Pressure     0.11075E-06     538   0.97934E-08   0.10652E+00 0.16198E+04 
c  nu_tilda     0.79609E-05      33   0.47539E-05   0.71293E-06 0.21616E+03 
c  TempC        0.42986E+02      27   0.27091E-03   0.73647E+01 0.30937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7998          9.5344          4.5729          4.5729
v  Velocity[Y]            -3.0431           7.201         0.22641         0.22641
v  Velocity[Z]       -6.9287e-015     7.3811e-015    -1.5291e-017    -1.5291e-017
v  ǁVelocityǁ         0.0027199          9.5359          5.0994          5.0994
v  Pressure                -24.63          28.134        0.089451        0.089451
v  nu_tilda           4.4079e-007       0.0043297       0.0017499       0.0017499
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3223e-014       0.0051023       0.0020568       0.0020568
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2365:        0.22840E+01

===============================================================


 INSTANT    0.236600000E+04   TIME STEP NUMBER            2366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12759E-01 0.89202E+00
   Friction velocity        uk    :  0.12759E-01 0.89202E+00
   Dimensionless distance   yplus :  0.10272E+00 0.71814E+01
   Friction thermal sca.    tstar : -0.76674E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76639E-01 0.53581E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10648E-01      33   0.24847E-03   0.46726E+01 0.18982E+03 
c  Velocity[X]                                      0.17762E+01 
c  Velocity[Y]                                      0.28964E+01 
c  Velocity[Z]                                      0.73351E-30 
c  Pressure     0.87897E-07     458   0.95693E-08   0.86448E-01 0.75730E+03 
c  nu_tilda     0.79627E-05      33   0.14005E-04   0.71301E-06 0.21616E+03 
c  TempC        0.42991E+02      27   0.30499E-03   0.44195E+01 0.24630E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8029          9.5332          4.5729          4.5729
v  Velocity[Y]            -3.0428          7.2088         0.22655         0.22655
v  Velocity[Z]       -6.9287e-015     6.6323e-015    -1.5274e-017    -1.5274e-017
v  ǁVelocityǁ         0.0031676          9.5347          5.0993          5.0993
v  Pressure               -24.663          28.087        0.070331        0.070331
v  nu_tilda           4.4072e-007       0.0043304         0.00175         0.00175
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3212e-014        0.005103        0.002057        0.002057
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2366:        0.20360E+01

===============================================================


 INSTANT    0.236700000E+04   TIME STEP NUMBER            2367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95516E-02 0.89160E+00
   Friction velocity        uk    :  0.95516E-02 0.89160E+00
   Dimensionless distance   yplus :  0.76897E-01 0.71780E+01
   Friction thermal sca.    tstar : -0.72602E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57374E-01 0.53556E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10649E-01      33   0.23756E-03   0.46887E+01 0.18994E+03 
c  Velocity[X]                                      0.17742E+01 
c  Velocity[Y]                                      0.29145E+01 
c  Velocity[Z]                                      0.73341E-30 
c  Pressure     0.10649E-06     488   0.95755E-08   0.10523E+00 0.75801E+03 
c  nu_tilda     0.79646E-05      33   0.47355E-05   0.71304E-06 0.21616E+03 
c  TempC        0.42996E+02      27   0.27082E-03   0.43133E+01 0.25564E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8058           9.532          4.5729          4.5729
v  Velocity[Y]            -3.0425          7.1819         0.22669         0.22669
v  Velocity[Z]       -6.9287e-015     7.4431e-015    -1.5265e-017    -1.5265e-017
v  ǁVelocityǁ         0.0028586          9.5335          5.0991          5.0991
v  Pressure               -24.606          28.082         0.10642         0.10642
v  nu_tilda           4.4075e-007        0.004331       0.0017503       0.0017503
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3192e-014       0.0051038       0.0020573       0.0020573
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2367:        0.21220E+01

===============================================================


 INSTANT    0.236800000E+04   TIME STEP NUMBER            2368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.26988E-02 0.89012E+00
   Friction velocity        uk    :  0.26988E-02 0.89012E+00
   Dimensionless distance   yplus :  0.21727E-01 0.71661E+01
   Friction thermal sca.    tstar : -0.67215E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16211E-01 0.53467E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10650E-01      33   0.23720E-03   0.46647E+01 0.18983E+03 
c  Velocity[X]                                      0.17661E+01 
c  Velocity[Y]                                      0.28986E+01 
c  Velocity[Z]                                      0.68645E-30 
c  Pressure     0.90562E-07     440   0.97861E-08   0.88094E-01 0.57853E+03 
c  nu_tilda     0.79665E-05      33   0.14007E-04   0.71314E-06 0.21615E+03 
c  TempC        0.43001E+02      26   0.25677E-03   0.49274E+01 0.24693E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8088          9.5307          4.5729          4.5729
v  Velocity[Y]            -3.0422          7.1976         0.22683         0.22683
v  Velocity[Z]       -6.9287e-015     6.6058e-015    -1.5257e-017    -1.5257e-017
v  ǁVelocityǁ         0.0027943          9.5323          5.0989          5.0989
v  Pressure               -24.644          28.086         0.09586         0.09586
v  nu_tilda           4.4075e-007       0.0043317       0.0017505       0.0017505
v  TempC                       21           73.05          22.051          22.051
v  TurbVisc           3.3198e-014       0.0051046       0.0020576       0.0020576
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2368:        0.20080E+01

===============================================================


 INSTANT    0.236900000E+04   TIME STEP NUMBER            2369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93427E-02 0.89138E+00
   Friction velocity        uk    :  0.93427E-02 0.89138E+00
   Dimensionless distance   yplus :  0.75215E-01 0.71762E+01
   Friction thermal sca.    tstar : -0.64346E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56119E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10650E-01      33   0.27401E-03   0.46629E+01 0.18985E+03 
c  Velocity[X]                                      0.17703E+01 
c  Velocity[Y]                                      0.28926E+01 
c  Velocity[Z]                                      0.78774E-30 
c  Pressure     0.90869E-07     505   0.95192E-08   0.90259E-01 0.83112E+03 
c  nu_tilda     0.79683E-05      33   0.47295E-05   0.71318E-06 0.21615E+03 
c  TempC        0.43006E+02      27   0.43060E-03   0.38531E+01 0.23758E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8117          9.5295          4.5729          4.5729
v  Velocity[Y]            -3.0418          7.1791         0.22697         0.22697
v  Velocity[Z]       -6.9287e-015     7.4824e-015    -1.5238e-017    -1.5238e-017
v  ǁVelocityǁ         0.0027639          9.5311          5.0987          5.0987
v  Pressure               -24.585          28.094         0.13748         0.13748
v  nu_tilda           4.4076e-007       0.0043324       0.0017508       0.0017508
v  TempC                       21           73.05          22.051          22.051
v  TurbVisc           3.3199e-014       0.0051053       0.0020578       0.0020578
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2369:        0.21580E+01

===============================================================


 INSTANT    0.237000000E+04   TIME STEP NUMBER            2370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15573E-01 0.89066E+00
   Friction velocity        uk    :  0.15573E-01 0.89066E+00
   Dimensionless distance   yplus :  0.12537E+00 0.71704E+01
   Friction thermal sca.    tstar : -0.60634E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93540E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10651E-01      33   0.22171E-03   0.47101E+01 0.19010E+03 
c  Velocity[X]                                      0.17986E+01 
c  Velocity[Y]                                      0.29115E+01 
c  Velocity[Z]                                      0.71636E-30 
c  Pressure     0.11815E-06     393   0.99186E-08   0.11636E+00 0.54309E+03 
c  nu_tilda     0.79702E-05      33   0.13995E-04   0.71328E-06 0.21615E+03 
c  TempC        0.43011E+02      27   0.30576E-03   0.79208E+01 0.32525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8147          9.5283          4.5729          4.5729
v  Velocity[Y]            -3.0414          7.2026         0.22711         0.22711
v  Velocity[Z]       -6.9287e-015     6.6021e-015    -1.5231e-017    -1.5231e-017
v  ǁVelocityǁ         0.0030931          9.5298          5.0985          5.0985
v  Pressure               -24.624          28.139          0.1353          0.1353
v  nu_tilda           4.4073e-007        0.004333       0.0017509       0.0017509
v  TempC                       21           73.05          22.051          22.051
v  TurbVisc           3.3202e-014       0.0051061       0.0020581       0.0020581
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2370:        0.18990E+01

===============================================================


 INSTANT    0.237100000E+04   TIME STEP NUMBER            2371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11151E-01 0.89213E+00
   Friction velocity        uk    :  0.11151E-01 0.89213E+00
   Dimensionless distance   yplus :  0.89774E-01 0.71822E+01
   Friction thermal sca.    tstar : -0.58683E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66982E-01 0.53588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10652E-01      33   0.22818E-03   0.46886E+01 0.19000E+03 
c  Velocity[X]                                      0.17913E+01 
c  Velocity[Y]                                      0.28973E+01 
c  Velocity[Z]                                      0.80004E-30 
c  Pressure     0.11823E-06     504   0.99441E-08   0.11371E+00 0.96160E+03 
c  nu_tilda     0.79720E-05      33   0.47113E-05   0.71333E-06 0.21615E+03 
c  TempC        0.43016E+02      27   0.29740E-03   0.50654E+01 0.26410E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8175           9.527          4.5729          4.5729
v  Velocity[Y]            -3.0412          7.2081         0.22725         0.22725
v  Velocity[Z]       -6.9287e-015     6.5328e-015    -1.5224e-017    -1.5224e-017
v  ǁVelocityǁ         0.0030356          9.5286          5.0983          5.0983
v  Pressure               -24.567          28.194         0.18348         0.18348
v  nu_tilda           4.4069e-007       0.0043337       0.0017512       0.0017512
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3195e-014       0.0051069       0.0020584       0.0020584
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2371:        0.21530E+01

===============================================================


 INSTANT    0.237200000E+04   TIME STEP NUMBER            2372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17001E-01 0.89189E+00
   Friction velocity        uk    :  0.17001E-01 0.89189E+00
   Dimensionless distance   yplus :  0.13687E+00 0.71803E+01
   Friction thermal sca.    tstar : -0.57645E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10212E+00 0.53573E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10653E-01      33   0.24035E-03   0.46769E+01 0.18994E+03 
c  Velocity[X]                                      0.17894E+01 
c  Velocity[Y]                                      0.28875E+01 
c  Velocity[Z]                                      0.74107E-30 
c  Pressure     0.98391E-07     520   0.95096E-08   0.98174E-01 0.12022E+04 
c  nu_tilda     0.79739E-05      33   0.13996E-04   0.71341E-06 0.21615E+03 
c  TempC        0.43020E+02      26   0.28835E-03   0.45862E+01 0.25411E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8204          9.5258          4.5729          4.5729
v  Velocity[Y]             -3.041          7.1817         0.22739         0.22739
v  Velocity[Z]       -6.9287e-015     7.2826e-015    -1.5205e-017    -1.5205e-017
v  ǁVelocityǁ         0.0028104          9.5274          5.0981          5.0981
v  Pressure                 -24.6          28.061         0.14602         0.14602
v  nu_tilda           4.4074e-007       0.0043343       0.0017514       0.0017514
v  TempC                       21           73.05          22.051          22.051
v  TurbVisc           3.3182e-014       0.0051077       0.0020587       0.0020587
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2372:        0.21830E+01

===============================================================


 INSTANT    0.237300000E+04   TIME STEP NUMBER            2373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15367E-01 0.89059E+00
   Friction velocity        uk    :  0.15367E-01 0.89059E+00
   Dimensionless distance   yplus :  0.12371E+00 0.71699E+01
   Friction thermal sca.    tstar : -0.58473E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92302E-01 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10654E-01      33   0.25296E-03   0.46758E+01 0.19009E+03 
c  Velocity[X]                                      0.17617E+01 
c  Velocity[Y]                                      0.29140E+01 
c  Velocity[Z]                                      0.66167E-30 
c  Pressure     0.83936E-07     552   0.92954E-08   0.82200E-01 0.16649E+04 
c  nu_tilda     0.79757E-05      33   0.47054E-05   0.71346E-06 0.21614E+03 
c  TempC        0.43025E+02      27   0.31616E-03   0.43113E+01 0.25676E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8232          9.5246          4.5729          4.5729
v  Velocity[Y]            -3.0407          7.2023         0.22753         0.22753
v  Velocity[Z]       -6.9287e-015     6.7176e-015    -1.5195e-017    -1.5195e-017
v  ǁVelocityǁ         0.0030432          9.5262          5.0979          5.0979
v  Pressure               -24.549          28.246         0.22135         0.22135
v  nu_tilda           4.4078e-007        0.004335       0.0017517       0.0017517
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3197e-014       0.0051084       0.0020589       0.0020589
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2373:        0.22740E+01

===============================================================


 INSTANT    0.237400000E+04   TIME STEP NUMBER            2374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16359E-01 0.89150E+00
   Friction velocity        uk    :  0.16359E-01 0.89150E+00
   Dimensionless distance   yplus :  0.13170E+00 0.71772E+01
   Friction thermal sca.    tstar : -0.57874E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98264E-01 0.53550E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10654E-01      33   0.24603E-03   0.46905E+01 0.19011E+03 
c  Velocity[X]                                      0.17955E+01 
c  Velocity[Y]                                      0.28950E+01 
c  Velocity[Z]                                      0.80783E-30 
c  Pressure     0.12678E-06     520   0.99430E-08   0.12372E+00 0.16527E+04 
c  nu_tilda     0.79776E-05      33   0.13985E-04   0.71355E-06 0.21614E+03 
c  TempC        0.43030E+02      27   0.30947E-03   0.59116E+01 0.29101E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8262          9.5233          4.5729          4.5729
v  Velocity[Y]            -3.0403          7.1751         0.22767         0.22767
v  Velocity[Z]       -6.9287e-015     7.4053e-015    -1.5173e-017    -1.5173e-017
v  ǁVelocityǁ          0.002729          9.5249          5.0977          5.0977
v  Pressure               -24.582          28.044          0.1661          0.1661
v  nu_tilda           4.4085e-007       0.0043356       0.0017518       0.0017518
v  TempC                       21           73.05          22.051          22.051
v  TurbVisc           3.3209e-014       0.0051092       0.0020592       0.0020592
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2374:        0.23830E+01

===============================================================


 INSTANT    0.237500000E+04   TIME STEP NUMBER            2375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15589E-01 0.89103E+00
   Friction velocity        uk    :  0.15589E-01 0.89103E+00
   Dimensionless distance   yplus :  0.12551E+00 0.71734E+01
   Friction thermal sca.    tstar : -0.62535E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93641E-01 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10655E-01      33   0.19602E-03   0.46642E+01 0.18998E+03 
c  Velocity[X]                                      0.17779E+01 
c  Velocity[Y]                                      0.28863E+01 
c  Velocity[Z]                                      0.72326E-30 
c  Pressure     0.97444E-07     570   0.97929E-08   0.95360E-01 0.19378E+04 
c  nu_tilda     0.79794E-05      33   0.46855E-05   0.71359E-06 0.21614E+03 
c  TempC        0.43035E+02      26   0.29080E-03   0.55713E+01 0.26657E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8292          9.5221          4.5729          4.5729
v  Velocity[Y]            -3.0399          7.2033          0.2278          0.2278
v  Velocity[Z]       -6.9287e-015     6.7693e-015    -1.5162e-017    -1.5162e-017
v  ǁVelocityǁ         0.0029253          9.5237          5.0975          5.0975
v  Pressure               -24.532          28.274         0.25106         0.25106
v  nu_tilda           4.4084e-007       0.0043363       0.0017521       0.0017521
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3229e-014       0.0051099       0.0020595       0.0020595
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2375:        0.25520E+01

===============================================================


 INSTANT    0.237600000E+04   TIME STEP NUMBER            2376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16938E-01 0.89230E+00
   Friction velocity        uk    :  0.16938E-01 0.89230E+00
   Dimensionless distance   yplus :  0.13636E+00 0.71836E+01
   Friction thermal sca.    tstar : -0.58792E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10174E+00 0.53598E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10656E-01      33   0.23684E-03   0.46579E+01 0.19001E+03 
c  Velocity[X]                                      0.17548E+01 
c  Velocity[Y]                                      0.29031E+01 
c  Velocity[Z]                                      0.67745E-30 
c  Pressure     0.88267E-07     521   0.99325E-08   0.86503E-01 0.80497E+03 
c  nu_tilda     0.79813E-05      33   0.13985E-04   0.71367E-06 0.21614E+03 
c  TempC        0.43040E+02      27   0.27598E-03   0.39760E+01 0.22978E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8322          9.5208          4.5729          4.5729
v  Velocity[Y]            -3.0395          7.2113         0.22794         0.22794
v  Velocity[Z]       -6.9287e-015     7.4515e-015    -1.5139e-017    -1.5139e-017
v  ǁVelocityǁ         0.0028397          9.5224          5.0973          5.0973
v  Pressure                -24.57          28.218         0.22676         0.22676
v  nu_tilda           4.4075e-007       0.0043369       0.0017523       0.0017523
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.3228e-014       0.0051107       0.0020597       0.0020597
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2376:        0.22110E+01

===============================================================


 INSTANT    0.237700000E+04   TIME STEP NUMBER            2377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16027E-01 0.89191E+00
   Friction velocity        uk    :  0.16027E-01 0.89191E+00
   Dimensionless distance   yplus :  0.12903E+00 0.71805E+01
   Friction thermal sca.    tstar : -0.57721E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96272E-01 0.53574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10657E-01      33   0.25762E-03   0.46941E+01 0.19015E+03 
c  Velocity[X]                                      0.18043E+01 
c  Velocity[Y]                                      0.28898E+01 
c  Velocity[Z]                                      0.89946E-30 
c  Pressure     0.12009E-06     473   0.99386E-08   0.11787E+00 0.68571E+03 
c  nu_tilda     0.79831E-05      33   0.46810E-05   0.71370E-06 0.21614E+03 
c  TempC        0.43045E+02      27   0.28280E-03   0.36180E+01 0.22862E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8351          9.5196          4.5729          4.5729
v  Velocity[Y]            -3.0393          7.1815         0.22807         0.22807
v  Velocity[Z]       -6.9287e-015      6.694e-015    -1.5131e-017    -1.5131e-017
v  ǁVelocityǁ         0.0024377          9.5212          5.0971          5.0971
v  Pressure               -24.513          28.167         0.25278         0.25278
v  nu_tilda           4.4076e-007       0.0043376       0.0017526       0.0017526
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3201e-014       0.0051115         0.00206         0.00206
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2377:        0.20840E+01

===============================================================


 INSTANT    0.237800000E+04   TIME STEP NUMBER            2378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12379E-01 0.89061E+00
   Friction velocity        uk    :  0.12379E-01 0.89061E+00
   Dimensionless distance   yplus :  0.99663E-01 0.71700E+01
   Friction thermal sca.    tstar : -0.58892E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74360E-01 0.53496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10657E-01      33   0.24962E-03   0.46976E+01 0.19019E+03 
c  Velocity[X]                                      0.18151E+01 
c  Velocity[Y]                                      0.28824E+01 
c  Velocity[Z]                                      0.75220E-30 
c  Pressure     0.10424E-06     362   0.99473E-08   0.10256E+00 0.54697E+03 
c  nu_tilda     0.79850E-05      33   0.13977E-04   0.71376E-06 0.21613E+03 
c  TempC        0.43050E+02      27   0.39137E-03   0.50868E+01 0.26667E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.838          9.5183          4.5729          4.5729
v  Velocity[Y]             -3.039          7.2022         0.22821         0.22821
v  Velocity[Z]       -6.9287e-015     7.2929e-015    -1.5112e-017    -1.5112e-017
v  ǁVelocityǁ         0.0023773            9.52          5.0969          5.0969
v  Pressure               -24.554          28.228         0.25255         0.25255
v  nu_tilda           4.4079e-007       0.0043382       0.0017527       0.0017527
v  TempC                       21           73.05          22.052          22.052
v  TurbVisc           3.3202e-014       0.0051123       0.0020602       0.0020602
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2378:        0.18120E+01

===============================================================


 INSTANT    0.237900000E+04   TIME STEP NUMBER            2379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11884E-01 0.89170E+00
   Friction velocity        uk    :  0.11884E-01 0.89170E+00
   Dimensionless distance   yplus :  0.95673E-01 0.71788E+01
   Friction thermal sca.    tstar : -0.62636E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71383E-01 0.53562E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10658E-01      33   0.24805E-03   0.46807E+01 0.19016E+03 
c  Velocity[X]                                      0.17811E+01 
c  Velocity[Y]                                      0.28996E+01 
c  Velocity[Z]                                      0.69699E-30 
c  Pressure     0.10434E-06     506   0.98839E-08   0.10304E+00 0.77846E+03 
c  nu_tilda     0.79868E-05      33   0.46601E-05   0.71379E-06 0.21612E+03 
c  TempC        0.43054E+02      27   0.29941E-03   0.64481E+01 0.30753E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8408          9.5171          4.5729          4.5729
v  Velocity[Y]            -3.0387          7.1805         0.22834         0.22834
v  Velocity[Z]       -6.9287e-015     7.4421e-015    -1.5103e-017    -1.5103e-017
v  ǁVelocityǁ         0.0020516          9.5187          5.0967          5.0967
v  Pressure               -24.496          28.229         0.29025         0.29025
v  nu_tilda           4.4085e-007       0.0043388        0.001753        0.001753
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3213e-014        0.005113       0.0020605       0.0020605
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2379:        0.21670E+01

===============================================================


 INSTANT    0.238000000E+04   TIME STEP NUMBER            2380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14880E-01 0.89065E+00
   Friction velocity        uk    :  0.14880E-01 0.89065E+00
   Dimensionless distance   yplus :  0.11979E+00 0.71704E+01
   Friction thermal sca.    tstar : -0.70942E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89380E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10659E-01      33   0.20319E-03   0.46654E+01 0.19009E+03 
c  Velocity[X]                                      0.17819E+01 
c  Velocity[Y]                                      0.28835E+01 
c  Velocity[Z]                                      0.73063E-30 
c  Pressure     0.10628E-06     458   0.95607E-08   0.10254E+00 0.57724E+03 
c  nu_tilda     0.79887E-05      33   0.13975E-04   0.71387E-06 0.21612E+03 
c  TempC        0.43059E+02      27   0.30098E-03   0.48804E+01 0.25103E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8436          9.5158          4.5729          4.5729
v  Velocity[Y]            -3.0384          7.1995         0.22848         0.22848
v  Velocity[Z]       -6.9287e-015     8.3472e-015    -1.5078e-017    -1.5078e-017
v  ǁVelocityǁ         0.0020398          9.5175          5.0965          5.0965
v  Pressure               -24.535          28.233          0.2771          0.2771
v  nu_tilda           4.4085e-007       0.0043395       0.0017532       0.0017532
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3231e-014       0.0051137       0.0020608       0.0020608
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2380:        0.20600E+01

===============================================================


 INSTANT    0.238100000E+04   TIME STEP NUMBER            2381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11102E-01 0.89216E+00
   Friction velocity        uk    :  0.11102E-01 0.89216E+00
   Dimensionless distance   yplus :  0.89375E-01 0.71825E+01
   Friction thermal sca.    tstar : -0.77577E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66684E-01 0.53589E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10660E-01      33   0.24485E-03   0.46563E+01 0.19008E+03 
c  Velocity[X]                                      0.17776E+01 
c  Velocity[Y]                                      0.28787E+01 
c  Velocity[Z]                                      0.70671E-30 
c  Pressure     0.81515E-07     522   0.98709E-08   0.80233E-01 0.12426E+04 
c  nu_tilda     0.79905E-05      33   0.46553E-05   0.71391E-06 0.21612E+03 
c  TempC        0.43064E+02      27   0.25323E-03   0.44239E+01 0.25266E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8464          9.5146          4.5729          4.5729
v  Velocity[Y]            -3.0379          7.2117         0.22861         0.22861
v  Velocity[Z]       -6.9287e-015     8.2411e-015    -1.5071e-017    -1.5071e-017
v  ǁVelocityǁ         0.0017428          9.5162          5.0963          5.0963
v  Pressure               -24.482          28.344         0.33691         0.33691
v  nu_tilda           4.4076e-007       0.0043401       0.0017534       0.0017534
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc            3.323e-014       0.0051145        0.002061        0.002061
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2381:        0.22020E+01

===============================================================


 INSTANT    0.238200000E+04   TIME STEP NUMBER            2382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.69145E-02 0.89161E+00
   Friction velocity        uk    :  0.69145E-02 0.89161E+00
   Dimensionless distance   yplus :  0.55666E-01 0.71781E+01
   Friction thermal sca.    tstar : -0.82271E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41533E-01 0.53556E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10660E-01      33   0.23605E-03   0.46813E+01 0.19021E+03 
c  Velocity[X]                                      0.17868E+01 
c  Velocity[Y]                                      0.28945E+01 
c  Velocity[Z]                                      0.65747E-30 
c  Pressure     0.98874E-07     521   0.95995E-08   0.98803E-01 0.14066E+04 
c  nu_tilda     0.79923E-05      33   0.13966E-04   0.71400E-06 0.21612E+03 
c  TempC        0.43069E+02      27   0.22253E-03   0.38957E+01 0.23789E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8492          9.5133          4.5729          4.5729
v  Velocity[Y]            -3.0375          7.1817         0.22874         0.22874
v  Velocity[Z]       -6.9287e-015     8.9673e-015    -1.5053e-017    -1.5053e-017
v  ǁVelocityǁ         0.0017432           9.515          5.0961          5.0961
v  Pressure               -24.517          28.181         0.28995         0.28995
v  nu_tilda           4.4073e-007       0.0043408       0.0017536       0.0017536
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3203e-014       0.0051153       0.0020613       0.0020613
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2382:        0.21930E+01

===============================================================


 INSTANT    0.238300000E+04   TIME STEP NUMBER            2383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13127E-01 0.89012E+00
   Friction velocity        uk    :  0.13127E-01 0.89012E+00
   Dimensionless distance   yplus :  0.10568E+00 0.71661E+01
   Friction thermal sca.    tstar : -0.94085E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78848E-01 0.53467E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10661E-01      33   0.24800E-03   0.46636E+01 0.19012E+03 
c  Velocity[X]                                      0.17839E+01 
c  Velocity[Y]                                      0.28797E+01 
c  Velocity[Z]                                      0.69608E-30 
c  Pressure     0.10193E-06     520   0.98296E-08   0.98268E-01 0.14921E+04 
c  nu_tilda     0.79942E-05      33   0.46340E-05   0.71403E-06 0.21611E+03 
c  TempC        0.43074E+02      26   0.34679E-03   0.32478E+01 0.22463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8519          9.5121          4.5729          4.5729
v  Velocity[Y]            -3.0373          7.1987         0.22887         0.22887
v  Velocity[Z]       -6.9287e-015     9.3142e-015    -1.5045e-017    -1.5045e-017
v  ǁVelocityǁ         0.0014871          9.5137          5.0959          5.0959
v  Pressure               -24.463          28.335          0.3597          0.3597
v  nu_tilda           4.4071e-007       0.0043414       0.0017539       0.0017539
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3195e-014        0.005116       0.0020615       0.0020615
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2383:        0.21620E+01

===============================================================


 INSTANT    0.238400000E+04   TIME STEP NUMBER            2384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11307E-01 0.89129E+00
   Friction velocity        uk    :  0.11307E-01 0.89129E+00
   Dimensionless distance   yplus :  0.91029E-01 0.71755E+01
   Friction thermal sca.    tstar : -0.10450E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67918E-01 0.53537E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10662E-01      33   0.25513E-03   0.46920E+01 0.19028E+03 
c  Velocity[X]                                      0.18182E+01 
c  Velocity[Y]                                      0.28738E+01 
c  Velocity[Z]                                      0.74649E-30 
c  Pressure     0.10842E-06     552   0.93427E-08   0.10783E+00 0.12602E+04 
c  nu_tilda     0.79960E-05      33   0.13966E-04   0.71410E-06 0.21611E+03 
c  TempC        0.43078E+02      27   0.26356E-03   0.63162E+01 0.29887E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8547          9.5108          4.5729          4.5729
v  Velocity[Y]             -3.037           7.178           0.229           0.229
v  Velocity[Z]       -6.9287e-015     9.9224e-015    -1.5029e-017    -1.5029e-017
v  ǁVelocityǁ         0.0014972          9.5125          5.0956          5.0956
v  Pressure               -24.498          28.194         0.31838         0.31838
v  nu_tilda           4.4069e-007        0.004342        0.001754        0.001754
v  TempC                       21           73.05          22.052          22.052
v  TurbVisc           3.3187e-014       0.0051168       0.0020618       0.0020618
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2384:        0.22410E+01

===============================================================


 INSTANT    0.238500000E+04   TIME STEP NUMBER            2385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.33495E-02 0.89065E+00
   Friction velocity        uk    :  0.33495E-02 0.89065E+00
   Dimensionless distance   yplus :  0.26966E-01 0.71704E+01
   Friction thermal sca.    tstar : -0.11666E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20119E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10663E-01      33   0.18739E-03   0.46752E+01 0.19027E+03 
c  Velocity[X]                                      0.17845E+01 
c  Velocity[Y]                                      0.28907E+01 
c  Velocity[Z]                                      0.71709E-30 
c  Pressure     0.87172E-07     553   0.96984E-08   0.85675E-01 0.17341E+04 
c  nu_tilda     0.79978E-05      33   0.46294E-05   0.71412E-06 0.21610E+03 
c  TempC        0.43083E+02      27   0.29831E-03   0.49915E+01 0.24596E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8575          9.5096          4.5729          4.5729
v  Velocity[Y]            -3.0367          7.2036         0.22913         0.22913
v  Velocity[Z]       -6.9287e-015     9.7156e-015    -1.5028e-017    -1.5028e-017
v  ǁVelocityǁ         0.0012777          9.5112          5.0954          5.0954
v  Pressure               -24.447          28.392         0.39629         0.39629
v  nu_tilda           4.4061e-007       0.0043426       0.0017543       0.0017543
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3182e-014       0.0051175       0.0020621       0.0020621
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2385:        0.22560E+01

===============================================================


 INSTANT    0.238600000E+04   TIME STEP NUMBER            2386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.84446E-02 0.89195E+00
   Friction velocity        uk    :  0.84446E-02 0.89195E+00
   Dimensionless distance   yplus :  0.67985E-01 0.71808E+01
   Friction thermal sca.    tstar : -0.17065E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50724E-01 0.53577E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10663E-01      33   0.24083E-03   0.46413E+01 0.19011E+03 
c  Velocity[X]                                      0.17657E+01 
c  Velocity[Y]                                      0.28756E+01 
c  Velocity[Z]                                      0.66213E-30 
c  Pressure     0.99762E-07     506   0.98698E-08   0.96936E-01 0.10180E+04 
c  nu_tilda     0.79996E-05      33   0.13955E-04   0.71421E-06 0.21610E+03 
c  TempC        0.43088E+02      26   0.31102E-03   0.45655E+01 0.25248E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8605          9.5083          4.5729          4.5729
v  Velocity[Y]            -3.0363          7.2067         0.22926         0.22926
v  Velocity[Z]       -6.9287e-015     1.0254e-014    -1.5013e-017    -1.5013e-017
v  ǁVelocityǁ         0.0012674            9.51          5.0952          5.0952
v  Pressure               -24.485            28.3         0.36264         0.36264
v  nu_tilda           4.4054e-007       0.0043433       0.0017545       0.0017545
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3157e-014       0.0051182       0.0020623       0.0020623
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2386:        0.21600E+01

===============================================================


 INSTANT    0.238700000E+04   TIME STEP NUMBER            2387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14750E-02 0.89171E+00
   Friction velocity        uk    :  0.14750E-02 0.89171E+00
   Dimensionless distance   yplus :  0.11875E-01 0.71788E+01
   Friction thermal sca.    tstar : -0.19051E+04 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88600E-02 0.53562E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10664E-01      33   0.24360E-03   0.46835E+01 0.19030E+03 
c  Velocity[X]                                      0.18119E+01 
c  Velocity[Y]                                      0.28716E+01 
c  Velocity[Z]                                      0.77060E-30 
c  Pressure     0.10814E-06     489   0.95646E-08   0.10729E+00 0.84298E+03 
c  nu_tilda     0.80015E-05      33   0.46069E-05   0.71425E-06 0.21610E+03 
c  TempC        0.43093E+02      26   0.31431E-03   0.52827E+01 0.26879E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8633           9.507          4.5729          4.5729
v  Velocity[Y]            -3.0359          7.1826         0.22939         0.22939
v  Velocity[Z]       -6.9287e-015     1.0341e-014    -1.5012e-017    -1.5012e-017
v  ǁVelocityǁ          0.001157          9.5087           5.095           5.095
v  Pressure               -24.425          28.312         0.40499         0.40499
v  nu_tilda           4.4056e-007       0.0043439       0.0017548       0.0017548
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3135e-014        0.005119       0.0020626       0.0020626
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2387:        0.21260E+01

===============================================================


 INSTANT    0.238800000E+04   TIME STEP NUMBER            2388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42373E-02 0.89027E+00
   Friction velocity        uk    :  0.42373E-02 0.89027E+00
   Dimensionless distance   yplus :  0.34113E-01 0.71673E+01
   Friction thermal sca.    tstar : -0.34469E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25452E-01 0.53476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10665E-01      33   0.23822E-03   0.46671E+01 0.19029E+03 
c  Velocity[X]                                      0.17810E+01 
c  Velocity[Y]                                      0.28861E+01 
c  Velocity[Z]                                      0.64298E-30 
c  Pressure     0.88449E-07     425   0.98828E-08   0.86763E-01 0.52742E+03 
c  nu_tilda     0.80033E-05      33   0.13957E-04   0.71434E-06 0.21609E+03 
c  TempC        0.43097E+02      27   0.26059E-03   0.51818E+01 0.26726E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8661          9.5058          4.5729          4.5729
v  Velocity[Y]            -3.0355          7.2001         0.22952         0.22952
v  Velocity[Z]       -6.9287e-015     1.0193e-014    -1.5002e-017    -1.5002e-017
v  ǁVelocityǁ         0.0011676          9.5075          5.0948          5.0948
v  Pressure               -24.469          28.351         0.39744         0.39744
v  nu_tilda           4.4057e-007       0.0043446       0.0017549       0.0017549
v  TempC                       21           73.05          22.052          22.052
v  TurbVisc           3.3143e-014       0.0051197       0.0020628       0.0020628
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2388:        0.19550E+01

===============================================================


 INSTANT    0.238900000E+04   TIME STEP NUMBER            2389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13613E-02 0.89121E+00
   Friction velocity        uk    :  0.13613E-02 0.89121E+00
   Dimensionless distance   yplus :  0.10959E-01 0.71749E+01
   Friction thermal sca.    tstar : -0.14128E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81770E-02 0.53533E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10665E-01      33   0.25682E-03   0.46687E+01 0.19027E+03 
c  Velocity[X]                                      0.17959E+01 
c  Velocity[Y]                                      0.28727E+01 
c  Velocity[Z]                                      0.75262E-30 
c  Pressure     0.11270E-06     458   0.97318E-08   0.11057E+00 0.74945E+03 
c  nu_tilda     0.80051E-05      33   0.46028E-05   0.71434E-06 0.21609E+03 
c  TempC        0.43102E+02      27   0.23361E-03   0.47002E+01 0.25105E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8688          9.5045          4.5729          4.5729
v  Velocity[Y]            -3.0352          7.1754         0.22965         0.22965
v  Velocity[Z]       -6.9287e-015     1.0276e-014    -1.4997e-017    -1.4997e-017
v  ǁVelocityǁ           0.00129          9.5062          5.0946          5.0946
v  Pressure               -24.406          28.304         0.42933         0.42933
v  nu_tilda           4.4065e-007       0.0043452       0.0017552       0.0017552
v  TempC                       21          73.051          22.052          22.052
v  TurbVisc           3.3146e-014       0.0051205       0.0020631       0.0020631
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2389:        0.20700E+01

===============================================================


 INSTANT    0.239000000E+04   TIME STEP NUMBER            2390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.20211E-02 0.89050E+00
   Friction velocity        uk    :  0.20211E-02 0.89050E+00
   Dimensionless distance   yplus :  0.16272E-01 0.71691E+01
   Friction thermal sca.    tstar : -0.18108E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12140E-01 0.53490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10666E-01      33   0.24848E-03   0.46876E+01 0.19040E+03 
c  Velocity[X]                                      0.18209E+01 
c  Velocity[Y]                                      0.28668E+01 
c  Velocity[Z]                                      0.76700E-30 
c  Pressure     0.10580E-06     410   0.95333E-08   0.10368E+00 0.54513E+03 
c  nu_tilda     0.80069E-05      33   0.13946E-04   0.71441E-06 0.21608E+03 
c  TempC        0.43107E+02      26   0.37213E-03   0.49771E+01 0.25580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8716          9.5032          4.5729          4.5729
v  Velocity[Y]            -3.0349          7.2001         0.22977         0.22977
v  Velocity[Z]       -6.9287e-015     1.0329e-014    -1.4994e-017    -1.4994e-017
v  ǁVelocityǁ         0.0014037          9.5049          5.0944          5.0944
v  Pressure               -24.451          28.356           0.423           0.423
v  nu_tilda           4.4064e-007       0.0043458       0.0017553       0.0017553
v  TempC                       21           73.05          22.052          22.052
v  TurbVisc            3.317e-014       0.0051212       0.0020633       0.0020633
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2390:        0.19390E+01

===============================================================


 INSTANT    0.239100000E+04   TIME STEP NUMBER            2391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51238E-02 0.89188E+00
   Friction velocity        uk    :  0.51238E-02 0.89188E+00
   Dimensionless distance   yplus :  0.41250E-01 0.71802E+01
   Friction thermal sca.    tstar : -0.13434E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30777E-01 0.53572E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10667E-01      33   0.23344E-03   0.46552E+01 0.19032E+03 
c  Velocity[X]                                      0.17720E+01 
c  Velocity[Y]                                      0.28832E+01 
c  Velocity[Z]                                      0.72117E-30 
c  Pressure     0.89066E-07     522   0.98523E-08   0.86923E-01 0.12612E+04 
c  nu_tilda     0.80087E-05      33   0.45807E-05   0.71443E-06 0.21608E+03 
c  TempC        0.43112E+02      27   0.26376E-03   0.78502E+01 0.32536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8743           9.502          4.5729          4.5729
v  Velocity[Y]            -3.0346          7.2086          0.2299          0.2299
v  Velocity[Z]       -6.9287e-015     1.0265e-014    -1.4988e-017    -1.4988e-017
v  ǁVelocityǁ         0.0018239          9.5037          5.0942          5.0942
v  Pressure               -24.393          28.468         0.48516         0.48516
v  nu_tilda           4.4057e-007       0.0043464       0.0017556       0.0017556
v  TempC                       21          73.052          22.053          22.053
v  TurbVisc           3.3166e-014        0.005122       0.0020636       0.0020636
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2391:        0.22700E+01

===============================================================


 INSTANT    0.239200000E+04   TIME STEP NUMBER            2392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.97956E-02 0.89125E+00
   Friction velocity        uk    :  0.97956E-02 0.89125E+00
   Dimensionless distance   yplus :  0.78861E-01 0.71751E+01
   Friction thermal sca.    tstar : -0.14521E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58839E-01 0.53535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10668E-01      33   0.22929E-03   0.46659E+01 0.19034E+03 
c  Velocity[X]                                      0.17971E+01 
c  Velocity[Y]                                      0.28687E+01 
c  Velocity[Z]                                      0.64720E-30 
c  Pressure     0.10417E-06     521   0.98949E-08   0.10247E+00 0.17468E+04 
c  nu_tilda     0.80105E-05      33   0.13946E-04   0.71452E-06 0.21607E+03 
c  TempC        0.43116E+02      27   0.28487E-03   0.45792E+01 0.25255E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.877          9.5007          4.5729          4.5729
v  Velocity[Y]            -3.0342          7.1757         0.23002         0.23002
v  Velocity[Z]       -6.9287e-015     1.0555e-014    -1.4978e-017    -1.4978e-017
v  ǁVelocityǁ         0.0015145          9.5024           5.094           5.094
v  Pressure                -24.43          28.249         0.42483         0.42483
v  nu_tilda           4.4061e-007       0.0043471       0.0017558       0.0017558
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3145e-014       0.0051227       0.0020638       0.0020638
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2392:        0.22580E+01

===============================================================


 INSTANT    0.239300000E+04   TIME STEP NUMBER            2393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11435E-01 0.89014E+00
   Friction velocity        uk    :  0.11435E-01 0.89014E+00
   Dimensionless distance   yplus :  0.92061E-01 0.71663E+01
   Friction thermal sca.    tstar : -0.12910E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68687E-01 0.53468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10668E-01      33   0.24040E-03   0.46626E+01 0.19035E+03 
c  Velocity[X]                                      0.17995E+01 
c  Velocity[Y]                                      0.28632E+01 
c  Velocity[Z]                                      0.79867E-30 
c  Pressure     0.80949E-07     552   0.98066E-08   0.79723E-01 0.18843E+04 
c  nu_tilda     0.80123E-05      33   0.45747E-05   0.71455E-06 0.21607E+03 
c  TempC        0.43121E+02      26   0.33991E-03   0.42756E+01 0.24992E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8797          9.4994          4.5729          4.5729
v  Velocity[Y]            -3.0337          7.1993         0.23015         0.23015
v  Velocity[Z]       -6.9287e-015     1.0355e-014    -1.4975e-017    -1.4975e-017
v  ǁVelocityǁ        0.00073483          9.5012          5.0938          5.0938
v  Pressure               -24.376          28.466         0.50951         0.50951
v  nu_tilda           4.4068e-007       0.0043477        0.001756        0.001756
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3159e-014       0.0051235       0.0020641       0.0020641
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2393:        0.24880E+01

===============================================================


 INSTANT    0.239400000E+04   TIME STEP NUMBER            2394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95257E-02 0.89116E+00
   Friction velocity        uk    :  0.95257E-02 0.89116E+00
   Dimensionless distance   yplus :  0.76688E-01 0.71745E+01
   Friction thermal sca.    tstar : -0.12530E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57218E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10669E-01      33   0.25158E-03   0.46789E+01 0.19053E+03 
c  Velocity[X]                                      0.17921E+01 
c  Velocity[Y]                                      0.28868E+01 
c  Velocity[Z]                                      0.64492E-30 
c  Pressure     0.98083E-07     537   0.91816E-08   0.97631E-01 0.14461E+04 
c  nu_tilda     0.80141E-05      33   0.13936E-04   0.71467E-06 0.21607E+03 
c  TempC        0.43126E+02      27   0.26975E-03   0.59402E+01 0.26445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8823          9.4982          4.5729          4.5729
v  Velocity[Y]            -3.0334          7.1751         0.23027         0.23027
v  Velocity[Z]       -6.9287e-015     1.0423e-014    -1.4966e-017    -1.4966e-017
v  ǁVelocityǁ        0.00043683          9.4999          5.0936          5.0936
v  Pressure               -24.415            28.3         0.45867         0.45867
v  nu_tilda           4.4077e-007       0.0043484       0.0017562       0.0017562
v  TempC                       21           73.05          22.053          22.053
v  TurbVisc            3.318e-014       0.0051243       0.0020643       0.0020643
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2394:        0.24630E+01

===============================================================


 INSTANT    0.239500000E+04   TIME STEP NUMBER            2395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72525E-02 0.89035E+00
   Friction velocity        uk    :  0.72525E-02 0.89035E+00
   Dimensionless distance   yplus :  0.58388E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.15314E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43564E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10670E-01      33   0.21078E-03   0.46685E+01 0.19042E+03 
c  Velocity[X]                                      0.18010E+01 
c  Velocity[Y]                                      0.28675E+01 
c  Velocity[Z]                                      0.64301E-30 
c  Pressure     0.11089E-06     520   0.97601E-08   0.10688E+00 0.15007E+04 
c  nu_tilda     0.80159E-05      33   0.45535E-05   0.71466E-06 0.21606E+03 
c  TempC        0.43130E+02      27   0.33016E-03   0.45951E+01 0.25468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.885          9.4969          4.5729          4.5729
v  Velocity[Y]            -3.0331          7.1976          0.2304          0.2304
v  Velocity[Z]       -6.9287e-015     1.0504e-014    -1.4964e-017    -1.4964e-017
v  ǁVelocityǁ        0.00024134          9.4986          5.0934          5.0934
v  Pressure               -24.361          28.454         0.52846         0.52846
v  nu_tilda           4.4082e-007        0.004349       0.0017565       0.0017565
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3205e-014        0.005125       0.0020646       0.0020646
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2395:        0.23600E+01

===============================================================


 INSTANT    0.239600000E+04   TIME STEP NUMBER            2396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50292E-02 0.89200E+00
   Friction velocity        uk    :  0.50292E-02 0.89200E+00
   Dimensionless distance   yplus :  0.40488E-01 0.71812E+01
   Friction thermal sca.    tstar : -0.26675E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30209E-01 0.53580E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10670E-01      33   0.25686E-03   0.46685E+01 0.19046E+03 
c  Velocity[X]                                      0.18093E+01 
c  Velocity[Y]                                      0.28592E+01 
c  Velocity[Z]                                      0.71563E-30 
c  Pressure     0.10329E-06     474   0.93832E-08   0.10130E+00 0.72372E+03 
c  nu_tilda     0.80177E-05      33   0.13936E-04   0.71471E-06 0.21605E+03 
c  TempC        0.43135E+02      27   0.28932E-03   0.54023E+01 0.29113E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8878          9.4956          4.5729          4.5729
v  Velocity[Y]            -3.0328          7.2077         0.23052         0.23052
v  Velocity[Z]       -6.9287e-015     1.0341e-014    -1.4952e-017    -1.4952e-017
v  ǁVelocityǁ        0.00039635          9.4973          5.0932          5.0932
v  Pressure               -24.403           28.42         0.50476         0.50476
v  nu_tilda           4.4081e-007       0.0043496       0.0017566       0.0017566
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3221e-014       0.0051258       0.0020648       0.0020648
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2396:        0.21460E+01

===============================================================


 INSTANT    0.239700000E+04   TIME STEP NUMBER            2397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57443E-02 0.89174E+00
   Friction velocity        uk    :  0.57443E-02 0.89174E+00
   Dimensionless distance   yplus :  0.46245E-01 0.71791E+01
   Friction thermal sca.    tstar : -0.50771E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34504E-01 0.53564E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10671E-01      33   0.22940E-03   0.46789E+01 0.19054E+03 
c  Velocity[X]                                      0.18023E+01 
c  Velocity[Y]                                      0.28765E+01 
c  Velocity[Z]                                      0.77669E-30 
c  Pressure     0.10298E-06     474   0.94168E-08   0.10264E+00 0.70370E+03 
c  nu_tilda     0.80195E-05      33   0.45467E-05   0.71472E-06 0.21605E+03 
c  TempC        0.43139E+02      27   0.32926E-03   0.64947E+01 0.27246E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8905          9.4943          4.5729          4.5729
v  Velocity[Y]            -3.0324          7.1815         0.23065         0.23065
v  Velocity[Z]       -6.9287e-015     1.0266e-014    -1.4957e-017    -1.4957e-017
v  ǁVelocityǁ        0.00095831          9.4961           5.093           5.093
v  Pressure               -24.347          28.397         0.53633         0.53633
v  nu_tilda           4.4079e-007       0.0043503       0.0017569       0.0017569
v  TempC                       21          73.052          22.053          22.053
v  TurbVisc           3.3218e-014       0.0051265       0.0020651       0.0020651
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2397:        0.21900E+01

===============================================================


 INSTANT    0.239800000E+04   TIME STEP NUMBER            2398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10644E-01 0.89021E+00
   Friction velocity        uk    :  0.10644E-01 0.89021E+00
   Dimensionless distance   yplus :  0.85694E-01 0.71668E+01
   Friction thermal sca.    tstar : -0.16707E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63937E-01 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10672E-01      33   0.23608E-03   0.46511E+01 0.19041E+03 
c  Velocity[X]                                      0.17903E+01 
c  Velocity[Y]                                      0.28608E+01 
c  Velocity[Z]                                      0.63683E-30 
c  Pressure     0.10215E-06     456   0.92190E-08   0.98965E-01 0.55870E+03 
c  nu_tilda     0.80213E-05      33   0.13928E-04   0.71481E-06 0.21605E+03 
c  TempC        0.43144E+02      27   0.24850E-03   0.59728E+01 0.27338E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8932          9.4931          4.5729          4.5729
v  Velocity[Y]             -3.032          7.1951         0.23077         0.23077
v  Velocity[Z]       -6.9287e-015     1.0181e-014    -1.4944e-017    -1.4944e-017
v  ǁVelocityǁ         0.0010208          9.4948          5.0928          5.0928
v  Pressure               -24.388          28.413         0.52365         0.52365
v  nu_tilda           4.4077e-007        0.004351        0.001757        0.001757
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3213e-014       0.0051273       0.0020653       0.0020653
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2398:        0.20460E+01

===============================================================


 INSTANT    0.239900000E+04   TIME STEP NUMBER            2399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.22637E-02 0.89136E+00
   Friction velocity        uk    :  0.22637E-02 0.89136E+00
   Dimensionless distance   yplus :  0.18224E-01 0.71761E+01
   Friction thermal sca.    tstar : -0.13536E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13597E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10672E-01      33   0.25566E-03   0.46767E+01 0.19054E+03 
c  Velocity[X]                                      0.18207E+01 
c  Velocity[Y]                                      0.28560E+01 
c  Velocity[Z]                                      0.72091E-30 
c  Pressure     0.10439E-06     458   0.96078E-08   0.10343E+00 0.77457E+03 
c  nu_tilda     0.80231E-05      33   0.45254E-05   0.71484E-06 0.21604E+03 
c  TempC        0.43149E+02      27   0.27666E-03   0.42457E+01 0.24390E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8959          9.4918          4.5729          4.5729
v  Velocity[Y]            -3.0315          7.1771         0.23089         0.23089
v  Velocity[Z]       -6.9287e-015     9.8695e-015    -1.4944e-017    -1.4944e-017
v  ǁVelocityǁ         0.0015384          9.4935          5.0926          5.0926
v  Pressure               -24.332          28.414         0.56192         0.56192
v  nu_tilda           4.4078e-007       0.0043516       0.0017573       0.0017573
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3206e-014        0.005128       0.0020656       0.0020656
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2399:        0.20360E+01

===============================================================


 INSTANT    0.240000000E+04   TIME STEP NUMBER            2400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.73465E-02 0.89050E+00
   Friction velocity        uk    :  0.73465E-02 0.89050E+00
   Dimensionless distance   yplus :  0.59144E-01 0.71691E+01
   Friction thermal sca.    tstar : -0.10872E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44128E-01 0.53490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10673E-01      33   0.19071E-03   0.46686E+01 0.19055E+03 
c  Velocity[X]                                      0.17977E+01 
c  Velocity[Y]                                      0.28709E+01 
c  Velocity[Z]                                      0.66148E-30 
c  Pressure     0.92893E-07     425   0.93572E-08   0.90874E-01 0.53276E+03 
c  nu_tilda     0.80249E-05      33   0.13927E-04   0.71489E-06 0.21604E+03 
c  TempC        0.43153E+02      27   0.37126E-03   0.52798E+01 0.25443E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8986          9.4905          4.5729          4.5729
v  Velocity[Y]            -3.0312          7.1994         0.23101         0.23101
v  Velocity[Z]       -6.9287e-015     9.7633e-015    -1.4938e-017    -1.4938e-017
v  ǁVelocityǁ         0.0015421          9.4922          5.0924          5.0924
v  Pressure               -24.377          28.461         0.55467         0.55467
v  nu_tilda           4.4075e-007       0.0043522       0.0017574       0.0017574
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3208e-014       0.0051288       0.0020658       0.0020658
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2400:        0.19600E+01

===============================================================


 INSTANT    0.240100000E+04   TIME STEP NUMBER            2401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.74172E-02 0.89177E+00
   Friction velocity        uk    :  0.74172E-02 0.89177E+00
   Dimensionless distance   yplus :  0.59714E-01 0.71794E+01
   Friction thermal sca.    tstar : -0.99067E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44553E-01 0.53566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10674E-01      33   0.24946E-03   0.46426E+01 0.19042E+03 
c  Velocity[X]                                      0.17853E+01 
c  Velocity[Y]                                      0.28573E+01 
c  Velocity[Z]                                      0.74915E-30 
c  Pressure     0.10485E-06     488   0.92319E-08   0.10159E+00 0.92310E+03 
c  nu_tilda     0.80267E-05      33   0.45183E-05   0.71488E-06 0.21603E+03 
c  TempC        0.43158E+02      27   0.24097E-03   0.65672E+01 0.30168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9012          9.4892          4.5729          4.5729
v  Velocity[Y]            -3.0309          7.2045         0.23113         0.23113
v  Velocity[Z]       -6.9287e-015     9.4374e-015    -1.4942e-017    -1.4942e-017
v  ǁVelocityǁ         0.0019785           9.491          5.0922          5.0922
v  Pressure               -24.322           28.51         0.60085         0.60085
v  nu_tilda           4.4069e-007       0.0043529       0.0017577       0.0017577
v  TempC                       21          73.052          22.053          22.053
v  TurbVisc           3.3201e-014       0.0051296       0.0020661       0.0020661
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2401:        0.21220E+01

===============================================================


 INSTANT    0.240200000E+04   TIME STEP NUMBER            2402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.34388E-02 0.89141E+00
   Friction velocity        uk    :  0.34388E-02 0.89141E+00
   Dimensionless distance   yplus :  0.27684E-01 0.71764E+01
   Friction thermal sca.    tstar : -0.87101E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20656E-01 0.53544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10674E-01      33   0.24813E-03   0.46917E+01 0.19067E+03 
c  Velocity[X]                                      0.18397E+01 
c  Velocity[Y]                                      0.28520E+01 
c  Velocity[Z]                                      0.72681E-30 
c  Pressure     0.11023E-06     506   0.98256E-08   0.11011E+00 0.13100E+04 
c  nu_tilda     0.80285E-05      33   0.13918E-04   0.71494E-06 0.21602E+03 
c  TempC        0.43162E+02      27   0.32324E-03   0.38918E+01 0.23511E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9038          9.4879          4.5729          4.5729
v  Velocity[Y]            -3.0306           7.178         0.23125         0.23125
v  Velocity[Z]       -6.9287e-015     9.3188e-015    -1.4932e-017    -1.4932e-017
v  ǁVelocityǁ         0.0019529          9.4897           5.092           5.092
v  Pressure                -24.36          28.361         0.55542         0.55542
v  nu_tilda           4.4068e-007       0.0043535       0.0017578       0.0017578
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc            3.318e-014       0.0051303       0.0020663       0.0020663
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2402:        0.21570E+01

===============================================================


 INSTANT    0.240300000E+04   TIME STEP NUMBER            2403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42717E-02 0.89017E+00
   Friction velocity        uk    :  0.42717E-02 0.89017E+00
   Dimensionless distance   yplus :  0.34390E-01 0.71665E+01
   Friction thermal sca.    tstar : -0.81163E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25659E-01 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10675E-01      33   0.23741E-03   0.46645E+01 0.19061E+03 
c  Velocity[X]                                      0.17969E+01 
c  Velocity[Y]                                      0.28676E+01 
c  Velocity[Z]                                      0.71064E-30 
c  Pressure     0.86183E-07     536   0.93517E-08   0.84110E-01 0.17302E+04 
c  nu_tilda     0.80303E-05      33   0.44974E-05   0.71497E-06 0.21602E+03 
c  TempC        0.43167E+02      27   0.32484E-03   0.79577E+01 0.30243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9064          9.4866          4.5729          4.5729
v  Velocity[Y]            -3.0302          7.1993         0.23137         0.23137
v  Velocity[Z]       -6.9287e-015      8.998e-015    -1.4936e-017    -1.4936e-017
v  ǁVelocityǁ         0.0023499          9.4884          5.0918          5.0918
v  Pressure               -24.309          28.559          0.6333          0.6333
v  nu_tilda           4.4066e-007       0.0043541       0.0017581       0.0017581
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3177e-014        0.005131       0.0020665       0.0020665
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2403:        0.22530E+01

===============================================================


 INSTANT    0.240400000E+04   TIME STEP NUMBER            2404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42189E-02 0.89115E+00
   Friction velocity        uk    :  0.42189E-02 0.89115E+00
   Dimensionless distance   yplus :  0.33965E-01 0.71743E+01
   Friction thermal sca.    tstar : -0.74693E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25342E-01 0.53529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10675E-01      33   0.24209E-03   0.46563E+01 0.19055E+03 
c  Velocity[X]                                      0.18033E+01 
c  Velocity[Y]                                      0.28530E+01 
c  Velocity[Z]                                      0.68483E-30 
c  Pressure     0.10301E-06     505   0.92257E-08   0.10111E+00 0.16084E+04 
c  nu_tilda     0.80320E-05      33   0.13917E-04   0.71507E-06 0.21602E+03 
c  TempC        0.43172E+02      26   0.30312E-03   0.61285E+01 0.28462E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.909          9.4853          4.5729          4.5729
v  Velocity[Y]            -3.0298          7.1727         0.23149         0.23149
v  Velocity[Z]       -6.9287e-015     8.8848e-015     -1.493e-017     -1.493e-017
v  ǁVelocityǁ         0.0022942          9.4871          5.0916          5.0916
v  Pressure               -24.347          28.364         0.57706         0.57706
v  nu_tilda           4.4068e-007       0.0043548       0.0017582       0.0017582
v  TempC                       21           73.05          22.053          22.053
v  TurbVisc           3.3172e-014       0.0051318       0.0020668       0.0020668
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2404:        0.24580E+01

===============================================================


 INSTANT    0.240500000E+04   TIME STEP NUMBER            2405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21857E-02 0.89058E+00
   Friction velocity        uk    :  0.21857E-02 0.89058E+00
   Dimensionless distance   yplus :  0.17596E-01 0.71698E+01
   Friction thermal sca.    tstar : -0.70866E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13129E-01 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10676E-01      33   0.19283E-03   0.46635E+01 0.19060E+03 
c  Velocity[X]                                      0.18155E+01 
c  Velocity[Y]                                      0.28481E+01 
c  Velocity[Z]                                      0.78113E-30 
c  Pressure     0.84357E-07     536   0.99390E-08   0.83178E-01 0.18238E+04 
c  nu_tilda     0.80338E-05      33   0.44883E-05   0.71509E-06 0.21601E+03 
c  TempC        0.43176E+02      27   0.31806E-03   0.41910E+01 0.25805E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9116           9.484          4.5729          4.5729
v  Velocity[Y]            -3.0293          7.2011         0.23161         0.23161
v  Velocity[Z]       -6.9287e-015     8.5632e-015    -1.4935e-017    -1.4935e-017
v  ǁVelocityǁ         0.0026948          9.4858          5.0914          5.0914
v  Pressure               -24.295          28.575         0.65824         0.65824
v  nu_tilda           4.4064e-007       0.0043554       0.0017585       0.0017585
v  TempC                       21          73.051          22.053          22.053
v  TurbVisc           3.3179e-014       0.0051325        0.002067        0.002067
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2405:        0.23100E+01

===============================================================


 INSTANT    0.240600000E+04   TIME STEP NUMBER            2406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.61491E-02 0.89195E+00
   Friction velocity        uk    :  0.61491E-02 0.89195E+00
   Dimensionless distance   yplus :  0.49505E-01 0.71808E+01
   Friction thermal sca.    tstar : -0.66455E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36936E-01 0.53577E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10677E-01      33   0.23901E-03   0.46436E+01 0.19058E+03 
c  Velocity[X]                                      0.17810E+01 
c  Velocity[Y]                                      0.28626E+01 
c  Velocity[Z]                                      0.68177E-30 
c  Pressure     0.84123E-07     490   0.93710E-08   0.82826E-01 0.87286E+03 
c  nu_tilda     0.80356E-05      33   0.13907E-04   0.71513E-06 0.21600E+03 
c  TempC        0.43181E+02      27   0.23501E-03   0.65895E+01 0.28445E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9141          9.4827          4.5729          4.5729
v  Velocity[Y]            -3.0289          7.2078         0.23172         0.23172
v  Velocity[Z]       -6.9287e-015     8.4644e-015    -1.4927e-017    -1.4927e-017
v  ǁVelocityǁ         0.0026349          9.4846          5.0911          5.0911
v  Pressure               -24.336          28.511         0.62885         0.62885
v  nu_tilda           4.4052e-007        0.004356       0.0017587       0.0017587
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3168e-014       0.0051333       0.0020673       0.0020673
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2406:        0.21170E+01

===============================================================


 INSTANT    0.240700000E+04   TIME STEP NUMBER            2407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.45535E-02 0.89149E+00
   Friction velocity        uk    :  0.45535E-02 0.89149E+00
   Dimensionless distance   yplus :  0.36659E-01 0.71771E+01
   Friction thermal sca.    tstar : -0.63934E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27351E-01 0.53549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10677E-01      33   0.25260E-03   0.46701E+01 0.19065E+03 
c  Velocity[X]                                      0.18197E+01 
c  Velocity[Y]                                      0.28503E+01 
c  Velocity[Z]                                      0.63336E-30 
c  Pressure     0.11634E-06     458   0.99261E-08   0.11383E+00 0.67207E+03 
c  nu_tilda     0.80374E-05      33   0.44683E-05   0.71514E-06 0.21599E+03 
c  TempC        0.43185E+02      27   0.36170E-03   0.44255E+01 0.25488E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9167          9.4815          4.5729          4.5729
v  Velocity[Y]            -3.0286           7.178         0.23184         0.23184
v  Velocity[Z]       -6.9287e-015      8.163e-015    -1.4934e-017    -1.4934e-017
v  ǁVelocityǁ         0.0028408          9.4833          5.0909          5.0909
v  Pressure               -24.279          28.461         0.65491         0.65491
v  nu_tilda           4.4053e-007       0.0043567       0.0017589       0.0017589
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc            3.313e-014        0.005134       0.0020675       0.0020675
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2407:        0.20400E+01

===============================================================


 INSTANT    0.240800000E+04   TIME STEP NUMBER            2408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.63821E-02 0.89020E+00
   Friction velocity        uk    :  0.63821E-02 0.89020E+00
   Dimensionless distance   yplus :  0.51381E-01 0.71667E+01
   Friction thermal sca.    tstar : -0.60189E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38336E-01 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10678E-01      33   0.25290E-03   0.46779E+01 0.19075E+03 
c  Velocity[X]                                      0.18345E+01 
c  Velocity[Y]                                      0.28434E+01 
c  Velocity[Z]                                      0.73280E-30 
c  Pressure     0.10260E-06     393   0.95707E-08   0.10059E+00 0.53716E+03 
c  nu_tilda     0.80391E-05      33   0.13909E-04   0.71520E-06 0.21599E+03 
c  TempC        0.43190E+02      27   0.27284E-03   0.64076E+01 0.30411E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9193          9.4802          4.5729          4.5729
v  Velocity[Y]            -3.0283           7.198         0.23196         0.23196
v  Velocity[Z]       -6.9287e-015     8.0477e-015    -1.4927e-017    -1.4927e-017
v  ǁVelocityǁ         0.0031059           9.482          5.0907          5.0907
v  Pressure               -24.323          28.518         0.65115         0.65115
v  nu_tilda           4.4058e-007       0.0043573       0.0017591       0.0017591
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3134e-014       0.0051348       0.0020678       0.0020678
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2408:        0.18990E+01

===============================================================


 INSTANT    0.240900000E+04   TIME STEP NUMBER            2409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.68581E-02 0.89131E+00
   Friction velocity        uk    :  0.68581E-02 0.89131E+00
   Dimensionless distance   yplus :  0.55212E-01 0.71757E+01
   Friction thermal sca.    tstar : -0.58422E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41194E-01 0.53539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10679E-01      33   0.24224E-03   0.46686E+01 0.19075E+03 
c  Velocity[X]                                      0.18083E+01 
c  Velocity[Y]                                      0.28603E+01 
c  Velocity[Z]                                      0.93109E-30 
c  Pressure     0.98159E-07     458   0.99858E-08   0.97617E-01 0.75575E+03 
c  nu_tilda     0.80409E-05      33   0.44591E-05   0.71522E-06 0.21598E+03 
c  TempC        0.43194E+02      27   0.24739E-03   0.61036E+01 0.26647E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9219          9.4789          4.5729          4.5729
v  Velocity[Y]            -3.0279           7.177         0.23207         0.23207
v  Velocity[Z]       -6.9287e-015      7.773e-015    -1.4935e-017    -1.4935e-017
v  ǁVelocityǁ         0.0028724          9.4807          5.0905          5.0905
v  Pressure               -24.264          28.508         0.68746         0.68746
v  nu_tilda           4.4062e-007       0.0043579       0.0017593       0.0017593
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3148e-014       0.0051355        0.002068        0.002068
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2409:        0.20570E+01

===============================================================


 INSTANT    0.241000000E+04   TIME STEP NUMBER            2410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93768E-02 0.89036E+00
   Friction velocity        uk    :  0.93768E-02 0.89036E+00
   Dimensionless distance   yplus :  0.75490E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.58610E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56324E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10679E-01      33   0.18789E-03   0.46521E+01 0.19066E+03 
c  Velocity[X]                                      0.18066E+01 
c  Velocity[Y]                                      0.28455E+01 
c  Velocity[Z]                                      0.73182E-30 
c  Pressure     0.10533E-06     426   0.93282E-08   0.10191E+00 0.54809E+03 
c  nu_tilda     0.80427E-05      33   0.13898E-04   0.71531E-06 0.21598E+03 
c  TempC        0.43199E+02      27   0.32427E-03   0.47052E+01 0.24120E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9245          9.4775          4.5729          4.5729
v  Velocity[Y]            -3.0274           7.195         0.23219         0.23219
v  Velocity[Z]       -6.9287e-015     7.6301e-015     -1.493e-017     -1.493e-017
v  ǁVelocityǁ         0.0026871          9.4794          5.0903          5.0903
v  Pressure                -24.31           28.53         0.67369         0.67369
v  nu_tilda           4.4063e-007       0.0043585       0.0017595       0.0017595
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3162e-014       0.0051362       0.0020682       0.0020682
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2410:        0.19830E+01

===============================================================


 INSTANT    0.241100000E+04   TIME STEP NUMBER            2411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93481E-02 0.89175E+00
   Friction velocity        uk    :  0.93481E-02 0.89175E+00
   Dimensionless distance   yplus :  0.75259E-01 0.71792E+01
   Friction thermal sca.    tstar : -0.57951E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56151E-01 0.53565E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10680E-01      33   0.24556E-03   0.46450E+01 0.19067E+03 
c  Velocity[X]                                      0.18051E+01 
c  Velocity[Y]                                      0.28399E+01 
c  Velocity[Z]                                      0.69206E-30 
c  Pressure     0.88501E-07     520   0.98233E-08   0.86595E-01 0.11863E+04 
c  nu_tilda     0.80444E-05      33   0.44379E-05   0.71533E-06 0.21598E+03 
c  TempC        0.43203E+02      27   0.29563E-03   0.59013E+01 0.29172E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9271          9.4763          4.5729          4.5729
v  Velocity[Y]            -3.0269          7.2068          0.2323          0.2323
v  Velocity[Z]       -6.9287e-015     7.3798e-015    -1.4938e-017    -1.4938e-017
v  ǁVelocityǁ         0.0020398          9.4781          5.0901          5.0901
v  Pressure               -24.253          28.627         0.73212         0.73212
v  nu_tilda           4.4063e-007       0.0043592       0.0017597       0.0017597
v  TempC                       21          73.052          22.054          22.054
v  TurbVisc           3.3165e-014        0.005137       0.0020685       0.0020685
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2411:        0.21920E+01

===============================================================


 INSTANT    0.241200000E+04   TIME STEP NUMBER            2412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11947E-01 0.89127E+00
   Friction velocity        uk    :  0.11947E-01 0.89127E+00
   Dimensionless distance   yplus :  0.96181E-01 0.71753E+01
   Friction thermal sca.    tstar : -0.57263E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71762E-01 0.53536E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10680E-01      33   0.23676E-03   0.46716E+01 0.19081E+03 
c  Velocity[X]                                      0.18157E+01 
c  Velocity[Y]                                      0.28559E+01 
c  Velocity[Z]                                      0.69260E-30 
c  Pressure     0.10282E-06     538   0.97181E-08   0.10248E+00 0.14337E+04 
c  nu_tilda     0.80462E-05      33   0.13898E-04   0.71536E-06 0.21596E+03 
c  TempC        0.43208E+02      27   0.28839E-03   0.53978E+01 0.26370E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9296           9.475          4.5729          4.5729
v  Velocity[Y]            -3.0266          7.1772         0.23242         0.23242
v  Velocity[Z]       -6.9287e-015      7.482e-015    -1.4935e-017    -1.4935e-017
v  ǁVelocityǁ         0.0017799          9.4768          5.0899          5.0899
v  Pressure               -24.293          28.461         0.68145         0.68145
v  nu_tilda           4.4065e-007       0.0043598       0.0017599       0.0017599
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3164e-014       0.0051377       0.0020687       0.0020687
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2412:        0.22290E+01

===============================================================


 INSTANT    0.241300000E+04   TIME STEP NUMBER            2413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12409E-01 0.88993E+00
   Friction velocity        uk    :  0.12409E-01 0.88993E+00
   Dimensionless distance   yplus :  0.99899E-01 0.71645E+01
   Friction thermal sca.    tstar : -0.57932E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74536E-01 0.53455E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10681E-01      33   0.24934E-03   0.46519E+01 0.19071E+03 
c  Velocity[X]                                      0.18105E+01 
c  Velocity[Y]                                      0.28414E+01 
c  Velocity[Z]                                      0.67406E-30 
c  Pressure     0.10052E-06     537   0.96240E-08   0.97377E-01 0.15051E+04 
c  nu_tilda     0.80480E-05      33   0.44296E-05   0.71535E-06 0.21595E+03 
c  TempC        0.43212E+02      26   0.31923E-03   0.45180E+01 0.24876E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9321          9.4737          4.5729          4.5729
v  Velocity[Y]            -3.0263           7.195         0.23253         0.23253
v  Velocity[Z]       -6.9287e-015     7.3814e-015    -1.4944e-017    -1.4944e-017
v  ǁVelocityǁ         0.0011292          9.4755          5.0897          5.0897
v  Pressure               -24.238          28.617         0.75191         0.75191
v  nu_tilda           4.4065e-007       0.0043604       0.0017601       0.0017601
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3171e-014       0.0051384       0.0020689       0.0020689
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2413:        0.22250E+01

===============================================================


 INSTANT    0.241400000E+04   TIME STEP NUMBER            2414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.97660E-02 0.89113E+00
   Friction velocity        uk    :  0.97660E-02 0.89113E+00
   Dimensionless distance   yplus :  0.78623E-01 0.71742E+01
   Friction thermal sca.    tstar : -0.57689E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58662E-01 0.53528E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10682E-01      33   0.25565E-03   0.46814E+01 0.19089E+03 
c  Velocity[X]                                      0.18456E+01 
c  Velocity[Y]                                      0.28358E+01 
c  Velocity[Z]                                      0.72879E-30 
c  Pressure     0.10757E-06     553   0.91302E-08   0.10709E+00 0.13176E+04 
c  nu_tilda     0.80497E-05      33   0.13889E-04   0.71541E-06 0.21595E+03 
c  TempC        0.43216E+02      27   0.26063E-03   0.63409E+01 0.27878E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9346          9.4723          4.5729          4.5729
v  Velocity[Y]            -3.0259          7.1741         0.23264         0.23264
v  Velocity[Z]       -6.9287e-015     7.5305e-015    -1.4941e-017    -1.4941e-017
v  ǁVelocityǁ        0.00089037          9.4742          5.0895          5.0895
v  Pressure               -24.279           28.47         0.70481         0.70481
v  nu_tilda           4.4072e-007        0.004361       0.0017603       0.0017603
v  TempC                       21           73.05          22.054          22.054
v  TurbVisc           3.3171e-014       0.0051392       0.0020692       0.0020692
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2414:        0.22770E+01

===============================================================


 INSTANT    0.241500000E+04   TIME STEP NUMBER            2415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.68853E-02 0.89047E+00
   Friction velocity        uk    :  0.68853E-02 0.89047E+00
   Dimensionless distance   yplus :  0.55432E-01 0.71689E+01
   Friction thermal sca.    tstar : -0.62363E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41358E-01 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10682E-01      33   0.17974E-03   0.46645E+01 0.19087E+03 
c  Velocity[X]                                      0.18122E+01 
c  Velocity[Y]                                      0.28523E+01 
c  Velocity[Z]                                      0.72625E-30 
c  Pressure     0.88506E-07     568   0.94609E-08   0.86482E-01 0.16985E+04 
c  nu_tilda     0.80515E-05      33   0.44071E-05   0.71545E-06 0.21595E+03 
c  TempC        0.43221E+02      27   0.32180E-03   0.51131E+01 0.25039E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9371           9.471          4.5729          4.5729
v  Velocity[Y]            -3.0255          7.1997         0.23275         0.23275
v  Velocity[Z]       -6.9287e-015     7.4291e-015     -1.495e-017     -1.495e-017
v  ǁVelocityǁ         0.0009223          9.4729          5.0893          5.0893
v  Pressure               -24.225          28.662         0.78185         0.78185
v  nu_tilda           4.4073e-007       0.0043616       0.0017605       0.0017605
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc            3.319e-014       0.0051399       0.0020694       0.0020694
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2415:        0.23140E+01

===============================================================


 INSTANT    0.241600000E+04   TIME STEP NUMBER            2416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.78717E-02 0.89178E+00
   Friction velocity        uk    :  0.78717E-02 0.89178E+00
   Dimensionless distance   yplus :  0.63372E-01 0.71794E+01
   Friction thermal sca.    tstar : -0.58805E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47283E-01 0.53566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10683E-01      33   0.23507E-03   0.46287E+01 0.19070E+03 
c  Velocity[X]                                      0.17917E+01 
c  Velocity[Y]                                      0.28371E+01 
c  Velocity[Z]                                      0.75087E-30 
c  Pressure     0.98447E-07     521   0.92440E-08   0.95475E-01 0.10317E+04 
c  nu_tilda     0.80532E-05      33   0.13887E-04   0.71553E-06 0.21595E+03 
c  TempC        0.43225E+02      27   0.23887E-03   0.48939E+01 0.25149E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9395          9.4697          4.5729          4.5729
v  Velocity[Y]             -3.025          7.2026         0.23286         0.23286
v  Velocity[Z]       -6.9287e-015     7.5711e-015    -1.4948e-017    -1.4948e-017
v  ǁVelocityǁ         0.0012076          9.4716          5.0891          5.0891
v  Pressure               -24.267          28.568         0.74477         0.74477
v  nu_tilda           4.4069e-007       0.0043622       0.0017606       0.0017606
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3193e-014       0.0051406       0.0020696       0.0020696
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2416:        0.23070E+01

===============================================================


 INSTANT    0.241700000E+04   TIME STEP NUMBER            2417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10822E-01 0.89154E+00
   Friction velocity        uk    :  0.10822E-01 0.89154E+00
   Dimensionless distance   yplus :  0.87125E-01 0.71775E+01
   Friction thermal sca.    tstar : -0.57693E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65005E-01 0.53552E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10683E-01      33   0.23735E-03   0.46687E+01 0.19088E+03 
c  Velocity[X]                                      0.18358E+01 
c  Velocity[Y]                                      0.28329E+01 
c  Velocity[Z]                                      0.86864E-30 
c  Pressure     0.97036E-07     458   0.94758E-08   0.96999E-01 0.80378E+03 
c  nu_tilda     0.80550E-05      33   0.43987E-05   0.71552E-06 0.21593E+03 
c  TempC        0.43230E+02      27   0.29753E-03   0.30804E+01 0.21352E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9419          9.4684          4.5729          4.5729
v  Velocity[Y]            -3.0245          7.1796         0.23297         0.23297
v  Velocity[Z]       -6.9287e-015     7.5055e-015    -1.4956e-017    -1.4956e-017
v  ǁVelocityǁ         0.0020111          9.4703          5.0889          5.0889
v  Pressure               -24.208          28.569         0.78502         0.78502
v  nu_tilda           4.4072e-007       0.0043629       0.0017609       0.0017609
v  TempC                       21          73.052          22.054          22.054
v  TurbVisc           3.3181e-014       0.0051413       0.0020699       0.0020699
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2417:        0.21920E+01

===============================================================


 INSTANT    0.241800000E+04   TIME STEP NUMBER            2418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13633E-01 0.89014E+00
   Friction velocity        uk    :  0.13633E-01 0.89014E+00
   Dimensionless distance   yplus :  0.10976E+00 0.71662E+01
   Friction thermal sca.    tstar : -0.58560E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81891E-01 0.53468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10684E-01      33   0.24134E-03   0.46622E+01 0.19098E+03 
c  Velocity[X]                                      0.18066E+01 
c  Velocity[Y]                                      0.28556E+01 
c  Velocity[Z]                                      0.72048E-30 
c  Pressure     0.89740E-07     440   0.97686E-08   0.88084E-01 0.53101E+03 
c  nu_tilda     0.80567E-05      33   0.13881E-04   0.71558E-06 0.21593E+03 
c  TempC        0.43234E+02      27   0.26730E-03   0.51145E+01 0.24428E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9445          9.4671          4.5729          4.5729
v  Velocity[Y]            -3.0242          7.1963         0.23309         0.23309
v  Velocity[Z]       -6.9287e-015       7.42e-015    -1.4953e-017    -1.4953e-017
v  ǁVelocityǁ         0.0023613           9.469          5.0887          5.0887
v  Pressure               -24.257          28.616         0.77481         0.77481
v  nu_tilda            4.407e-007       0.0043635        0.001761        0.001761
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3189e-014       0.0051421       0.0020701       0.0020701
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2418:        0.20190E+01

===============================================================


 INSTANT    0.241900000E+04   TIME STEP NUMBER            2419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15027E-01 0.89103E+00
   Friction velocity        uk    :  0.15027E-01 0.89103E+00
   Dimensionless distance   yplus :  0.12098E+00 0.71734E+01
   Friction thermal sca.    tstar : -0.57733E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90262E-01 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10684E-01      33   0.26347E-03   0.46629E+01 0.19091E+03 
c  Velocity[X]                                      0.18259E+01 
c  Velocity[Y]                                      0.28370E+01 
c  Velocity[Z]                                      0.60904E-30 
c  Pressure     0.11672E-06     441   0.99636E-08   0.11383E+00 0.68722E+03 
c  nu_tilda     0.80584E-05      33   0.43760E-05   0.71558E-06 0.21592E+03 
c  TempC        0.43238E+02      27   0.27463E-03   0.42476E+01 0.23421E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.947          9.4658          4.5729          4.5729
v  Velocity[Y]            -3.0238           7.172          0.2332          0.2332
v  Velocity[Z]       -6.9287e-015     7.3388e-015    -1.4962e-017    -1.4962e-017
v  ǁVelocityǁ         0.0024039          9.4677          5.0884          5.0884
v  Pressure               -24.198          28.551         0.79875         0.79875
v  nu_tilda           4.4071e-007       0.0043641       0.0017613       0.0017613
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3184e-014       0.0051428       0.0020703       0.0020703
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2419:        0.20390E+01

===============================================================


 INSTANT    0.242000000E+04   TIME STEP NUMBER            2420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.80727E-02 0.89041E+00
   Friction velocity        uk    :  0.80727E-02 0.89041E+00
   Dimensionless distance   yplus :  0.64990E-01 0.71684E+01
   Friction thermal sca.    tstar : -0.58721E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48490E-01 0.53484E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10685E-01      33   0.20861E-03   0.46789E+01 0.19101E+03 
c  Velocity[X]                                      0.18501E+01 
c  Velocity[Y]                                      0.28287E+01 
c  Velocity[Z]                                      0.73057E-30 
c  Pressure     0.10881E-06     378   0.93348E-08   0.10635E+00 0.56276E+03 
c  nu_tilda     0.80602E-05      33   0.13879E-04   0.71565E-06 0.21591E+03 
c  TempC        0.43243E+02      27   0.33134E-03   0.35723E+01 0.22882E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9495          9.4645          4.5729          4.5729
v  Velocity[Y]            -3.0234          7.1968         0.23331         0.23331
v  Velocity[Z]       -6.9287e-015     7.3231e-015    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ          0.003184          9.4664          5.0882          5.0882
v  Pressure               -24.246          28.626         0.79487         0.79487
v  nu_tilda           4.4064e-007       0.0043646       0.0017614       0.0017614
v  TempC                       21          73.051          22.054          22.054
v  TurbVisc           3.3188e-014       0.0051435       0.0020706       0.0020706
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2420:        0.18790E+01

===============================================================


 INSTANT    0.242100000E+04   TIME STEP NUMBER            2421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15634E-01 0.89183E+00
   Friction velocity        uk    :  0.15634E-01 0.89183E+00
   Dimensionless distance   yplus :  0.12587E+00 0.71798E+01
   Friction thermal sca.    tstar : -0.57451E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93910E-01 0.53569E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10685E-01      33   0.22750E-03   0.46420E+01 0.19091E+03 
c  Velocity[X]                                      0.17979E+01 
c  Velocity[Y]                                      0.28441E+01 
c  Velocity[Z]                                      0.74305E-30 
c  Pressure     0.83335E-07     536   0.93019E-08   0.81786E-01 0.10522E+04 
c  nu_tilda     0.80619E-05      33   0.43682E-05   0.71566E-06 0.21591E+03 
c  TempC        0.43247E+02      27   0.25588E-03   0.56603E+01 0.28020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.952          9.4632          4.5729          4.5729
v  Velocity[Y]             -3.023          7.2068         0.23341         0.23341
v  Velocity[Z]       -6.9287e-015     7.2692e-015    -1.4961e-017    -1.4961e-017
v  ǁVelocityǁ         0.0026624          9.4651           5.088           5.088
v  Pressure               -24.193          28.709          0.8462          0.8462
v  nu_tilda            4.405e-007       0.0043653       0.0017617       0.0017617
v  TempC                       21          73.052          22.054          22.054
v  TurbVisc           3.3167e-014       0.0051442       0.0020708       0.0020708
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2421:        0.22360E+01

===============================================================


 INSTANT    0.242200000E+04   TIME STEP NUMBER            2422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53843E-02 0.89127E+00
   Friction velocity        uk    :  0.53843E-02 0.89127E+00
   Dimensionless distance   yplus :  0.43347E-01 0.71753E+01
   Friction thermal sca.    tstar : -0.57232E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32342E-01 0.53536E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10686E-01      33   0.23249E-03   0.46544E+01 0.19093E+03 
c  Velocity[X]                                      0.18243E+01 
c  Velocity[Y]                                      0.28302E+01 
c  Velocity[Z]                                      0.71099E-30 
c  Pressure     0.10576E-06     538   0.94443E-08   0.10411E+00 0.16747E+04 
c  nu_tilda     0.80637E-05      33   0.13871E-04   0.71572E-06 0.21590E+03 
c  TempC        0.43251E+02      27   0.31696E-03   0.39512E+01 0.24415E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9545          9.4618          4.5729          4.5729
v  Velocity[Y]            -3.0226          7.1736         0.23352         0.23352
v  Velocity[Z]       -6.9287e-015     7.4834e-015    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ         0.0029358          9.4638          5.0878          5.0878
v  Pressure               -24.236          28.504         0.78515         0.78515
v  nu_tilda           4.4052e-007       0.0043659       0.0017618       0.0017618
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3126e-014       0.0051449        0.002071        0.002071
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2422:        0.22670E+01

===============================================================


 INSTANT    0.242300000E+04   TIME STEP NUMBER            2423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.63657E-02 0.89005E+00
   Friction velocity        uk    :  0.63657E-02 0.89005E+00
   Dimensionless distance   yplus :  0.51248E-01 0.71655E+01
   Friction thermal sca.    tstar : -0.62260E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38237E-01 0.53463E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10686E-01      33   0.24063E-03   0.46539E+01 0.19095E+03 
c  Velocity[X]                                      0.18297E+01 
c  Velocity[Y]                                      0.28242E+01 
c  Velocity[Z]                                      0.80662E-30 
c  Pressure     0.87920E-07     522   0.98782E-08   0.85989E-01 0.18527E+04 
c  nu_tilda     0.80654E-05      33   0.43436E-05   0.71569E-06 0.21589E+03 
c  TempC        0.43256E+02      27   0.26940E-03   0.43396E+01 0.24239E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9569          9.4605          4.5729          4.5729
v  Velocity[Y]             -3.022          7.1971         0.23363         0.23363
v  Velocity[Z]       -6.9287e-015      7.479e-015    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ         0.0023844          9.4624          5.0876          5.0876
v  Pressure               -24.183          28.718         0.86781         0.86781
v  nu_tilda           4.4056e-007       0.0043665       0.0017621       0.0017621
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc            3.313e-014       0.0051456       0.0020712       0.0020712
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2423:        0.21790E+01

===============================================================


 INSTANT    0.242400000E+04   TIME STEP NUMBER            2424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.61110E-02 0.89106E+00
   Friction velocity        uk    :  0.61110E-02 0.89106E+00
   Dimensionless distance   yplus :  0.49198E-01 0.71737E+01
   Friction thermal sca.    tstar : -0.61340E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36707E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10687E-01      33   0.24665E-03   0.46602E+01 0.19103E+03 
c  Velocity[X]                                      0.18200E+01 
c  Velocity[Y]                                      0.28401E+01 
c  Velocity[Z]                                      0.68547E-30 
c  Pressure     0.10015E-06     506   0.98112E-08   0.99579E-01 0.15399E+04 
c  nu_tilda     0.80671E-05      33   0.13869E-04   0.71573E-06 0.21588E+03 
c  TempC        0.43260E+02      27   0.28256E-03   0.36058E+01 0.22444E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9593          9.4592          4.5729          4.5729
v  Velocity[Y]            -3.0217          7.1727         0.23374         0.23374
v  Velocity[Z]       -6.9287e-015     7.2961e-015    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ         0.0029496          9.4611          5.0874          5.0874
v  Pressure               -24.227          28.542         0.80974         0.80974
v  nu_tilda           4.4062e-007       0.0043671       0.0017622       0.0017622
v  TempC                       21           73.05          22.055          22.055
v  TurbVisc           3.3144e-014       0.0051464       0.0020715       0.0020715
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2424:        0.21610E+01

===============================================================


 INSTANT    0.242500000E+04   TIME STEP NUMBER            2425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11687E-01 0.89020E+00
   Friction velocity        uk    :  0.11687E-01 0.89020E+00
   Dimensionless distance   yplus :  0.94085E-01 0.71667E+01
   Friction thermal sca.    tstar : -0.63838E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70198E-01 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10688E-01      33   0.20424E-03   0.46514E+01 0.19096E+03 
c  Velocity[X]                                      0.18253E+01 
c  Velocity[Y]                                      0.28261E+01 
c  Velocity[Z]                                      0.70158E-30 
c  Pressure     0.10371E-06     538   0.93601E-08   0.10057E+00 0.14517E+04 
c  nu_tilda     0.80688E-05      33   0.43364E-05   0.71573E-06 0.21587E+03 
c  TempC        0.43264E+02      27   0.32294E-03   0.41751E+01 0.24640E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9617          9.4579          4.5729          4.5729
v  Velocity[Y]            -3.0213          7.1954         0.23384         0.23384
v  Velocity[Z]       -6.9287e-015       7.41e-015    -1.4961e-017    -1.4961e-017
v  ǁVelocityǁ          0.003061          9.4598          5.0872          5.0872
v  Pressure               -24.175           28.69         0.87733         0.87733
v  nu_tilda           4.4061e-007       0.0043677       0.0017625       0.0017625
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc            3.316e-014       0.0051471       0.0020717       0.0020717
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2425:        0.22550E+01

===============================================================


 INSTANT    0.242600000E+04   TIME STEP NUMBER            2426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.98709E-02 0.89186E+00
   Friction velocity        uk    :  0.98709E-02 0.89186E+00
   Dimensionless distance   yplus :  0.79467E-01 0.71801E+01
   Friction thermal sca.    tstar : -0.67906E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59291E-01 0.53571E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10688E-01      33   0.25396E-03   0.46543E+01 0.19104E+03 
c  Velocity[X]                                      0.18345E+01 
c  Velocity[Y]                                      0.28198E+01 
c  Velocity[Z]                                      0.72794E-30 
c  Pressure     0.99674E-07     473   0.98814E-08   0.97991E-01 0.75772E+03 
c  nu_tilda     0.80706E-05      33   0.13861E-04   0.71580E-06 0.21587E+03 
c  TempC        0.43269E+02      27   0.26114E-03   0.54481E+01 0.27991E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9641          9.4565          4.5729          4.5729
v  Velocity[Y]            -3.0209          7.2061         0.23395         0.23395
v  Velocity[Z]       -6.9287e-015      7.478e-015    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ         0.0030462          9.4585           5.087           5.087
v  Pressure               -24.221           28.65         0.84939         0.84939
v  nu_tilda           4.4057e-007       0.0043683       0.0017626       0.0017626
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3159e-014       0.0051478       0.0020719       0.0020719
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2426:        0.20770E+01

===============================================================


 INSTANT    0.242700000E+04   TIME STEP NUMBER            2427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10905E-01 0.89163E+00
   Friction velocity        uk    :  0.10905E-01 0.89163E+00
   Dimensionless distance   yplus :  0.87792E-01 0.71782E+01
   Friction thermal sca.    tstar : -0.70688E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65503E-01 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10689E-01      33   0.22983E-03   0.46708E+01 0.19114E+03 
c  Velocity[X]                                      0.18336E+01 
c  Velocity[Y]                                      0.28372E+01 
c  Velocity[Z]                                      0.69881E-30 
c  Pressure     0.11060E-06     504   0.96156E-08   0.10938E+00 0.78739E+03 
c  nu_tilda     0.80723E-05      33   0.43117E-05   0.71582E-06 0.21586E+03 
c  TempC        0.43273E+02      27   0.31316E-03   0.40164E+01 0.24841E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9665          9.4553          4.5729          4.5729
v  Velocity[Y]            -3.0205          7.1784         0.23406         0.23406
v  Velocity[Z]       -6.9287e-015     7.4441e-015    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ         0.0025804          9.4572          5.0868          5.0868
v  Pressure               -24.163          28.659         0.88889         0.88889
v  nu_tilda           4.4055e-007       0.0043689       0.0017628       0.0017628
v  TempC                       21          73.052          22.055          22.055
v  TurbVisc           3.3146e-014       0.0051484       0.0020721       0.0020721
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2427:        0.21620E+01

===============================================================


 INSTANT    0.242800000E+04   TIME STEP NUMBER            2428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95977E-02 0.89001E+00
   Friction velocity        uk    :  0.95977E-02 0.89001E+00
   Dimensionless distance   yplus :  0.77268E-01 0.71652E+01
   Friction thermal sca.    tstar : -0.76573E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57651E-01 0.53460E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10689E-01      33   0.23111E-03   0.46400E+01 0.19100E+03 
c  Velocity[X]                                      0.18187E+01 
c  Velocity[Y]                                      0.28213E+01 
c  Velocity[Z]                                      0.66609E-30 
c  Pressure     0.98568E-07     458   0.93095E-08   0.95394E-01 0.67333E+03 
c  nu_tilda     0.80740E-05      33   0.13862E-04   0.71588E-06 0.21586E+03 
c  TempC        0.43277E+02      27   0.29505E-03   0.46476E+01 0.25320E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9688           9.454          4.5729          4.5729
v  Velocity[Y]              -3.02          7.1933         0.23416         0.23416
v  Velocity[Z]       -6.9287e-015     7.3208e-015    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ         0.0026882          9.4558          5.0866          5.0866
v  Pressure               -24.211          28.639         0.86468         0.86468
v  nu_tilda           4.4053e-007       0.0043695        0.001763        0.001763
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3139e-014       0.0051492       0.0020724       0.0020724
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2428:        0.20370E+01

===============================================================


 INSTANT    0.242900000E+04   TIME STEP NUMBER            2429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11145E-01 0.89127E+00
   Friction velocity        uk    :  0.11145E-01 0.89127E+00
   Dimensionless distance   yplus :  0.89725E-01 0.71753E+01
   Friction thermal sca.    tstar : -0.80749E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66945E-01 0.53536E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10690E-01      33   0.24987E-03   0.46588E+01 0.19110E+03 
c  Velocity[X]                                      0.18422E+01 
c  Velocity[Y]                                      0.28166E+01 
c  Velocity[Z]                                      0.89595E-30 
c  Pressure     0.93803E-07     489   0.90997E-08   0.93495E-01 0.75771E+03 
c  nu_tilda     0.80757E-05      33   0.43034E-05   0.71586E-06 0.21585E+03 
c  TempC        0.43281E+02      27   0.33826E-03   0.48742E+01 0.26769E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9711          9.4527          4.5729          4.5729
v  Velocity[Y]            -3.0195          7.1755         0.23426         0.23426
v  Velocity[Z]       -6.9287e-015     7.2607e-015    -1.4964e-017    -1.4964e-017
v  ǁVelocityǁ         0.0027372          9.4545          5.0863          5.0863
v  Pressure               -24.154          28.643         0.90197         0.90197
v  nu_tilda           4.4059e-007       0.0043701       0.0017632       0.0017632
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3134e-014       0.0051499       0.0020726       0.0020726
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2429:        0.22450E+01

===============================================================


 INSTANT    0.243000000E+04   TIME STEP NUMBER            2430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10212E-01 0.89039E+00
   Friction velocity        uk    :  0.10212E-01 0.89039E+00
   Dimensionless distance   yplus :  0.82212E-01 0.71682E+01
   Friction thermal sca.    tstar : -0.90470E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61339E-01 0.53483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10690E-01      33   0.19424E-03   0.46841E+01 0.19167E+03 
c  Velocity[X]                                      0.18251E+01 
c  Velocity[Y]                                      0.28590E+01 
c  Velocity[Z]                                      0.76425E-30 
c  Pressure     0.95055E-07     425   0.97209E-08   0.93011E-01 0.52892E+03 
c  nu_tilda     0.80774E-05      33   0.13852E-04   0.71587E-06 0.21583E+03 
c  TempC        0.43286E+02      27   0.32174E-03   0.79708E+01 0.31570E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9735          9.4514          4.5729          4.5729
v  Velocity[Y]            -3.0191          7.1965         0.23437         0.23437
v  Velocity[Z]       -6.9287e-015     7.4714e-015    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ         0.0027031          9.4532          5.0861          5.0861
v  Pressure               -24.202            28.7         0.89494         0.89494
v  nu_tilda           4.4059e-007       0.0043707       0.0017633       0.0017633
v  TempC                       21           73.05          22.055          22.055
v  TurbVisc            3.315e-014       0.0051506       0.0020728       0.0020728
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2430:        0.20910E+01

===============================================================


 INSTANT    0.243100000E+04   TIME STEP NUMBER            2431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11184E-01 0.89146E+00
   Friction velocity        uk    :  0.11184E-01 0.89146E+00
   Dimensionless distance   yplus :  0.90036E-01 0.71768E+01
   Friction thermal sca.    tstar : -0.96410E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67177E-01 0.53547E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10691E-01      33   0.25363E-03   0.47708E+01 0.19353E+03 
c  Velocity[X]                                      0.18202E+01 
c  Velocity[Y]                                      0.29506E+01 
c  Velocity[Z]                                      0.58590E-30 
c  Pressure     0.11262E-06     506   0.94160E-08   0.10846E+00 0.89985E+03 
c  nu_tilda     0.80791E-05      33   0.42793E-05   0.71586E-06 0.21582E+03 
c  TempC        0.43290E+02      26   0.28521E-03   0.59937E+01 0.28199E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9759          9.4501          4.5729          4.5729
v  Velocity[Y]            -3.0188          7.2016         0.23446         0.23446
v  Velocity[Z]       -6.9287e-015     7.3621e-015    -1.4962e-017    -1.4962e-017
v  ǁVelocityǁ         0.0027162          9.4519          5.0859          5.0859
v  Pressure               -24.143          28.734         0.94088         0.94088
v  nu_tilda           4.4058e-007       0.0043713       0.0017636       0.0017636
v  TempC                       21          73.052          22.055          22.055
v  TurbVisc           3.3153e-014       0.0051513        0.002073        0.002073
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2431:        0.21550E+01

===============================================================


 INSTANT    0.243200000E+04   TIME STEP NUMBER            2432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72287E-02 0.89117E+00
   Friction velocity        uk    :  0.72287E-02 0.89117E+00
   Dimensionless distance   yplus :  0.58196E-01 0.71746E+01
   Friction thermal sca.    tstar : -0.11289E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43421E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10691E-01      33   0.24982E-03   0.48212E+01 0.19350E+03 
c  Velocity[X]                                      0.18757E+01 
c  Velocity[Y]                                      0.29454E+01 
c  Velocity[Z]                                      0.18093E-29 
c  Pressure     0.11754E-06     505   0.95790E-08   0.11698E+00 0.12964E+04 
c  nu_tilda     0.80809E-05      33   0.13851E-04   0.71593E-06 0.21582E+03 
c  TempC        0.43294E+02      26   0.24373E-03   0.39740E+01 0.24447E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9784          9.4488          4.5729          4.5729
v  Velocity[Y]            -3.0183          7.1746         0.23456         0.23456
v  Velocity[Z]       -6.9287e-015     7.3915e-015    -1.4956e-017    -1.4956e-017
v  ǁVelocityǁ         0.0026248          9.4505          5.0857          5.0857
v  Pressure               -24.185          28.594         0.89346         0.89346
v  nu_tilda           4.4064e-007       0.0043718       0.0017637       0.0017637
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3148e-014        0.005152       0.0020733       0.0020733
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2432:        0.21540E+01

===============================================================


 INSTANT    0.243300000E+04   TIME STEP NUMBER            2433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.30041E-02 0.88993E+00
   Friction velocity        uk    :  0.30041E-02 0.88993E+00
   Dimensionless distance   yplus :  0.24185E-01 0.71646E+01
   Friction thermal sca.    tstar : -0.12954E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18045E-01 0.53456E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10692E-01      33   0.23168E-03   0.47758E+01 0.19298E+03 
c  Velocity[X]                                      0.18282E+01 
c  Velocity[Y]                                      0.29476E+01 
c  Velocity[Z]                                      0.10841E-29 
c  Pressure     0.91464E-07     570   0.99757E-08   0.89600E-01 0.16858E+04 
c  nu_tilda     0.80826E-05      33   0.42700E-05   0.71593E-06 0.21581E+03 
c  TempC        0.43298E+02      26   0.24869E-03   0.36319E+01 0.23769E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9807          9.4475          4.5729          4.5729
v  Velocity[Y]            -3.0179          7.1963         0.23465         0.23465
v  Velocity[Z]       -6.9287e-015      7.263e-015    -1.4956e-017    -1.4956e-017
v  ǁVelocityǁ         0.0019163          9.4492          5.0855          5.0855
v  Pressure               -24.132          28.782         0.97014         0.97014
v  nu_tilda           4.4069e-007       0.0043724        0.001764        0.001764
v  TempC                       21          73.052          22.055          22.055
v  TurbVisc           3.3166e-014       0.0051526       0.0020735       0.0020735
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2433:        0.26090E+01

===============================================================


 INSTANT    0.243400000E+04   TIME STEP NUMBER            2434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96587E-02 0.89092E+00
   Friction velocity        uk    :  0.96587E-02 0.89092E+00
   Dimensionless distance   yplus :  0.77759E-01 0.71725E+01
   Friction thermal sca.    tstar : -0.17654E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58017E-01 0.53515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10692E-01      33   0.24498E-03   0.47616E+01 0.19265E+03 
c  Velocity[X]                                      0.18366E+01 
c  Velocity[Y]                                      0.29250E+01 
c  Velocity[Z]                                      0.88205E-30 
c  Pressure     0.11290E-06     520   0.93194E-08   0.11084E+00 0.16276E+04 
c  nu_tilda     0.80843E-05      33   0.13843E-04   0.71599E-06 0.21581E+03 
c  TempC        0.43303E+02      26   0.36795E-03   0.41133E+01 0.23516E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9831          9.4462          4.5729          4.5729
v  Velocity[Y]            -3.0174          7.1693         0.23474         0.23474
v  Velocity[Z]       -6.9287e-015     7.3319e-015     -1.495e-017     -1.495e-017
v  ǁVelocityǁ         0.0018742          9.4479          5.0853          5.0853
v  Pressure               -24.174          28.589         0.91008         0.91008
v  nu_tilda           4.4069e-007        0.004373       0.0017641       0.0017641
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3181e-014       0.0051533       0.0020737       0.0020737
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2434:        0.23280E+01

===============================================================


 INSTANT    0.243500000E+04   TIME STEP NUMBER            2435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89830E-02 0.89031E+00
   Friction velocity        uk    :  0.89830E-02 0.89031E+00
   Dimensionless distance   yplus :  0.72319E-01 0.71676E+01
   Friction thermal sca.    tstar : -0.27830E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53958E-01 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10692E-01      33   0.19343E-03   0.47848E+01 0.19307E+03 
c  Velocity[X]                                      0.18532E+01 
c  Velocity[Y]                                      0.29316E+01 
c  Velocity[Z]                                      0.11406E-29 
c  Pressure     0.10370E-06     585   0.98482E-08   0.10137E+00 0.17701E+04 
c  nu_tilda     0.80860E-05      33   0.42456E-05   0.71608E-06 0.21580E+03 
c  TempC        0.43307E+02      27   0.25694E-03   0.69561E+01 0.30195E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9854          9.4449          4.5729          4.5729
v  Velocity[Y]            -3.0168          7.1976         0.23483         0.23483
v  Velocity[Z]       -6.9287e-015     7.2694e-015    -1.4946e-017    -1.4946e-017
v  ǁVelocityǁ         0.0026291          9.4466          5.0851          5.0851
v  Pressure               -24.119          28.786         0.99043         0.99043
v  nu_tilda           4.4064e-007       0.0043736       0.0017643       0.0017643
v  TempC                       21          73.052          22.055          22.055
v  TurbVisc           3.3182e-014        0.005154       0.0020739       0.0020739
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2435:        0.23540E+01

===============================================================


 INSTANT    0.243600000E+04   TIME STEP NUMBER            2436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10916E-01 0.89173E+00
   Friction velocity        uk    :  0.10916E-01 0.89173E+00
   Dimensionless distance   yplus :  0.87880E-01 0.71790E+01
   Friction thermal sca.    tstar : -0.26327E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65569E-01 0.53564E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10693E-01      33   0.23309E-03   0.47838E+01 0.19350E+03 
c  Velocity[X]                                      0.18193E+01 
c  Velocity[Y]                                      0.29645E+01 
c  Velocity[Z]                                      0.33203E-29 
c  Pressure     0.10399E-06     536   0.98052E-08   0.10195E+00 0.87356E+03 
c  nu_tilda     0.80877E-05      33   0.13841E-04   0.71613E-06 0.21579E+03 
c  TempC        0.43311E+02      26   0.25755E-03   0.39727E+01 0.23888E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9877          9.4436          4.5729          4.5729
v  Velocity[Y]            -3.0165          7.2046         0.23492         0.23492
v  Velocity[Z]       -6.9287e-015     7.3755e-015    -1.4929e-017    -1.4929e-017
v  ǁVelocityǁ        0.00060007          9.4453          5.0849          5.0849
v  Pressure               -24.167          28.727         0.95593         0.95593
v  nu_tilda           4.4054e-007       0.0043742       0.0017644       0.0017644
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3168e-014       0.0051547       0.0020741       0.0020741
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2436:        0.22350E+01

===============================================================


 INSTANT    0.243700000E+04   TIME STEP NUMBER            2437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53656E-02 0.89132E+00
   Friction velocity        uk    :  0.53656E-02 0.89132E+00
   Dimensionless distance   yplus :  0.43196E-01 0.71757E+01
   Friction thermal sca.    tstar : -0.18024E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32229E-01 0.53539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10693E-01      33   0.24640E-03   0.47793E+01 0.19299E+03 
c  Velocity[X]                                      0.18550E+01 
c  Velocity[Y]                                      0.29243E+01 
c  Velocity[Z]                                      0.89400E-30 
c  Pressure     0.12535E-06     490   0.94684E-08   0.12302E+00 0.69937E+03 
c  nu_tilda     0.80893E-05      33   0.42358E-05   0.71617E-06 0.21579E+03 
c  TempC        0.43315E+02      27   0.34682E-03   0.39485E+01 0.22517E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.99          9.4423          4.5729          4.5729
v  Velocity[Y]            -3.0161          7.1754         0.23501         0.23501
v  Velocity[Z]       -6.9287e-015     7.3215e-015    -1.4926e-017    -1.4926e-017
v  ǁVelocityǁ         0.0015091           9.444          5.0847          5.0847
v  Pressure               -24.107          28.673         0.98286         0.98286
v  nu_tilda           4.4054e-007       0.0043748       0.0017647       0.0017647
v  TempC                       21          73.052          22.055          22.055
v  TurbVisc           3.3136e-014       0.0051554       0.0020743       0.0020743
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2437:        0.21170E+01

===============================================================


 INSTANT    0.243800000E+04   TIME STEP NUMBER            2438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85695E-02 0.89008E+00
   Friction velocity        uk    :  0.85695E-02 0.89008E+00
   Dimensionless distance   yplus :  0.68990E-01 0.71657E+01
   Friction thermal sca.    tstar : -0.12620E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51474E-01 0.53464E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10694E-01      33   0.24945E-03   0.47750E+01 0.19295E+03 
c  Velocity[X]                                      0.18680E+01 
c  Velocity[Y]                                      0.29070E+01 
c  Velocity[Z]                                      0.18120E-29 
c  Pressure     0.11791E-06     425   0.92776E-08   0.11548E+00 0.54366E+03 
c  nu_tilda     0.80910E-05      33   0.13836E-04   0.71625E-06 0.21578E+03 
c  TempC        0.43319E+02      27   0.25968E-03   0.63428E+01 0.26794E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9923           9.441          4.5729          4.5729
v  Velocity[Y]            -3.0157          7.1952          0.2351          0.2351
v  Velocity[Z]       -6.9287e-015      7.423e-015    -1.4919e-017    -1.4919e-017
v  ǁVelocityǁ         0.0025948          9.4427          5.0845          5.0845
v  Pressure               -24.157          28.735         0.97522         0.97522
v  nu_tilda           4.4056e-007       0.0043753       0.0017648       0.0017648
v  TempC                       21          73.051          22.055          22.055
v  TurbVisc           3.3136e-014       0.0051561       0.0020746       0.0020746
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2438:        0.19790E+01

===============================================================


 INSTANT    0.243900000E+04   TIME STEP NUMBER            2439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.92606E-02 0.89115E+00
   Friction velocity        uk    :  0.92606E-02 0.89115E+00
   Dimensionless distance   yplus :  0.74554E-01 0.71744E+01
   Friction thermal sca.    tstar : -0.11334E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55626E-01 0.53529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10694E-01      33   0.23975E-03   0.48380E+01 0.19419E+03 
c  Velocity[X]                                      0.18516E+01 
c  Velocity[Y]                                      0.29864E+01 
c  Velocity[Z]                                      0.14860E-29 
c  Pressure     0.12444E-06     457   0.98676E-08   0.12254E+00 0.76273E+03 
c  nu_tilda     0.80927E-05      33   0.42125E-05   0.71624E-06 0.21578E+03 
c  TempC        0.43323E+02      27   0.30459E-03   0.32805E+01 0.22444E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9945          9.4397          4.5729          4.5729
v  Velocity[Y]            -3.0152          7.1739          0.2352          0.2352
v  Velocity[Z]       -6.9287e-015     7.3598e-015    -1.4922e-017    -1.4922e-017
v  ǁVelocityǁ         0.0018382          9.4414          5.0843          5.0843
v  Pressure               -24.097          28.725          1.0122          1.0122
v  nu_tilda           4.4059e-007       0.0043759        0.001765        0.001765
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3142e-014       0.0051568       0.0020748       0.0020748
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2439:        0.20340E+01

===============================================================


 INSTANT    0.244000000E+04   TIME STEP NUMBER            2440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12278E-01 0.89021E+00
   Friction velocity        uk    :  0.12278E-01 0.89021E+00
   Dimensionless distance   yplus :  0.98850E-01 0.71668E+01
   Friction thermal sca.    tstar : -0.96488E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73753E-01 0.53473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10695E-01      33   0.18209E-03   0.48184E+01 0.19398E+03 
c  Velocity[X]                                      0.18484E+01 
c  Velocity[Y]                                      0.29699E+01 
c  Velocity[Z]                                      0.35298E-29 
c  Pressure     0.12764E-06     441   0.97606E-08   0.12283E+00 0.59335E+03 
c  nu_tilda     0.80944E-05      33   0.13833E-04   0.71628E-06 0.21577E+03 
c  TempC        0.43328E+02      27   0.30154E-03   0.34831E+01 0.23245E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9967          9.4384          4.5729          4.5729
v  Velocity[Y]            -3.0147          7.1924         0.23529         0.23529
v  Velocity[Z]       -6.9287e-015     7.4552e-015    -1.4921e-017    -1.4921e-017
v  ǁVelocityǁ          0.002821          9.4401          5.0841          5.0841
v  Pressure               -24.148          28.733          0.9913          0.9913
v  nu_tilda           4.4057e-007       0.0043765       0.0017652       0.0017652
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3152e-014       0.0051575        0.002075        0.002075
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2440:        0.20030E+01

===============================================================


 INSTANT    0.244100000E+04   TIME STEP NUMBER            2441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50674E-02 0.89168E+00
   Friction velocity        uk    :  0.50674E-02 0.89168E+00
   Dimensionless distance   yplus :  0.40796E-01 0.71787E+01
   Friction thermal sca.    tstar : -0.90161E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30438E-01 0.53561E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10695E-01      33   0.24609E-03   0.47971E+01 0.19369E+03 
c  Velocity[X]                                      0.18492E+01 
c  Velocity[Y]                                      0.29479E+01 
c  Velocity[Z]                                      0.11586E-29 
c  Pressure     0.10921E-06     506   0.97678E-08   0.10722E+00 0.11748E+04 
c  nu_tilda     0.80961E-05      33   0.42004E-05   0.71621E-06 0.21575E+03 
c  TempC        0.43332E+02      27   0.27984E-03   0.48379E+01 0.24417E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9991          9.4371          4.5729          4.5729
v  Velocity[Y]            -3.0142          7.2046         0.23538         0.23538
v  Velocity[Z]       -6.9287e-015     7.3951e-015    -1.4923e-017    -1.4923e-017
v  ǁVelocityǁ         0.0012058          9.4388          5.0839          5.0839
v  Pressure               -24.093          28.834          1.0478          1.0478
v  nu_tilda            4.405e-007       0.0043771       0.0017654       0.0017654
v  TempC                       21          73.052          22.056          22.056
v  TurbVisc           3.3144e-014       0.0051582       0.0020752       0.0020752
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2441:        0.21300E+01

===============================================================


 INSTANT    0.244200000E+04   TIME STEP NUMBER            2442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10184E-01 0.89117E+00
   Friction velocity        uk    :  0.10184E-01 0.89117E+00
   Dimensionless distance   yplus :  0.81986E-01 0.71745E+01
   Friction thermal sca.    tstar : -0.81344E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61171E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10696E-01      33   0.23744E-03   0.48038E+01 0.19349E+03 
c  Velocity[X]                                      0.18558E+01 
c  Velocity[Y]                                      0.29480E+01 
c  Velocity[Z]                                      0.12840E-29 
c  Pressure     0.11982E-06     506   0.96623E-08   0.11919E+00 0.15183E+04 
c  nu_tilda     0.80978E-05      33   0.13826E-04   0.71623E-06 0.21574E+03 
c  TempC        0.43336E+02      26   0.33593E-03   0.53928E+01 0.25574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0013          9.4358          4.5729          4.5729
v  Velocity[Y]            -3.0138          7.1746         0.23548         0.23548
v  Velocity[Z]       -6.9287e-015     7.4832e-015    -1.4918e-017    -1.4918e-017
v  ǁVelocityǁ         0.0028698          9.4375          5.0837          5.0837
v  Pressure               -24.142          28.659         0.98829         0.98829
v  nu_tilda           4.4047e-007       0.0043777       0.0017655       0.0017655
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3123e-014       0.0051588       0.0020754       0.0020754
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2442:        0.21800E+01

===============================================================


 INSTANT    0.244300000E+04   TIME STEP NUMBER            2443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15644E-01 0.88970E+00
   Friction velocity        uk    :  0.15644E-01 0.88970E+00
   Dimensionless distance   yplus :  0.12595E+00 0.71627E+01
   Friction thermal sca.    tstar : -0.76910E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93969E-01 0.53442E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10696E-01      33   0.25248E-03   0.47920E+01 0.19358E+03 
c  Velocity[X]                                      0.18542E+01 
c  Velocity[Y]                                      0.29378E+01 
c  Velocity[Z]                                      0.19732E-29 
c  Pressure     0.12459E-06     522   0.95856E-08   0.11966E+00 0.14130E+04 
c  nu_tilda     0.80995E-05      33   0.41783E-05   0.71621E-06 0.21573E+03 
c  TempC        0.43340E+02      27   0.30635E-03   0.60796E+01 0.29731E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0036          9.4345          4.5729          4.5729
v  Velocity[Y]            -3.0134          7.1922         0.23557         0.23557
v  Velocity[Z]       -6.9287e-015     7.4167e-015    -1.4914e-017    -1.4914e-017
v  ǁVelocityǁ          0.002537          9.4363          5.0835          5.0835
v  Pressure               -24.089          28.803          1.0536          1.0536
v  nu_tilda           4.4046e-007       0.0043782       0.0017658       0.0017658
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3117e-014       0.0051595       0.0020756       0.0020756
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2443:        0.21850E+01

===============================================================


 INSTANT    0.244400000E+04   TIME STEP NUMBER            2444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12760E-01 0.89096E+00
   Friction velocity        uk    :  0.12760E-01 0.89096E+00
   Dimensionless distance   yplus :  0.10273E+00 0.71728E+01
   Friction thermal sca.    tstar : -0.71201E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76648E-01 0.53517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10697E-01      33   0.25767E-03   0.49170E+01 0.19551E+03 
c  Velocity[X]                                      0.18953E+01 
c  Velocity[Y]                                      0.30217E+01 
c  Velocity[Z]                                      0.19882E-29 
c  Pressure     0.13724E-06     522   0.92294E-08   0.13589E+00 0.13793E+04 
c  nu_tilda     0.81011E-05      33   0.13824E-04   0.71625E-06 0.21572E+03 
c  TempC        0.43344E+02      26   0.31986E-03   0.51816E+01 0.27606E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0059          9.4332          4.5729          4.5729
v  Velocity[Y]             -3.013          7.1712         0.23566         0.23566
v  Velocity[Z]       -6.9287e-015     7.5214e-015    -1.4902e-017    -1.4902e-017
v  ǁVelocityǁ         0.0028507          9.4349          5.0833          5.0833
v  Pressure               -24.137           28.65         0.99959         0.99959
v  nu_tilda            4.405e-007       0.0043788       0.0017659       0.0017659
v  TempC                       21           73.05          22.056          22.056
v  TurbVisc           3.3112e-014       0.0051602       0.0020758       0.0020758
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2444:        0.21990E+01

===============================================================


 INSTANT    0.244500000E+04   TIME STEP NUMBER            2445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.74461E-02 0.89036E+00
   Friction velocity        uk    :  0.74461E-02 0.89036E+00
   Dimensionless distance   yplus :  0.59946E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.68218E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44727E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10697E-01      33   0.18269E-03   0.48461E+01 0.19441E+03 
c  Velocity[X]                                      0.18552E+01 
c  Velocity[Y]                                      0.29909E+01 
c  Velocity[Z]                                      0.20947E-29 
c  Pressure     0.11869E-06     537   0.98034E-08   0.11620E+00 0.16914E+04 
c  nu_tilda     0.81028E-05      33   0.41645E-05   0.71624E-06 0.21572E+03 
c  TempC        0.43348E+02      27   0.26705E-03   0.51506E+01 0.27396E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0082          9.4319          4.5729          4.5729
v  Velocity[Y]            -3.0125          7.1971         0.23576         0.23576
v  Velocity[Z]       -6.9287e-015     7.4582e-015    -1.4902e-017    -1.4902e-017
v  ǁVelocityǁ         0.0029143          9.4336          5.0831          5.0831
v  Pressure               -24.089           28.85           1.073           1.073
v  nu_tilda           4.4052e-007       0.0043794       0.0017661       0.0017661
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3126e-014       0.0051608        0.002076        0.002076
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2445:        0.22190E+01

===============================================================


 INSTANT    0.244600000E+04   TIME STEP NUMBER            2446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15435E-01 0.89165E+00
   Friction velocity        uk    :  0.15435E-01 0.89165E+00
   Dimensionless distance   yplus :  0.12426E+00 0.71784E+01
   Friction thermal sca.    tstar : -0.64295E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92715E-01 0.53559E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10697E-01      33   0.23956E-03   0.48020E+01 0.19405E+03 
c  Velocity[X]                                      0.18368E+01 
c  Velocity[Y]                                      0.29652E+01 
c  Velocity[Z]                                      0.48054E-29 
c  Pressure     0.12668E-06     505   0.96201E-08   0.12251E+00 0.12072E+04 
c  nu_tilda     0.81045E-05      33   0.13816E-04   0.71626E-06 0.21570E+03 
c  TempC        0.43352E+02      27   0.25420E-03   0.53887E+01 0.26731E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0104          9.4306          4.5729          4.5729
v  Velocity[Y]            -3.0119          7.2016         0.23585         0.23585
v  Velocity[Z]       -6.9287e-015     7.5465e-015     -1.489e-017     -1.489e-017
v  ǁVelocityǁ          0.002986          9.4323          5.0829          5.0829
v  Pressure               -24.145          28.733          1.0206          1.0206
v  nu_tilda            4.405e-007         0.00438       0.0017662       0.0017662
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc            3.313e-014       0.0051615       0.0020762       0.0020762
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2446:        0.21540E+01

===============================================================


 INSTANT    0.244700000E+04   TIME STEP NUMBER            2447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17564E-01 0.89148E+00
   Friction velocity        uk    :  0.17564E-01 0.89148E+00
   Dimensionless distance   yplus :  0.14140E+00 0.71770E+01
   Friction thermal sca.    tstar : -0.62223E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10550E+00 0.53549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10698E-01      33   0.23840E-03   0.48341E+01 0.19407E+03 
c  Velocity[X]                                      0.18819E+01 
c  Velocity[Y]                                      0.29522E+01 
c  Velocity[Z]                                      0.10055E-29 
c  Pressure     0.13032E-06     488   0.94298E-08   0.12902E+00 0.70802E+03 
c  nu_tilda     0.81061E-05      33   0.41426E-05   0.71624E-06 0.21569E+03 
c  TempC        0.43356E+02      27   0.33097E-03   0.48659E+01 0.24142E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0126          9.4293          4.5729          4.5729
v  Velocity[Y]            -3.0114          7.1775         0.23595         0.23595
v  Velocity[Z]       -6.9287e-015     7.4957e-015     -1.488e-017     -1.488e-017
v  ǁVelocityǁ          0.002829          9.4311          5.0827          5.0827
v  Pressure               -24.091          28.732          1.0542          1.0542
v  nu_tilda           4.4056e-007       0.0043806       0.0017665       0.0017665
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3126e-014       0.0051622       0.0020764       0.0020764
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2447:        0.21080E+01

===============================================================


 INSTANT    0.244800000E+04   TIME STEP NUMBER            2448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16556E-01 0.89001E+00
   Friction velocity        uk    :  0.16556E-01 0.89001E+00
   Dimensionless distance   yplus :  0.13329E+00 0.71652E+01
   Friction thermal sca.    tstar : -0.59524E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99446E-01 0.53460E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10698E-01      33   0.23671E-03   0.48193E+01 0.19414E+03 
c  Velocity[X]                                      0.18502E+01 
c  Velocity[Y]                                      0.29690E+01 
c  Velocity[Z]                                      0.23184E-29 
c  Pressure     0.11630E-06     473   0.92335E-08   0.11368E+00 0.56880E+03 
c  nu_tilda     0.81078E-05      33   0.13816E-04   0.71631E-06 0.21569E+03 
c  TempC        0.43360E+02      27   0.26256E-03   0.44865E+01 0.25177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0148           9.428          4.5729          4.5729
v  Velocity[Y]             -3.011          7.1947         0.23604         0.23604
v  Velocity[Z]       -6.9287e-015     7.5879e-015    -1.4866e-017    -1.4866e-017
v  ǁVelocityǁ         0.0028891          9.4298          5.0825          5.0825
v  Pressure               -24.151          28.767          1.0331          1.0331
v  nu_tilda            4.406e-007       0.0043811       0.0017666       0.0017666
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3142e-014       0.0051629       0.0020767       0.0020767
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2448:        0.20860E+01

===============================================================


 INSTANT    0.244900000E+04   TIME STEP NUMBER            2449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53376E-02 0.89091E+00
   Friction velocity        uk    :  0.53376E-02 0.89091E+00
   Dimensionless distance   yplus :  0.42971E-01 0.71724E+01
   Friction thermal sca.    tstar : -0.57477E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32061E-01 0.53514E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10699E-01      33   0.25833E-03   0.48586E+01 0.19483E+03 
c  Velocity[X]                                      0.18691E+01 
c  Velocity[Y]                                      0.29895E+01 
c  Velocity[Z]                                      0.28884E-29 
c  Pressure     0.14043E-06     456   0.95073E-08   0.13728E+00 0.67293E+03 
c  nu_tilda     0.81095E-05      33   0.41278E-05   0.71631E-06 0.21568E+03 
c  TempC        0.43364E+02      27   0.30754E-03   0.34966E+01 0.23013E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0169          9.4267          4.5729          4.5729
v  Velocity[Y]            -3.0106          7.1711         0.23613         0.23613
v  Velocity[Z]       -6.9287e-015     7.5302e-015    -1.4852e-017    -1.4852e-017
v  ǁVelocityǁ         0.0028554          9.4284          5.0823          5.0823
v  Pressure               -24.092          28.699          1.0549          1.0549
v  nu_tilda           4.4063e-007       0.0043817       0.0017668       0.0017668
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3154e-014       0.0051636       0.0020769       0.0020769
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2449:        0.20340E+01

===============================================================


 INSTANT    0.245000000E+04   TIME STEP NUMBER            2450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11114E-01 0.89026E+00
   Friction velocity        uk    :  0.11114E-01 0.89026E+00
   Dimensionless distance   yplus :  0.89472E-01 0.71672E+01
   Friction thermal sca.    tstar : -0.58750E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66756E-01 0.53475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10699E-01      33   0.20464E-03   0.48617E+01 0.19464E+03 
c  Velocity[X]                                      0.18920E+01 
c  Velocity[Y]                                      0.29697E+01 
c  Velocity[Z]                                      0.17073E-29 
c  Pressure     0.13452E-06     410   0.99564E-08   0.13117E+00 0.56710E+03 
c  nu_tilda     0.81111E-05      33   0.13809E-04   0.71634E-06 0.21567E+03 
c  TempC        0.43368E+02      27   0.25729E-03   0.50524E+01 0.24179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.019          9.4254          4.5729          4.5729
v  Velocity[Y]            -3.0101          7.1949         0.23623         0.23623
v  Velocity[Z]       -6.9287e-015     7.6199e-015    -1.4839e-017    -1.4839e-017
v  ǁVelocityǁ         0.0028773          9.4271          5.0821          5.0821
v  Pressure               -24.149          28.773          1.0452          1.0452
v  nu_tilda           4.4057e-007       0.0043823       0.0017669       0.0017669
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3163e-014       0.0051643       0.0020771       0.0020771
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2450:        0.19280E+01

===============================================================


 INSTANT    0.245100000E+04   TIME STEP NUMBER            2451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11909E-01 0.89155E+00
   Friction velocity        uk    :  0.11909E-01 0.89155E+00
   Dimensionless distance   yplus :  0.95877E-01 0.71776E+01
   Friction thermal sca.    tstar : -0.57790E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71535E-01 0.53553E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10699E-01      33   0.23325E-03   0.48176E+01 0.19437E+03 
c  Velocity[X]                                      0.18443E+01 
c  Velocity[Y]                                      0.29733E+01 
c  Velocity[Z]                                      0.40487E-29 
c  Pressure     0.12281E-06     488   0.96507E-08   0.11935E+00 0.10459E+04 
c  nu_tilda     0.81128E-05      33   0.41071E-05   0.71631E-06 0.21566E+03 
c  TempC        0.43372E+02      27   0.24873E-03   0.37714E+01 0.22388E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0212          9.4241          4.5729          4.5729
v  Velocity[Y]            -3.0096          7.2035         0.23632         0.23632
v  Velocity[Z]       -6.9287e-015     7.4956e-015    -1.4837e-017    -1.4837e-017
v  ǁVelocityǁ         0.0027346          9.4258          5.0819          5.0819
v  Pressure               -24.098          28.853          1.0956          1.0956
v  nu_tilda           4.4048e-007       0.0043829       0.0017672       0.0017672
v  TempC                       21          73.052          22.056          22.056
v  TurbVisc           3.3147e-014        0.005165       0.0020773       0.0020773
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2451:        0.21210E+01

===============================================================


 INSTANT    0.245200000E+04   TIME STEP NUMBER            2452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.73002E-02 0.89096E+00
   Friction velocity        uk    :  0.73002E-02 0.89096E+00
   Dimensionless distance   yplus :  0.58771E-01 0.71728E+01
   Friction thermal sca.    tstar : -0.57038E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43850E-01 0.53517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10700E-01      33   0.23054E-03   0.48346E+01 0.19439E+03 
c  Velocity[X]                                      0.18708E+01 
c  Velocity[Y]                                      0.29638E+01 
c  Velocity[Z]                                      0.13281E-29 
c  Pressure     0.13309E-06     553   0.95383E-08   0.13027E+00 0.18151E+04 
c  nu_tilda     0.81144E-05      33   0.13806E-04   0.71635E-06 0.21565E+03 
c  TempC        0.43376E+02      26   0.35247E-03   0.49130E+01 0.25482E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0233          9.4228          4.5729          4.5729
v  Velocity[Y]            -3.0091          7.1714         0.23641         0.23641
v  Velocity[Z]       -6.9287e-015      7.383e-015    -1.4834e-017    -1.4834e-017
v  ǁVelocityǁ         0.0024967          9.4245          5.0817          5.0817
v  Pressure                -24.15          28.637          1.0221          1.0221
v  nu_tilda           4.4049e-007       0.0043835       0.0017673       0.0017673
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3117e-014       0.0051657       0.0020775       0.0020775
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2452:        0.22420E+01

===============================================================


 INSTANT    0.245300000E+04   TIME STEP NUMBER            2453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60650E-02 0.88990E+00
   Friction velocity        uk    :  0.60650E-02 0.88990E+00
   Dimensionless distance   yplus :  0.48827E-01 0.71643E+01
   Friction thermal sca.    tstar : -0.58030E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36430E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10700E-01      33   0.23904E-03   0.48293E+01 0.19443E+03 
c  Velocity[X]                                      0.18723E+01 
c  Velocity[Y]                                      0.29570E+01 
c  Velocity[Z]                                      0.23823E-29 
c  Pressure     0.11308E-06     553   0.91548E-08   0.11089E+00 0.17707E+04 
c  nu_tilda     0.81161E-05      33   0.40893E-05   0.71633E-06 0.21564E+03 
c  TempC        0.43380E+02      27   0.28572E-03   0.67615E+01 0.30342E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0255          9.4215          4.5729          4.5729
v  Velocity[Y]            -3.0086           7.195         0.23651         0.23651
v  Velocity[Z]       -6.9287e-015     7.4081e-015    -1.4822e-017    -1.4822e-017
v  ǁVelocityǁ         0.0027963          9.4232          5.0815          5.0815
v  Pressure               -24.101          28.845           1.099           1.099
v  nu_tilda            4.405e-007       0.0043841       0.0017675       0.0017675
v  TempC                       21          73.052          22.056          22.056
v  TurbVisc           3.3121e-014       0.0051664       0.0020777       0.0020777
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2453:        0.22640E+01

===============================================================


 INSTANT    0.245400000E+04   TIME STEP NUMBER            2454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.21293E-02 0.89086E+00
   Friction velocity        uk    :  0.21293E-02 0.89086E+00
   Dimensionless distance   yplus :  0.17143E-01 0.71720E+01
   Friction thermal sca.    tstar : -0.57353E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.12790E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10701E-01      33   0.24550E-03   0.48483E+01 0.19483E+03 
c  Velocity[X]                                      0.18631E+01 
c  Velocity[Y]                                      0.29853E+01 
c  Velocity[Z]                                      0.28930E-29 
c  Pressure     0.12786E-06     538   0.99043E-08   0.12676E+00 0.16149E+04 
c  nu_tilda     0.81177E-05      33   0.13801E-04   0.71635E-06 0.21563E+03 
c  TempC        0.43384E+02      26   0.32026E-03   0.57994E+01 0.26144E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0278          9.4201          4.5729          4.5729
v  Velocity[Y]            -3.0082          7.1707          0.2366          0.2366
v  Velocity[Z]       -6.9287e-015     7.4181e-015    -1.4807e-017    -1.4807e-017
v  ǁVelocityǁ         0.0024933          9.4219          5.0813          5.0813
v  Pressure               -24.153          28.659          1.0334          1.0334
v  nu_tilda           4.4052e-007       0.0043847       0.0017676       0.0017676
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3124e-014       0.0051671       0.0020779       0.0020779
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2454:        0.22300E+01

===============================================================


 INSTANT    0.245500000E+04   TIME STEP NUMBER            2455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27528E-02 0.89001E+00
   Friction velocity        uk    :  0.27528E-02 0.89001E+00
   Dimensionless distance   yplus :  0.22162E-01 0.71652E+01
   Friction thermal sca.    tstar : -0.61928E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16536E-01 0.53460E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10701E-01      33   0.20959E-03   0.48381E+01 0.19465E+03 
c  Velocity[X]                                      0.18720E+01 
c  Velocity[Y]                                      0.29661E+01 
c  Velocity[Z]                                      0.18641E-29 
c  Pressure     0.13380E-06     536   0.97428E-08   0.12858E+00 0.13787E+04 
c  nu_tilda     0.81194E-05      33   0.40693E-05   0.71635E-06 0.21562E+03 
c  TempC        0.43388E+02      26   0.30564E-03   0.65320E+01 0.28286E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.03          9.4188          4.5729          4.5729
v  Velocity[Y]            -3.0078          7.1929         0.23669         0.23669
v  Velocity[Z]       -6.9287e-015     7.3858e-015    -1.4811e-017    -1.4811e-017
v  ǁVelocityǁ         0.0019393          9.4206          5.0811          5.0811
v  Pressure               -24.102            28.8          1.0967          1.0967
v  nu_tilda           4.4051e-007       0.0043852       0.0017678       0.0017678
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3131e-014       0.0051678       0.0020781       0.0020781
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2455:        0.22160E+01

===============================================================


 INSTANT    0.245600000E+04   TIME STEP NUMBER            2456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94357E-02 0.89163E+00
   Friction velocity        uk    :  0.94357E-02 0.89163E+00
   Dimensionless distance   yplus :  0.75964E-01 0.71782E+01
   Friction thermal sca.    tstar : -0.58981E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56678E-01 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10701E-01      33   0.25505E-03   0.48291E+01 0.19453E+03 
c  Velocity[X]                                      0.18800E+01 
c  Velocity[Y]                                      0.29491E+01 
c  Velocity[Z]                                      0.28232E-29 
c  Pressure     0.13129E-06     488   0.97126E-08   0.12827E+00 0.81145E+03 
c  nu_tilda     0.81210E-05      33   0.13797E-04   0.71642E-06 0.21562E+03 
c  TempC        0.43392E+02      27   0.29353E-03   0.52963E+01 0.27814E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0322          9.4175          4.5729          4.5729
v  Velocity[Y]            -3.0073          7.2029         0.23679         0.23679
v  Velocity[Z]       -6.9287e-015     7.4856e-015    -1.4806e-017    -1.4806e-017
v  ǁVelocityǁ        0.00099993          9.4193          5.0809          5.0809
v  Pressure               -24.159          28.756          1.0603          1.0603
v  nu_tilda           4.4047e-007       0.0043858       0.0017679       0.0017679
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3127e-014       0.0051685       0.0020783       0.0020783
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2456:        0.21110E+01

===============================================================


 INSTANT    0.245700000E+04   TIME STEP NUMBER            2457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.92081E-02 0.89137E+00
   Friction velocity        uk    :  0.92081E-02 0.89137E+00
   Dimensionless distance   yplus :  0.74132E-01 0.71762E+01
   Friction thermal sca.    tstar : -0.67025E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55311E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10702E-01      33   0.22862E-03   0.48431E+01 0.19457E+03 
c  Velocity[X]                                      0.18730E+01 
c  Velocity[Y]                                      0.29700E+01 
c  Velocity[Z]                                      0.36910E-29 
c  Pressure     0.13050E-06     473   0.91698E-08   0.12941E+00 0.67090E+03 
c  nu_tilda     0.81227E-05      33   0.40502E-05   0.71638E-06 0.21560E+03 
c  TempC        0.43396E+02      26   0.30360E-03   0.53477E+01 0.27315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0343          9.4162          4.5729          4.5729
v  Velocity[Y]            -3.0068          7.1761         0.23688         0.23688
v  Velocity[Z]       -6.9287e-015     7.3537e-015    -1.4808e-017    -1.4808e-017
v  ǁVelocityǁ         0.0010625           9.418          5.0807          5.0807
v  Pressure               -24.106          28.744          1.0909          1.0909
v  nu_tilda           4.4044e-007       0.0043864       0.0017682       0.0017682
v  TempC                       21          73.052          22.056          22.056
v  TurbVisc           3.3114e-014       0.0051692       0.0020785       0.0020785
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2457:        0.20730E+01

===============================================================


 INSTANT    0.245800000E+04   TIME STEP NUMBER            2458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.30442E-02 0.88979E+00
   Friction velocity        uk    :  0.30442E-02 0.88979E+00
   Dimensionless distance   yplus :  0.24508E-01 0.71634E+01
   Friction thermal sca.    tstar : -0.21240E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18286E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10702E-01      33   0.23540E-03   0.48145E+01 0.19450E+03 
c  Velocity[X]                                      0.18600E+01 
c  Velocity[Y]                                      0.29545E+01 
c  Velocity[Z]                                      0.12641E-29 
c  Pressure     0.13004E-06     489   0.90339E-08   0.12549E+00 0.76417E+03 
c  nu_tilda     0.81243E-05      33   0.13796E-04   0.71639E-06 0.21559E+03 
c  TempC        0.43400E+02      26   0.28393E-03   0.55972E+01 0.26966E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0364          9.4149          4.5729          4.5729
v  Velocity[Y]            -3.0062          7.1904         0.23697         0.23697
v  Velocity[Z]       -6.9287e-015     7.3457e-015    -1.4809e-017    -1.4809e-017
v  ǁVelocityǁ         0.0024291          9.4167          5.0805          5.0805
v  Pressure               -24.166          28.719           1.055           1.055
v  nu_tilda           4.4041e-007        0.004387       0.0017683       0.0017683
v  TempC                       21          73.051          22.056          22.056
v  TurbVisc           3.3108e-014       0.0051699       0.0020787       0.0020787
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2458:        0.21020E+01

===============================================================


 INSTANT    0.245900000E+04   TIME STEP NUMBER            2459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85410E-02 0.89104E+00
   Friction velocity        uk    :  0.85410E-02 0.89104E+00
   Dimensionless distance   yplus :  0.68761E-01 0.71735E+01
   Friction thermal sca.    tstar : -0.57986E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51304E-01 0.53522E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10702E-01      33   0.25421E-03   0.48334E+01 0.19449E+03 
c  Velocity[X]                                      0.18905E+01 
c  Velocity[Y]                                      0.29430E+01 
c  Velocity[Z]                                      0.38430E-29 
c  Pressure     0.14016E-06     472   0.92859E-08   0.13867E+00 0.73011E+03 
c  nu_tilda     0.81259E-05      33   0.40302E-05   0.71639E-06 0.21558E+03 
c  TempC        0.43404E+02      27   0.35253E-03   0.60474E+01 0.26360E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0385          9.4136          4.5729          4.5729
v  Velocity[Y]            -3.0057           7.172         0.23706         0.23706
v  Velocity[Z]       -6.9287e-015     7.4391e-015    -1.4803e-017    -1.4803e-017
v  ǁVelocityǁ         0.0017143          9.4154          5.0803          5.0803
v  Pressure               -24.112          28.725          1.0903          1.0903
v  nu_tilda           4.4045e-007       0.0043876       0.0017685       0.0017685
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3099e-014       0.0051705       0.0020789       0.0020789
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2459:        0.20870E+01

===============================================================


 INSTANT    0.246000000E+04   TIME STEP NUMBER            2460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10682E-01 0.89017E+00
   Friction velocity        uk    :  0.10682E-01 0.89017E+00
   Dimensionless distance   yplus :  0.85995E-01 0.71664E+01
   Friction thermal sca.    tstar : -0.58283E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64162E-01 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.18928E-03   0.48498E+01 0.19504E+03 
c  Velocity[X]                                      0.18687E+01 
c  Velocity[Y]                                      0.29811E+01 
c  Velocity[Z]                                      0.15306E-29 
c  Pressure     0.12936E-06     457   0.94945E-08   0.12618E+00 0.56249E+03 
c  nu_tilda     0.81275E-05      33   0.13789E-04   0.71642E-06 0.21557E+03 
c  TempC        0.43408E+02      27   0.29691E-03   0.61810E+01 0.29757E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0406          9.4122          4.5729          4.5729
v  Velocity[Y]            -3.0053          7.1941         0.23715         0.23715
v  Velocity[Z]       -6.9287e-015     7.4765e-015    -1.4797e-017    -1.4797e-017
v  ǁVelocityǁ         0.0012447           9.414          5.0801          5.0801
v  Pressure               -24.172          28.765          1.0702          1.0702
v  nu_tilda           4.4046e-007       0.0043881       0.0017686       0.0017686
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3109e-014       0.0051712       0.0020791       0.0020791
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2460:        0.20410E+01

===============================================================


 INSTANT    0.246100000E+04   TIME STEP NUMBER            2461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89520E-02 0.89142E+00
   Friction velocity        uk    :  0.89520E-02 0.89142E+00
   Dimensionless distance   yplus :  0.72070E-01 0.71765E+01
   Friction thermal sca.    tstar : -0.57072E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53772E-01 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.24788E-03   0.48170E+01 0.19472E+03 
c  Velocity[X]                                      0.18570E+01 
c  Velocity[Y]                                      0.29601E+01 
c  Velocity[Z]                                      0.28001E-29 
c  Pressure     0.13490E-06     489   0.92830E-08   0.13021E+00 0.83158E+03 
c  nu_tilda     0.81292E-05      33   0.40089E-05   0.71640E-06 0.21556E+03 
c  TempC        0.43411E+02      26   0.31573E-03   0.40132E+01 0.24732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0427          9.4109          4.5729          4.5729
v  Velocity[Y]            -3.0048          7.1998         0.23724         0.23724
v  Velocity[Z]       -6.9287e-015     7.2702e-015    -1.4804e-017    -1.4804e-017
v  ǁVelocityǁ         0.0014652          9.4128          5.0799          5.0799
v  Pressure                -24.12            28.8           1.111           1.111
v  nu_tilda           4.4046e-007       0.0043887       0.0017688       0.0017688
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3114e-014       0.0051719       0.0020793       0.0020793
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2461:        0.21060E+01

===============================================================


 INSTANT    0.246200000E+04   TIME STEP NUMBER            2462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.92016E-02 0.89113E+00
   Friction velocity        uk    :  0.92016E-02 0.89113E+00
   Dimensionless distance   yplus :  0.74079E-01 0.71742E+01
   Friction thermal sca.    tstar : -0.57529E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55271E-01 0.53528E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.24663E-03   0.48576E+01 0.19473E+03 
c  Velocity[X]                                      0.19102E+01 
c  Velocity[Y]                                      0.29474E+01 
c  Velocity[Z]                                      0.32148E-29 
c  Pressure     0.14105E-06     520   0.93234E-08   0.13998E+00 0.14618E+04 
c  nu_tilda     0.81308E-05      33   0.13789E-04   0.71648E-06 0.21556E+03 
c  TempC        0.43415E+02      27   0.27615E-03   0.50099E+01 0.25998E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0447          9.4096          4.5729          4.5729
v  Velocity[Y]            -3.0043          7.1728         0.23734         0.23734
v  Velocity[Z]       -6.9287e-015     7.2367e-015    -1.4805e-017    -1.4805e-017
v  ǁVelocityǁ         0.0013758          9.4115          5.0797          5.0797
v  Pressure               -24.177          28.644          1.0475          1.0475
v  nu_tilda            4.405e-007       0.0043893       0.0017689       0.0017689
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3112e-014       0.0051725       0.0020795       0.0020795
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2462:        0.23340E+01

===============================================================


 INSTANT    0.246300000E+04   TIME STEP NUMBER            2463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.34008E-02 0.88983E+00
   Friction velocity        uk    :  0.34008E-02 0.88983E+00
   Dimensionless distance   yplus :  0.27379E-01 0.71638E+01
   Friction thermal sca.    tstar : -0.61991E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20428E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10704E-01      33   0.23604E-03   0.48388E+01 0.19487E+03 
c  Velocity[X]                                      0.18683E+01 
c  Velocity[Y]                                      0.29705E+01 
c  Velocity[Z]                                      0.90418E-30 
c  Pressure     0.11976E-06     505   0.96275E-08   0.11613E+00 0.15702E+04 
c  nu_tilda     0.81324E-05      33   0.39908E-05   0.71646E-06 0.21555E+03 
c  TempC        0.43419E+02      27   0.26203E-03   0.46061E+01 0.24133E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0467          9.4083          4.5729          4.5729
v  Velocity[Y]            -3.0038          7.1941         0.23743         0.23743
v  Velocity[Z]       -6.9287e-015     7.2883e-015    -1.4803e-017    -1.4803e-017
v  ǁVelocityǁ         0.0010389          9.4101          5.0795          5.0795
v  Pressure               -24.133          28.824          1.1149          1.1149
v  nu_tilda           4.4055e-007       0.0043899       0.0017692       0.0017692
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3126e-014       0.0051732       0.0020796       0.0020796
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2463:        0.24290E+01

===============================================================


 INSTANT    0.246400000E+04   TIME STEP NUMBER            2464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.63417E-02 0.89080E+00
   Friction velocity        uk    :  0.63417E-02 0.89080E+00
   Dimensionless distance   yplus :  0.51055E-01 0.71715E+01
   Friction thermal sca.    tstar : -0.61778E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38093E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10704E-01      33   0.24046E-03   0.48138E+01 0.19456E+03 
c  Velocity[X]                                      0.18727E+01 
c  Velocity[Y]                                      0.29411E+01 
c  Velocity[Z]                                      0.42407E-29 
c  Pressure     0.13439E-06     553   0.93588E-08   0.13102E+00 0.17959E+04 
c  nu_tilda     0.81340E-05      33   0.13782E-04   0.71649E-06 0.21554E+03 
c  TempC        0.43423E+02      27   0.29991E-03   0.45685E+01 0.24194E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0488           9.407          4.5729          4.5729
v  Velocity[Y]            -3.0032          7.1677         0.23752         0.23752
v  Velocity[Z]       -6.9287e-015      7.351e-015    -1.4801e-017    -1.4801e-017
v  ǁVelocityǁ        0.00074051          9.4088          5.0793          5.0793
v  Pressure               -24.189           28.61          1.0404          1.0404
v  nu_tilda           4.4061e-007       0.0043905       0.0017693       0.0017693
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc            3.314e-014       0.0051739       0.0020799       0.0020799
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2464:        0.22660E+01

===============================================================


 INSTANT    0.246500000E+04   TIME STEP NUMBER            2465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10853E-01 0.89027E+00
   Friction velocity        uk    :  0.10853E-01 0.89027E+00
   Dimensionless distance   yplus :  0.87372E-01 0.71672E+01
   Friction thermal sca.    tstar : -0.63913E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65189E-01 0.53476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10704E-01      33   0.19162E-03   0.48064E+01 0.19439E+03 
c  Velocity[X]                                      0.18829E+01 
c  Velocity[Y]                                      0.29235E+01 
c  Velocity[Z]                                      0.17673E-29 
c  Pressure     0.11798E-06     522   0.93060E-08   0.11553E+00 0.17215E+04 
c  nu_tilda     0.81357E-05      33   0.39638E-05   0.71643E-06 0.21552E+03 
c  TempC        0.43427E+02      27   0.27449E-03   0.51452E+01 0.26419E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0509          9.4057          4.5729          4.5729
v  Velocity[Y]            -3.0027          7.1957         0.23761         0.23761
v  Velocity[Z]       -6.9287e-015      7.237e-015    -1.4803e-017    -1.4803e-017
v  ǁVelocityǁ         0.0015413          9.4075          5.0791          5.0791
v  Pressure               -24.145          28.815          1.1132          1.1132
v  nu_tilda           4.4058e-007        0.004391       0.0017695       0.0017695
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3159e-014       0.0051746         0.00208         0.00208
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2465:        0.22050E+01

===============================================================


 INSTANT    0.246600000E+04   TIME STEP NUMBER            2466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17104E-02 0.89161E+00
   Friction velocity        uk    :  0.17104E-02 0.89161E+00
   Dimensionless distance   yplus :  0.13770E-01 0.71781E+01
   Friction thermal sca.    tstar : -0.67603E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10274E-01 0.53557E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10705E-01      33   0.23770E-03   0.48140E+01 0.19488E+03 
c  Velocity[X]                                      0.18510E+01 
c  Velocity[Y]                                      0.29630E+01 
c  Velocity[Z]                                      0.20132E-29 
c  Pressure     0.11908E-06     554   0.94401E-08   0.11649E+00 0.10250E+04 
c  nu_tilda     0.81373E-05      33   0.13782E-04   0.71650E-06 0.21552E+03 
c  TempC        0.43431E+02      26   0.30428E-03   0.60266E+01 0.25374E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.053          9.4043          4.5729          4.5729
v  Velocity[Y]            -3.0023          7.2027          0.2377          0.2377
v  Velocity[Z]       -6.9287e-015     7.2313e-015    -1.4811e-017    -1.4811e-017
v  ǁVelocityǁ         0.0030226          9.4062          5.0789          5.0789
v  Pressure               -24.203          28.735          1.0662          1.0662
v  nu_tilda           4.4047e-007       0.0043916       0.0017696       0.0017696
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3149e-014       0.0051753       0.0020802       0.0020802
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2466:        0.22590E+01

===============================================================


 INSTANT    0.246700000E+04   TIME STEP NUMBER            2467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18900E-01 0.89118E+00
   Friction velocity        uk    :  0.18900E-01 0.89118E+00
   Dimensionless distance   yplus :  0.15216E+00 0.71746E+01
   Friction thermal sca.    tstar : -0.69908E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11353E+00 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10705E-01      33   0.25365E-03   0.48281E+01 0.19461E+03 
c  Velocity[X]                                      0.18913E+01 
c  Velocity[Y]                                      0.29368E+01 
c  Velocity[Z]                                      0.25602E-29 
c  Pressure     0.15199E-06     472   0.95120E-08   0.14764E+00 0.58546E+03 
c  nu_tilda     0.81389E-05      33   0.39500E-05   0.71655E-06 0.21552E+03 
c  TempC        0.43435E+02      27   0.28728E-03   0.69549E+01 0.28148E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0551           9.403          4.5729          4.5729
v  Velocity[Y]            -3.0018          7.1726          0.2378          0.2378
v  Velocity[Z]       -6.9287e-015     7.2064e-015     -1.482e-017     -1.482e-017
v  ǁVelocityǁ         0.0020367          9.4049          5.0787          5.0787
v  Pressure               -24.155          28.696          1.0889          1.0889
v  nu_tilda           4.4047e-007       0.0043921       0.0017698       0.0017698
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3115e-014       0.0051759       0.0020804       0.0020804
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2467:        0.20860E+01

===============================================================


 INSTANT    0.246800000E+04   TIME STEP NUMBER            2468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10827E-01 0.88989E+00
   Friction velocity        uk    :  0.10827E-01 0.88989E+00
   Dimensionless distance   yplus :  0.87167E-01 0.71642E+01
   Friction thermal sca.    tstar : -0.74778E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65036E-01 0.53453E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10705E-01      33   0.25175E-03   0.48350E+01 0.19479E+03 
c  Velocity[X]                                      0.19033E+01 
c  Velocity[Y]                                      0.29318E+01 
c  Velocity[Z]                                      0.27739E-29 
c  Pressure     0.13188E-06     521   0.94479E-08   0.12830E+00 0.70596E+03 
c  nu_tilda     0.81405E-05      33   0.13776E-04   0.71655E-06 0.21550E+03 
c  TempC        0.43438E+02      26   0.31802E-03   0.55530E+01 0.26970E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0572          9.4017          4.5729          4.5729
v  Velocity[Y]            -3.0013          7.1934         0.23789         0.23789
v  Velocity[Z]       -6.9287e-015     7.1858e-015    -1.4829e-017    -1.4829e-017
v  ǁVelocityǁ         0.0021435          9.4035          5.0784          5.0784
v  Pressure               -24.219            28.7          1.0538          1.0538
v  nu_tilda           4.4051e-007       0.0043927       0.0017699       0.0017699
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3115e-014       0.0051766       0.0020806       0.0020806
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2468:        0.21890E+01

===============================================================


 INSTANT    0.246900000E+04   TIME STEP NUMBER            2469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.62850E-02 0.89107E+00
   Friction velocity        uk    :  0.62850E-02 0.89107E+00
   Dimensionless distance   yplus :  0.50598E-01 0.71737E+01
   Friction thermal sca.    tstar : -0.78904E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37752E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.24103E-03   0.48096E+01 0.19454E+03 
c  Velocity[X]                                      0.18756E+01 
c  Velocity[Y]                                      0.29340E+01 
c  Velocity[Z]                                      0.22621E-29 
c  Pressure     0.12836E-06     488   0.97514E-08   0.12653E+00 0.62362E+03 
c  nu_tilda     0.81421E-05      33   0.39212E-05   0.71651E-06 0.21549E+03 
c  TempC        0.43442E+02      26   0.28532E-03   0.56902E+01 0.28107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0592          9.4003          4.5729          4.5729
v  Velocity[Y]            -3.0008          7.1717         0.23798         0.23798
v  Velocity[Z]       -6.9287e-015     7.1539e-015    -1.4837e-017    -1.4837e-017
v  ǁVelocityǁ         0.0019624          9.4022          5.0782          5.0782
v  Pressure                -24.17          28.695          1.0818          1.0818
v  nu_tilda           4.4055e-007       0.0043933       0.0017701       0.0017701
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3127e-014       0.0051773       0.0020808       0.0020808
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2469:        0.21080E+01

===============================================================


 INSTANT    0.247000000E+04   TIME STEP NUMBER            2470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.77927E-02 0.88999E+00
   Friction velocity        uk    :  0.77927E-02 0.88999E+00
   Dimensionless distance   yplus :  0.62737E-01 0.71650E+01
   Friction thermal sca.    tstar : -0.87842E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46808E-01 0.53459E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.18618E-03   0.47776E+01 0.19423E+03 
c  Velocity[X]                                      0.18719E+01 
c  Velocity[Y]                                      0.29058E+01 
c  Velocity[Z]                                      0.37656E-29 
c  Pressure     0.13285E-06     506   0.97255E-08   0.12758E+00 0.75556E+03 
c  nu_tilda     0.81437E-05      33   0.13776E-04   0.71653E-06 0.21548E+03 
c  TempC        0.43446E+02      26   0.23675E-03   0.58401E+01 0.25574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0612           9.399          4.5729          4.5729
v  Velocity[Y]            -3.0002          7.1903         0.23807         0.23807
v  Velocity[Z]       -6.9287e-015     7.1561e-015    -1.4833e-017    -1.4833e-017
v  ǁVelocityǁ         0.0021878          9.4009           5.078           5.078
v  Pressure               -24.235          28.674          1.0444          1.0444
v  nu_tilda           4.4055e-007       0.0043939       0.0017702       0.0017702
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc            3.314e-014       0.0051779        0.002081        0.002081
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2470:        0.21520E+01

===============================================================


 INSTANT    0.247100000E+04   TIME STEP NUMBER            2471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72683E-02 0.89143E+00
   Friction velocity        uk    :  0.72683E-02 0.89143E+00
   Dimensionless distance   yplus :  0.58515E-01 0.71767E+01
   Friction thermal sca.    tstar : -0.93440E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43659E-01 0.53546E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.24676E-03   0.47852E+01 0.19438E+03 
c  Velocity[X]                                      0.18758E+01 
c  Velocity[Y]                                      0.29094E+01 
c  Velocity[Z]                                      0.14341E-29 
c  Pressure     0.12315E-06     522   0.95114E-08   0.11974E+00 0.11479E+04 
c  nu_tilda     0.81453E-05      33   0.39065E-05   0.71653E-06 0.21547E+03 
c  TempC        0.43450E+02      27   0.29667E-03   0.41087E+01 0.21405E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0632          9.3977          4.5729          4.5729
v  Velocity[Y]            -2.9997          7.2019         0.23816         0.23816
v  Velocity[Z]       -6.9287e-015     7.1582e-015    -1.4846e-017    -1.4846e-017
v  ǁVelocityǁ         0.0022697          9.3996          5.0778          5.0778
v  Pressure               -24.189          28.781          1.0966          1.0966
v  nu_tilda           4.4051e-007       0.0043944       0.0017705       0.0017705
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3138e-014       0.0051786       0.0020812       0.0020812
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2471:        0.21940E+01

===============================================================


 INSTANT    0.247200000E+04   TIME STEP NUMBER            2472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53159E-02 0.89094E+00
   Friction velocity        uk    :  0.53159E-02 0.89094E+00
   Dimensionless distance   yplus :  0.42797E-01 0.71726E+01
   Friction thermal sca.    tstar : -0.10619E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31931E-01 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.23293E-03   0.48070E+01 0.19455E+03 
c  Velocity[X]                                      0.18804E+01 
c  Velocity[Y]                                      0.29266E+01 
c  Velocity[Z]                                      0.17607E-29 
c  Pressure     0.12849E-06     554   0.93260E-08   0.12710E+00 0.17877E+04 
c  nu_tilda     0.81469E-05      33   0.13768E-04   0.71658E-06 0.21546E+03 
c  TempC        0.43453E+02      27   0.27279E-03   0.44463E+01 0.24090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0652          9.3964          4.5729          4.5729
v  Velocity[Y]            -2.9992          7.1722         0.23826         0.23826
v  Velocity[Z]       -6.9287e-015      7.174e-015    -1.4854e-017    -1.4854e-017
v  ǁVelocityǁ          0.002184          9.3982          5.0776          5.0776
v  Pressure               -24.254           28.58          1.0171          1.0171
v  nu_tilda           4.4052e-007       0.0043949       0.0017705       0.0017705
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3128e-014       0.0051792       0.0020814       0.0020814
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2472:        0.22670E+01

===============================================================


 INSTANT    0.247300000E+04   TIME STEP NUMBER            2473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.83368E-02 0.88953E+00
   Friction velocity        uk    :  0.83368E-02 0.88953E+00
   Dimensionless distance   yplus :  0.67117E-01 0.71613E+01
   Friction thermal sca.    tstar : -0.11984E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50077E-01 0.53431E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.24755E-03   0.47639E+01 0.19408E+03 
c  Velocity[X]                                      0.18724E+01 
c  Velocity[Y]                                      0.28915E+01 
c  Velocity[Z]                                      0.31818E-29 
c  Pressure     0.12948E-06     568   0.94697E-08   0.12461E+00 0.13696E+04 
c  nu_tilda     0.81485E-05      33   0.38796E-05   0.71657E-06 0.21546E+03 
c  TempC        0.43457E+02      27   0.36762E-03   0.45762E+01 0.24515E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0672           9.395          4.5729          4.5729
v  Velocity[Y]            -2.9988            7.19         0.23835         0.23835
v  Velocity[Z]       -6.9287e-015     7.1805e-015    -1.4868e-017    -1.4868e-017
v  ǁVelocityǁ         0.0027328          9.3969          5.0774          5.0774
v  Pressure               -24.212          28.724          1.0762          1.0762
v  nu_tilda           4.4053e-007       0.0043955       0.0017708       0.0017708
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3131e-014       0.0051799       0.0020815       0.0020815
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2473:        0.22960E+01

===============================================================


 INSTANT    0.247400000E+04   TIME STEP NUMBER            2474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72553E-02 0.89078E+00
   Friction velocity        uk    :  0.72553E-02 0.89078E+00
   Dimensionless distance   yplus :  0.58410E-01 0.71714E+01
   Friction thermal sca.    tstar : -0.14711E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43581E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.24723E-03   0.47611E+01 0.19400E+03 
c  Velocity[X]                                      0.18903E+01 
c  Velocity[Y]                                      0.28708E+01 
c  Velocity[Z]                                      0.85745E-30 
c  Pressure     0.13052E-06     570   0.96436E-08   0.12933E+00 0.15782E+04 
c  nu_tilda     0.81501E-05      33   0.13768E-04   0.71660E-06 0.21545E+03 
c  TempC        0.43461E+02      27   0.24205E-03   0.72548E+01 0.29981E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.069          9.3937          4.5729          4.5729
v  Velocity[Y]            -2.9983          7.1689         0.23844         0.23844
v  Velocity[Z]       -6.9287e-015     7.2119e-015    -1.4876e-017    -1.4876e-017
v  ǁVelocityǁ          0.002186          9.3956          5.0772          5.0772
v  Pressure               -24.273          28.559          1.0058          1.0058
v  nu_tilda           4.4056e-007       0.0043961       0.0017709       0.0017709
v  TempC                       21           73.05          22.057          22.057
v  TurbVisc           3.3132e-014       0.0051805       0.0020817       0.0020817
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2474:        0.23130E+01

===============================================================


 INSTANT    0.247500000E+04   TIME STEP NUMBER            2475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90492E-02 0.89000E+00
   Friction velocity        uk    :  0.90492E-02 0.89000E+00
   Dimensionless distance   yplus :  0.72852E-01 0.71651E+01
   Friction thermal sca.    tstar : -0.20033E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54356E-01 0.53460E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.22227E-03   0.47587E+01 0.19403E+03 
c  Velocity[X]                                      0.18676E+01 
c  Velocity[Y]                                      0.28911E+01 
c  Velocity[Z]                                      0.27503E-29 
c  Pressure     0.11603E-06     584   0.95439E-08   0.11251E+00 0.15113E+04 
c  nu_tilda     0.81517E-05      33   0.38636E-05   0.71655E-06 0.21543E+03 
c  TempC        0.43465E+02      26   0.24377E-03   0.38319E+01 0.23550E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.071          9.3923          4.5729          4.5729
v  Velocity[Y]            -2.9977           7.195         0.23853         0.23853
v  Velocity[Z]       -6.9287e-015     7.2213e-015     -1.488e-017     -1.488e-017
v  ǁVelocityǁ        0.00065342          9.3943           5.077           5.077
v  Pressure               -24.225          28.724          1.0729          1.0729
v  nu_tilda           4.4056e-007       0.0043966       0.0017711       0.0017711
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3142e-014       0.0051812       0.0020819       0.0020819
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2475:        0.23370E+01

===============================================================


 INSTANT    0.247600000E+04   TIME STEP NUMBER            2476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49986E-02 0.89140E+00
   Friction velocity        uk    :  0.49986E-02 0.89140E+00
   Dimensionless distance   yplus :  0.40243E-01 0.71764E+01
   Friction thermal sca.    tstar : -0.56673E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30025E-01 0.53544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.21686E-03   0.47941E+01 0.19468E+03 
c  Velocity[X]                                      0.18797E+01 
c  Velocity[Y]                                      0.29144E+01 
c  Velocity[Z]                                      0.13438E-29 
c  Pressure     0.14422E-06     522   0.94461E-08   0.13811E+00 0.12155E+04 
c  nu_tilda     0.81532E-05      33   0.13760E-04   0.71659E-06 0.21542E+03 
c  TempC        0.43468E+02      27   0.32820E-03   0.41736E+01 0.22753E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.073           9.391          4.5729          4.5729
v  Velocity[Y]            -2.9971          7.1986         0.23862         0.23862
v  Velocity[Z]       -6.9287e-015      7.238e-015    -1.4888e-017    -1.4888e-017
v  ǁVelocityǁ         0.0021794          9.3929          5.0768          5.0768
v  Pressure               -24.286          28.614          1.0173          1.0173
v  nu_tilda           4.4056e-007       0.0043972       0.0017712       0.0017712
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3143e-014       0.0051819       0.0020821       0.0020821
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2476:        0.21990E+01

===============================================================


 INSTANT    0.247700000E+04   TIME STEP NUMBER            2477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.84763E-02 0.89136E+00
   Friction velocity        uk    :  0.84763E-02 0.89136E+00
   Dimensionless distance   yplus :  0.68240E-01 0.71761E+01
   Friction thermal sca.    tstar : -0.22981E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50915E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.23445E-03   0.47849E+01 0.19442E+03 
c  Velocity[X]                                      0.18899E+01 
c  Velocity[Y]                                      0.28949E+01 
c  Velocity[Z]                                      0.20488E-29 
c  Pressure     0.13262E-06     490   0.92993E-08   0.13180E+00 0.77444E+03 
c  nu_tilda     0.81548E-05      33   0.38368E-05   0.71661E-06 0.21541E+03 
c  TempC        0.43472E+02      27   0.26399E-03   0.54757E+01 0.25657E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.075          9.3897          4.5729          4.5729
v  Velocity[Y]            -2.9966          7.1754          0.2387          0.2387
v  Velocity[Z]       -6.9287e-015     7.2452e-015    -1.4904e-017    -1.4904e-017
v  ǁVelocityǁ        0.00073016          9.3916          5.0766          5.0766
v  Pressure               -24.235          28.635          1.0551          1.0551
v  nu_tilda           4.4058e-007       0.0043977       0.0017714       0.0017714
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3143e-014       0.0051825       0.0020823       0.0020823
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2477:        0.21220E+01

===============================================================


 INSTANT    0.247800000E+04   TIME STEP NUMBER            2478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.28270E-02 0.88982E+00
   Friction velocity        uk    :  0.28270E-02 0.88982E+00
   Dimensionless distance   yplus :  0.22759E-01 0.71637E+01
   Friction thermal sca.    tstar : -0.22069E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16981E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.23756E-03   0.47595E+01 0.19419E+03 
c  Velocity[X]                                      0.18663E+01 
c  Velocity[Y]                                      0.28932E+01 
c  Velocity[Z]                                      0.25089E-29 
c  Pressure     0.11032E-06     521   0.94590E-08   0.10740E+00 0.66582E+03 
c  nu_tilda     0.81564E-05      33   0.13762E-04   0.71661E-06 0.21540E+03 
c  TempC        0.43476E+02      27   0.31566E-03   0.41724E+01 0.23058E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.077          9.3883          4.5729          4.5729
v  Velocity[Y]            -2.9962           7.193         0.23879         0.23879
v  Velocity[Z]       -6.9287e-015      7.271e-015    -1.4908e-017    -1.4908e-017
v  ǁVelocityǁ         0.0014435          9.3902          5.0764          5.0764
v  Pressure                 -24.3          28.645          1.0234          1.0234
v  nu_tilda           4.4055e-007       0.0043983       0.0017715       0.0017715
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc            3.315e-014       0.0051832       0.0020825       0.0020825
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2478:        0.21920E+01

===============================================================


 INSTANT    0.247900000E+04   TIME STEP NUMBER            2479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.33257E-02 0.89081E+00
   Friction velocity        uk    :  0.33257E-02 0.89081E+00
   Dimensionless distance   yplus :  0.26774E-01 0.71716E+01
   Friction thermal sca.    tstar : -0.12817E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19977E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.26110E-03   0.47750E+01 0.19423E+03 
c  Velocity[X]                                      0.18919E+01 
c  Velocity[Y]                                      0.28831E+01 
c  Velocity[Z]                                      0.15947E-29 
c  Pressure     0.14130E-06     458   0.95134E-08   0.13689E+00 0.65536E+03 
c  nu_tilda     0.81580E-05      33   0.38202E-05   0.71660E-06 0.21540E+03 
c  TempC        0.43479E+02      27   0.28991E-03   0.55874E+01 0.25648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0789           9.387          4.5729          4.5729
v  Velocity[Y]            -2.9957          7.1683         0.23887         0.23887
v  Velocity[Z]       -6.9287e-015     7.2811e-015    -1.4918e-017    -1.4918e-017
v  ǁVelocityǁ         0.0027491          9.3889          5.0762          5.0762
v  Pressure               -24.243          28.594          1.0495          1.0495
v  nu_tilda            4.406e-007       0.0043988       0.0017717       0.0017717
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc            3.314e-014       0.0051838       0.0020826       0.0020826
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2479:        0.20430E+01

===============================================================


 INSTANT    0.248000000E+04   TIME STEP NUMBER            2480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12455E-02 0.89011E+00
   Friction velocity        uk    :  0.12455E-02 0.89011E+00
   Dimensionless distance   yplus :  0.10027E-01 0.71660E+01
   Friction thermal sca.    tstar : -0.10639E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74816E-02 0.53466E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.22474E-03   0.47888E+01 0.19424E+03 
c  Velocity[X]                                      0.19199E+01 
c  Velocity[Y]                                      0.28689E+01 
c  Velocity[Z]                                      0.29177E-29 
c  Pressure     0.13166E-06     502   0.98540E-08   0.12770E+00 0.59031E+03 
c  nu_tilda     0.81595E-05      33   0.13756E-04   0.71664E-06 0.21539E+03 
c  TempC        0.43483E+02      27   0.19945E-03   0.48020E+01 0.23743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0808          9.3856          4.5729          4.5729
v  Velocity[Y]            -2.9951          7.1925         0.23896         0.23896
v  Velocity[Z]       -6.9287e-015     7.3022e-015    -1.4917e-017    -1.4917e-017
v  ǁVelocityǁ          0.002349          9.3875           5.076           5.076
v  Pressure               -24.304           28.64          1.0276          1.0276
v  nu_tilda           4.4055e-007       0.0043994       0.0017718       0.0017718
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3154e-014       0.0051844       0.0020828       0.0020828
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2480:        0.21630E+01

===============================================================


 INSTANT    0.248100000E+04   TIME STEP NUMBER            2481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12893E-02 0.89141E+00
   Friction velocity        uk    :  0.12893E-02 0.89141E+00
   Dimensionless distance   yplus :  0.10380E-01 0.71765E+01
   Friction thermal sca.    tstar : -0.48442E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77444E-02 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.23485E-03   0.47762E+01 0.19456E+03 
c  Velocity[X]                                      0.18741E+01 
c  Velocity[Y]                                      0.29021E+01 
c  Velocity[Z]                                      0.13315E-29 
c  Pressure     0.11749E-06     536   0.98806E-08   0.11428E+00 0.11495E+04 
c  nu_tilda     0.81611E-05      33   0.37939E-05   0.71663E-06 0.21537E+03 
c  TempC        0.43486E+02      26   0.35366E-03   0.34093E+01 0.22570E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0828          9.3843          4.5729          4.5729
v  Velocity[Y]            -2.9946          7.2028         0.23904         0.23904
v  Velocity[Z]       -6.9287e-015     7.3132e-015     -1.492e-017     -1.492e-017
v  ǁVelocityǁ         0.0031172          9.3862          5.0758          5.0758
v  Pressure               -24.246          28.727          1.0851          1.0851
v  nu_tilda            4.404e-007       0.0043999        0.001772        0.001772
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc           3.3139e-014       0.0051851        0.002083        0.002083
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2481:        0.22320E+01

===============================================================


 INSTANT    0.248200000E+04   TIME STEP NUMBER            2482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.65935E-02 0.89092E+00
   Friction velocity        uk    :  0.65935E-02 0.89092E+00
   Dimensionless distance   yplus :  0.53083E-01 0.71725E+01
   Friction thermal sca.    tstar : -0.86929E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39606E-01 0.53515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.23214E-03   0.47709E+01 0.19430E+03 
c  Velocity[X]                                      0.18899E+01 
c  Velocity[Y]                                      0.28809E+01 
c  Velocity[Z]                                      0.21404E-29 
c  Pressure     0.12968E-06     553   0.98133E-08   0.12650E+00 0.18492E+04 
c  nu_tilda     0.81627E-05      33   0.13752E-04   0.71664E-06 0.21536E+03 
c  TempC        0.43490E+02      27   0.26404E-03   0.65969E+01 0.29412E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0846          9.3829          4.5729          4.5729
v  Velocity[Y]             -2.994          7.1695         0.23913         0.23913
v  Velocity[Z]       -6.9287e-015     7.3287e-015    -1.4922e-017    -1.4922e-017
v  ǁVelocityǁ         0.0030339          9.3848          5.0756          5.0756
v  Pressure               -24.304          28.511          1.0078          1.0078
v  nu_tilda           4.4035e-007       0.0044005       0.0017721       0.0017721
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc           3.3093e-014       0.0051858       0.0020832       0.0020832
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2482:        0.22600E+01

===============================================================


 INSTANT    0.248300000E+04   TIME STEP NUMBER            2483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90854E-02 0.88969E+00
   Friction velocity        uk    :  0.90854E-02 0.88969E+00
   Dimensionless distance   yplus :  0.73144E-01 0.71626E+01
   Friction thermal sca.    tstar : -0.81262E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54573E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.24129E-03   0.47587E+01 0.19424E+03 
c  Velocity[X]                                      0.18937E+01 
c  Velocity[Y]                                      0.28651E+01 
c  Velocity[Z]                                      0.28014E-29 
c  Pressure     0.11627E-06     570   0.98886E-08   0.11273E+00 0.18258E+04 
c  nu_tilda     0.81642E-05      33   0.37744E-05   0.71660E-06 0.21535E+03 
c  TempC        0.43494E+02      27   0.36294E-03   0.43511E+01 0.23625E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0865          9.3815          4.5729          4.5729
v  Velocity[Y]            -2.9935          7.1932         0.23921         0.23921
v  Velocity[Z]       -6.9287e-015      7.344e-015    -1.4927e-017    -1.4927e-017
v  ǁVelocityǁ         0.0032433          9.3835          5.0754          5.0754
v  Pressure               -24.248          28.718          1.0902          1.0902
v  nu_tilda           4.4035e-007        0.004401       0.0017723       0.0017723
v  TempC                       21          73.052          22.057          22.057
v  TurbVisc            3.308e-014       0.0051864       0.0020834       0.0020834
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2483:        0.22970E+01

===============================================================


 INSTANT    0.248400000E+04   TIME STEP NUMBER            2484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96441E-02 0.89071E+00
   Friction velocity        uk    :  0.96441E-02 0.89071E+00
   Dimensionless distance   yplus :  0.77642E-01 0.71709E+01
   Friction thermal sca.    tstar : -0.75078E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57930E-01 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.24586E-03   0.47727E+01 0.19437E+03 
c  Velocity[X]                                      0.18855E+01 
c  Velocity[Y]                                      0.28872E+01 
c  Velocity[Z]                                      0.15243E-29 
c  Pressure     0.12643E-06     489   0.93834E-08   0.12476E+00 0.14372E+04 
c  nu_tilda     0.81658E-05      33   0.13749E-04   0.71665E-06 0.21534E+03 
c  TempC        0.43497E+02      27   0.32787E-03   0.60383E+01 0.28493E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0884          9.3802          4.5729          4.5729
v  Velocity[Y]             -2.993          7.1694         0.23928         0.23928
v  Velocity[Z]       -6.9287e-015     7.3035e-015    -1.4926e-017    -1.4926e-017
v  ǁVelocityǁ         0.0017423          9.3821          5.0752          5.0752
v  Pressure               -24.299          28.555          1.0333          1.0333
v  nu_tilda            4.404e-007       0.0044015       0.0017724       0.0017724
v  TempC                       21          73.051          22.057          22.057
v  TurbVisc            3.308e-014        0.005187       0.0020836       0.0020836
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2484:        0.21290E+01

===============================================================


 INSTANT    0.248500000E+04   TIME STEP NUMBER            2485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.73848E-02 0.88991E+00
   Friction velocity        uk    :  0.73848E-02 0.88991E+00
   Dimensionless distance   yplus :  0.59452E-01 0.71644E+01
   Friction thermal sca.    tstar : -0.72510E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44358E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.20005E-03   0.47845E+01 0.19474E+03 
c  Velocity[X]                                      0.18920E+01 
c  Velocity[Y]                                      0.28924E+01 
c  Velocity[Z]                                      0.27370E-29 
c  Pressure     0.12825E-06     536   0.99691E-08   0.12324E+00 0.14259E+04 
c  nu_tilda     0.81673E-05      33   0.37494E-05   0.71667E-06 0.21534E+03 
c  TempC        0.43501E+02      27   0.30506E-03   0.71542E+01 0.28891E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0902          9.3788          4.5729          4.5729
v  Velocity[Y]            -2.9925          7.1918         0.23936         0.23936
v  Velocity[Z]       -6.9287e-015     7.1641e-015    -1.4926e-017    -1.4926e-017
v  ǁVelocityǁ          0.003168          9.3808           5.075           5.075
v  Pressure               -24.238            28.7          1.1018          1.1018
v  nu_tilda            4.404e-007       0.0044021       0.0017726       0.0017726
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3095e-014       0.0051876       0.0020837       0.0020837
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2485:        0.22310E+01

===============================================================


 INSTANT    0.248600000E+04   TIME STEP NUMBER            2486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95384E-02 0.89153E+00
   Friction velocity        uk    :  0.95384E-02 0.89153E+00
   Dimensionless distance   yplus :  0.76790E-01 0.71774E+01
   Friction thermal sca.    tstar : -0.67327E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57294E-01 0.53551E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.27083E-03   0.47658E+01 0.19444E+03 
c  Velocity[X]                                      0.18912E+01 
c  Velocity[Y]                                      0.28745E+01 
c  Velocity[Z]                                      0.13351E-29 
c  Pressure     0.12055E-06     522   0.92827E-08   0.11757E+00 0.82411E+03 
c  nu_tilda     0.81689E-05      33   0.13744E-04   0.71669E-06 0.21532E+03 
c  TempC        0.43504E+02      26   0.31353E-03   0.64229E+01 0.26761E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.092          9.3775          4.5729          4.5729
v  Velocity[Y]             -2.992          7.2019         0.23944         0.23944
v  Velocity[Z]       -6.9287e-015     7.1867e-015    -1.4921e-017    -1.4921e-017
v  ǁVelocityǁ         0.0030529          9.3794          5.0748          5.0748
v  Pressure               -24.293          28.654          1.0661          1.0661
v  nu_tilda           4.4033e-007       0.0044026       0.0017727       0.0017727
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3094e-014       0.0051883       0.0020839       0.0020839
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2486:        0.21890E+01

===============================================================


 INSTANT    0.248700000E+04   TIME STEP NUMBER            2487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10598E-01 0.89119E+00
   Friction velocity        uk    :  0.10598E-01 0.89119E+00
   Dimensionless distance   yplus :  0.85319E-01 0.71747E+01
   Friction thermal sca.    tstar : -0.65063E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63658E-01 0.53531E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.23443E-03   0.47848E+01 0.19439E+03 
c  Velocity[X]                                      0.19090E+01 
c  Velocity[Y]                                      0.28758E+01 
c  Velocity[Z]                                      0.20652E-29 
c  Pressure     0.13309E-06     473   0.92198E-08   0.13041E+00 0.77302E+03 
c  nu_tilda     0.81705E-05      33   0.37264E-05   0.71664E-06 0.21531E+03 
c  TempC        0.43508E+02      26   0.26060E-03   0.51152E+01 0.25660E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0939          9.3761          4.5729          4.5729
v  Velocity[Y]            -2.9914          7.1753         0.23952         0.23952
v  Velocity[Z]       -6.9287e-015      7.183e-015     -1.493e-017     -1.493e-017
v  ǁVelocityǁ         0.0030445          9.3781          5.0745          5.0745
v  Pressure                -24.23          28.642          1.1045          1.1045
v  nu_tilda           4.4036e-007       0.0044032       0.0017729       0.0017729
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3075e-014       0.0051889       0.0020841       0.0020841
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2487:        0.20860E+01

===============================================================


 INSTANT    0.248800000E+04   TIME STEP NUMBER            2488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85155E-02 0.88968E+00
   Friction velocity        uk    :  0.85155E-02 0.88968E+00
   Dimensionless distance   yplus :  0.68555E-01 0.71625E+01
   Friction thermal sca.    tstar : -0.61277E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51150E-01 0.53440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.23119E-03   0.47522E+01 0.19431E+03 
c  Velocity[X]                                      0.18847E+01 
c  Velocity[Y]                                      0.28676E+01 
c  Velocity[Z]                                      0.26640E-29 
c  Pressure     0.11940E-06     473   0.97717E-08   0.11454E+00 0.63171E+03 
c  nu_tilda     0.81720E-05      33   0.13746E-04   0.71665E-06 0.21529E+03 
c  TempC        0.43512E+02      26   0.33999E-03   0.55694E+01 0.25865E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0957          9.3747          4.5729          4.5729
v  Velocity[Y]            -2.9907           7.189         0.23959         0.23959
v  Velocity[Z]       -6.9287e-015     7.2918e-015     -1.493e-017     -1.493e-017
v  ǁVelocityǁ         0.0030492          9.3767          5.0743          5.0743
v  Pressure               -24.283           28.64          1.0798          1.0798
v  nu_tilda           4.4038e-007       0.0044037        0.001773        0.001773
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3082e-014       0.0051896       0.0020843       0.0020843
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2488:        0.20760E+01

===============================================================


 INSTANT    0.248900000E+04   TIME STEP NUMBER            2489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95140E-02 0.89084E+00
   Friction velocity        uk    :  0.95140E-02 0.89084E+00
   Dimensionless distance   yplus :  0.76594E-01 0.71719E+01
   Friction thermal sca.    tstar : -0.59666E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57148E-01 0.53510E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.24970E-03   0.47673E+01 0.19437E+03 
c  Velocity[X]                                      0.19076E+01 
c  Velocity[Y]                                      0.28598E+01 
c  Velocity[Z]                                      0.16682E-29 
c  Pressure     0.12527E-06     521   0.94292E-08   0.12375E+00 0.96483E+03 
c  nu_tilda     0.81735E-05      33   0.37032E-05   0.71664E-06 0.21529E+03 
c  TempC        0.43515E+02      26   0.30404E-03   0.61712E+01 0.28292E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0976          9.3733          4.5729          4.5729
v  Velocity[Y]            -2.9903           7.171         0.23967         0.23967
v  Velocity[Z]       -6.9287e-015     7.2922e-015    -1.4937e-017    -1.4937e-017
v  ǁVelocityǁ         0.0030208          9.3754          5.0741          5.0741
v  Pressure               -24.217          28.668          1.1312          1.1312
v  nu_tilda           4.4038e-007       0.0044042       0.0017732       0.0017732
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3087e-014       0.0051902       0.0020844       0.0020844
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2489:        0.21880E+01

===============================================================


 INSTANT    0.249000000E+04   TIME STEP NUMBER            2490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49415E-02 0.88994E+00
   Friction velocity        uk    :  0.49415E-02 0.88994E+00
   Dimensionless distance   yplus :  0.39782E-01 0.71646E+01
   Friction thermal sca.    tstar : -0.58219E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29682E-01 0.53456E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.19391E-03   0.47835E+01 0.19481E+03 
c  Velocity[X]                                      0.18899E+01 
c  Velocity[Y]                                      0.28936E+01 
c  Velocity[Z]                                      0.24469E-29 
c  Pressure     0.12311E-06     473   0.95923E-08   0.11923E+00 0.57067E+03 
c  nu_tilda     0.81751E-05      33   0.13738E-04   0.71669E-06 0.21528E+03 
c  TempC        0.43519E+02      27   0.24762E-03   0.50960E+01 0.24942E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.0995           9.372          4.5729          4.5729
v  Velocity[Y]            -2.9898          7.1927         0.23974         0.23974
v  Velocity[Z]       -6.9287e-015     7.2655e-015    -1.4931e-017    -1.4931e-017
v  ǁVelocityǁ         0.0028838           9.374          5.0739          5.0739
v  Pressure               -24.267          28.694          1.1131          1.1131
v  nu_tilda           4.4034e-007       0.0044047       0.0017733       0.0017733
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc            3.309e-014       0.0051908       0.0020846       0.0020846
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2490:        0.20880E+01

===============================================================


 INSTANT    0.249100000E+04   TIME STEP NUMBER            2491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11014E-01 0.89118E+00
   Friction velocity        uk    :  0.11014E-01 0.89118E+00
   Dimensionless distance   yplus :  0.88672E-01 0.71746E+01
   Friction thermal sca.    tstar : -0.57529E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66159E-01 0.53531E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.24877E-03   0.47505E+01 0.19446E+03 
c  Velocity[X]                                      0.18826E+01 
c  Velocity[Y]                                      0.28679E+01 
c  Velocity[Z]                                      0.13735E-29 
c  Pressure     0.13351E-06     489   0.99906E-08   0.12734E+00 0.10077E+04 
c  nu_tilda     0.81766E-05      33   0.36750E-05   0.71668E-06 0.21527E+03 
c  TempC        0.43522E+02      27   0.34439E-03   0.43038E+01 0.23773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1014          9.3706          4.5729          4.5729
v  Velocity[Y]            -2.9893           7.197         0.23981         0.23981
v  Velocity[Z]       -6.9287e-015     7.1678e-015    -1.4936e-017    -1.4936e-017
v  ǁVelocityǁ         0.0015163          9.3726          5.0737          5.0737
v  Pressure               -24.204          28.749          1.1657          1.1657
v  nu_tilda           4.4033e-007       0.0044053       0.0017735       0.0017735
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3075e-014       0.0051914       0.0020848       0.0020848
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2491:        0.23320E+01

===============================================================


 INSTANT    0.249200000E+04   TIME STEP NUMBER            2492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89998E-02 0.89079E+00
   Friction velocity        uk    :  0.89998E-02 0.89079E+00
   Dimensionless distance   yplus :  0.72454E-01 0.71715E+01
   Friction thermal sca.    tstar : -0.57101E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54059E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.25880E-03   0.47899E+01 0.19457E+03 
c  Velocity[X]                                      0.19268E+01 
c  Velocity[Y]                                      0.28631E+01 
c  Velocity[Z]                                      0.29370E-29 
c  Pressure     0.12766E-06     521   0.93673E-08   0.12574E+00 0.13958E+04 
c  nu_tilda     0.81782E-05      33   0.13740E-04   0.71670E-06 0.21526E+03 
c  TempC        0.43526E+02      27   0.29017E-03   0.59694E+01 0.27160E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1031          9.3692          4.5729          4.5729
v  Velocity[Y]            -2.9887          7.1707         0.23988         0.23988
v  Velocity[Z]        -6.958e-015     7.3089e-015    -1.4942e-017    -1.4942e-017
v  ǁVelocityǁ         0.0030751          9.3712          5.0735          5.0735
v  Pressure               -24.254          28.595          1.1099          1.1099
v  nu_tilda           4.4041e-007       0.0044058       0.0017736       0.0017736
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3073e-014        0.005192       0.0020849       0.0020849
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2492:        0.23830E+01

===============================================================


 INSTANT    0.249300000E+04   TIME STEP NUMBER            2493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93668E-02 0.88963E+00
   Friction velocity        uk    :  0.93668E-02 0.88963E+00
   Dimensionless distance   yplus :  0.75409E-01 0.71621E+01
   Friction thermal sca.    tstar : -0.57736E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56264E-01 0.53437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.23532E-03   0.47760E+01 0.19461E+03 
c  Velocity[X]                                      0.18999E+01 
c  Velocity[Y]                                      0.28762E+01 
c  Velocity[Z]                                      0.10103E-29 
c  Pressure     0.10941E-06     584   0.92260E-08   0.10618E+00 0.18067E+04 
c  nu_tilda     0.81797E-05      33   0.36564E-05   0.71663E-06 0.21524E+03 
c  TempC        0.43529E+02      27   0.34434E-03   0.50123E+01 0.24615E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.105          9.3679          4.5729          4.5729
v  Velocity[Y]            -2.9881          7.1925         0.23995         0.23995
v  Velocity[Z]       -7.2571e-015      7.273e-015    -1.4943e-017    -1.4943e-017
v  ǁVelocityǁ         0.0033113          9.3699          5.0733          5.0733
v  Pressure               -24.191          28.792          1.1952          1.1952
v  nu_tilda           4.4046e-007       0.0044063       0.0017738       0.0017738
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3098e-014       0.0051927       0.0020851       0.0020851
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2493:        0.23430E+01

===============================================================


 INSTANT    0.249400000E+04   TIME STEP NUMBER            2494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72464E-02 0.89064E+00
   Friction velocity        uk    :  0.72464E-02 0.89064E+00
   Dimensionless distance   yplus :  0.58338E-01 0.71703E+01
   Friction thermal sca.    tstar : -0.57273E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43527E-01 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.24155E-03   0.47498E+01 0.19434E+03 
c  Velocity[X]                                      0.18978E+01 
c  Velocity[Y]                                      0.28520E+01 
c  Velocity[Z]                                      0.29737E-29 
c  Pressure     0.13107E-06     522   0.98029E-08   0.12739E+00 0.16433E+04 
c  nu_tilda     0.81812E-05      33   0.13731E-04   0.71664E-06 0.21523E+03 
c  TempC        0.43533E+02      27   0.29034E-03   0.53918E+01 0.25566E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1067          9.3665          4.5729          4.5729
v  Velocity[Y]            -2.9875          7.1643         0.24003         0.24003
v  Velocity[Z]       -7.1016e-015      7.255e-015    -1.4939e-017    -1.4939e-017
v  ǁVelocityǁ          0.002839          9.3685          5.0731          5.0731
v  Pressure               -24.241          28.599          1.1312          1.1312
v  nu_tilda           4.4052e-007       0.0044069       0.0017738       0.0017738
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3111e-014       0.0051933       0.0020853       0.0020853
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2494:        0.21870E+01

===============================================================


 INSTANT    0.249500000E+04   TIME STEP NUMBER            2495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10372E-01 0.88998E+00
   Friction velocity        uk    :  0.10372E-01 0.88998E+00
   Dimensionless distance   yplus :  0.83501E-01 0.71649E+01
   Friction thermal sca.    tstar : -0.61924E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62301E-01 0.53458E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.19750E-03   0.47673E+01 0.19463E+03 
c  Velocity[X]                                      0.19113E+01 
c  Velocity[Y]                                      0.28561E+01 
c  Velocity[Z]                                      0.11803E-29 
c  Pressure     0.11739E-06     570   0.93975E-08   0.11366E+00 0.17316E+04 
c  nu_tilda     0.81827E-05      33   0.36244E-05   0.71667E-06 0.21523E+03 
c  TempC        0.43536E+02      27   0.29677E-03   0.48322E+01 0.25110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1085          9.3651          4.5729          4.5729
v  Velocity[Y]             -2.987          7.1927         0.24009         0.24009
v  Velocity[Z]       -7.3377e-015     7.1756e-015    -1.4943e-017    -1.4943e-017
v  ǁVelocityǁ         0.0016043          9.3671          5.0729          5.0729
v  Pressure               -24.176          28.787          1.2134          1.2134
v  nu_tilda           4.4055e-007       0.0044074       0.0017741       0.0017741
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3131e-014       0.0051939       0.0020854       0.0020854
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2495:        0.23120E+01

===============================================================


 INSTANT    0.249600000E+04   TIME STEP NUMBER            2496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.83778E-02 0.89139E+00
   Friction velocity        uk    :  0.83778E-02 0.89139E+00
   Dimensionless distance   yplus :  0.67447E-01 0.71763E+01
   Friction thermal sca.    tstar : -0.58663E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50323E-01 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.23237E-03   0.47440E+01 0.19454E+03 
c  Velocity[X]                                      0.18760E+01 
c  Velocity[Y]                                      0.28680E+01 
c  Velocity[Z]                                      0.16117E-29 
c  Pressure     0.11349E-06     488   0.96772E-08   0.11010E+00 0.92236E+03 
c  nu_tilda     0.81843E-05      33   0.13733E-04   0.71669E-06 0.21522E+03 
c  TempC        0.43539E+02      26   0.25342E-03   0.45422E+01 0.26280E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1102          9.3637          4.5729          4.5729
v  Velocity[Y]            -2.9865          7.2003         0.24016         0.24016
v  Velocity[Z]       -7.3971e-015     7.2577e-015    -1.4946e-017    -1.4946e-017
v  ǁVelocityǁ          0.003406          9.3658          5.0727          5.0727
v  Pressure                -24.23          28.722          1.1743          1.1743
v  nu_tilda           4.4047e-007       0.0044079       0.0017741       0.0017741
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3139e-014       0.0051946       0.0020856       0.0020856
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2496:        0.21150E+01

===============================================================


 INSTANT    0.249700000E+04   TIME STEP NUMBER            2497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10353E-01 0.89102E+00
   Friction velocity        uk    :  0.10353E-01 0.89102E+00
   Dimensionless distance   yplus :  0.83348E-01 0.71734E+01
   Friction thermal sca.    tstar : -0.57268E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62187E-01 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.22753E-03   0.47666E+01 0.19448E+03 
c  Velocity[X]                                      0.19133E+01 
c  Velocity[Y]                                      0.28532E+01 
c  Velocity[Z]                                      0.31394E-29 
c  Pressure     0.12916E-06     457   0.92589E-08   0.12546E+00 0.76462E+03 
c  nu_tilda     0.81858E-05      33   0.36068E-05   0.71667E-06 0.21520E+03 
c  TempC        0.43543E+02      26   0.25524E-03   0.49425E+01 0.25115E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1119          9.3624          4.5729          4.5729
v  Velocity[Y]             -2.986          7.1701         0.24023         0.24023
v  Velocity[Z]       -7.3326e-015     7.2758e-015    -1.4952e-017    -1.4952e-017
v  ǁVelocityǁ         0.0029584          9.3644          5.0725          5.0725
v  Pressure               -24.163          28.681          1.2093          1.2093
v  nu_tilda           4.4045e-007       0.0044084       0.0017743       0.0017743
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3116e-014       0.0051951       0.0020858       0.0020858
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2497:        0.20360E+01

===============================================================


 INSTANT    0.249800000E+04   TIME STEP NUMBER            2498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96710E-02 0.88974E+00
   Friction velocity        uk    :  0.96710E-02 0.88974E+00
   Dimensionless distance   yplus :  0.77858E-01 0.71630E+01
   Friction thermal sca.    tstar : -0.58370E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58091E-01 0.53444E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.26701E-03   0.47587E+01 0.19449E+03 
c  Velocity[X]                                      0.19175E+01 
c  Velocity[Y]                                      0.28411E+01 
c  Velocity[Z]                                      0.91593E-30 
c  Pressure     0.11856E-06     410   0.93985E-08   0.11507E+00 0.54618E+03 
c  nu_tilda     0.81873E-05      33   0.13728E-04   0.71667E-06 0.21519E+03 
c  TempC        0.43546E+02      26   0.36980E-03   0.52918E+01 0.24779E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1136           9.361          4.5729          4.5729
v  Velocity[Y]            -2.9854          7.1903          0.2403          0.2403
v  Velocity[Z]       -7.2268e-015     7.2827e-015    -1.4951e-017    -1.4951e-017
v  ǁVelocityǁ         0.0027812           9.363          5.0723          5.0723
v  Pressure               -24.219          28.732          1.1963          1.1963
v  nu_tilda           4.4046e-007       0.0044089       0.0017744       0.0017744
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc            3.311e-014       0.0051958       0.0020859       0.0020859
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2498:        0.19190E+01

===============================================================


 INSTANT    0.249900000E+04   TIME STEP NUMBER            2499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90512E-02 0.89087E+00
   Friction velocity        uk    :  0.90512E-02 0.89087E+00
   Dimensionless distance   yplus :  0.72868E-01 0.71721E+01
   Friction thermal sca.    tstar : -0.57842E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54368E-01 0.53512E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.24762E-03   0.47704E+01 0.19452E+03 
c  Velocity[X]                                      0.19187E+01 
c  Velocity[Y]                                      0.28516E+01 
c  Velocity[Z]                                      0.27735E-29 
c  Pressure     0.12881E-06     472   0.94530E-08   0.12559E+00 0.83074E+03 
c  nu_tilda     0.81888E-05      33   0.35767E-05   0.71662E-06 0.21517E+03 
c  TempC        0.43550E+02      27   0.31291E-03   0.61801E+01 0.30220E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1154          9.3597          4.5729          4.5729
v  Velocity[Y]            -2.9848          7.1689         0.24036         0.24036
v  Velocity[Z]       -7.4075e-015     7.1927e-015    -1.4951e-017    -1.4951e-017
v  ǁVelocityǁ         0.0030474          9.3616           5.072           5.072
v  Pressure               -24.153          28.735          1.2392          1.2392
v  nu_tilda            4.405e-007       0.0044095       0.0017746       0.0017746
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3112e-014       0.0051964       0.0020861       0.0020861
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2499:        0.20740E+01

===============================================================


 INSTANT    0.250000000E+04   TIME STEP NUMBER            2500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12952E-01 0.88990E+00
   Friction velocity        uk    :  0.12952E-01 0.88990E+00
   Dimensionless distance   yplus :  0.10427E+00 0.71643E+01
   Friction thermal sca.    tstar : -0.57928E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77800E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.18212E-03   0.47579E+01 0.19470E+03 
c  Velocity[X]                                      0.19050E+01 
c  Velocity[Y]                                      0.28529E+01 
c  Velocity[Z]                                      0.12808E-29 
c  Pressure     0.12842E-06     474   0.97556E-08   0.12255E+00 0.63115E+03 
c  nu_tilda     0.81903E-05      33   0.13726E-04   0.71664E-06 0.21516E+03 
c  TempC        0.43553E+02      26   0.25223E-03   0.43190E+01 0.25096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1172          9.3583          4.5729          4.5729
v  Velocity[Y]            -2.9842           7.188         0.24043         0.24043
v  Velocity[Z]       -7.1766e-015     7.2717e-015    -1.4951e-017    -1.4951e-017
v  ǁVelocityǁ           0.00325          9.3602          5.0718          5.0718
v  Pressure               -24.206          28.731          1.2153          1.2153
v  nu_tilda           4.4051e-007         0.00441       0.0017747       0.0017747
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3126e-014        0.005197       0.0020863       0.0020863
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2500:        0.20860E+01

===============================================================


 INSTANT    0.250100000E+04   TIME STEP NUMBER            2501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15363E-02 0.89145E+00
   Friction velocity        uk    :  0.15363E-02 0.89145E+00
   Dimensionless distance   yplus :  0.12368E-01 0.71768E+01
   Friction thermal sca.    tstar : -0.57388E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92279E-02 0.53547E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.24577E-03   0.47448E+01 0.19455E+03 
c  Velocity[X]                                      0.19052E+01 
c  Velocity[Y]                                      0.28396E+01 
c  Velocity[Z]                                      0.15071E-29 
c  Pressure     0.11011E-06     489   0.91273E-08   0.10696E+00 0.13163E+04 
c  nu_tilda     0.81918E-05      33   0.35568E-05   0.71664E-06 0.21516E+03 
c  TempC        0.43557E+02      27   0.31944E-03   0.43494E+01 0.22504E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.119           9.357          4.5729          4.5729
v  Velocity[Y]            -2.9837          7.1997         0.24049         0.24049
v  Velocity[Z]        -7.105e-015     7.2133e-015    -1.4955e-017    -1.4955e-017
v  ǁVelocityǁ         0.0033953          9.3588          5.0716          5.0716
v  Pressure                -24.14          28.849           1.282           1.282
v  nu_tilda           4.4047e-007       0.0044105       0.0017749       0.0017749
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3127e-014       0.0051976       0.0020864       0.0020864
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2501:        0.21190E+01

===============================================================


 INSTANT    0.250200000E+04   TIME STEP NUMBER            2502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14642E-01 0.89085E+00
   Friction velocity        uk    :  0.14642E-01 0.89085E+00
   Dimensionless distance   yplus :  0.11787E+00 0.71719E+01
   Friction thermal sca.    tstar : -0.56980E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87947E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.23669E-03   0.47652E+01 0.19457E+03 
c  Velocity[X]                                      0.19115E+01 
c  Velocity[Y]                                      0.28537E+01 
c  Velocity[Z]                                      0.30471E-29 
c  Pressure     0.12282E-06     500   0.93538E-08   0.12094E+00 0.16239E+04 
c  nu_tilda     0.81933E-05      33   0.13720E-04   0.71670E-06 0.21515E+03 
c  TempC        0.43560E+02      27   0.28049E-03   0.57497E+01 0.25594E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1207          9.3556          4.5729          4.5729
v  Velocity[Y]            -2.9832          7.1706         0.24056         0.24056
v  Velocity[Z]       -6.9733e-015     7.1798e-015     -1.496e-017     -1.496e-017
v  ǁVelocityǁ          0.002717          9.3574          5.0714          5.0714
v  Pressure               -24.191          28.658          1.2178          1.2178
v  nu_tilda           4.4051e-007        0.004411        0.001775        0.001775
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3114e-014       0.0051982       0.0020866       0.0020866
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2502:        0.21420E+01

===============================================================


 INSTANT    0.250300000E+04   TIME STEP NUMBER            2503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48860E-02 0.88948E+00
   Friction velocity        uk    :  0.48860E-02 0.88948E+00
   Dimensionless distance   yplus :  0.39336E-01 0.71609E+01
   Friction thermal sca.    tstar : -0.61778E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29349E-01 0.53428E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.23006E-03   0.47488E+01 0.19454E+03 
c  Velocity[X]                                      0.19081E+01 
c  Velocity[Y]                                      0.28407E+01 
c  Velocity[Z]                                      0.80615E-30 
c  Pressure     0.11780E-06     489   0.94236E-08   0.11262E+00 0.16340E+04 
c  nu_tilda     0.81948E-05      33   0.35278E-05   0.71666E-06 0.21514E+03 
c  TempC        0.43563E+02      26   0.33901E-03   0.43949E+01 0.25129E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1224          9.3542          4.5729          4.5729
v  Velocity[Y]            -2.9827          7.1883         0.24062         0.24062
v  Velocity[Z]       -6.9287e-015     7.1687e-015    -1.4958e-017    -1.4958e-017
v  ǁVelocityǁ         0.0032062           9.356          5.0712          5.0712
v  Pressure               -24.127          28.826          1.2968          1.2968
v  nu_tilda           4.4052e-007       0.0044116       0.0017752       0.0017752
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3127e-014       0.0051988       0.0020868       0.0020868
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2503:        0.21140E+01

===============================================================


 INSTANT    0.250400000E+04   TIME STEP NUMBER            2504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16209E-01 0.89061E+00
   Friction velocity        uk    :  0.16209E-01 0.89061E+00
   Dimensionless distance   yplus :  0.13050E+00 0.71700E+01
   Friction thermal sca.    tstar : -0.59694E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97365E-01 0.53496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.27333E-03   0.47319E+01 0.19439E+03 
c  Velocity[X]                                      0.19088E+01 
c  Velocity[Y]                                      0.28231E+01 
c  Velocity[Z]                                      0.28844E-29 
c  Pressure     0.11609E-06     488   0.92284E-08   0.11391E+00 0.13924E+04 
c  nu_tilda     0.81963E-05      33   0.13718E-04   0.71665E-06 0.21512E+03 
c  TempC        0.43567E+02      26   0.23757E-03   0.60556E+01 0.28865E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1241          9.3529          4.5729          4.5729
v  Velocity[Y]            -2.9821           7.166         0.24068         0.24068
v  Velocity[Z]       -6.9287e-015     7.2071e-015    -1.4957e-017    -1.4957e-017
v  ǁVelocityǁ         0.0030044          9.3546           5.071           5.071
v  Pressure               -24.174          28.673          1.2427          1.2427
v  nu_tilda           4.4054e-007       0.0044121       0.0017752       0.0017752
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3132e-014       0.0051995       0.0020869       0.0020869
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2504:        0.21070E+01

===============================================================


 INSTANT    0.250500000E+04   TIME STEP NUMBER            2505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15427E-01 0.88995E+00
   Friction velocity        uk    :  0.15427E-01 0.88995E+00
   Dimensionless distance   yplus :  0.12419E+00 0.71647E+01
   Friction thermal sca.    tstar : -0.61496E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92663E-01 0.53457E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.21413E-03   0.47827E+01 0.19484E+03 
c  Velocity[X]                                      0.19313E+01 
c  Velocity[Y]                                      0.28514E+01 
c  Velocity[Z]                                      0.10701E-29 
c  Pressure     0.13743E-06     520   0.91881E-08   0.13349E+00 0.18441E+04 
c  nu_tilda     0.81978E-05      33   0.35049E-05   0.71663E-06 0.21511E+03 
c  TempC        0.43570E+02      26   0.26735E-03   0.40358E+01 0.23502E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1258          9.3515          4.5729          4.5729
v  Velocity[Y]            -2.9814          7.1928         0.24073         0.24073
v  Velocity[Z]       -6.9287e-015      7.181e-015    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ         0.0032558          9.3533          5.0708          5.0708
v  Pressure               -24.112          28.874          1.3298          1.3298
v  nu_tilda            4.405e-007       0.0044127       0.0017754       0.0017754
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3136e-014       0.0052001       0.0020871       0.0020871
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2505:        0.21880E+01

===============================================================


 INSTANT    0.250600000E+04   TIME STEP NUMBER            2506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16739E-01 0.89140E+00
   Friction velocity        uk    :  0.16739E-01 0.89140E+00
   Dimensionless distance   yplus :  0.13476E+00 0.71764E+01
   Friction thermal sca.    tstar : -0.64327E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10055E+00 0.53544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.22502E-03   0.47551E+01 0.19465E+03 
c  Velocity[X]                                      0.19205E+01 
c  Velocity[Y]                                      0.28346E+01 
c  Velocity[Z]                                      0.16889E-29 
c  Pressure     0.12993E-06     489   0.93991E-08   0.12433E+00 0.12284E+04 
c  nu_tilda     0.81993E-05      33   0.13714E-04   0.71668E-06 0.21510E+03 
c  TempC        0.43573E+02      27   0.36964E-03   0.48935E+01 0.24615E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1274          9.3502          4.5729          4.5729
v  Velocity[Y]            -2.9808          7.1961         0.24079         0.24079
v  Velocity[Z]       -6.9287e-015     7.2064e-015    -1.4964e-017    -1.4964e-017
v  ǁVelocityǁ         0.0020789          9.3519          5.0706          5.0706
v  Pressure               -24.161          28.758          1.2796          1.2796
v  nu_tilda           4.4043e-007       0.0044132       0.0017755       0.0017755
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3126e-014       0.0052008       0.0020872       0.0020872
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2506:        0.21080E+01

===============================================================


 INSTANT    0.250700000E+04   TIME STEP NUMBER            2507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.64555E-02 0.89129E+00
   Friction velocity        uk    :  0.64555E-02 0.89129E+00
   Dimensionless distance   yplus :  0.51971E-01 0.71755E+01
   Friction thermal sca.    tstar : -0.66923E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38776E-01 0.53537E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.24542E-03   0.47269E+01 0.19427E+03 
c  Velocity[X]                                      0.19199E+01 
c  Velocity[Y]                                      0.28069E+01 
c  Velocity[Z]                                      0.29935E-29 
c  Pressure     0.13186E-06     489   0.91279E-08   0.12915E+00 0.96211E+03 
c  nu_tilda     0.82008E-05      33   0.34769E-05   0.71665E-06 0.21509E+03 
c  TempC        0.43577E+02      27   0.25722E-03   0.58276E+01 0.26745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1291          9.3488          4.5729          4.5729
v  Velocity[Y]            -2.9803          7.1724         0.24085         0.24085
v  Velocity[Z]       -6.9287e-015     7.1755e-015    -1.4971e-017    -1.4971e-017
v  ǁVelocityǁ         0.0030312          9.3506          5.0704          5.0704
v  Pressure               -24.094          28.791          1.3308          1.3308
v  nu_tilda           4.4043e-007       0.0044137       0.0017757       0.0017757
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3104e-014       0.0052014       0.0020874       0.0020874
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2507:        0.21060E+01

===============================================================


 INSTANT    0.250800000E+04   TIME STEP NUMBER            2508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13356E-01 0.88986E+00
   Friction velocity        uk    :  0.13356E-01 0.88986E+00
   Dimensionless distance   yplus :  0.10752E+00 0.71640E+01
   Friction thermal sca.    tstar : -0.71910E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80226E-01 0.53452E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.25218E-03   0.47353E+01 0.19448E+03 
c  Velocity[X]                                      0.19020E+01 
c  Velocity[Y]                                      0.28333E+01 
c  Velocity[Z]                                      0.92366E-30 
c  Pressure     0.11322E-06     472   0.99959E-08   0.10945E+00 0.57544E+03 
c  nu_tilda     0.82023E-05      33   0.13712E-04   0.71668E-06 0.21508E+03 
c  TempC        0.43580E+02      27   0.24405E-03   0.35341E+01 0.22018E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1307          9.3474          4.5729          4.5729
v  Velocity[Y]            -2.9798          7.1904         0.24091         0.24091
v  Velocity[Z]       -6.9287e-015      7.264e-015    -1.4973e-017    -1.4973e-017
v  ǁVelocityǁ           0.00332          9.3492          5.0701          5.0701
v  Pressure               -24.148          28.811          1.3106          1.3106
v  nu_tilda           4.4043e-007       0.0044143       0.0017758       0.0017758
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3105e-014        0.005202       0.0020876       0.0020876
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2508:        0.20840E+01

===============================================================


 INSTANT    0.250900000E+04   TIME STEP NUMBER            2509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12306E-01 0.89092E+00
   Friction velocity        uk    :  0.12306E-01 0.89092E+00
   Dimensionless distance   yplus :  0.99075E-01 0.71725E+01
   Friction thermal sca.    tstar : -0.74419E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73921E-01 0.53515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24534E-03   0.47547E+01 0.19443E+03 
c  Velocity[X]                                      0.19411E+01 
c  Velocity[Y]                                      0.28136E+01 
c  Velocity[Z]                                      0.26730E-29 
c  Pressure     0.14280E-06     457   0.96813E-08   0.13764E+00 0.81581E+03 
c  nu_tilda     0.82037E-05      33   0.34497E-05   0.71665E-06 0.21507E+03 
c  TempC        0.43583E+02      26   0.35281E-03   0.45474E+01 0.25316E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1323           9.346          4.5729          4.5729
v  Velocity[Y]            -2.9792          7.1662         0.24096         0.24096
v  Velocity[Z]       -6.9287e-015     7.2053e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ         0.0028889          9.3478          5.0699          5.0699
v  Pressure               -24.075          28.764          1.3481          1.3481
v  nu_tilda           4.4045e-007       0.0044148        0.001776        0.001776
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3103e-014       0.0052026       0.0020877       0.0020877
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2509:        0.20470E+01

===============================================================


 INSTANT    0.251000000E+04   TIME STEP NUMBER            2510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95902E-02 0.89033E+00
   Friction velocity        uk    :  0.95902E-02 0.89033E+00
   Dimensionless distance   yplus :  0.77208E-01 0.71677E+01
   Friction thermal sca.    tstar : -0.81557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57606E-01 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.19316E-03   0.47588E+01 0.19488E+03 
c  Velocity[X]                                      0.19272E+01 
c  Velocity[Y]                                      0.28316E+01 
c  Velocity[Z]                                      0.11477E-29 
c  Pressure     0.11763E-06     410   0.93215E-08   0.11485E+00 0.57524E+03 
c  nu_tilda     0.82052E-05      33   0.13711E-04   0.71667E-06 0.21505E+03 
c  TempC        0.43586E+02      27   0.27083E-03   0.76976E+01 0.30388E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1339          9.3447          4.5729          4.5729
v  Velocity[Y]            -2.9787          7.1912         0.24101         0.24101
v  Velocity[Z]       -6.9287e-015     7.2001e-015    -1.4973e-017    -1.4973e-017
v  ǁVelocityǁ         0.0015781          9.3465          5.0697          5.0697
v  Pressure               -24.133          28.834          1.3384          1.3384
v  nu_tilda           4.4039e-007       0.0044153        0.001776        0.001776
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.3109e-014       0.0052033       0.0020879       0.0020879
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2510:        0.19230E+01

===============================================================


 INSTANT    0.251100000E+04   TIME STEP NUMBER            2511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48653E-02 0.89164E+00
   Friction velocity        uk    :  0.48653E-02 0.89164E+00
   Dimensionless distance   yplus :  0.39169E-01 0.71783E+01
   Friction thermal sca.    tstar : -0.83957E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29225E-01 0.53558E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.22966E-03   0.47300E+01 0.19464E+03 
c  Velocity[X]                                      0.18939E+01 
c  Velocity[Y]                                      0.28361E+01 
c  Velocity[Z]                                      0.14900E-29 
c  Pressure     0.10872E-06     505   0.97813E-08   0.10472E+00 0.11383E+04 
c  nu_tilda     0.82067E-05      33   0.34260E-05   0.71662E-06 0.21504E+03 
c  TempC        0.43590E+02      26   0.30907E-03   0.47396E+01 0.24642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1356          9.3433          4.5729          4.5729
v  Velocity[Y]             -2.978          7.2024         0.24107         0.24107
v  Velocity[Z]       -6.9287e-015     7.1871e-015    -1.4975e-017    -1.4975e-017
v  ǁVelocityǁ         0.0033476          9.3451          5.0695          5.0695
v  Pressure               -24.064          28.915           1.398           1.398
v  nu_tilda           4.4026e-007       0.0044159       0.0017762       0.0017762
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.3092e-014       0.0052039        0.002088        0.002088
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2511:        0.21410E+01

===============================================================


 INSTANT    0.251200000E+04   TIME STEP NUMBER            2512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11062E-01 0.89117E+00
   Friction velocity        uk    :  0.11062E-01 0.89117E+00
   Dimensionless distance   yplus :  0.89056E-01 0.71746E+01
   Friction thermal sca.    tstar : -0.95089E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66445E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24843E-03   0.47560E+01 0.19462E+03 
c  Velocity[X]                                      0.19379E+01 
c  Velocity[Y]                                      0.28181E+01 
c  Velocity[Z]                                      0.29114E-29 
c  Pressure     0.13263E-06     506   0.99972E-08   0.12862E+00 0.17296E+04 
c  nu_tilda     0.82082E-05      33   0.13705E-04   0.71667E-06 0.21504E+03 
c  TempC        0.43593E+02      26   0.30895E-03   0.53214E+01 0.27291E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1373          9.3419          4.5729          4.5729
v  Velocity[Y]            -2.9774          7.1696         0.24112         0.24112
v  Velocity[Z]       -6.9287e-015     7.2274e-015     -1.498e-017     -1.498e-017
v  ǁVelocityǁ         0.0029507          9.3437          5.0693          5.0693
v  Pressure               -24.114          28.705          1.3301          1.3301
v  nu_tilda           4.4024e-007       0.0044164       0.0017763       0.0017763
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3053e-014       0.0052045       0.0020882       0.0020882
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2512:        0.21510E+01

===============================================================


 INSTANT    0.251300000E+04   TIME STEP NUMBER            2513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16854E-01 0.88996E+00
   Friction velocity        uk    :  0.16854E-01 0.88996E+00
   Dimensionless distance   yplus :  0.13568E+00 0.71648E+01
   Friction thermal sca.    tstar : -0.10367E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10124E+00 0.53457E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24695E-03   0.47506E+01 0.19455E+03 
c  Velocity[X]                                      0.19486E+01 
c  Velocity[Y]                                      0.28020E+01 
c  Velocity[Z]                                      0.11000E-29 
c  Pressure     0.11994E-06     504   0.96159E-08   0.11621E+00 0.19660E+04 
c  nu_tilda     0.82096E-05      33   0.33902E-05   0.71666E-06 0.21503E+03 
c  TempC        0.43596E+02      27   0.31922E-03   0.56589E+01 0.27270E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.139          9.3405          4.5729          4.5729
v  Velocity[Y]            -2.9769          7.1928         0.24117         0.24117
v  Velocity[Z]       -6.9287e-015     7.2167e-015    -1.4979e-017    -1.4979e-017
v  ǁVelocityǁ         0.0032499          9.3423          5.0691          5.0691
v  Pressure               -24.053          28.933          1.4205          1.4205
v  nu_tilda           4.4027e-007       0.0044169       0.0017765       0.0017765
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3046e-014       0.0052051       0.0020883       0.0020883
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2513:        0.21760E+01

===============================================================


 INSTANT    0.251400000E+04   TIME STEP NUMBER            2514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17963E-01 0.89088E+00
   Friction velocity        uk    :  0.17963E-01 0.89088E+00
   Dimensionless distance   yplus :  0.14461E+00 0.71722E+01
   Friction thermal sca.    tstar : -0.12200E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10790E+00 0.53512E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24496E-03   0.47437E+01 0.19459E+03 
c  Velocity[X]                                      0.19232E+01 
c  Velocity[Y]                                      0.28204E+01 
c  Velocity[Z]                                      0.28810E-29 
c  Pressure     0.11905E-06     536   0.97745E-08   0.11695E+00 0.15677E+04 
c  nu_tilda     0.82111E-05      33   0.13706E-04   0.71667E-06 0.21501E+03 
c  TempC        0.43599E+02      27   0.24149E-03   0.56211E+01 0.26236E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1405          9.3391          4.5729          4.5729
v  Velocity[Y]            -2.9764           7.169         0.24122         0.24122
v  Velocity[Z]       -6.9287e-015     7.2503e-015    -1.4974e-017    -1.4974e-017
v  ǁVelocityǁ         0.0025835           9.341          5.0689          5.0689
v  Pressure               -24.104          28.754          1.3582          1.3582
v  nu_tilda           4.4032e-007       0.0044174       0.0017766       0.0017766
v  TempC                       21           73.05          22.059          22.059
v  TurbVisc           3.3056e-014       0.0052057       0.0020885       0.0020885
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2514:        0.22330E+01

===============================================================


 INSTANT    0.251500000E+04   TIME STEP NUMBER            2515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.40830E-02 0.89001E+00
   Friction velocity        uk    :  0.40830E-02 0.89001E+00
   Dimensionless distance   yplus :  0.32871E-01 0.71652E+01
   Friction thermal sca.    tstar : -0.13933E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24525E-01 0.53460E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23282E-03   0.47483E+01 0.19479E+03 
c  Velocity[X]                                      0.19299E+01 
c  Velocity[Y]                                      0.28185E+01 
c  Velocity[Z]                                      0.12591E-29 
c  Pressure     0.13393E-06     520   0.95095E-08   0.12706E+00 0.17402E+04 
c  nu_tilda     0.82126E-05      33   0.33715E-05   0.71662E-06 0.21500E+03 
c  TempC        0.43603E+02      26   0.21698E-03   0.39546E+01 0.24063E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1422          9.3378          4.5729          4.5729
v  Velocity[Y]            -2.9758          7.1901         0.24127         0.24127
v  Velocity[Z]       -6.9287e-015     7.2408e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ         0.0031607          9.3396          5.0686          5.0686
v  Pressure               -24.037          28.935          1.4427          1.4427
v  nu_tilda           4.4032e-007        0.004418       0.0017768       0.0017768
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc            3.307e-014       0.0052064       0.0020886       0.0020886
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2515:        0.21910E+01

===============================================================


 INSTANT    0.251600000E+04   TIME STEP NUMBER            2516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11449E-01 0.89134E+00
   Friction velocity        uk    :  0.11449E-01 0.89134E+00
   Dimensionless distance   yplus :  0.92169E-01 0.71759E+01
   Friction thermal sca.    tstar : -0.19090E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68768E-01 0.53540E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24277E-03   0.47308E+01 0.19459E+03 
c  Velocity[X]                                      0.19262E+01 
c  Velocity[Y]                                      0.28046E+01 
c  Velocity[Z]                                      0.15493E-29 
c  Pressure     0.11005E-06     488   0.95692E-08   0.10680E+00 0.97610E+03 
c  nu_tilda     0.82140E-05      33   0.13697E-04   0.71665E-06 0.21499E+03 
c  TempC        0.43606E+02      27   0.37093E-03   0.39090E+01 0.24150E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1438          9.3364          4.5729          4.5729
v  Velocity[Y]            -2.9752           7.199         0.24132         0.24132
v  Velocity[Z]       -6.9287e-015     7.3368e-015    -1.4974e-017    -1.4974e-017
v  ǁVelocityǁ         0.0030311          9.3382          5.0684          5.0684
v  Pressure               -24.094          28.867          1.3986          1.3986
v  nu_tilda           4.4028e-007       0.0044185       0.0017768       0.0017768
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc            3.307e-014        0.005207       0.0020888       0.0020888
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2516:        0.21100E+01

===============================================================


 INSTANT    0.251700000E+04   TIME STEP NUMBER            2517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94066E-02 0.89097E+00
   Friction velocity        uk    :  0.94066E-02 0.89097E+00
   Dimensionless distance   yplus :  0.75730E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.29706E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56503E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23010E-03   0.47291E+01 0.19440E+03 
c  Velocity[X]                                      0.19262E+01 
c  Velocity[Y]                                      0.28028E+01 
c  Velocity[Z]                                      0.28850E-29 
c  Pressure     0.12346E-06     504   0.92571E-08   0.12147E+00 0.83004E+03 
c  nu_tilda     0.82155E-05      33   0.33362E-05   0.71664E-06 0.21498E+03 
c  TempC        0.43609E+02      27   0.28554E-03   0.78555E+01 0.31362E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1454           9.335          4.5729          4.5729
v  Velocity[Y]            -2.9745          7.1722         0.24137         0.24137
v  Velocity[Z]       -6.9287e-015     7.2948e-015    -1.4976e-017    -1.4976e-017
v  ǁVelocityǁ         0.0018506          9.3368          5.0682          5.0682
v  Pressure               -24.026          28.863          1.4416          1.4416
v  nu_tilda           4.4031e-007        0.004419        0.001777        0.001777
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3058e-014       0.0052076       0.0020889       0.0020889
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2517:        0.21500E+01

===============================================================


 INSTANT    0.251800000E+04   TIME STEP NUMBER            2518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12244E-01 0.88938E+00
   Friction velocity        uk    :  0.12244E-01 0.88938E+00
   Dimensionless distance   yplus :  0.98572E-01 0.71601E+01
   Friction thermal sca.    tstar : -0.22817E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73545E-01 0.53423E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24228E-03   0.47167E+01 0.19448E+03 
c  Velocity[X]                                      0.19191E+01 
c  Velocity[Y]                                      0.27976E+01 
c  Velocity[Z]                                      0.91987E-30 
c  Pressure     0.11961E-06     488   0.98626E-08   0.11456E+00 0.63833E+03 
c  nu_tilda     0.82169E-05      33   0.13700E-04   0.71664E-06 0.21496E+03 
c  TempC        0.43612E+02      27   0.36144E-03   0.49500E+01 0.25600E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1469          9.3336          4.5729          4.5729
v  Velocity[Y]             -2.974          7.1869         0.24142         0.24142
v  Velocity[Z]       -6.9287e-015     7.2912e-015    -1.4973e-017    -1.4973e-017
v  ǁVelocityǁ         0.0019266          9.3354           5.068           5.068
v  Pressure                -24.08          28.858          1.4159          1.4159
v  nu_tilda           4.4032e-007       0.0044195       0.0017771       0.0017771
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3068e-014       0.0052082       0.0020891       0.0020891
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2518:        0.21170E+01

===============================================================


 INSTANT    0.251900000E+04   TIME STEP NUMBER            2519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60074E-02 0.89068E+00
   Friction velocity        uk    :  0.60074E-02 0.89068E+00
   Dimensionless distance   yplus :  0.48364E-01 0.71705E+01
   Friction thermal sca.    tstar : -0.17762E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36085E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.26906E-03   0.47359E+01 0.19455E+03 
c  Velocity[X]                                      0.19455E+01 
c  Velocity[Y]                                      0.27904E+01 
c  Velocity[Z]                                      0.27720E-29 
c  Pressure     0.13088E-06     490   0.93670E-08   0.12788E+00 0.91274E+03 
c  nu_tilda     0.82184E-05      33   0.33146E-05   0.71662E-06 0.21495E+03 
c  TempC        0.43615E+02      27   0.28212E-03   0.71476E+01 0.31177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1484          9.3322          4.5729          4.5729
v  Velocity[Y]            -2.9734          7.1689         0.24146         0.24146
v  Velocity[Z]       -6.9287e-015     7.2789e-015    -1.4971e-017    -1.4971e-017
v  ǁVelocityǁ         0.0012089           9.334          5.0678          5.0678
v  Pressure               -24.013          28.879          1.4646          1.4646
v  nu_tilda           4.4033e-007         0.00442       0.0017773       0.0017773
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3071e-014       0.0052088       0.0020892       0.0020892
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2519:        0.21290E+01

===============================================================


 INSTANT    0.252000000E+04   TIME STEP NUMBER            2520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.75749E-02 0.88987E+00
   Friction velocity        uk    :  0.75749E-02 0.88987E+00
   Dimensionless distance   yplus :  0.60983E-01 0.71641E+01
   Friction thermal sca.    tstar : -0.12824E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45500E-01 0.53452E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.19662E-03   0.47694E+01 0.19510E+03 
c  Velocity[X]                                      0.19414E+01 
c  Velocity[Y]                                      0.28280E+01 
c  Velocity[Z]                                      0.11838E-29 
c  Pressure     0.12065E-06     440   0.89434E-08   0.11712E+00 0.55454E+03 
c  nu_tilda     0.82198E-05      33   0.13692E-04   0.71667E-06 0.21495E+03 
c  TempC        0.43618E+02      27   0.26773E-03   0.49503E+01 0.26153E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1499          9.3308          4.5729          4.5729
v  Velocity[Y]            -2.9729          7.1919          0.2415          0.2415
v  Velocity[Z]       -6.9287e-015     7.3029e-015    -1.4968e-017    -1.4968e-017
v  ǁVelocityǁ         0.0011968          9.3326          5.0676          5.0676
v  Pressure               -24.069          28.908          1.4466          1.4466
v  nu_tilda           4.4032e-007       0.0044205       0.0017773       0.0017773
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3074e-014       0.0052094       0.0020894       0.0020894
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2520:        0.20530E+01

===============================================================


 INSTANT    0.252100000E+04   TIME STEP NUMBER            2521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.67655E-02 0.89136E+00
   Friction velocity        uk    :  0.67655E-02 0.89136E+00
   Dimensionless distance   yplus :  0.54467E-01 0.71761E+01
   Friction thermal sca.    tstar : -0.12046E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40638E-01 0.53542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23692E-03   0.47170E+01 0.19460E+03 
c  Velocity[X]                                      0.19180E+01 
c  Velocity[Y]                                      0.27990E+01 
c  Velocity[Z]                                      0.16069E-29 
c  Pressure     0.12582E-06     490   0.92914E-08   0.12035E+00 0.10490E+04 
c  nu_tilda     0.82213E-05      33   0.32829E-05   0.71663E-06 0.21493E+03 
c  TempC        0.43622E+02      26   0.30921E-03   0.37621E+01 0.23505E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1515          9.3294          4.5729          4.5729
v  Velocity[Y]            -2.9723           7.198         0.24154         0.24154
v  Velocity[Z]       -6.9287e-015     7.3548e-015    -1.4967e-017    -1.4967e-017
v  ǁVelocityǁ        0.00033571          9.3312          5.0674          5.0674
v  Pressure               -23.998          28.969          1.5024          1.5024
v  nu_tilda            4.403e-007       0.0044211       0.0017775       0.0017775
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3071e-014       0.0052101       0.0020895       0.0020895
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2521:        0.23950E+01

===============================================================


 INSTANT    0.252200000E+04   TIME STEP NUMBER            2522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.97229E-03 0.89100E+00
   Friction velocity        uk    :  0.97229E-03 0.89100E+00
   Dimensionless distance   yplus :  0.78276E-02 0.71732E+01
   Friction thermal sca.    tstar : -0.99595E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58403E-02 0.53520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23821E-03   0.47580E+01 0.19477E+03 
c  Velocity[X]                                      0.19603E+01 
c  Velocity[Y]                                      0.27977E+01 
c  Velocity[Z]                                      0.33868E-29 
c  Pressure     0.11788E-06     504   0.89957E-08   0.11634E+00 0.14677E+04 
c  nu_tilda     0.82227E-05      33   0.13692E-04   0.71664E-06 0.21492E+03 
c  TempC        0.43625E+02      26   0.26447E-03   0.73110E+01 0.29045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.153           9.328          4.5729          4.5729
v  Velocity[Y]            -2.9717          7.1717         0.24159         0.24159
v  Velocity[Z]       -6.9287e-015     7.3478e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ        0.00081099          9.3298          5.0671          5.0671
v  Pressure               -24.054          28.804           1.441           1.441
v  nu_tilda           4.4032e-007       0.0044216       0.0017776       0.0017776
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3063e-014       0.0052107       0.0020897       0.0020897
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2522:        0.22300E+01

===============================================================


 INSTANT    0.252300000E+04   TIME STEP NUMBER            2523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.65467E-02 0.88966E+00
   Friction velocity        uk    :  0.65467E-02 0.88966E+00
   Dimensionless distance   yplus :  0.52705E-01 0.71624E+01
   Friction thermal sca.    tstar : -0.92788E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39324E-01 0.53440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23227E-03   0.47307E+01 0.19470E+03 
c  Velocity[X]                                      0.19230E+01 
c  Velocity[Y]                                      0.28077E+01 
c  Velocity[Z]                                      0.92189E-30 
c  Pressure     0.10801E-06     536   0.93629E-08   0.10397E+00 0.19467E+04 
c  nu_tilda     0.82241E-05      33   0.32570E-05   0.71663E-06 0.21491E+03 
c  TempC        0.43628E+02      27   0.30715E-03   0.47713E+01 0.24850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1547          9.3266          4.5729          4.5729
v  Velocity[Y]             -2.971          7.1911         0.24163         0.24163
v  Velocity[Z]       -6.9287e-015     7.2611e-015    -1.4971e-017    -1.4971e-017
v  ǁVelocityǁ         0.0024016          9.3284          5.0669          5.0669
v  Pressure               -23.988          29.024          1.5329          1.5329
v  nu_tilda           4.4032e-007       0.0044221       0.0017778       0.0017778
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc            3.307e-014       0.0052113       0.0020898       0.0020898
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2523:        0.22360E+01

===============================================================


 INSTANT    0.252400000E+04   TIME STEP NUMBER            2524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50312E-02 0.89045E+00
   Friction velocity        uk    :  0.50312E-02 0.89045E+00
   Dimensionless distance   yplus :  0.40505E-01 0.71687E+01
   Friction thermal sca.    tstar : -0.84399E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30221E-01 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.25404E-03   0.47204E+01 0.19456E+03 
c  Velocity[X]                                      0.19347E+01 
c  Velocity[Y]                                      0.27856E+01 
c  Velocity[Z]                                      0.25903E-29 
c  Pressure     0.12592E-06     554   0.94935E-08   0.12201E+00 0.18795E+04 
c  nu_tilda     0.82256E-05      33   0.13687E-04   0.71664E-06 0.21490E+03 
c  TempC        0.43631E+02      27   0.25372E-03   0.37912E+01 0.23719E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1561          9.3252          4.5729          4.5729
v  Velocity[Y]            -2.9704          7.1637         0.24167         0.24167
v  Velocity[Z]       -6.9287e-015     7.1869e-015    -1.4969e-017    -1.4969e-017
v  ǁVelocityǁ         0.0011644           9.327          5.0667          5.0667
v  Pressure               -24.038          28.794           1.459           1.459
v  nu_tilda           4.4039e-007       0.0044226       0.0017778       0.0017778
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc            3.307e-014       0.0052119         0.00209         0.00209
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2524:        0.22610E+01

===============================================================


 INSTANT    0.252500000E+04   TIME STEP NUMBER            2525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10499E-01 0.88989E+00
   Friction velocity        uk    :  0.10499E-01 0.88989E+00
   Dimensionless distance   yplus :  0.84523E-01 0.71642E+01
   Friction thermal sca.    tstar : -0.79702E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63064E-01 0.53453E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.22077E-03   0.47471E+01 0.19494E+03 
c  Velocity[X]                                      0.19519E+01 
c  Velocity[Y]                                      0.27952E+01 
c  Velocity[Z]                                      0.12519E-29 
c  Pressure     0.12311E-06     584   0.94879E-08   0.11903E+00 0.20437E+04 
c  nu_tilda     0.82270E-05      33   0.32266E-05   0.71661E-06 0.21488E+03 
c  TempC        0.43634E+02      27   0.31087E-03   0.37058E+01 0.22351E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1577          9.3238          4.5729          4.5729
v  Velocity[Y]            -2.9699          7.1915         0.24171         0.24171
v  Velocity[Z]       -6.9287e-015     7.1639e-015    -1.4967e-017    -1.4967e-017
v  ǁVelocityǁ        0.00065758          9.3256          5.0665          5.0665
v  Pressure               -23.975           29.03          1.5534          1.5534
v  nu_tilda           4.4035e-007       0.0044231        0.001778        0.001778
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3091e-014       0.0052125       0.0020901       0.0020901
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2525:        0.23360E+01

===============================================================


 INSTANT    0.252600000E+04   TIME STEP NUMBER            2526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51494E-02 0.89117E+00
   Friction velocity        uk    :  0.51494E-02 0.89117E+00
   Dimensionless distance   yplus :  0.41456E-01 0.71746E+01
   Friction thermal sca.    tstar : -0.74502E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30931E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24024E-03   0.47295E+01 0.19474E+03 
c  Velocity[X]                                      0.19288E+01 
c  Velocity[Y]                                      0.28007E+01 
c  Velocity[Z]                                      0.14580E-29 
c  Pressure     0.11310E-06     536   0.97667E-08   0.10942E+00 0.10934E+04 
c  nu_tilda     0.82284E-05      33   0.13683E-04   0.71664E-06 0.21487E+03 
c  TempC        0.43637E+02      27   0.28450E-03   0.52929E+01 0.24805E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1592          9.3223          4.5729          4.5729
v  Velocity[Y]            -2.9693          7.1975         0.24175         0.24175
v  Velocity[Z]       -6.9287e-015     7.2093e-015     -1.497e-017     -1.497e-017
v  ǁVelocityǁ         0.0010417          9.3242          5.0663          5.0663
v  Pressure               -24.032          28.945          1.5037          1.5037
v  nu_tilda           4.4021e-007       0.0044236       0.0017781       0.0017781
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3079e-014        0.005213       0.0020903       0.0020903
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2526:        0.22200E+01

===============================================================


 INSTANT    0.252700000E+04   TIME STEP NUMBER            2527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.83246E-02 0.89070E+00
   Friction velocity        uk    :  0.83246E-02 0.89070E+00
   Dimensionless distance   yplus :  0.67018E-01 0.71708E+01
   Friction thermal sca.    tstar : -0.71381E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50003E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23063E-03   0.47284E+01 0.19452E+03 
c  Velocity[X]                                      0.19524E+01 
c  Velocity[Y]                                      0.27760E+01 
c  Velocity[Z]                                      0.30822E-29 
c  Pressure     0.13702E-06     506   0.95296E-08   0.13190E+00 0.78450E+03 
c  nu_tilda     0.82298E-05      33   0.31949E-05   0.71662E-06 0.21486E+03 
c  TempC        0.43640E+02      27   0.24645E-03   0.69582E+01 0.28221E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1608          9.3209          4.5729          4.5729
v  Velocity[Y]            -2.9687          7.1671         0.24179         0.24179
v  Velocity[Z]       -6.9287e-015     7.1986e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ         0.0022798          9.3228          5.0661          5.0661
v  Pressure               -23.961          28.899          1.5397          1.5397
v  nu_tilda           4.4019e-007       0.0044241       0.0017782       0.0017782
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3037e-014       0.0052137       0.0020904       0.0020904
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2527:        0.21630E+01

===============================================================


 INSTANT    0.252800000E+04   TIME STEP NUMBER            2528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13914E-01 0.88945E+00
   Friction velocity        uk    :  0.13914E-01 0.88945E+00
   Dimensionless distance   yplus :  0.11202E+00 0.71607E+01
   Friction thermal sca.    tstar : -0.66296E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83576E-01 0.53427E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23726E-03   0.47242E+01 0.19460E+03 
c  Velocity[X]                                      0.19513E+01 
c  Velocity[Y]                                      0.27728E+01 
c  Velocity[Z]                                      0.89312E-30 
c  Pressure     0.10865E-06     458   0.98863E-08   0.10526E+00 0.58332E+03 
c  nu_tilda     0.82312E-05      33   0.13685E-04   0.71661E-06 0.21485E+03 
c  TempC        0.43643E+02      26   0.32481E-03   0.58720E+01 0.26965E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1622          9.3195          4.5729          4.5729
v  Velocity[Y]            -2.9681          7.1877         0.24183         0.24183
v  Velocity[Z]       -6.9287e-015     7.2276e-015    -1.4971e-017    -1.4971e-017
v  ǁVelocityǁ         0.0028628          9.3214          5.0659          5.0659
v  Pressure               -24.024           28.94          1.5177          1.5177
v  nu_tilda           4.4023e-007       0.0044246       0.0017783       0.0017783
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3031e-014       0.0052143       0.0020906       0.0020906
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2528:        0.20410E+01

===============================================================


 INSTANT    0.252900000E+04   TIME STEP NUMBER            2529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12705E-01 0.89061E+00
   Friction velocity        uk    :  0.12705E-01 0.89061E+00
   Dimensionless distance   yplus :  0.10229E+00 0.71700E+01
   Friction thermal sca.    tstar : -0.64596E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76318E-01 0.53496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23837E-03   0.47233E+01 0.19463E+03 
c  Velocity[X]                                      0.19362E+01 
c  Velocity[Y]                                      0.27871E+01 
c  Velocity[Z]                                      0.26289E-29 
c  Pressure     0.11947E-06     489   0.99743E-08   0.11712E+00 0.87363E+03 
c  nu_tilda     0.82327E-05      33   0.31696E-05   0.71657E-06 0.21483E+03 
c  TempC        0.43646E+02      26   0.31056E-03   0.54356E+01 0.27978E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1638          9.3181          4.5729          4.5729
v  Velocity[Y]            -2.9674          7.1668         0.24186         0.24186
v  Velocity[Z]       -6.9287e-015     7.1786e-015    -1.4966e-017    -1.4966e-017
v  ǁVelocityǁ         0.0030385            9.32          5.0656          5.0656
v  Pressure               -23.954           28.94          1.5641          1.5641
v  nu_tilda           4.4031e-007       0.0044251       0.0017785       0.0017785
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3045e-014       0.0052149       0.0020907       0.0020907
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2529:        0.21130E+01

===============================================================


 INSTANT    0.253000000E+04   TIME STEP NUMBER            2530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57914E-02 0.88967E+00
   Friction velocity        uk    :  0.57914E-02 0.88967E+00
   Dimensionless distance   yplus :  0.46625E-01 0.71625E+01
   Friction thermal sca.    tstar : -0.61138E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34787E-01 0.53440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.19785E-03   0.47227E+01 0.19487E+03 
c  Velocity[X]                                      0.19376E+01 
c  Velocity[Y]                                      0.27851E+01 
c  Velocity[Z]                                      0.94060E-30 
c  Pressure     0.12833E-06     490   0.96303E-08   0.12292E+00 0.68818E+03 
c  nu_tilda     0.82341E-05      33   0.13677E-04   0.71661E-06 0.21483E+03 
c  TempC        0.43649E+02      26   0.23374E-03   0.71761E+01 0.28845E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1652          9.3167          4.5729          4.5729
v  Velocity[Y]            -2.9668          7.1864          0.2419          0.2419
v  Velocity[Z]       -6.9287e-015     7.1557e-015    -1.4966e-017    -1.4966e-017
v  ǁVelocityǁ         0.0027441          9.3186          5.0654          5.0654
v  Pressure               -24.013          28.932          1.5332          1.5332
v  nu_tilda           4.4033e-007       0.0044256       0.0017785       0.0017785
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3067e-014       0.0052155       0.0020908       0.0020908
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2530:        0.21330E+01

===============================================================


 INSTANT    0.253100000E+04   TIME STEP NUMBER            2531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.40344E-02 0.89142E+00
   Friction velocity        uk    :  0.40344E-02 0.89142E+00
   Dimensionless distance   yplus :  0.32479E-01 0.71766E+01
   Friction thermal sca.    tstar : -0.60053E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24233E-01 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.27023E-03   0.47126E+01 0.19475E+03 
c  Velocity[X]                                      0.19393E+01 
c  Velocity[Y]                                      0.27734E+01 
c  Velocity[Z]                                      0.15652E-29 
c  Pressure     0.12346E-06     505   0.99587E-08   0.11890E+00 0.12440E+04 
c  nu_tilda     0.82355E-05      33   0.31284E-05   0.71661E-06 0.21482E+03 
c  TempC        0.43652E+02      27   0.31413E-03   0.43736E+01 0.24060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1667          9.3152          4.5729          4.5729
v  Velocity[Y]            -2.9663             7.2         0.24193         0.24193
v  Velocity[Z]       -6.9287e-015     7.2232e-015    -1.4968e-017    -1.4968e-017
v  ǁVelocityǁ          0.001863          9.3172          5.0652          5.0652
v  Pressure               -23.948          29.038          1.5965          1.5965
v  nu_tilda           4.4031e-007       0.0044261       0.0017787       0.0017787
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3074e-014        0.005216        0.002091        0.002091
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2531:        0.21610E+01

===============================================================


 INSTANT    0.253200000E+04   TIME STEP NUMBER            2532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12225E-01 0.89105E+00
   Friction velocity        uk    :  0.12225E-01 0.89105E+00
   Dimensionless distance   yplus :  0.98419E-01 0.71735E+01
   Friction thermal sca.    tstar : -0.57066E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73432E-01 0.53523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23858E-03   0.47569E+01 0.19491E+03 
c  Velocity[X]                                      0.19649E+01 
c  Velocity[Y]                                      0.27920E+01 
c  Velocity[Z]                                      0.27470E-29 
c  Pressure     0.12488E-06     521   0.98122E-08   0.12230E+00 0.15584E+04 
c  nu_tilda     0.82369E-05      33   0.13680E-04   0.71662E-06 0.21480E+03 
c  TempC        0.43655E+02      27   0.29839E-03   0.55529E+01 0.27417E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.168          9.3138          4.5729          4.5729
v  Velocity[Y]            -2.9657          7.1699         0.24197         0.24197
v  Velocity[Z]       -6.9287e-015     7.1948e-015    -1.4971e-017    -1.4971e-017
v  ǁVelocityǁ         0.0014507          9.3157           5.065           5.065
v  Pressure               -24.007          28.864          1.5298          1.5298
v  nu_tilda           4.4033e-007       0.0044266       0.0017788       0.0017788
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3066e-014       0.0052166       0.0020911       0.0020911
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2532:        0.21860E+01

===============================================================


 INSTANT    0.253300000E+04   TIME STEP NUMBER            2533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72540E-02 0.88960E+00
   Friction velocity        uk    :  0.72540E-02 0.88960E+00
   Dimensionless distance   yplus :  0.58400E-01 0.71619E+01
   Friction thermal sca.    tstar : -0.57610E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43573E-01 0.53436E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23207E-03   0.47186E+01 0.19469E+03 
c  Velocity[X]                                      0.19462E+01 
c  Velocity[Y]                                      0.27724E+01 
c  Velocity[Z]                                      0.77719E-30 
c  Pressure     0.11944E-06     520   0.93039E-08   0.11389E+00 0.16238E+04 
c  nu_tilda     0.82383E-05      33   0.31087E-05   0.71658E-06 0.21479E+03 
c  TempC        0.43658E+02      27   0.30384E-03   0.62505E+01 0.28666E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1695          9.3124          4.5729          4.5729
v  Velocity[Y]            -2.9651          7.1875           0.242           0.242
v  Velocity[Z]       -6.9287e-015     7.1325e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ         0.0016895          9.3143          5.0648          5.0648
v  Pressure                -23.94          29.028          1.6094          1.6094
v  nu_tilda           4.4037e-007       0.0044271        0.001779        0.001779
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3075e-014       0.0052172       0.0020912       0.0020912
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2533:        0.21850E+01

===============================================================


 INSTANT    0.253400000E+04   TIME STEP NUMBER            2534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.87902E-02 0.89074E+00
   Friction velocity        uk    :  0.87902E-02 0.89074E+00
   Dimensionless distance   yplus :  0.70767E-01 0.71711E+01
   Friction thermal sca.    tstar : -0.57398E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52800E-01 0.53504E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.25148E-03   0.47321E+01 0.19472E+03 
c  Velocity[X]                                      0.19707E+01 
c  Velocity[Y]                                      0.27614E+01 
c  Velocity[Z]                                      0.24901E-29 
c  Pressure     0.11768E-06     538   0.95292E-08   0.11572E+00 0.15590E+04 
c  nu_tilda     0.82397E-05      33   0.13672E-04   0.71659E-06 0.21478E+03 
c  TempC        0.43661E+02      27   0.28090E-03   0.50013E+01 0.25311E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1709           9.311          4.5729          4.5729
v  Velocity[Y]            -2.9644          7.1666         0.24204         0.24204
v  Velocity[Z]       -6.9287e-015      7.047e-015    -1.4969e-017    -1.4969e-017
v  ǁVelocityǁ         0.0024052          9.3129          5.0646          5.0646
v  Pressure               -23.999          28.856          1.5422          1.5422
v  nu_tilda           4.4039e-007       0.0044276        0.001779        0.001779
v  TempC                       21           73.05          22.059          22.059
v  TurbVisc           3.3085e-014       0.0052178       0.0020914       0.0020914
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2534:        0.23460E+01

===============================================================


 INSTANT    0.253500000E+04   TIME STEP NUMBER            2535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.98243E-02 0.88997E+00
   Friction velocity        uk    :  0.98243E-02 0.88997E+00
   Dimensionless distance   yplus :  0.79092E-01 0.71649E+01
   Friction thermal sca.    tstar : -0.62071E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59012E-01 0.53458E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23468E-03   0.47354E+01 0.19501E+03 
c  Velocity[X]                                      0.19436E+01 
c  Velocity[Y]                                      0.27918E+01 
c  Velocity[Z]                                      0.12985E-29 
c  Pressure     0.11379E-06     538   0.93711E-08   0.10919E+00 0.19525E+04 
c  nu_tilda     0.82411E-05      33   0.30676E-05   0.71657E-06 0.21476E+03 
c  TempC        0.43664E+02      27   0.33015E-03   0.39750E+01 0.22460E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1724          9.3095          4.5729          4.5729
v  Velocity[Y]            -2.9637          7.1906         0.24207         0.24207
v  Velocity[Z]       -6.9287e-015     7.1016e-015    -1.4965e-017    -1.4965e-017
v  ǁVelocityǁ          0.003362          9.3115          5.0643          5.0643
v  Pressure               -23.935          29.079          1.6336          1.6336
v  nu_tilda           4.4036e-007       0.0044281       0.0017792       0.0017792
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc            3.309e-014       0.0052184       0.0020915       0.0020915
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2535:        0.24370E+01

===============================================================


 INSTANT    0.253600000E+04   TIME STEP NUMBER            2536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17739E-01 0.89101E+00
   Friction velocity        uk    :  0.17739E-01 0.89101E+00
   Dimensionless distance   yplus :  0.14281E+00 0.71732E+01
   Friction thermal sca.    tstar : -0.58275E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10655E+00 0.53520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.24910E-03   0.46968E+01 0.19470E+03 
c  Velocity[X]                                      0.19264E+01 
c  Velocity[Y]                                      0.27703E+01 
c  Velocity[Z]                                      0.13075E-29 
c  Pressure     0.11930E-06     520   0.96487E-08   0.11393E+00 0.13374E+04 
c  nu_tilda     0.82425E-05      33   0.13672E-04   0.71660E-06 0.21476E+03 
c  TempC        0.43667E+02      28   0.27603E-03   0.46246E+01 0.24755E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1739          9.3081          4.5729          4.5729
v  Velocity[Y]            -2.9632           7.193          0.2421          0.2421
v  Velocity[Z]       -6.9287e-015      7.145e-015    -1.4969e-017    -1.4969e-017
v  ǁVelocityǁ          0.001504            9.31          5.0641          5.0641
v  Pressure               -23.992          28.944          1.5746          1.5746
v  nu_tilda           4.4034e-007       0.0044286       0.0017792       0.0017792
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3082e-014        0.005219       0.0020917       0.0020917
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2536:        0.23840E+01

===============================================================


 INSTANT    0.253700000E+04   TIME STEP NUMBER            2537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93523E-02 0.89083E+00
   Friction velocity        uk    :  0.93523E-02 0.89083E+00
   Dimensionless distance   yplus :  0.75293E-01 0.71718E+01
   Friction thermal sca.    tstar : -0.57466E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56177E-01 0.53510E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10714E-01      33   0.23119E-03   0.47056E+01 0.19455E+03 
c  Velocity[X]                                      0.19557E+01 
c  Velocity[Y]                                      0.27500E+01 
c  Velocity[Z]                                      0.29573E-29 
c  Pressure     0.12247E-06     474   0.97436E-08   0.12081E+00 0.85632E+03 
c  nu_tilda     0.82438E-05      33   0.30445E-05   0.71660E-06 0.21475E+03 
c  TempC        0.43670E+02      27   0.22427E-03   0.40099E+01 0.24108E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1754          9.3066          4.5729          4.5729
v  Velocity[Y]            -2.9626          7.1696         0.24213         0.24213
v  Velocity[Z]       -6.9287e-015      7.019e-015    -1.4972e-017    -1.4972e-017
v  ǁVelocityǁ         0.0030474          9.3086          5.0639          5.0639
v  Pressure               -23.926          28.959          1.6199          1.6199
v  nu_tilda           4.4038e-007       0.0044291       0.0017794       0.0017794
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3078e-014       0.0052195       0.0020918       0.0020918
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2537:        0.22820E+01

===============================================================


 INSTANT    0.253800000E+04   TIME STEP NUMBER            2538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.50130E-02 0.88938E+00
   Friction velocity        uk    :  0.50130E-02 0.88938E+00
   Dimensionless distance   yplus :  0.40358E-01 0.71601E+01
   Friction thermal sca.    tstar : -0.58176E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30112E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.27121E-03   0.47079E+01 0.19471E+03 
c  Velocity[X]                                      0.19331E+01 
c  Velocity[Y]                                      0.27748E+01 
c  Velocity[Z]                                      0.80697E-30 
c  Pressure     0.10456E-06     521   0.93318E-08   0.10125E+00 0.64468E+03 
c  nu_tilda     0.82452E-05      33   0.13668E-04   0.71663E-06 0.21474E+03 
c  TempC        0.43673E+02      27   0.37009E-03   0.29184E+01 0.20868E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1768          9.3052          4.5729          4.5729
v  Velocity[Y]             -2.962          7.1882         0.24216         0.24216
v  Velocity[Z]       -6.9287e-015     6.9856e-015     -1.497e-017     -1.497e-017
v  ǁVelocityǁ         0.0026983          9.3072          5.0637          5.0637
v  Pressure               -23.989          28.973          1.5903          1.5903
v  nu_tilda           4.4039e-007       0.0044296       0.0017795       0.0017795
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3089e-014       0.0052201       0.0020919       0.0020919
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2538:        0.23330E+01

===============================================================


 INSTANT    0.253900000E+04   TIME STEP NUMBER            2539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96402E-02 0.89049E+00
   Friction velocity        uk    :  0.96402E-02 0.89049E+00
   Dimensionless distance   yplus :  0.77610E-01 0.71690E+01
   Friction thermal sca.    tstar : -0.57598E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57906E-01 0.53489E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.23362E-03   0.47437E+01 0.19481E+03 
c  Velocity[X]                                      0.19839E+01 
c  Velocity[Y]                                      0.27598E+01 
c  Velocity[Z]                                      0.24032E-29 
c  Pressure     0.15266E-06     504   0.96220E-08   0.14605E+00 0.81388E+03 
c  nu_tilda     0.82466E-05      33   0.30080E-05   0.71657E-06 0.21472E+03 
c  TempC        0.43676E+02      27   0.30496E-03   0.60893E+01 0.25997E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1782          9.3038          4.5729          4.5729
v  Velocity[Y]            -2.9614          7.1648         0.24219         0.24219
v  Velocity[Z]       -6.9287e-015      7.056e-015    -1.4968e-017    -1.4968e-017
v  ǁVelocityǁ        0.00078103          9.3058          5.0635          5.0635
v  Pressure               -23.917          28.936            1.63            1.63
v  nu_tilda           4.4045e-007       0.0044301       0.0017796       0.0017796
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3091e-014       0.0052207       0.0020921       0.0020921
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2539:        0.22670E+01

===============================================================


 INSTANT    0.254000000E+04   TIME STEP NUMBER            2540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57060E-02 0.89002E+00
   Friction velocity        uk    :  0.57060E-02 0.89002E+00
   Dimensionless distance   yplus :  0.45937E-01 0.71653E+01
   Friction thermal sca.    tstar : -0.58383E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34274E-01 0.53461E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.18601E-03   0.47305E+01 0.19508E+03 
c  Velocity[X]                                      0.19615E+01 
c  Velocity[Y]                                      0.27690E+01 
c  Velocity[Z]                                      0.13972E-29 
c  Pressure     0.11866E-06     472   0.98797E-08   0.11556E+00 0.59146E+03 
c  nu_tilda     0.82480E-05      33   0.13666E-04   0.71658E-06 0.21470E+03 
c  TempC        0.43679E+02      28   0.29331E-03   0.42481E+01 0.22954E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1797          9.3023          4.5729          4.5729
v  Velocity[Y]            -2.9607          7.1898         0.24222         0.24222
v  Velocity[Z]       -6.9287e-015     6.9638e-015    -1.4967e-017    -1.4967e-017
v  ǁVelocityǁ         0.0014409          9.3043          5.0633          5.0633
v  Pressure               -23.982          28.998          1.6118          1.6118
v  nu_tilda           4.4041e-007       0.0044306       0.0017797       0.0017797
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc            3.311e-014       0.0052213       0.0020922       0.0020922
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2540:        0.20940E+01

===============================================================


 INSTANT    0.254100000E+04   TIME STEP NUMBER            2541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.61026E-02 0.89138E+00
   Friction velocity        uk    :  0.61026E-02 0.89138E+00
   Dimensionless distance   yplus :  0.49130E-01 0.71763E+01
   Friction thermal sca.    tstar : -0.57217E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36657E-01 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.24642E-03   0.46945E+01 0.19477E+03 
c  Velocity[X]                                      0.19235E+01 
c  Velocity[Y]                                      0.27710E+01 
c  Velocity[Z]                                      0.14242E-29 
c  Pressure     0.10126E-06     521   0.96477E-08   0.98063E-01 0.10598E+04 
c  nu_tilda     0.82494E-05      33   0.29796E-05   0.71657E-06 0.21470E+03 
c  TempC        0.43681E+02      27   0.25234E-03   0.40160E+01 0.22574E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1811          9.3009          4.5729          4.5729
v  Velocity[Y]              -2.96          7.2003         0.24224         0.24224
v  Velocity[Z]       -6.9287e-015     6.9792e-015    -1.4966e-017    -1.4966e-017
v  ǁVelocityǁ         0.0033909          9.3029          5.0631          5.0631
v  Pressure               -23.915          29.071          1.6671          1.6671
v  nu_tilda           4.4028e-007        0.004431       0.0017799       0.0017799
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3098e-014       0.0052219       0.0020923       0.0020923
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2541:        0.22050E+01

===============================================================


 INSTANT    0.254200000E+04   TIME STEP NUMBER            2542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15762E-01 0.89085E+00
   Friction velocity        uk    :  0.15762E-01 0.89085E+00
   Dimensionless distance   yplus :  0.12690E+00 0.71720E+01
   Friction thermal sca.    tstar : -0.57135E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94679E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.21356E-03   0.47293E+01 0.19487E+03 
c  Velocity[X]                                      0.19674E+01 
c  Velocity[Y]                                      0.27619E+01 
c  Velocity[Z]                                      0.27759E-29 
c  Pressure     0.13095E-06     553   0.97204E-08   0.12676E+00 0.18068E+04 
c  nu_tilda     0.82507E-05      33   0.13662E-04   0.71660E-06 0.21469E+03 
c  TempC        0.43684E+02      27   0.25752E-03   0.35900E+01 0.21105E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1825          9.2995          4.5729          4.5729
v  Velocity[Y]            -2.9595          7.1681         0.24227         0.24227
v  Velocity[Z]       -6.9287e-015     7.0175e-015    -1.4969e-017    -1.4969e-017
v  ǁVelocityǁ         0.0026362          9.3014          5.0628          5.0628
v  Pressure               -23.973          28.856          1.5911          1.5911
v  nu_tilda           4.4025e-007       0.0044315       0.0017799       0.0017799
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3058e-014       0.0052224       0.0020925       0.0020925
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2542:        0.22620E+01

===============================================================


 INSTANT    0.254300000E+04   TIME STEP NUMBER            2543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89512E-02 0.88974E+00
   Friction velocity        uk    :  0.89512E-02 0.88974E+00
   Dimensionless distance   yplus :  0.72063E-01 0.71631E+01
   Friction thermal sca.    tstar : -0.62098E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53767E-01 0.53444E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.23729E-03   0.46985E+01 0.19476E+03 
c  Velocity[X]                                      0.19478E+01 
c  Velocity[Y]                                      0.27507E+01 
c  Velocity[Z]                                      0.11122E-29 
c  Pressure     0.11390E-06     553   0.96056E-08   0.11012E+00 0.19676E+04 
c  nu_tilda     0.82521E-05      33   0.29459E-05   0.71658E-06 0.21468E+03 
c  TempC        0.43687E+02      26   0.32667E-03   0.48037E+01 0.26184E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1838           9.298          4.5729          4.5729
v  Velocity[Y]            -2.9589          7.1908          0.2423          0.2423
v  Velocity[Z]       -6.9287e-015     6.8955e-015     -1.497e-017     -1.497e-017
v  ǁVelocityǁ          0.003184             9.3          5.0626          5.0626
v  Pressure               -23.914          29.087          1.6802          1.6802
v  nu_tilda           4.4023e-007        0.004432       0.0017801       0.0017801
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3048e-014        0.005223       0.0020926       0.0020926
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2543:        0.22620E+01

===============================================================


 INSTANT    0.254400000E+04   TIME STEP NUMBER            2544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10421E-01 0.89054E+00
   Friction velocity        uk    :  0.10421E-01 0.89054E+00
   Dimensionless distance   yplus :  0.83896E-01 0.71695E+01
   Friction thermal sca.    tstar : -0.58437E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62596E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.24507E-03   0.47117E+01 0.19479E+03 
c  Velocity[X]                                      0.19489E+01 
c  Velocity[Y]                                      0.27627E+01 
c  Velocity[Z]                                      0.24838E-29 
c  Pressure     0.11562E-06     568   0.94304E-08   0.11332E+00 0.17386E+04 
c  nu_tilda     0.82535E-05      33   0.13659E-04   0.71658E-06 0.21466E+03 
c  TempC        0.43690E+02      27   0.28628E-03   0.62773E+01 0.29314E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1852          9.2966          4.5729          4.5729
v  Velocity[Y]            -2.9583          7.1667         0.24233         0.24233
v  Velocity[Z]       -6.9287e-015     6.8583e-015    -1.4966e-017    -1.4966e-017
v  ǁVelocityǁ         0.0018825          9.2986          5.0624          5.0624
v  Pressure               -23.974          28.888          1.6053          1.6053
v  nu_tilda           4.4028e-007       0.0044325       0.0017801       0.0017801
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3045e-014       0.0052235       0.0020927       0.0020927
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2544:        0.23000E+01

===============================================================


 INSTANT    0.254500000E+04   TIME STEP NUMBER            2545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12104E-01 0.88969E+00
   Friction velocity        uk    :  0.12104E-01 0.88969E+00
   Dimensionless distance   yplus :  0.97442E-01 0.71626E+01
   Friction thermal sca.    tstar : -0.58258E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72703E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.25358E-03   0.47330E+01 0.19508E+03 
c  Velocity[X]                                      0.19728E+01 
c  Velocity[Y]                                      0.27602E+01 
c  Velocity[Z]                                      0.10285E-29 
c  Pressure     0.13617E-06     504   0.97704E-08   0.12983E+00 0.16622E+04 
c  nu_tilda     0.82548E-05      33   0.29074E-05   0.71654E-06 0.21465E+03 
c  TempC        0.43693E+02      26   0.30226E-03   0.56403E+01 0.25095E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1866          9.2951          4.5729          4.5729
v  Velocity[Y]            -2.9576          7.1879         0.24235         0.24235
v  Velocity[Z]       -6.9287e-015     6.9229e-015    -1.4961e-017    -1.4961e-017
v  ǁVelocityǁ         0.0032494          9.2971          5.0622          5.0622
v  Pressure               -23.912          29.064          1.6844          1.6844
v  nu_tilda           4.4028e-007        0.004433       0.0017803       0.0017803
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3058e-014       0.0052241       0.0020928       0.0020928
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2545:        0.21420E+01

===============================================================


 INSTANT    0.254600000E+04   TIME STEP NUMBER            2546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13905E-01 0.89105E+00
   Friction velocity        uk    :  0.13905E-01 0.89105E+00
   Dimensionless distance   yplus :  0.11194E+00 0.71736E+01
   Friction thermal sca.    tstar : -0.59088E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83523E-01 0.53523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.24975E-03   0.47229E+01 0.19498E+03 
c  Velocity[X]                                      0.19770E+01 
c  Velocity[Y]                                      0.27459E+01 
c  Velocity[Z]                                      0.13586E-29 
c  Pressure     0.12079E-06     506   0.92914E-08   0.11721E+00 0.10478E+04 
c  nu_tilda     0.82562E-05      33   0.13659E-04   0.71653E-06 0.21463E+03 
c  TempC        0.43696E+02      26   0.28615E-03   0.46816E+01 0.25168E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.188          9.2937          4.5729          4.5729
v  Velocity[Y]            -2.9569          7.1969         0.24238         0.24238
v  Velocity[Z]       -6.9287e-015     6.8812e-015    -1.4964e-017    -1.4964e-017
v  ǁVelocityǁ         0.0025844          9.2957           5.062           5.062
v  Pressure               -23.975          28.987          1.6335          1.6335
v  nu_tilda            4.402e-007       0.0044334       0.0017803       0.0017803
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3057e-014       0.0052247        0.002093        0.002093
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2546:        0.21730E+01

===============================================================


 INSTANT    0.254700000E+04   TIME STEP NUMBER            2547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.79918E-02 0.89075E+00
   Friction velocity        uk    :  0.79918E-02 0.89075E+00
   Dimensionless distance   yplus :  0.64339E-01 0.71711E+01
   Friction thermal sca.    tstar : -0.60659E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48004E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10713E-01      33   0.22765E-03   0.47255E+01 0.19491E+03 
c  Velocity[X]                                      0.19622E+01 
c  Velocity[Y]                                      0.27633E+01 
c  Velocity[Z]                                      0.27381E-29 
c  Pressure     0.12391E-06     488   0.98526E-08   0.12089E+00 0.75403E+03 
c  nu_tilda     0.82575E-05      33   0.28830E-05   0.71653E-06 0.21462E+03 
c  TempC        0.43698E+02      27   0.29747E-03   0.44625E+01 0.25140E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1894          9.2922          4.5729          4.5729
v  Velocity[Y]            -2.9562          7.1696          0.2424          0.2424
v  Velocity[Z]       -6.9287e-015     6.8331e-015    -1.4964e-017    -1.4964e-017
v  ǁVelocityǁ         0.0024037          9.2942          5.0618          5.0618
v  Pressure               -23.912          28.986          1.6719          1.6719
v  nu_tilda           4.4023e-007       0.0044339       0.0017805       0.0017805
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3036e-014       0.0052253       0.0020931       0.0020931
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2547:        0.21270E+01

===============================================================


 INSTANT    0.254800000E+04   TIME STEP NUMBER            2548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10141E-01 0.88922E+00
   Friction velocity        uk    :  0.10141E-01 0.88922E+00
   Dimensionless distance   yplus :  0.81642E-01 0.71588E+01
   Friction thermal sca.    tstar : -0.64366E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60914E-01 0.53413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.23298E-03   0.46956E+01 0.19483E+03 
c  Velocity[X]                                      0.19488E+01 
c  Velocity[Y]                                      0.27469E+01 
c  Velocity[Z]                                      0.82927E-30 
c  Pressure     0.11588E-06     490   0.91869E-08   0.11070E+00 0.81958E+03 
c  nu_tilda     0.82589E-05      33   0.13655E-04   0.71660E-06 0.21462E+03 
c  TempC        0.43701E+02      26   0.34388E-03   0.55725E+01 0.25340E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1908          9.2908          4.5729          4.5729
v  Velocity[Y]            -2.9557          7.1846         0.24243         0.24243
v  Velocity[Z]       -6.9287e-015        6.9e-015    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ         0.0024783          9.2928          5.0616          5.0616
v  Pressure               -23.979          28.955          1.6298          1.6298
v  nu_tilda           4.4025e-007       0.0044344       0.0017806       0.0017806
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3042e-014       0.0052258       0.0020932       0.0020932
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2548:        0.21270E+01

===============================================================


 INSTANT    0.254900000E+04   TIME STEP NUMBER            2549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14416E-01 0.89057E+00
   Friction velocity        uk    :  0.14416E-01 0.89057E+00
   Dimensionless distance   yplus :  0.11606E+00 0.71697E+01
   Friction thermal sca.    tstar : -0.66114E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86594E-01 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.24910E-03   0.47091E+01 0.19479E+03 
c  Velocity[X]                                      0.19756E+01 
c  Velocity[Y]                                      0.27335E+01 
c  Velocity[Z]                                      0.24870E-29 
c  Pressure     0.11815E-06     490   0.99096E-08   0.11610E+00 0.87014E+03 
c  nu_tilda     0.82602E-05      33   0.28336E-05   0.71657E-06 0.21461E+03 
c  TempC        0.43704E+02      27   0.23957E-03   0.47246E+01 0.24740E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1922          9.2893          4.5729          4.5729
v  Velocity[Y]            -2.9551          7.1666         0.24245         0.24245
v  Velocity[Z]       -6.9287e-015     6.8089e-015    -1.4955e-017    -1.4955e-017
v  ǁVelocityǁ         0.0028404          9.2914          5.0614          5.0614
v  Pressure               -23.912          28.971           1.676           1.676
v  nu_tilda           4.4026e-007       0.0044348       0.0017807       0.0017807
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3049e-014       0.0052264       0.0020934       0.0020934
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2549:        0.23710E+01

===============================================================


 INSTANT    0.255000000E+04   TIME STEP NUMBER            2550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.62141E-02 0.88974E+00
   Friction velocity        uk    :  0.62141E-02 0.88974E+00
   Dimensionless distance   yplus :  0.50028E-01 0.71630E+01
   Friction thermal sca.    tstar : -0.70794E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37326E-01 0.53444E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.19530E-03   0.47198E+01 0.19514E+03 
c  Velocity[X]                                      0.19558E+01 
c  Velocity[Y]                                      0.27640E+01 
c  Velocity[Z]                                      0.11323E-29 
c  Pressure     0.11451E-06     520   0.97839E-08   0.11112E+00 0.63935E+03 
c  nu_tilda     0.82616E-05      33   0.13655E-04   0.71655E-06 0.21459E+03 
c  TempC        0.43707E+02      27   0.28191E-03   0.33860E+01 0.21100E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1936          9.2879          4.5729          4.5729
v  Velocity[Y]            -2.9544          7.1896         0.24247         0.24247
v  Velocity[Z]       -6.9287e-015      6.763e-015    -1.4947e-017    -1.4947e-017
v  ǁVelocityǁ         0.0026832          9.2899          5.0612          5.0612
v  Pressure               -23.983          28.996          1.6455          1.6455
v  nu_tilda           4.4021e-007       0.0044353       0.0017808       0.0017808
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3052e-014       0.0052269       0.0020935       0.0020935
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2550:        0.23680E+01

===============================================================


 INSTANT    0.255100000E+04   TIME STEP NUMBER            2551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.84911E-02 0.89120E+00
   Friction velocity        uk    :  0.84911E-02 0.89120E+00
   Dimensionless distance   yplus :  0.68359E-01 0.71748E+01
   Friction thermal sca.    tstar : -0.71998E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51003E-01 0.53532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.25132E-03   0.46888E+01 0.19479E+03 
c  Velocity[X]                                      0.19463E+01 
c  Velocity[Y]                                      0.27426E+01 
c  Velocity[Z]                                      0.13202E-29 
c  Pressure     0.12462E-06     520   0.99201E-08   0.11857E+00 0.91116E+03 
c  nu_tilda     0.82629E-05      33   0.28144E-05   0.71653E-06 0.21458E+03 
c  TempC        0.43710E+02      27   0.29819E-03   0.35963E+01 0.22865E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1949          9.2864          4.5729          4.5729
v  Velocity[Y]            -2.9538          7.1968          0.2425          0.2425
v  Velocity[Z]       -6.9287e-015     6.7847e-015    -1.4948e-017    -1.4948e-017
v  ǁVelocityǁ         0.0018043          9.2885          5.0609          5.0609
v  Pressure               -23.919          29.044          1.6931          1.6931
v  nu_tilda            4.402e-007       0.0044358       0.0017809       0.0017809
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3037e-014       0.0052275       0.0020936       0.0020936
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2551:        0.21900E+01

===============================================================


 INSTANT    0.255200000E+04   TIME STEP NUMBER            2552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.29281E-03 0.89095E+00
   Friction velocity        uk    :  0.29281E-03 0.89095E+00
   Dimensionless distance   yplus :  0.23573E-02 0.71727E+01
   Friction thermal sca.    tstar : -0.78487E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17588E-02 0.53517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.24524E-03   0.47220E+01 0.19481E+03 
c  Velocity[X]                                      0.19983E+01 
c  Velocity[Y]                                      0.27237E+01 
c  Velocity[Z]                                      0.26805E-29 
c  Pressure     0.13113E-06     553   0.96478E-08   0.12856E+00 0.15525E+04 
c  nu_tilda     0.82642E-05      33   0.13649E-04   0.71654E-06 0.21457E+03 
c  TempC        0.43712E+02      27   0.28264E-03   0.40319E+01 0.23839E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1963           9.285          4.5729          4.5729
v  Velocity[Y]             -2.953          7.1693         0.24252         0.24252
v  Velocity[Z]       -6.9287e-015     6.8794e-015    -1.4945e-017    -1.4945e-017
v  ǁVelocityǁ         0.0027779           9.287          5.0607          5.0607
v  Pressure               -23.983          28.874          1.6228          1.6228
v  nu_tilda           4.4028e-007       0.0044363        0.001781        0.001781
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3035e-014       0.0052281       0.0020937       0.0020937
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2552:        0.22860E+01

===============================================================


 INSTANT    0.255300000E+04   TIME STEP NUMBER            2553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11174E-01 0.88957E+00
   Friction velocity        uk    :  0.11174E-01 0.88957E+00
   Dimensionless distance   yplus :  0.89956E-01 0.71617E+01
   Friction thermal sca.    tstar : -0.82554E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67118E-01 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.23029E-03   0.47000E+01 0.19483E+03 
c  Velocity[X]                                      0.19561E+01 
c  Velocity[Y]                                      0.27439E+01 
c  Velocity[Z]                                      0.80687E-30 
c  Pressure     0.10199E-06     538   0.95812E-08   0.98558E-01 0.16900E+04 
c  nu_tilda     0.82656E-05      33   0.27663E-05   0.71653E-06 0.21456E+03 
c  TempC        0.43715E+02      27   0.31673E-03   0.44435E+01 0.22700E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1976          9.2835          4.5729          4.5729
v  Velocity[Y]            -2.9524          7.1902         0.24254         0.24254
v  Velocity[Z]       -6.9287e-015     6.7517e-015    -1.4942e-017    -1.4942e-017
v  ǁVelocityǁ         0.0011643          9.2856          5.0605          5.0605
v  Pressure               -23.925          29.064          1.7006          1.7006
v  nu_tilda           4.4031e-007       0.0044367       0.0017812       0.0017812
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3058e-014       0.0052286       0.0020939       0.0020939
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2553:        0.22240E+01

===============================================================


 INSTANT    0.255400000E+04   TIME STEP NUMBER            2554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18315E-01 0.89046E+00
   Friction velocity        uk    :  0.18315E-01 0.89046E+00
   Dimensionless distance   yplus :  0.14745E+00 0.71688E+01
   Friction thermal sca.    tstar : -0.91263E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11001E+00 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10712E-01      33   0.24038E-03   0.46886E+01 0.19476E+03 
c  Velocity[X]                                      0.19612E+01 
c  Velocity[Y]                                      0.27274E+01 
c  Velocity[Z]                                      0.23651E-29 
c  Pressure     0.12354E-06     554   0.99105E-08   0.11955E+00 0.17998E+04 
c  nu_tilda     0.82669E-05      33   0.13648E-04   0.71655E-06 0.21455E+03 
c  TempC        0.43718E+02      27   0.27470E-03   0.58247E+01 0.27314E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.1989           9.282          4.5729          4.5729
v  Velocity[Y]            -2.9518          7.1625         0.24256         0.24256
v  Velocity[Z]       -6.9287e-015      6.705e-015    -1.4934e-017    -1.4934e-017
v  ǁVelocityǁ         0.0025973          9.2841          5.0603          5.0603
v  Pressure               -23.989          28.857          1.6215          1.6215
v  nu_tilda           4.4036e-007       0.0044372       0.0017812       0.0017812
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3068e-014       0.0052292        0.002094        0.002094
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2554:        0.22690E+01

===============================================================


 INSTANT    0.255500000E+04   TIME STEP NUMBER            2555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.77407E-02 0.88978E+00
   Friction velocity        uk    :  0.77407E-02 0.88978E+00
   Dimensionless distance   yplus :  0.62318E-01 0.71633E+01
   Friction thermal sca.    tstar : -0.97147E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46496E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.19089E-03   0.47162E+01 0.19516E+03 
c  Velocity[X]                                      0.19775E+01 
c  Velocity[Y]                                      0.27388E+01 
c  Velocity[Z]                                      0.13236E-29 
c  Pressure     0.11622E-06     521   0.99466E-08   0.11184E+00 0.18905E+04 
c  nu_tilda     0.82682E-05      33   0.27412E-05   0.71655E-06 0.21454E+03 
c  TempC        0.43720E+02      26   0.29838E-03   0.41980E+01 0.24304E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2002          9.2806          4.5729          4.5729
v  Velocity[Y]            -2.9512          7.1898         0.24258         0.24258
v  Velocity[Z]       -6.9287e-015     6.8182e-015    -1.4928e-017    -1.4928e-017
v  ǁVelocityǁ         0.0016314          9.2826          5.0601          5.0601
v  Pressure               -23.928          29.073          1.7082          1.7082
v  nu_tilda           4.4035e-007       0.0044376       0.0017814       0.0017814
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3083e-014       0.0052297       0.0020941       0.0020941
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2555:        0.21840E+01

===============================================================


 INSTANT    0.255600000E+04   TIME STEP NUMBER            2556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12671E-01 0.89100E+00
   Friction velocity        uk    :  0.12671E-01 0.89100E+00
   Dimensionless distance   yplus :  0.10201E+00 0.71732E+01
   Friction thermal sca.    tstar : -0.10977E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.76112E-01 0.53520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.23645E-03   0.46838E+01 0.19493E+03 
c  Velocity[X]                                      0.19396E+01 
c  Velocity[Y]                                      0.27442E+01 
c  Velocity[Z]                                      0.13683E-29 
c  Pressure     0.10878E-06     537   0.93361E-08   0.10516E+00 0.12280E+04 
c  nu_tilda     0.82695E-05      33   0.13644E-04   0.71652E-06 0.21452E+03 
c  TempC        0.43723E+02      27   0.28163E-03   0.47744E+01 0.25629E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2015          9.2791          4.5729          4.5729
v  Velocity[Y]            -2.9505          7.1953         0.24261         0.24261
v  Velocity[Z]       -6.9287e-015     6.7823e-015    -1.4926e-017    -1.4926e-017
v  ǁVelocityǁ         0.0034389          9.2812          5.0599          5.0599
v  Pressure               -23.998          28.972          1.6466          1.6466
v  nu_tilda           4.4028e-007       0.0044381       0.0017814       0.0017814
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3081e-014       0.0052302       0.0020942       0.0020942
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2556:        0.22220E+01

===============================================================


 INSTANT    0.255700000E+04   TIME STEP NUMBER            2557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.19069E-01 0.89055E+00
   Friction velocity        uk    :  0.19069E-01 0.89055E+00
   Dimensionless distance   yplus :  0.15352E+00 0.71695E+01
   Friction thermal sca.    tstar : -0.11975E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11454E+00 0.53493E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.25192E-03   0.47109E+01 0.19490E+03 
c  Velocity[X]                                      0.19799E+01 
c  Velocity[Y]                                      0.27310E+01 
c  Velocity[Z]                                      0.25277E-29 
c  Pressure     0.12980E-06     488   0.92509E-08   0.12561E+00 0.68296E+03 
c  nu_tilda     0.82708E-05      33   0.26984E-05   0.71649E-06 0.21450E+03 
c  TempC        0.43726E+02      27   0.32288E-03   0.44128E+01 0.25148E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2028          9.2777          4.5729          4.5729
v  Velocity[Y]            -2.9498          7.1659         0.24263         0.24263
v  Velocity[Z]       -6.9287e-015     6.6535e-015    -1.4927e-017    -1.4927e-017
v  ǁVelocityǁ           0.00304          9.2797          5.0597          5.0597
v  Pressure               -23.934          28.928          1.6765          1.6765
v  nu_tilda           4.4025e-007       0.0044386       0.0017816       0.0017816
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3059e-014       0.0052308       0.0020943       0.0020943
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2557:        0.21230E+01

===============================================================


 INSTANT    0.255800000E+04   TIME STEP NUMBER            2558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14473E-01 0.88937E+00
   Friction velocity        uk    :  0.14473E-01 0.88937E+00
   Dimensionless distance   yplus :  0.11652E+00 0.71600E+01
   Friction thermal sca.    tstar : -0.16264E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86935E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.25172E-03   0.47144E+01 0.19502E+03 
c  Velocity[X]                                      0.19913E+01 
c  Velocity[Y]                                      0.27231E+01 
c  Velocity[Z]                                      0.89213E-30 
c  Pressure     0.12105E-06     490   0.98399E-08   0.11698E+00 0.63567E+03 
c  nu_tilda     0.82722E-05      33   0.13643E-04   0.71652E-06 0.21450E+03 
c  TempC        0.43729E+02      27   0.27345E-03   0.63304E+01 0.28300E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2041          9.2762          4.5729          4.5729
v  Velocity[Y]            -2.9491          7.1867         0.24265         0.24265
v  Velocity[Z]       -6.9287e-015     6.6303e-015     -1.492e-017     -1.492e-017
v  ǁVelocityǁ         0.0024819          9.2783          5.0595          5.0595
v  Pressure               -24.004          28.962          1.6465          1.6465
v  nu_tilda           4.4024e-007       0.0044391       0.0017816       0.0017816
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3049e-014       0.0052313       0.0020945       0.0020945
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2558:        0.21220E+01

===============================================================


 INSTANT    0.255900000E+04   TIME STEP NUMBER            2559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.40203E-02 0.89054E+00
   Friction velocity        uk    :  0.40203E-02 0.89054E+00
   Dimensionless distance   yplus :  0.32366E-01 0.71695E+01
   Friction thermal sca.    tstar : -0.19136E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24149E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10711E-01      33   0.22825E-03   0.46974E+01 0.19487E+03 
c  Velocity[X]                                      0.19659E+01 
c  Velocity[Y]                                      0.27315E+01 
c  Velocity[Z]                                      0.24017E-29 
c  Pressure     0.12197E-06     489   0.94764E-08   0.11858E+00 0.69886E+03 
c  nu_tilda     0.82735E-05      33   0.26635E-05   0.71652E-06 0.21449E+03 
c  TempC        0.43731E+02      27   0.25213E-03   0.67401E+01 0.26660E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2054          9.2747          4.5729          4.5729
v  Velocity[Y]            -2.9485          7.1657         0.24267         0.24267
v  Velocity[Z]       -6.9287e-015     6.7632e-015    -1.4915e-017    -1.4915e-017
v  ǁVelocityǁ         0.0012785          9.2768          5.0593          5.0593
v  Pressure               -23.943          28.947           1.681           1.681
v  nu_tilda           4.4029e-007       0.0044395       0.0017818       0.0017818
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3047e-014       0.0052319       0.0020946       0.0020946
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2559:        0.21280E+01

===============================================================


 INSTANT    0.256000000E+04   TIME STEP NUMBER            2560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42165E-02 0.88965E+00
   Friction velocity        uk    :  0.42165E-02 0.88965E+00
   Dimensionless distance   yplus :  0.33946E-01 0.71623E+01
   Friction thermal sca.    tstar : -0.65401E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25327E-01 0.53439E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.18492E-03   0.46935E+01 0.19508E+03 
c  Velocity[X]                                      0.19620E+01 
c  Velocity[Y]                                      0.27315E+01 
c  Velocity[Z]                                      0.11047E-29 
c  Pressure     0.12107E-06     521   0.92206E-08   0.11584E+00 0.76379E+03 
c  nu_tilda     0.82748E-05      33   0.13641E-04   0.71655E-06 0.21448E+03 
c  TempC        0.43734E+02      27   0.28823E-03   0.40525E+01 0.23162E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2068          9.2733          4.5729          4.5729
v  Velocity[Y]            -2.9479           7.185         0.24269         0.24269
v  Velocity[Z]       -6.9287e-015     6.6807e-015    -1.4911e-017    -1.4911e-017
v  ǁVelocityǁ         0.0032842          9.2754          5.0591          5.0591
v  Pressure               -24.013          28.929          1.6409          1.6409
v  nu_tilda           4.4032e-007         0.00444       0.0017818       0.0017818
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3062e-014       0.0052324       0.0020947       0.0020947
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2560:        0.22000E+01

===============================================================


 INSTANT    0.256100000E+04   TIME STEP NUMBER            2561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.84547E-02 0.89130E+00
   Friction velocity        uk    :  0.84547E-02 0.89130E+00
   Dimensionless distance   yplus :  0.68066E-01 0.71756E+01
   Friction thermal sca.    tstar : -0.32616E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50785E-01 0.53538E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.24558E-03   0.46843E+01 0.19494E+03 
c  Velocity[X]                                      0.19671E+01 
c  Velocity[Y]                                      0.27173E+01 
c  Velocity[Z]                                      0.13682E-29 
c  Pressure     0.11059E-06     522   0.94920E-08   0.10723E+00 0.12537E+04 
c  nu_tilda     0.82761E-05      33   0.26277E-05   0.71651E-06 0.21446E+03 
c  TempC        0.43736E+02      26   0.27490E-03   0.49777E+01 0.25732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2081          9.2718          4.5729          4.5729
v  Velocity[Y]            -2.9472           7.198          0.2427          0.2427
v  Velocity[Z]       -6.9287e-015      6.825e-015    -1.4911e-017    -1.4911e-017
v  ǁVelocityǁ           0.00331          9.2739          5.0589          5.0589
v  Pressure                -23.95          29.043          1.7033          1.7033
v  nu_tilda           4.4028e-007       0.0044405        0.001782        0.001782
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3072e-014        0.005233       0.0020948       0.0020948
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2561:        0.21960E+01

===============================================================


 INSTANT    0.256200000E+04   TIME STEP NUMBER            2562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14881E-01 0.89081E+00
   Friction velocity        uk    :  0.14881E-01 0.89081E+00
   Dimensionless distance   yplus :  0.11980E+00 0.71716E+01
   Friction thermal sca.    tstar : -0.17142E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89386E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.23289E-03   0.47063E+01 0.19500E+03 
c  Velocity[X]                                      0.19717E+01 
c  Velocity[Y]                                      0.27346E+01 
c  Velocity[Z]                                      0.25435E-29 
c  Pressure     0.11826E-06     538   0.97148E-08   0.11605E+00 0.18526E+04 
c  nu_tilda     0.82774E-05      33   0.13637E-04   0.71652E-06 0.21445E+03 
c  TempC        0.43739E+02      26   0.28879E-03   0.50424E+01 0.24988E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2094          9.2704          4.5729          4.5729
v  Velocity[Y]            -2.9466          7.1688         0.24272         0.24272
v  Velocity[Z]       -6.9287e-015     6.6739e-015    -1.4911e-017    -1.4911e-017
v  ǁVelocityǁ         0.0024794          9.2724          5.0587          5.0587
v  Pressure               -24.021          28.834          1.6179          1.6179
v  nu_tilda            4.403e-007        0.004441        0.001782        0.001782
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3058e-014       0.0052336       0.0020949       0.0020949
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2562:        0.22330E+01

===============================================================


 INSTANT    0.256300000E+04   TIME STEP NUMBER            2563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24975E-02 0.88940E+00
   Friction velocity        uk    :  0.24975E-02 0.88940E+00
   Dimensionless distance   yplus :  0.20107E-01 0.71603E+01
   Friction thermal sca.    tstar : -0.20786E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15002E-01 0.53424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.22934E-03   0.46832E+01 0.19488E+03 
c  Velocity[X]                                      0.19659E+01 
c  Velocity[Y]                                      0.27173E+01 
c  Velocity[Z]                                      0.75812E-30 
c  Pressure     0.11166E-06     522   0.97110E-08   0.10638E+00 0.15307E+04 
c  nu_tilda     0.82787E-05      33   0.25795E-05   0.71649E-06 0.21444E+03 
c  TempC        0.43742E+02      27   0.29268E-03   0.38818E+01 0.23485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2106          9.2689          4.5729          4.5729
v  Velocity[Y]            -2.9458          7.1857         0.24274         0.24274
v  Velocity[Z]       -6.9287e-015     6.7772e-015    -1.4908e-017    -1.4908e-017
v  ǁVelocityǁ         0.0012783           9.271          5.0584          5.0584
v  Pressure               -23.961          28.995          1.6903          1.6903
v  nu_tilda           4.4033e-007       0.0044415       0.0017821       0.0017821
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3065e-014       0.0052342        0.002095        0.002095
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2563:        0.21930E+01

===============================================================


 INSTANT    0.256400000E+04   TIME STEP NUMBER            2564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24955E-02 0.89045E+00
   Friction velocity        uk    :  0.24955E-02 0.89045E+00
   Dimensionless distance   yplus :  0.20090E-01 0.71687E+01
   Friction thermal sca.    tstar : -0.33689E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14990E-01 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10710E-01      33   0.28041E-03   0.46826E+01 0.19486E+03 
c  Velocity[X]                                      0.19781E+01 
c  Velocity[Y]                                      0.27045E+01 
c  Velocity[Z]                                      0.23135E-29 
c  Pressure     0.11527E-06     521   0.97806E-08   0.11273E+00 0.16381E+04 
c  nu_tilda     0.82800E-05      33   0.13639E-04   0.71650E-06 0.21442E+03 
c  TempC        0.43744E+02      27   0.33247E-03   0.48434E+01 0.25746E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2119          9.2674          4.5729          4.5729
v  Velocity[Y]            -2.9451          7.1634         0.24276         0.24276
v  Velocity[Z]       -6.9287e-015     6.6142e-015    -1.4905e-017    -1.4905e-017
v  ǁVelocityǁ          0.002219          9.2695          5.0582          5.0582
v  Pressure               -24.029          28.819          1.6141          1.6141
v  nu_tilda           4.4036e-007       0.0044419       0.0017822       0.0017822
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3074e-014       0.0052347       0.0020952       0.0020952
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2564:        0.21810E+01

===============================================================


 INSTANT    0.256500000E+04   TIME STEP NUMBER            2565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.84211E-02 0.88980E+00
   Friction velocity        uk    :  0.84211E-02 0.88980E+00
   Dimensionless distance   yplus :  0.67795E-01 0.71635E+01
   Friction thermal sca.    tstar : -0.22986E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50583E-01 0.53448E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.23939E-03   0.47332E+01 0.19533E+03 
c  Velocity[X]                                      0.19973E+01 
c  Velocity[Y]                                      0.27359E+01 
c  Velocity[Z]                                      0.10660E-29 
c  Pressure     0.13144E-06     569   0.94682E-08   0.12669E+00 0.17559E+04 
c  nu_tilda     0.82812E-05      33   0.25521E-05   0.71652E-06 0.21442E+03 
c  TempC        0.43747E+02      27   0.31907E-03   0.70209E+01 0.28616E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2131           9.266          4.5729          4.5729
v  Velocity[Y]            -2.9445          7.1899         0.24278         0.24278
v  Velocity[Z]       -6.9287e-015      6.767e-015    -1.4898e-017    -1.4898e-017
v  ǁVelocityǁ         0.0029637          9.2681           5.058           5.058
v  Pressure               -23.972          29.016          1.6944          1.6944
v  nu_tilda           4.4032e-007       0.0044424       0.0017823       0.0017823
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3082e-014       0.0052353       0.0020953       0.0020953
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2565:        0.22950E+01

===============================================================


 INSTANT    0.256600000E+04   TIME STEP NUMBER            2566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.64684E-02 0.89105E+00
   Friction velocity        uk    :  0.64684E-02 0.89105E+00
   Dimensionless distance   yplus :  0.52075E-01 0.71736E+01
   Friction thermal sca.    tstar : -0.12024E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38854E-01 0.53523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.21265E-03   0.46773E+01 0.19496E+03 
c  Velocity[X]                                      0.19650E+01 
c  Velocity[Y]                                      0.27123E+01 
c  Velocity[Z]                                      0.12832E-29 
c  Pressure     0.12446E-06     538   0.94463E-08   0.11856E+00 0.13669E+04 
c  nu_tilda     0.82825E-05      33   0.13631E-04   0.71653E-06 0.21441E+03 
c  TempC        0.43749E+02      27   0.28210E-03   0.55187E+01 0.26039E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2144          9.2645          4.5729          4.5729
v  Velocity[Y]            -2.9439          7.1905          0.2428          0.2428
v  Velocity[Z]       -6.9287e-015       6.65e-015    -1.4899e-017    -1.4899e-017
v  ǁVelocityǁ         0.0025438          9.2666          5.0578          5.0578
v  Pressure               -24.042          28.895          1.6267          1.6267
v  nu_tilda           4.4025e-007       0.0044429       0.0017824       0.0017824
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3069e-014       0.0052358       0.0020954       0.0020954
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2566:        0.22210E+01

===============================================================


 INSTANT    0.256700000E+04   TIME STEP NUMBER            2567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.38227E-02 0.89077E+00
   Friction velocity        uk    :  0.38227E-02 0.89077E+00
   Dimensionless distance   yplus :  0.30776E-01 0.71713E+01
   Friction thermal sca.    tstar : -0.11255E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22962E-01 0.53506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.23677E-03   0.46772E+01 0.19486E+03 
c  Velocity[X]                                      0.19729E+01 
c  Velocity[Y]                                      0.27043E+01 
c  Velocity[Z]                                      0.25912E-29 
c  Pressure     0.12113E-06     506   0.95874E-08   0.11925E+00 0.74457E+03 
c  nu_tilda     0.82838E-05      33   0.25024E-05   0.71650E-06 0.21439E+03 
c  TempC        0.43752E+02      27   0.29307E-03   0.39866E+01 0.23116E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2156          9.2631          4.5729          4.5729
v  Velocity[Y]            -2.9432          7.1673         0.24281         0.24281
v  Velocity[Z]       -6.9287e-015     6.6432e-015    -1.4898e-017    -1.4898e-017
v  ǁVelocityǁ         0.0014449          9.2651          5.0576          5.0576
v  Pressure               -23.981          28.893          1.6648          1.6648
v  nu_tilda            4.403e-007       0.0044434       0.0017825       0.0017825
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3051e-014       0.0052364       0.0020955       0.0020955
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2567:        0.22690E+01

===============================================================


 INSTANT    0.256800000E+04   TIME STEP NUMBER            2568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53830E-02 0.88940E+00
   Friction velocity        uk    :  0.53830E-02 0.88940E+00
   Dimensionless distance   yplus :  0.43336E-01 0.71603E+01
   Friction thermal sca.    tstar : -0.16586E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32334E-01 0.53424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.25601E-03   0.46806E+01 0.19499E+03 
c  Velocity[X]                                      0.19584E+01 
c  Velocity[Y]                                      0.27222E+01 
c  Velocity[Z]                                      0.81165E-30 
c  Pressure     0.10667E-06     505   0.95536E-08   0.10235E+00 0.75104E+03 
c  nu_tilda     0.82851E-05      33   0.13634E-04   0.71650E-06 0.21438E+03 
c  TempC        0.43754E+02      27   0.31350E-03   0.53564E+01 0.26483E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2167          9.2617          4.5729          4.5729
v  Velocity[Y]            -2.9425          7.1854         0.24283         0.24283
v  Velocity[Z]       -6.9287e-015     6.7932e-015    -1.4893e-017    -1.4893e-017
v  ǁVelocityǁ         0.0033336          9.2637          5.0574          5.0574
v  Pressure               -24.057          28.898           1.624           1.624
v  nu_tilda           4.4033e-007       0.0044439       0.0017825       0.0017825
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3066e-014        0.005237       0.0020956       0.0020956
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2568:        0.22800E+01

===============================================================


 INSTANT    0.256900000E+04   TIME STEP NUMBER            2569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.77287E-02 0.89057E+00
   Friction velocity        uk    :  0.77287E-02 0.89057E+00
   Dimensionless distance   yplus :  0.62221E-01 0.71697E+01
   Friction thermal sca.    tstar : -0.96137E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46424E-01 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10709E-01      33   0.24705E-03   0.46992E+01 0.19492E+03 
c  Velocity[X]                                      0.19984E+01 
c  Velocity[Y]                                      0.27008E+01 
c  Velocity[Z]                                      0.22976E-29 
c  Pressure     0.14303E-06     457   0.99724E-08   0.13733E+00 0.67649E+03 
c  nu_tilda     0.82864E-05      33   0.24744E-05   0.71647E-06 0.21437E+03 
c  TempC        0.43757E+02      27   0.30768E-03   0.59710E+01 0.26895E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.218          9.2603          4.5729          4.5729
v  Velocity[Y]            -2.9418          7.1625         0.24285         0.24285
v  Velocity[Z]       -6.9287e-015     6.6524e-015    -1.4889e-017    -1.4889e-017
v  ǁVelocityǁ         0.0018975          9.2622          5.0572          5.0572
v  Pressure               -23.992          28.846          1.6517          1.6517
v  nu_tilda           4.4037e-007       0.0044443       0.0017827       0.0017827
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3074e-014       0.0052375       0.0020957       0.0020957
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2569:        0.21190E+01

===============================================================


 INSTANT    0.257000000E+04   TIME STEP NUMBER            2570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15485E-01 0.89008E+00
   Friction velocity        uk    :  0.15485E-01 0.89008E+00
   Dimensionless distance   yplus :  0.12466E+00 0.71657E+01
   Friction thermal sca.    tstar : -0.90082E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93012E-01 0.53464E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.19702E-03   0.46992E+01 0.19520E+03 
c  Velocity[X]                                      0.19929E+01 
c  Velocity[Y]                                      0.27063E+01 
c  Velocity[Z]                                      0.11035E-29 
c  Pressure     0.11662E-06     520   0.97212E-08   0.11337E+00 0.66924E+03 
c  nu_tilda     0.82876E-05      33   0.13629E-04   0.71651E-06 0.21436E+03 
c  TempC        0.43759E+02      27   0.25938E-03   0.45424E+01 0.24191E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2192          9.2588          4.5729          4.5729
v  Velocity[Y]             -2.941          7.1882         0.24286         0.24286
v  Velocity[Z]       -6.9287e-015     6.8327e-015    -1.4883e-017    -1.4883e-017
v  ǁVelocityǁ         0.0023304          9.2607           5.057           5.057
v  Pressure                -24.07          28.893          1.6206          1.6206
v  nu_tilda           4.4037e-007       0.0044448       0.0017827       0.0017827
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3085e-014       0.0052381       0.0020958       0.0020958
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2570:        0.21820E+01

===============================================================


 INSTANT    0.257100000E+04   TIME STEP NUMBER            2571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60493E-02 0.89149E+00
   Friction velocity        uk    :  0.60493E-02 0.89149E+00
   Dimensionless distance   yplus :  0.48701E-01 0.71771E+01
   Friction thermal sca.    tstar : -0.69341E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36337E-01 0.53549E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.22584E-03   0.46658E+01 0.19498E+03 
c  Velocity[X]                                      0.19482E+01 
c  Velocity[Y]                                      0.27176E+01 
c  Velocity[Z]                                      0.13063E-29 
c  Pressure     0.10226E-06     521   0.93631E-08   0.98754E-01 0.11096E+04 
c  nu_tilda     0.82889E-05      33   0.24289E-05   0.71649E-06 0.21435E+03 
c  TempC        0.43762E+02      27   0.22066E-03   0.36585E+01 0.22075E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2205          9.2574          4.5729          4.5729
v  Velocity[Y]            -2.9404          7.1984         0.24288         0.24288
v  Velocity[Z]       -6.9287e-015     6.7421e-015    -1.4883e-017    -1.4883e-017
v  ǁVelocityǁ         0.0017121          9.2593          5.0568          5.0568
v  Pressure               -24.007          28.983          1.6772          1.6772
v  nu_tilda           4.4029e-007       0.0044452       0.0017829       0.0017829
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3087e-014       0.0052386       0.0020959       0.0020959
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2571:        0.21810E+01

===============================================================


 INSTANT    0.257200000E+04   TIME STEP NUMBER            2572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89937E-02 0.89093E+00
   Friction velocity        uk    :  0.89937E-02 0.89093E+00
   Dimensionless distance   yplus :  0.72405E-01 0.71726E+01
   Friction thermal sca.    tstar : -0.65128E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54022E-01 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.24486E-03   0.46810E+01 0.19495E+03 
c  Velocity[X]                                      0.19781E+01 
c  Velocity[Y]                                      0.27028E+01 
c  Velocity[Z]                                      0.24110E-29 
c  Pressure     0.12649E-06     585   0.95106E-08   0.12179E+00 0.20782E+04 
c  nu_tilda     0.82902E-05      33   0.13627E-04   0.71652E-06 0.21434E+03 
c  TempC        0.43764E+02      26   0.34514E-03   0.38170E+01 0.22666E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2217           9.256          4.5729          4.5729
v  Velocity[Y]            -2.9398          7.1667          0.2429          0.2429
v  Velocity[Z]       -6.9287e-015     6.6735e-015    -1.4884e-017    -1.4884e-017
v  ǁVelocityǁ         0.0029953          9.2578          5.0566          5.0566
v  Pressure                -24.08          28.738          1.5825          1.5825
v  nu_tilda           4.4027e-007       0.0044457       0.0017829       0.0017829
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3062e-014       0.0052392        0.002096        0.002096
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2572:        0.23360E+01

===============================================================


 INSTANT    0.257300000E+04   TIME STEP NUMBER            2573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.63724E-02 0.88978E+00
   Friction velocity        uk    :  0.63724E-02 0.88978E+00
   Dimensionless distance   yplus :  0.51302E-01 0.71633E+01
   Friction thermal sca.    tstar : -0.63016E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.38277E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10708E-01      33   0.26207E-03   0.46934E+01 0.19505E+03 
c  Velocity[X]                                      0.20003E+01 
c  Velocity[Y]                                      0.26931E+01 
c  Velocity[Z]                                      0.90819E-30 
c  Pressure     0.11486E-06     538   0.92628E-08   0.11096E+00 0.18228E+04 
c  nu_tilda     0.82914E-05      33   0.23913E-05   0.71648E-06 0.21432E+03 
c  TempC        0.43767E+02      26   0.33555E-03   0.79258E+01 0.30516E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2229          9.2546          4.5729          4.5729
v  Velocity[Y]            -2.9391          7.1902         0.24291         0.24291
v  Velocity[Z]       -6.9287e-015      6.765e-015     -1.488e-017     -1.488e-017
v  ǁVelocityǁ          0.002392          9.2564          5.0564          5.0564
v  Pressure               -24.024          28.954          1.6634          1.6634
v  nu_tilda           4.4026e-007       0.0044462       0.0017831       0.0017831
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3054e-014       0.0052397       0.0020961       0.0020961
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2573:        0.22460E+01

===============================================================


 INSTANT    0.257400000E+04   TIME STEP NUMBER            2574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18120E-01 0.89072E+00
   Friction velocity        uk    :  0.18120E-01 0.89072E+00
   Dimensionless distance   yplus :  0.14588E+00 0.71709E+01
   Friction thermal sca.    tstar : -0.59965E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10884E+00 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.24312E-03   0.46781E+01 0.19494E+03 
c  Velocity[X]                                      0.19748E+01 
c  Velocity[Y]                                      0.27034E+01 
c  Velocity[Z]                                      0.21646E-29 
c  Pressure     0.11720E-06     569   0.92352E-08   0.11448E+00 0.17570E+04 
c  nu_tilda     0.82927E-05      33   0.13626E-04   0.71648E-06 0.21431E+03 
c  TempC        0.43769E+02      26   0.31572E-03   0.68919E+01 0.28520E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2241          9.2531          4.5729          4.5729
v  Velocity[Y]            -2.9384          7.1661         0.24293         0.24293
v  Velocity[Z]       -6.9287e-015     6.7096e-015    -1.4879e-017    -1.4879e-017
v  ǁVelocityǁ         0.0014504           9.255          5.0562          5.0562
v  Pressure               -24.093          28.758          1.5823          1.5823
v  nu_tilda           4.4028e-007       0.0044467       0.0017831       0.0017831
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3054e-014       0.0052403       0.0020963       0.0020963
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2574:        0.22780E+01

===============================================================


 INSTANT    0.257500000E+04   TIME STEP NUMBER            2575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.62123E-02 0.88985E+00
   Friction velocity        uk    :  0.62123E-02 0.88985E+00
   Dimensionless distance   yplus :  0.50013E-01 0.71639E+01
   Friction thermal sca.    tstar : -0.62003E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37316E-01 0.53451E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.24572E-03   0.46794E+01 0.19510E+03 
c  Velocity[X]                                      0.19793E+01 
c  Velocity[Y]                                      0.27002E+01 
c  Velocity[Z]                                      0.10421E-29 
c  Pressure     0.12620E-06     521   0.93682E-08   0.12017E+00 0.16120E+04 
c  nu_tilda     0.82939E-05      33   0.23537E-05   0.71647E-06 0.21430E+03 
c  TempC        0.43772E+02      26   0.27847E-03   0.54299E+01 0.27251E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2253          9.2517          4.5729          4.5729
v  Velocity[Y]            -2.9376          7.1875         0.24294         0.24294
v  Velocity[Z]       -6.9287e-015     6.8521e-015    -1.4873e-017    -1.4873e-017
v  ǁVelocityǁ         0.0021638          9.2535           5.056           5.056
v  Pressure               -24.037          28.934          1.6571          1.6571
v  nu_tilda           4.4027e-007       0.0044471       0.0017833       0.0017833
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3059e-014       0.0052409       0.0020964       0.0020964
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2575:        0.21790E+01

===============================================================


 INSTANT    0.257600000E+04   TIME STEP NUMBER            2576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10586E-01 0.89114E+00
   Friction velocity        uk    :  0.10586E-01 0.89114E+00
   Dimensionless distance   yplus :  0.85226E-01 0.71743E+01
   Friction thermal sca.    tstar : -0.58709E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63588E-01 0.53528E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.24509E-03   0.46613E+01 0.19497E+03 
c  Velocity[X]                                      0.19738E+01 
c  Velocity[Y]                                      0.26875E+01 
c  Velocity[Z]                                      0.12849E-29 
c  Pressure     0.10592E-06     537   0.96142E-08   0.10260E+00 0.11967E+04 
c  nu_tilda     0.82952E-05      33   0.13621E-04   0.71650E-06 0.21429E+03 
c  TempC        0.43774E+02      27   0.25601E-03   0.52770E+01 0.26337E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2265          9.2503          4.5729          4.5729
v  Velocity[Y]            -2.9369          7.1961         0.24296         0.24296
v  Velocity[Z]       -6.9287e-015     6.7286e-015    -1.4876e-017    -1.4876e-017
v  ǁVelocityǁ         0.0024035          9.2521          5.0558          5.0558
v  Pressure               -24.111          28.846          1.5941          1.5941
v  nu_tilda           4.4019e-007       0.0044476       0.0017833       0.0017833
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3055e-014       0.0052414       0.0020965       0.0020965
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2576:        0.22270E+01

===============================================================


 INSTANT    0.257700000E+04   TIME STEP NUMBER            2577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.37486E-02 0.89074E+00
   Friction velocity        uk    :  0.37486E-02 0.89074E+00
   Dimensionless distance   yplus :  0.30179E-01 0.71711E+01
   Friction thermal sca.    tstar : -0.57331E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22517E-01 0.53504E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10707E-01      33   0.23450E-03   0.46828E+01 0.19501E+03 
c  Velocity[X]                                      0.19787E+01 
c  Velocity[Y]                                      0.27042E+01 
c  Velocity[Z]                                      0.23675E-29 
c  Pressure     0.12583E-06     520   0.94432E-08   0.12264E+00 0.68635E+03 
c  nu_tilda     0.82964E-05      33   0.23096E-05   0.71650E-06 0.21428E+03 
c  TempC        0.43777E+02      26   0.35712E-03   0.51940E+01 0.25633E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2277          9.2489          4.5729          4.5729
v  Velocity[Y]            -2.9363          7.1692         0.24297         0.24297
v  Velocity[Z]       -6.9287e-015     6.6851e-015    -1.4879e-017    -1.4879e-017
v  ǁVelocityǁ         0.0024643          9.2507          5.0556          5.0556
v  Pressure               -24.049           28.83          1.6278          1.6278
v  nu_tilda           4.4018e-007        0.004448       0.0017834       0.0017834
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3032e-014       0.0052419       0.0020966       0.0020966
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2577:        0.22700E+01

===============================================================


 INSTANT    0.257800000E+04   TIME STEP NUMBER            2578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13459E-01 0.88919E+00
   Friction velocity        uk    :  0.13459E-01 0.88919E+00
   Dimensionless distance   yplus :  0.10836E+00 0.71586E+01
   Friction thermal sca.    tstar : -0.58036E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80845E-01 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.24447E-03   0.46569E+01 0.19494E+03 
c  Velocity[X]                                      0.19691E+01 
c  Velocity[Y]                                      0.26878E+01 
c  Velocity[Z]                                      0.78150E-30 
c  Pressure     0.11631E-06     490   0.97096E-08   0.11087E+00 0.86415E+03 
c  nu_tilda     0.82977E-05      33   0.13626E-04   0.71650E-06 0.21427E+03 
c  TempC        0.43779E+02      27   0.27793E-03   0.79625E+01 0.31354E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2289          9.2474          4.5729          4.5729
v  Velocity[Y]            -2.9356          7.1841         0.24299         0.24299
v  Velocity[Z]       -6.9287e-015     6.8316e-015    -1.4881e-017    -1.4881e-017
v  ǁVelocityǁ         0.0019611          9.2493          5.0554          5.0554
v  Pressure               -24.125          28.804            1.58            1.58
v  nu_tilda           4.4014e-007       0.0044485       0.0017834       0.0017834
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3028e-014       0.0052424       0.0020967       0.0020967
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2578:        0.24660E+01

===============================================================


 INSTANT    0.257900000E+04   TIME STEP NUMBER            2579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.84076E-02 0.89053E+00
   Friction velocity        uk    :  0.84076E-02 0.89053E+00
   Dimensionless distance   yplus :  0.67687E-01 0.71693E+01
   Friction thermal sca.    tstar : -0.57820E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50502E-01 0.53491E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.25210E-03   0.46774E+01 0.19494E+03 
c  Velocity[X]                                      0.20024E+01 
c  Velocity[Y]                                      0.26751E+01 
c  Velocity[Z]                                      0.21900E-29 
c  Pressure     0.12661E-06     520   0.98934E-08   0.12391E+00 0.75067E+03 
c  nu_tilda     0.82989E-05      33   0.22810E-05   0.71647E-06 0.21425E+03 
c  TempC        0.43782E+02      27   0.29006E-03   0.46641E+01 0.25044E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2299           9.246          4.5729          4.5729
v  Velocity[Y]            -2.9349           7.166           0.243           0.243
v  Velocity[Z]       -6.9287e-015      6.778e-015    -1.4881e-017    -1.4881e-017
v  ǁVelocityǁ         0.0020555          9.2478          5.0552          5.0552
v  Pressure               -24.064          28.811          1.6188          1.6188
v  nu_tilda           4.4014e-007        0.004449       0.0017836       0.0017836
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3017e-014        0.005243       0.0020968       0.0020968
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2579:        0.21830E+01

===============================================================


 INSTANT    0.258000000E+04   TIME STEP NUMBER            2580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94622E-02 0.88972E+00
   Friction velocity        uk    :  0.94622E-02 0.88972E+00
   Dimensionless distance   yplus :  0.76177E-01 0.71628E+01
   Friction thermal sca.    tstar : -0.58074E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56837E-01 0.53443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.18778E-03   0.46788E+01 0.19521E+03 
c  Velocity[X]                                      0.19744E+01 
c  Velocity[Y]                                      0.27044E+01 
c  Velocity[Z]                                      0.10347E-29 
c  Pressure     0.10910E-06     505   0.97441E-08   0.10572E+00 0.72419E+03 
c  nu_tilda     0.83001E-05      33   0.13618E-04   0.71649E-06 0.21424E+03 
c  TempC        0.43784E+02      26   0.29002E-03   0.46611E+01 0.25685E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2311          9.2446          4.5729          4.5729
v  Velocity[Y]            -2.9342          7.1887         0.24301         0.24301
v  Velocity[Z]       -6.9287e-015     6.8294e-015    -1.4883e-017    -1.4883e-017
v  ǁVelocityǁ         0.0015235          9.2464           5.055           5.055
v  Pressure               -24.143          28.829          1.5802          1.5802
v  nu_tilda           4.4008e-007       0.0044494       0.0017836       0.0017836
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3016e-014       0.0052436       0.0020969       0.0020969
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2580:        0.21540E+01

===============================================================


 INSTANT    0.258100000E+04   TIME STEP NUMBER            2581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.33565E-02 0.89113E+00
   Friction velocity        uk    :  0.33565E-02 0.89113E+00
   Dimensionless distance   yplus :  0.27022E-01 0.71742E+01
   Friction thermal sca.    tstar : -0.57037E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.20161E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10706E-01      33   0.23933E-03   0.46454E+01 0.19490E+03 
c  Velocity[X]                                      0.19630E+01 
c  Velocity[Y]                                      0.26824E+01 
c  Velocity[Z]                                      0.13034E-29 
c  Pressure     0.12464E-06     504   0.93693E-08   0.11833E+00 0.92539E+03 
c  nu_tilda     0.83014E-05      33   0.22510E-05   0.71646E-06 0.21423E+03 
c  TempC        0.43786E+02      26   0.33053E-03   0.46983E+01 0.25373E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2322          9.2431          4.5729          4.5729
v  Velocity[Y]            -2.9334          7.1955         0.24302         0.24302
v  Velocity[Z]       -6.9287e-015     6.6676e-015    -1.4887e-017    -1.4887e-017
v  ǁVelocityǁ         0.0019532           9.245          5.0548          5.0548
v  Pressure               -24.079          28.883          1.6282          1.6282
v  nu_tilda           4.4002e-007       0.0044499       0.0017838       0.0017838
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2998e-014       0.0052441        0.002097        0.002097
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2581:        0.21480E+01

===============================================================


 INSTANT    0.258200000E+04   TIME STEP NUMBER            2582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.28910E-02 0.89082E+00
   Friction velocity        uk    :  0.28910E-02 0.89082E+00
   Dimensionless distance   yplus :  0.23274E-01 0.71717E+01
   Friction thermal sca.    tstar : -0.57105E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17365E-01 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10705E-01      33   0.23593E-03   0.46836E+01 0.19503E+03 
c  Velocity[X]                                      0.20060E+01 
c  Velocity[Y]                                      0.26776E+01 
c  Velocity[Z]                                      0.23062E-29 
c  Pressure     0.11561E-06     569   0.92739E-08   0.11349E+00 0.18036E+04 
c  nu_tilda     0.83026E-05      33   0.13621E-04   0.71651E-06 0.21422E+03 
c  TempC        0.43789E+02      26   0.31313E-03   0.78711E+01 0.30234E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2334          9.2417          4.5729          4.5729
v  Velocity[Y]            -2.9328          7.1682         0.24304         0.24304
v  Velocity[Z]       -6.9287e-015     6.6347e-015    -1.4894e-017    -1.4894e-017
v  ǁVelocityǁ         0.0022527          9.2436          5.0546          5.0546
v  Pressure               -24.154          28.685          1.5421          1.5421
v  nu_tilda           4.4007e-007       0.0044503       0.0017838       0.0017838
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2981e-014       0.0052446       0.0020971       0.0020971
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2582:        0.22980E+01

===============================================================


 INSTANT    0.258300000E+04   TIME STEP NUMBER            2583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24461E-02 0.88944E+00
   Friction velocity        uk    :  0.24461E-02 0.88944E+00
   Dimensionless distance   yplus :  0.19693E-01 0.71606E+01
   Friction thermal sca.    tstar : -0.61937E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14693E-01 0.53426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10705E-01      33   0.23143E-03   0.46578E+01 0.19498E+03 
c  Velocity[X]                                      0.19671E+01 
c  Velocity[Y]                                      0.26907E+01 
c  Velocity[Z]                                      0.80502E-30 
c  Pressure     0.99697E-07     584   0.92987E-08   0.96212E-01 0.17701E+04 
c  nu_tilda     0.83038E-05      33   0.22305E-05   0.71650E-06 0.21421E+03 
c  TempC        0.43791E+02      26   0.27582E-03   0.66179E+01 0.28269E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2346          9.2403          4.5729          4.5729
v  Velocity[Y]            -2.9321           7.188         0.24305         0.24305
v  Velocity[Z]       -6.9287e-015     6.7515e-015    -1.4896e-017    -1.4896e-017
v  ǁVelocityǁ         0.0023993          9.2421          5.0544          5.0544
v  Pressure               -24.098          28.892          1.6217          1.6217
v  nu_tilda            4.401e-007       0.0044508       0.0017839       0.0017839
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2995e-014       0.0052452       0.0020972       0.0020972
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2583:        0.23480E+01

===============================================================


 INSTANT    0.258400000E+04   TIME STEP NUMBER            2584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90728E-02 0.89022E+00
   Friction velocity        uk    :  0.90728E-02 0.89022E+00
   Dimensionless distance   yplus :  0.73043E-01 0.71669E+01
   Friction thermal sca.    tstar : -0.58198E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54498E-01 0.53473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10705E-01      33   0.25189E-03   0.46472E+01 0.19485E+03 
c  Velocity[X]                                      0.19769E+01 
c  Velocity[Y]                                      0.26702E+01 
c  Velocity[Z]                                      0.21317E-29 
c  Pressure     0.12208E-06     553   0.94191E-08   0.11792E+00 0.20477E+04 
c  nu_tilda     0.83050E-05      33   0.13615E-04   0.71650E-06 0.21420E+03 
c  TempC        0.43793E+02      26   0.32037E-03   0.48151E+01 0.24796E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2357          9.2388          4.5729          4.5729
v  Velocity[Y]            -2.9314          7.1612         0.24307         0.24307
v  Velocity[Z]       -6.9287e-015     6.6713e-015    -1.4901e-017    -1.4901e-017
v  ǁVelocityǁ         0.0028964          9.2407          5.0542          5.0542
v  Pressure               -24.169          28.651          1.5288          1.5288
v  nu_tilda           4.4017e-007       0.0044512       0.0017839       0.0017839
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3003e-014       0.0052457       0.0020973       0.0020973
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2584:        0.22660E+01

===============================================================


 INSTANT    0.258500000E+04   TIME STEP NUMBER            2585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13485E-01 0.88967E+00
   Friction velocity        uk    :  0.13485E-01 0.88967E+00
   Dimensionless distance   yplus :  0.10856E+00 0.71624E+01
   Friction thermal sca.    tstar : -0.58410E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80998E-01 0.53440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10704E-01      33   0.20354E-03   0.46785E+01 0.19520E+03 
c  Velocity[X]                                      0.20026E+01 
c  Velocity[Y]                                      0.26759E+01 
c  Velocity[Z]                                      0.10758E-29 
c  Pressure     0.12570E-06     553   0.92116E-08   0.12037E+00 0.19161E+04 
c  nu_tilda     0.83062E-05      33   0.22240E-05   0.71649E-06 0.21419E+03 
c  TempC        0.43796E+02      27   0.23560E-03   0.56313E+01 0.26413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2369          9.2374          4.5729          4.5729
v  Velocity[Y]            -2.9307          7.1887         0.24308         0.24308
v  Velocity[Z]       -6.9287e-015     6.7478e-015    -1.4899e-017    -1.4899e-017
v  ǁVelocityǁ         0.0033412          9.2393          5.0541          5.0541
v  Pressure               -24.112          28.876          1.6143          1.6143
v  nu_tilda           4.4019e-007       0.0044517       0.0017841       0.0017841
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3024e-014       0.0052462       0.0020974       0.0020974
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2585:        0.22750E+01

===============================================================


 INSTANT    0.258600000E+04   TIME STEP NUMBER            2586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.81340E-02 0.89099E+00
   Friction velocity        uk    :  0.81340E-02 0.89099E+00
   Dimensionless distance   yplus :  0.65484E-01 0.71731E+01
   Friction thermal sca.    tstar : -0.57468E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48859E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10704E-01      33   0.23507E-03   0.46462E+01 0.19502E+03 
c  Velocity[X]                                      0.19611E+01 
c  Velocity[Y]                                      0.26851E+01 
c  Velocity[Z]                                      0.11832E-29 
c  Pressure     0.10327E-06     536   0.97719E-08   0.99468E-01 0.12477E+04 
c  nu_tilda     0.83075E-05      33   0.13614E-04   0.71650E-06 0.21418E+03 
c  TempC        0.43798E+02      26   0.36425E-03   0.50320E+01 0.25509E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.238           9.236          4.5729          4.5729
v  Velocity[Y]            -2.9299          7.1939         0.24309         0.24309
v  Velocity[Z]       -6.9287e-015      6.697e-015    -1.4909e-017    -1.4909e-017
v  ǁVelocityǁ         0.0023987          9.2379          5.0539          5.0539
v  Pressure               -24.187          28.779          1.5491          1.5491
v  nu_tilda           4.4011e-007       0.0044521       0.0017841       0.0017841
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3031e-014       0.0052468       0.0020975       0.0020975
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2586:        0.22350E+01

===============================================================


 INSTANT    0.258700000E+04   TIME STEP NUMBER            2587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.86577E-02 0.89050E+00
   Friction velocity        uk    :  0.86577E-02 0.89050E+00
   Dimensionless distance   yplus :  0.69701E-01 0.71691E+01
   Friction thermal sca.    tstar : -0.57180E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52004E-01 0.53490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10704E-01      33   0.23163E-03   0.46645E+01 0.19495E+03 
c  Velocity[X]                                      0.19930E+01 
c  Velocity[Y]                                      0.26715E+01 
c  Velocity[Z]                                      0.22752E-29 
c  Pressure     0.12672E-06     473   0.99426E-08   0.12223E+00 0.62563E+03 
c  nu_tilda     0.83087E-05      33   0.22240E-05   0.71650E-06 0.21417E+03 
c  TempC        0.43800E+02      26   0.26984E-03   0.77624E+01 0.31903E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2391          9.2345          4.5729          4.5729
v  Velocity[Y]            -2.9291          7.1646          0.2431          0.2431
v  Velocity[Z]       -6.9287e-015     6.8116e-015    -1.4914e-017    -1.4914e-017
v  ǁVelocityǁ         0.0030688          9.2364          5.0537          5.0537
v  Pressure               -24.125           28.72          1.5718          1.5718
v  nu_tilda           4.4011e-007       0.0044526       0.0017843       0.0017843
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3008e-014       0.0052473       0.0020976       0.0020976
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2587:        0.20890E+01

===============================================================


 INSTANT    0.258800000E+04   TIME STEP NUMBER            2588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16750E-01 0.88932E+00
   Friction velocity        uk    :  0.16750E-01 0.88932E+00
   Dimensionless distance   yplus :  0.13485E+00 0.71596E+01
   Friction thermal sca.    tstar : -0.57897E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10061E+00 0.53419E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.23714E-03   0.46566E+01 0.19498E+03 
c  Velocity[X]                                      0.19929E+01 
c  Velocity[Y]                                      0.26637E+01 
c  Velocity[Z]                                      0.82588E-30 
c  Pressure     0.10589E-06     506   0.98027E-08   0.10231E+00 0.70060E+03 
c  nu_tilda     0.83099E-05      33   0.13620E-04   0.71652E-06 0.21416E+03 
c  TempC        0.43803E+02      26   0.29334E-03   0.41393E+01 0.24222E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2402          9.2331          4.5729          4.5729
v  Velocity[Y]            -2.9285          7.1853         0.24311         0.24311
v  Velocity[Z]       -6.9287e-015     6.7563e-015    -1.4918e-017    -1.4918e-017
v  ǁVelocityǁ         0.0024735           9.235          5.0535          5.0535
v  Pressure               -24.203          28.747          1.5354          1.5354
v  nu_tilda           4.4015e-007        0.004453       0.0017843       0.0017843
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3008e-014       0.0052478       0.0020977       0.0020977
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2588:        0.21550E+01

===============================================================


 INSTANT    0.258900000E+04   TIME STEP NUMBER            2589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18744E-01 0.89044E+00
   Friction velocity        uk    :  0.18744E-01 0.89044E+00
   Dimensionless distance   yplus :  0.15090E+00 0.71686E+01
   Friction thermal sca.    tstar : -0.57420E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11259E+00 0.53486E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.24126E-03   0.46492E+01 0.19490E+03 
c  Velocity[X]                                      0.19763E+01 
c  Velocity[Y]                                      0.26728E+01 
c  Velocity[Z]                                      0.22096E-29 
c  Pressure     0.11765E-06     473   0.99247E-08   0.11412E+00 0.67263E+03 
c  nu_tilda     0.83111E-05      33   0.22291E-05   0.71651E-06 0.21415E+03 
c  TempC        0.43805E+02      26   0.26372E-03   0.50345E+01 0.26677E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2413          9.2317          4.5729          4.5729
v  Velocity[Y]            -2.9278          7.1639         0.24312         0.24312
v  Velocity[Z]       -6.9287e-015     6.7421e-015     -1.492e-017     -1.492e-017
v  ǁVelocityǁ         0.0030967          9.2336          5.0533          5.0533
v  Pressure               -24.142           28.73          1.5685          1.5685
v  nu_tilda            4.402e-007       0.0044534       0.0017844       0.0017844
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3019e-014       0.0052483       0.0020977       0.0020977
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2589:        0.20840E+01

===============================================================


 INSTANT    0.259000000E+04   TIME STEP NUMBER            2590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10684E-01 0.88950E+00
   Friction velocity        uk    :  0.10684E-01 0.88950E+00
   Dimensionless distance   yplus :  0.86011E-01 0.71611E+01
   Friction thermal sca.    tstar : -0.60433E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64174E-01 0.53430E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.20551E-03   0.46494E+01 0.19511E+03 
c  Velocity[X]                                      0.19788E+01 
c  Velocity[Y]                                      0.26707E+01 
c  Velocity[Z]                                      0.10304E-29 
c  Pressure     0.11726E-06     522   0.93953E-08   0.11185E+00 0.85214E+03 
c  nu_tilda     0.83123E-05      33   0.13611E-04   0.71655E-06 0.21414E+03 
c  TempC        0.43807E+02      27   0.26762E-03   0.53199E+01 0.25059E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2424          9.2302          4.5729          4.5729
v  Velocity[Y]            -2.9271          7.1836         0.24313         0.24313
v  Velocity[Z]       -6.9287e-015     6.8179e-015    -1.4925e-017    -1.4925e-017
v  ǁVelocityǁ         0.0022168          9.2322          5.0531          5.0531
v  Pressure               -24.219          28.706          1.5214          1.5214
v  nu_tilda           4.4024e-007       0.0044539       0.0017844       0.0017844
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3036e-014       0.0052488       0.0020978       0.0020978
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2590:        0.21940E+01

===============================================================


 INSTANT    0.259100000E+04   TIME STEP NUMBER            2591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.74982E-02 0.89121E+00
   Friction velocity        uk    :  0.74982E-02 0.89121E+00
   Dimensionless distance   yplus :  0.60365E-01 0.71748E+01
   Friction thermal sca.    tstar : -0.61313E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45039E-01 0.53532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10703E-01      33   0.25053E-03   0.46457E+01 0.19502E+03 
c  Velocity[X]                                      0.19881E+01 
c  Velocity[Y]                                      0.26576E+01 
c  Velocity[Z]                                      0.12180E-29 
c  Pressure     0.11727E-06     504   0.92022E-08   0.11303E+00 0.11189E+04 
c  nu_tilda     0.83134E-05      33   0.22287E-05   0.71650E-06 0.21412E+03 
c  TempC        0.43809E+02      26   0.36776E-03   0.60491E+01 0.25970E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2434          9.2288          4.5729          4.5729
v  Velocity[Y]            -2.9264          7.1975         0.24314         0.24314
v  Velocity[Z]       -6.9287e-015     6.7781e-015    -1.4929e-017    -1.4929e-017
v  ǁVelocityǁ          0.002449          9.2307          5.0529          5.0529
v  Pressure                -24.16          28.804          1.5767          1.5767
v  nu_tilda           4.4023e-007       0.0044544       0.0017846       0.0017846
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3046e-014       0.0052494       0.0020979       0.0020979
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2591:        0.21760E+01

===============================================================


 INSTANT    0.259200000E+04   TIME STEP NUMBER            2592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18608E-01 0.89088E+00
   Friction velocity        uk    :  0.18608E-01 0.89088E+00
   Dimensionless distance   yplus :  0.14981E+00 0.71722E+01
   Friction thermal sca.    tstar : -0.64728E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11177E+00 0.53513E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10702E-01      33   0.22997E-03   0.46624E+01 0.19505E+03 
c  Velocity[X]                                      0.19880E+01 
c  Velocity[Y]                                      0.26744E+01 
c  Velocity[Z]                                      0.21937E-29 
c  Pressure     0.11610E-06     538   0.97422E-08   0.11353E+00 0.17648E+04 
c  nu_tilda     0.83146E-05      33   0.13603E-04   0.71654E-06 0.21411E+03 
c  TempC        0.43812E+02      27   0.25898E-03   0.65234E+01 0.30462E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2444          9.2274          4.5729          4.5729
v  Velocity[Y]            -2.9256          7.1674         0.24316         0.24316
v  Velocity[Z]       -6.9287e-015     6.8468e-015    -1.4936e-017    -1.4936e-017
v  ǁVelocityǁ           0.00168          9.2293          5.0527          5.0527
v  Pressure               -24.233          28.613          1.4929          1.4929
v  nu_tilda           4.4027e-007       0.0044548       0.0017846       0.0017846
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3043e-014       0.0052499        0.002098        0.002098
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2592:        0.22340E+01

===============================================================


 INSTANT    0.259300000E+04   TIME STEP NUMBER            2593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17785E-01 0.88936E+00
   Friction velocity        uk    :  0.17785E-01 0.88936E+00
   Dimensionless distance   yplus :  0.14318E+00 0.71600E+01
   Friction thermal sca.    tstar : -0.66854E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10683E+00 0.53421E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10702E-01      33   0.23488E-03   0.46390E+01 0.19490E+03 
c  Velocity[X]                                      0.19823E+01 
c  Velocity[Y]                                      0.26567E+01 
c  Velocity[Z]                                      0.75028E-30 
c  Pressure     0.11835E-06     521   0.97806E-08   0.11174E+00 0.14377E+04 
c  nu_tilda     0.83158E-05      33   0.22326E-05   0.71652E-06 0.21410E+03 
c  TempC        0.43814E+02      27   0.31451E-03   0.40719E+01 0.23964E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2455          9.2259          4.5729          4.5729
v  Velocity[Y]            -2.9248          7.1842         0.24316         0.24316
v  Velocity[Z]       -6.9287e-015      6.856e-015    -1.4938e-017    -1.4938e-017
v  ǁVelocityǁ        0.00089774          9.2279          5.0525          5.0525
v  Pressure               -24.176          28.762          1.5603          1.5603
v  nu_tilda           4.4029e-007       0.0044552       0.0017847       0.0017847
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3055e-014       0.0052504       0.0020981       0.0020981
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2593:        0.21990E+01

===============================================================


 INSTANT    0.259400000E+04   TIME STEP NUMBER            2594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15922E-01 0.89051E+00
   Friction velocity        uk    :  0.15922E-01 0.89051E+00
   Dimensionless distance   yplus :  0.12818E+00 0.71692E+01
   Friction thermal sca.    tstar : -0.71245E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95638E-01 0.53490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10702E-01      33   0.25184E-03   0.46559E+01 0.19494E+03 
c  Velocity[X]                                      0.20103E+01 
c  Velocity[Y]                                      0.26456E+01 
c  Velocity[Z]                                      0.20339E-29 
c  Pressure     0.11521E-06     585   0.95793E-08   0.11253E+00 0.16783E+04 
c  nu_tilda     0.83170E-05      33   0.13593E-04   0.71654E-06 0.21409E+03 
c  TempC        0.43816E+02      27   0.32461E-03   0.68239E+01 0.28506E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2465          9.2245          4.5729          4.5729
v  Velocity[Y]            -2.9241          7.1634         0.24317         0.24317
v  Velocity[Z]       -6.9287e-015     6.8857e-015     -1.494e-017     -1.494e-017
v  ǁVelocityǁ        0.00031384          9.2264          5.0523          5.0523
v  Pressure               -24.251          28.582          1.4795          1.4795
v  nu_tilda            4.403e-007       0.0044556       0.0017847       0.0017847
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3062e-014       0.0052509       0.0020982       0.0020982
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2594:        0.23500E+01

===============================================================


 INSTANT    0.259500000E+04   TIME STEP NUMBER            2595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93740E-02 0.88980E+00
   Friction velocity        uk    :  0.93740E-02 0.88980E+00
   Dimensionless distance   yplus :  0.75467E-01 0.71635E+01
   Friction thermal sca.    tstar : -0.73573E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56307E-01 0.53448E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10701E-01      33   0.23002E-03   0.46521E+01 0.19515E+03 
c  Velocity[X]                                      0.19798E+01 
c  Velocity[Y]                                      0.26723E+01 
c  Velocity[Z]                                      0.10943E-29 
c  Pressure     0.10857E-06     538   0.96827E-08   0.10442E+00 0.18118E+04 
c  nu_tilda     0.83182E-05      33   0.22343E-05   0.71653E-06 0.21408E+03 
c  TempC        0.43818E+02      26   0.31552E-03   0.66376E+01 0.28240E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2476          9.2231          4.5729          4.5729
v  Velocity[Y]            -2.9234          7.1879         0.24318         0.24318
v  Velocity[Z]       -6.9287e-015      6.884e-015    -1.4938e-017    -1.4938e-017
v  ǁVelocityǁ         0.0007039           9.225          5.0521          5.0521
v  Pressure               -24.192          28.795          1.5616          1.5616
v  nu_tilda           4.4024e-007       0.0044561       0.0017849       0.0017849
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3065e-014       0.0052514       0.0020983       0.0020983
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2595:        0.22350E+01

===============================================================


 INSTANT    0.259600000E+04   TIME STEP NUMBER            2596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.51394E-02 0.89082E+00
   Friction velocity        uk    :  0.51394E-02 0.89082E+00
   Dimensionless distance   yplus :  0.41375E-01 0.71717E+01
   Friction thermal sca.    tstar : -0.78571E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.30871E-01 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10701E-01      33   0.24784E-03   0.46121E+01 0.19490E+03 
c  Velocity[X]                                      0.19606E+01 
c  Velocity[Y]                                      0.26515E+01 
c  Velocity[Z]                                      0.12381E-29 
c  Pressure     0.11952E-06     552   0.98494E-08   0.11362E+00 0.15584E+04 
c  nu_tilda     0.83193E-05      33   0.13583E-04   0.71655E-06 0.21407E+03 
c  TempC        0.43820E+02      26   0.26947E-03   0.63145E+01 0.28368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2487          9.2216          4.5729          4.5729
v  Velocity[Y]            -2.9227          7.1903         0.24319         0.24319
v  Velocity[Z]       -6.9287e-015     6.8881e-015    -1.4945e-017    -1.4945e-017
v  ǁVelocityǁ         0.0014313          9.2236           5.052           5.052
v  Pressure               -24.268          28.643          1.4838          1.4838
v  nu_tilda           4.4022e-007       0.0044565       0.0017849       0.0017849
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3047e-014       0.0052519       0.0020984       0.0020984
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2596:        0.22850E+01

===============================================================


 INSTANT    0.259700000E+04   TIME STEP NUMBER            2597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10073E-01 0.89063E+00
   Friction velocity        uk    :  0.10073E-01 0.89063E+00
   Dimensionless distance   yplus :  0.81097E-01 0.71702E+01
   Friction thermal sca.    tstar : -0.82148E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60507E-01 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10700E-01      33   0.23819E-03   0.46429E+01 0.19495E+03 
c  Velocity[X]                                      0.19980E+01 
c  Velocity[Y]                                      0.26450E+01 
c  Velocity[Z]                                      0.23571E-29 
c  Pressure     0.12311E-06     505   0.95222E-08   0.12095E+00 0.72936E+03 
c  nu_tilda     0.83205E-05      33   0.22354E-05   0.71653E-06 0.21406E+03 
c  TempC        0.43822E+02      26   0.22754E-03   0.48999E+01 0.25840E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2498          9.2202          4.5729          4.5729
v  Velocity[Y]             -2.922          7.1673          0.2432          0.2432
v  Velocity[Z]       -6.9287e-015     6.8957e-015    -1.4948e-017    -1.4948e-017
v  ǁVelocityǁ          0.002251          9.2221          5.0518          5.0518
v  Pressure               -24.207          28.648          1.5213          1.5213
v  nu_tilda           4.4027e-007        0.004457        0.001785        0.001785
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3039e-014       0.0052525       0.0020985       0.0020985
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2597:        0.21650E+01

===============================================================


 INSTANT    0.259800000E+04   TIME STEP NUMBER            2598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17159E-01 0.88924E+00
   Friction velocity        uk    :  0.17159E-01 0.88924E+00
   Dimensionless distance   yplus :  0.13814E+00 0.71590E+01
   Friction thermal sca.    tstar : -0.92242E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10307E+00 0.53414E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10700E-01      33   0.26632E-03   0.46321E+01 0.19498E+03 
c  Velocity[X]                                      0.19722E+01 
c  Velocity[Y]                                      0.26599E+01 
c  Velocity[Z]                                      0.80877E-30 
c  Pressure     0.10368E-06     504   0.97071E-08   0.99265E-01 0.75719E+03 
c  nu_tilda     0.83217E-05      33   0.13575E-04   0.71654E-06 0.21405E+03 
c  TempC        0.43825E+02      26   0.32908E-03   0.35784E+01 0.20986E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2509          9.2188          4.5729          4.5729
v  Velocity[Y]            -2.9212          7.1854         0.24321         0.24321
v  Velocity[Z]       -6.9287e-015     6.9022e-015    -1.4951e-017    -1.4951e-017
v  ǁVelocityǁ          0.002264          9.2207          5.0516          5.0516
v  Pressure               -24.287          28.661          1.4797          1.4797
v  nu_tilda           4.4028e-007       0.0044574        0.001785        0.001785
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3054e-014        0.005253       0.0020986       0.0020986
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2598:        0.21430E+01

===============================================================


 INSTANT    0.259900000E+04   TIME STEP NUMBER            2599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15566E-01 0.89033E+00
   Friction velocity        uk    :  0.15566E-01 0.89033E+00
   Dimensionless distance   yplus :  0.12532E+00 0.71677E+01
   Friction thermal sca.    tstar : -0.95986E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93502E-01 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10700E-01      33   0.22636E-03   0.46544E+01 0.19493E+03 
c  Velocity[X]                                      0.20128E+01 
c  Velocity[Y]                                      0.26415E+01 
c  Velocity[Z]                                      0.18557E-29 
c  Pressure     0.13840E-06     458   0.93430E-08   0.13267E+00 0.64360E+03 
c  nu_tilda     0.83228E-05      33   0.22405E-05   0.71653E-06 0.21403E+03 
c  TempC        0.43827E+02      27   0.27854E-03   0.53688E+01 0.25357E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2519          9.2173          4.5729          4.5729
v  Velocity[Y]            -2.9204          7.1624         0.24322         0.24322
v  Velocity[Z]       -6.9287e-015     6.9571e-015    -1.4949e-017    -1.4949e-017
v  ǁVelocityǁ          0.002027          9.2193          5.0514          5.0514
v  Pressure               -24.224          28.599          1.5036          1.5036
v  nu_tilda           4.4033e-007       0.0044578       0.0017852       0.0017852
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc            3.306e-014       0.0052535       0.0020986       0.0020986
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2599:        0.20510E+01

===============================================================


 INSTANT    0.260000000E+04   TIME STEP NUMBER            2600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15949E-01 0.88983E+00
   Friction velocity        uk    :  0.15949E-01 0.88983E+00
   Dimensionless distance   yplus :  0.12840E+00 0.71638E+01
   Friction thermal sca.    tstar : -0.11273E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95799E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10699E-01      33   0.18671E-03   0.46371E+01 0.19508E+03 
c  Velocity[X]                                      0.19921E+01 
c  Velocity[Y]                                      0.26449E+01 
c  Velocity[Z]                                      0.11723E-29 
c  Pressure     0.11043E-06     490   0.92310E-08   0.10725E+00 0.68997E+03 
c  nu_tilda     0.83240E-05      33   0.13565E-04   0.71657E-06 0.21403E+03 
c  TempC        0.43829E+02      26   0.32508E-03   0.48965E+01 0.25437E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.253          9.2159          4.5729          4.5729
v  Velocity[Y]            -2.9197          7.1872         0.24322         0.24322
v  Velocity[Z]       -6.9287e-015     6.9279e-015    -1.4949e-017    -1.4949e-017
v  ǁVelocityǁ         0.0022633          9.2179          5.0512          5.0512
v  Pressure               -24.303          28.645          1.4701          1.4701
v  nu_tilda           4.4032e-007       0.0044582       0.0017852       0.0017852
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3074e-014        0.005254       0.0020987       0.0020987
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2600:        0.21670E+01

===============================================================


 INSTANT    0.260100000E+04   TIME STEP NUMBER            2601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18629E-01 0.89115E+00
   Friction velocity        uk    :  0.18629E-01 0.89115E+00
   Dimensionless distance   yplus :  0.14998E+00 0.71743E+01
   Friction thermal sca.    tstar : -0.11756E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11190E+00 0.53529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10699E-01      33   0.22837E-03   0.46123E+01 0.19493E+03 
c  Velocity[X]                                      0.19565E+01 
c  Velocity[Y]                                      0.26558E+01 
c  Velocity[Z]                                      0.11762E-29 
c  Pressure     0.93054E-07     536   0.99264E-08   0.89824E-01 0.10099E+04 
c  nu_tilda     0.83252E-05      33   0.22416E-05   0.71654E-06 0.21402E+03 
c  TempC        0.43831E+02      26   0.31647E-03   0.57764E+01 0.28816E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.254          9.2145          4.5729          4.5729
v  Velocity[Y]             -2.919          7.1977         0.24323         0.24323
v  Velocity[Z]       -6.9287e-015     6.8958e-015    -1.4952e-017    -1.4952e-017
v  ǁVelocityǁ         0.0019039          9.2164           5.051           5.051
v  Pressure               -24.244          28.721          1.5212          1.5212
v  nu_tilda           4.4022e-007       0.0044587       0.0017853       0.0017853
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3071e-014       0.0052545       0.0020988       0.0020988
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2601:        0.22510E+01

===============================================================


 INSTANT    0.260200000E+04   TIME STEP NUMBER            2602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55133E-02 0.89065E+00
   Friction velocity        uk    :  0.55133E-02 0.89065E+00
   Dimensionless distance   yplus :  0.44386E-01 0.71703E+01
   Friction thermal sca.    tstar : -0.14857E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33117E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10699E-01      33   0.24647E-03   0.46348E+01 0.19495E+03 
c  Velocity[X]                                      0.19932E+01 
c  Velocity[Y]                                      0.26416E+01 
c  Velocity[Z]                                      0.20987E-29 
c  Pressure     0.12381E-06     601   0.96808E-08   0.11909E+00 0.19988E+04 
c  nu_tilda     0.83263E-05      33   0.13555E-04   0.71659E-06 0.21401E+03 
c  TempC        0.43833E+02      26   0.26580E-03   0.59758E+01 0.25926E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.255           9.213          4.5729          4.5729
v  Velocity[Y]            -2.9183          7.1652         0.24324         0.24324
v  Velocity[Z]       -6.9287e-015     6.8428e-015    -1.4956e-017    -1.4956e-017
v  ǁVelocityǁ         0.0017108           9.215          5.0508          5.0508
v  Pressure               -24.314          28.491          1.4297          1.4297
v  nu_tilda           4.4018e-007       0.0044591       0.0017853       0.0017853
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3041e-014        0.005255       0.0020989       0.0020989
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2602:        0.23750E+01

===============================================================


 INSTANT    0.260300000E+04   TIME STEP NUMBER            2603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14506E-01 0.88946E+00
   Friction velocity        uk    :  0.14506E-01 0.88946E+00
   Dimensionless distance   yplus :  0.11678E+00 0.71608E+01
   Friction thermal sca.    tstar : -0.18787E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87134E-01 0.53427E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10698E-01      33   0.26135E-03   0.46447E+01 0.19502E+03 
c  Velocity[X]                                      0.20129E+01 
c  Velocity[Y]                                      0.26318E+01 
c  Velocity[Z]                                      0.11203E-29 
c  Pressure     0.11401E-06     570   0.98325E-08   0.10976E+00 0.17471E+04 
c  nu_tilda     0.83274E-05      33   0.22453E-05   0.71655E-06 0.21399E+03 
c  TempC        0.43835E+02      27   0.29694E-03   0.42791E+01 0.23179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2559          9.2116          4.5729          4.5729
v  Velocity[Y]            -2.9175           7.189         0.24325         0.24325
v  Velocity[Z]       -6.9287e-015     6.8135e-015    -1.4955e-017    -1.4955e-017
v  ǁVelocityǁ        0.00036846          9.2136          5.0507          5.0507
v  Pressure                -24.26          28.693          1.5074          1.5074
v  nu_tilda           4.4017e-007       0.0044595       0.0017855       0.0017855
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3029e-014       0.0052555        0.002099        0.002099
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2603:        0.23070E+01

===============================================================


 INSTANT    0.260400000E+04   TIME STEP NUMBER            2604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47761E-02 0.89046E+00
   Friction velocity        uk    :  0.47761E-02 0.89046E+00
   Dimensionless distance   yplus :  0.38451E-01 0.71688E+01
   Friction thermal sca.    tstar : -0.57052E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28689E-01 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10698E-01      33   0.25024E-03   0.46393E+01 0.19498E+03 
c  Velocity[X]                                      0.19965E+01 
c  Velocity[Y]                                      0.26428E+01 
c  Velocity[Z]                                      0.19781E-29 
c  Pressure     0.11325E-06     600   0.98191E-08   0.11020E+00 0.19002E+04 
c  nu_tilda     0.83286E-05      33   0.13547E-04   0.71657E-06 0.21398E+03 
c  TempC        0.43837E+02      26   0.26810E-03   0.47701E+01 0.25360E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2569          9.2102          4.5729          4.5729
v  Velocity[Y]            -2.9167          7.1643         0.24325         0.24325
v  Velocity[Z]       -6.9287e-015     6.8369e-015    -1.4953e-017    -1.4953e-017
v  ǁVelocityǁ         0.0008782          9.2121          5.0505          5.0505
v  Pressure               -24.332          28.487          1.4182          1.4182
v  nu_tilda           4.4023e-007         0.00446       0.0017855       0.0017855
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3027e-014        0.005256       0.0020991       0.0020991
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2604:        0.23750E+01

===============================================================


 INSTANT    0.260500000E+04   TIME STEP NUMBER            2605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10490E-01 0.88958E+00
   Friction velocity        uk    :  0.10490E-01 0.88958E+00
   Dimensionless distance   yplus :  0.84456E-01 0.71617E+01
   Friction thermal sca.    tstar : -0.25972E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63013E-01 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10698E-01      33   0.23441E-03   0.46325E+01 0.19505E+03 
c  Velocity[X]                                      0.19942E+01 
c  Velocity[Y]                                      0.26382E+01 
c  Velocity[Z]                                      0.10130E-29 
c  Pressure     0.12135E-06     585   0.94272E-08   0.11536E+00 0.18115E+04 
c  nu_tilda     0.83297E-05      33   0.22459E-05   0.71656E-06 0.21397E+03 
c  TempC        0.43839E+02      26   0.30146E-03   0.44924E+01 0.24344E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2578          9.2087          4.5729          4.5729
v  Velocity[Y]             -2.916          7.1857         0.24326         0.24326
v  Velocity[Z]       -6.9287e-015     6.7974e-015    -1.4953e-017    -1.4953e-017
v  ǁVelocityǁ         0.0016044          9.2107          5.0503          5.0503
v  Pressure               -24.277          28.685          1.5006          1.5006
v  nu_tilda           4.4023e-007       0.0044604       0.0017856       0.0017856
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3043e-014       0.0052565       0.0020991       0.0020991
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2605:        0.23500E+01

===============================================================


 INSTANT    0.260600000E+04   TIME STEP NUMBER            2606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.87694E-02 0.89092E+00
   Friction velocity        uk    :  0.87694E-02 0.89092E+00
   Dimensionless distance   yplus :  0.70600E-01 0.71725E+01
   Friction thermal sca.    tstar : -0.18464E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52675E-01 0.53515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10697E-01      33   0.24315E-03   0.46135E+01 0.19494E+03 
c  Velocity[X]                                      0.19871E+01 
c  Velocity[Y]                                      0.26264E+01 
c  Velocity[Z]                                      0.12599E-29 
c  Pressure     0.99835E-07     586   0.99252E-08   0.96429E-01 0.14961E+04 
c  nu_tilda     0.83309E-05      33   0.13537E-04   0.71659E-06 0.21396E+03 
c  TempC        0.43841E+02      27   0.28213E-03   0.58937E+01 0.26424E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2588          9.2073          4.5729          4.5729
v  Velocity[Y]            -2.9152          7.1947         0.24326         0.24326
v  Velocity[Z]       -6.9287e-015     6.8004e-015    -1.4956e-017    -1.4956e-017
v  ǁVelocityǁ         0.0034593          9.2093          5.0501          5.0501
v  Pressure               -24.351          28.559          1.4242          1.4242
v  nu_tilda           4.4017e-007       0.0044608       0.0017856       0.0017856
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3043e-014        0.005257       0.0020992       0.0020992
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2606:        0.26220E+01

===============================================================


 INSTANT    0.260700000E+04   TIME STEP NUMBER            2607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16336E-02 0.89058E+00
   Friction velocity        uk    :  0.16336E-02 0.89058E+00
   Dimensionless distance   yplus :  0.13152E-01 0.71698E+01
   Friction thermal sca.    tstar : -0.14071E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98127E-02 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10697E-01      33   0.22940E-03   0.46324E+01 0.19496E+03 
c  Velocity[X]                                      0.19895E+01 
c  Velocity[Y]                                      0.26428E+01 
c  Velocity[Z]                                      0.21018E-29 
c  Pressure     0.12316E-06     536   0.97563E-08   0.11985E+00 0.94121E+03 
c  nu_tilda     0.83320E-05      33   0.22518E-05   0.71661E-06 0.21396E+03 
c  TempC        0.43843E+02      26   0.36707E-03   0.49662E+01 0.26090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2598          9.2059          4.5729          4.5729
v  Velocity[Y]            -2.9145          7.1672         0.24327         0.24327
v  Velocity[Z]       -6.9287e-015     6.7846e-015    -1.4961e-017    -1.4961e-017
v  ǁVelocityǁ         0.0026095          9.2078          5.0499          5.0499
v  Pressure               -24.291          28.595           1.474           1.474
v  nu_tilda            4.402e-007       0.0044612       0.0017857       0.0017857
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3025e-014       0.0052575       0.0020993       0.0020993
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2607:        0.23190E+01

===============================================================


 INSTANT    0.260800000E+04   TIME STEP NUMBER            2608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.30396E-02 0.88900E+00
   Friction velocity        uk    :  0.30396E-02 0.88900E+00
   Dimensionless distance   yplus :  0.24471E-01 0.71570E+01
   Friction thermal sca.    tstar : -0.11789E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18258E-01 0.53400E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10696E-01      33   0.24161E-03   0.46043E+01 0.19487E+03 
c  Velocity[X]                                      0.19788E+01 
c  Velocity[Y]                                      0.26255E+01 
c  Velocity[Z]                                      0.91323E-30 
c  Pressure     0.11053E-06     537   0.99842E-08   0.10500E+00 0.12391E+04 
c  nu_tilda     0.83331E-05      33   0.13530E-04   0.71661E-06 0.21394E+03 
c  TempC        0.43845E+02      27   0.30702E-03   0.64791E+01 0.29716E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2608          9.2044          4.5729          4.5729
v  Velocity[Y]            -2.9138          7.1822         0.24327         0.24327
v  Velocity[Z]       -6.9287e-015     6.7542e-015    -1.4961e-017    -1.4961e-017
v  ǁVelocityǁ         0.0027413          9.2064          5.0498          5.0498
v  Pressure               -24.367          28.516          1.4069          1.4069
v  nu_tilda           4.4024e-007       0.0044616       0.0017857       0.0017857
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3036e-014        0.005258       0.0020994       0.0020994
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2608:        0.22180E+01

===============================================================


 INSTANT    0.260900000E+04   TIME STEP NUMBER            2609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10563E-01 0.89036E+00
   Friction velocity        uk    :  0.10563E-01 0.89036E+00
   Dimensionless distance   yplus :  0.85036E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.10530E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63446E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10696E-01      33   0.27189E-03   0.46191E+01 0.19484E+03 
c  Velocity[X]                                      0.20062E+01 
c  Velocity[Y]                                      0.26128E+01 
c  Velocity[Z]                                      0.20370E-29 
c  Pressure     0.12054E-06     490   0.92198E-08   0.11794E+00 0.97552E+03 
c  nu_tilda     0.83342E-05      33   0.22496E-05   0.71658E-06 0.21393E+03 
c  TempC        0.43847E+02      26   0.21641E-03   0.50253E+01 0.26660E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2618           9.203          4.5729          4.5729
v  Velocity[Y]             -2.913           7.165         0.24328         0.24328
v  Velocity[Z]       -6.9287e-015     6.8217e-015    -1.4965e-017    -1.4965e-017
v  ǁVelocityǁ         0.0025408           9.205          5.0496          5.0496
v  Pressure               -24.308           28.56          1.4581          1.4581
v  nu_tilda           4.4024e-007        0.004462       0.0017859       0.0017859
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3045e-014       0.0052585       0.0020995       0.0020995
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2609:        0.21060E+01

===============================================================


 INSTANT    0.261000000E+04   TIME STEP NUMBER            2610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17173E-01 0.88959E+00
   Friction velocity        uk    :  0.17173E-01 0.88959E+00
   Dimensionless distance   yplus :  0.13826E+00 0.71618E+01
   Friction thermal sca.    tstar : -0.94710E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10316E+00 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10696E-01      33   0.19293E-03   0.46478E+01 0.19534E+03 
c  Velocity[X]                                      0.20012E+01 
c  Velocity[Y]                                      0.26465E+01 
c  Velocity[Z]                                      0.10492E-29 
c  Pressure     0.11672E-06     521   0.96533E-08   0.11246E+00 0.89914E+03 
c  nu_tilda     0.83354E-05      33   0.13519E-04   0.71660E-06 0.21392E+03 
c  TempC        0.43849E+02      27   0.32173E-03   0.31282E+01 0.20906E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2628          9.2015          4.5729          4.5729
v  Velocity[Y]            -2.9121          7.1876         0.24328         0.24328
v  Velocity[Z]       -6.9287e-015     6.7849e-015    -1.4963e-017    -1.4963e-017
v  ǁVelocityǁ         0.0034379          9.2035          5.0494          5.0494
v  Pressure               -24.384          28.546          1.4079          1.4079
v  nu_tilda            4.402e-007       0.0044625       0.0017859       0.0017859
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3047e-014        0.005259       0.0020995       0.0020995
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2610:        0.21910E+01

===============================================================


 INSTANT    0.261100000E+04   TIME STEP NUMBER            2611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18964E-01 0.89104E+00
   Friction velocity        uk    :  0.18964E-01 0.89104E+00
   Dimensionless distance   yplus :  0.15267E+00 0.71735E+01
   Friction thermal sca.    tstar : -0.89942E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11391E+00 0.53522E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10695E-01      33   0.23615E-03   0.46087E+01 0.19499E+03 
c  Velocity[X]                                      0.19787E+01 
c  Velocity[Y]                                      0.26300E+01 
c  Velocity[Z]                                      0.11849E-29 
c  Pressure     0.13219E-06     520   0.96986E-08   0.12667E+00 0.10017E+04 
c  nu_tilda     0.83365E-05      33   0.22580E-05   0.71660E-06 0.21391E+03 
c  TempC        0.43851E+02      27   0.31018E-03   0.66433E+01 0.26492E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2638          9.2001          4.5729          4.5729
v  Velocity[Y]            -2.9114          7.1938         0.24328         0.24328
v  Velocity[Z]       -6.9287e-015     6.7494e-015    -1.4971e-017    -1.4971e-017
v  ǁVelocityǁ         0.0024127          9.2021          5.0492          5.0492
v  Pressure               -24.324          28.611          1.4597          1.4597
v  nu_tilda           4.4015e-007       0.0044629        0.001786        0.001786
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3034e-014       0.0052595       0.0020996       0.0020996
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2611:        0.21930E+01

===============================================================


 INSTANT    0.261200000E+04   TIME STEP NUMBER            2612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12569E-01 0.89072E+00
   Friction velocity        uk    :  0.12569E-01 0.89072E+00
   Dimensionless distance   yplus :  0.10119E+00 0.71709E+01
   Friction thermal sca.    tstar : -0.81784E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75496E-01 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10695E-01      33   0.23501E-03   0.46377E+01 0.19507E+03 
c  Velocity[X]                                      0.20168E+01 
c  Velocity[Y]                                      0.26209E+01 
c  Velocity[Z]                                      0.20191E-29 
c  Pressure     0.11031E-06     537   0.95054E-08   0.10836E+00 0.18849E+04 
c  nu_tilda     0.83376E-05      33   0.13512E-04   0.71666E-06 0.21391E+03 
c  TempC        0.43853E+02      26   0.31084E-03   0.51936E+01 0.26314E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2648          9.1987          4.5729          4.5729
v  Velocity[Y]            -2.9107          7.1671         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.7149e-015    -1.4979e-017    -1.4979e-017
v  ǁVelocityǁ         0.0031092          9.2007           5.049           5.049
v  Pressure               -24.398          28.409          1.3698          1.3698
v  nu_tilda           4.4018e-007       0.0044633        0.001786        0.001786
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3021e-014       0.0052599       0.0020997       0.0020997
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2612:        0.22260E+01

===============================================================


 INSTANT    0.261300000E+04   TIME STEP NUMBER            2613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.74913E-02 0.88937E+00
   Friction velocity        uk    :  0.74913E-02 0.88937E+00
   Dimensionless distance   yplus :  0.60310E-01 0.71600E+01
   Friction thermal sca.    tstar : -0.76930E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.44998E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10694E-01      33   0.23631E-03   0.46051E+01 0.19487E+03 
c  Velocity[X]                                      0.19781E+01 
c  Velocity[Y]                                      0.26271E+01 
c  Velocity[Z]                                      0.88612E-30 
c  Pressure     0.97322E-07     552   0.96701E-08   0.94032E-01 0.19546E+04 
c  nu_tilda     0.83387E-05      33   0.22546E-05   0.71664E-06 0.21390E+03 
c  TempC        0.43855E+02      26   0.28055E-03   0.48631E+01 0.27004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2657          9.1972          4.5729          4.5729
v  Velocity[Y]              -2.91          7.1875         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015      6.726e-015    -1.4983e-017    -1.4983e-017
v  ǁVelocityǁ         0.0033872          9.1992          5.0489          5.0489
v  Pressure               -24.344          28.631          1.4566          1.4566
v  nu_tilda           4.4017e-007       0.0044637       0.0017861       0.0017861
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc            3.303e-014       0.0052604       0.0020998       0.0020998
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2613:        0.22810E+01

===============================================================


 INSTANT    0.261400000E+04   TIME STEP NUMBER            2614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12547E-01 0.89021E+00
   Friction velocity        uk    :  0.12547E-01 0.89021E+00
   Dimensionless distance   yplus :  0.10101E+00 0.71668E+01
   Friction thermal sca.    tstar : -0.73283E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75365E-01 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10694E-01      33   0.25143E-03   0.45986E+01 0.19478E+03 
c  Velocity[X]                                      0.19903E+01 
c  Velocity[Y]                                      0.26082E+01 
c  Velocity[Z]                                      0.19182E-29 
c  Pressure     0.11817E-06     569   0.99002E-08   0.11395E+00 0.22635E+04 
c  nu_tilda     0.83398E-05      33   0.13501E-04   0.71665E-06 0.21388E+03 
c  TempC        0.43857E+02      27   0.26669E-03   0.77739E+01 0.29558E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2666          9.1958          4.5729          4.5729
v  Velocity[Y]            -2.9092          7.1594         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.7035e-015    -1.4986e-017    -1.4986e-017
v  ǁVelocityǁ         0.0030825          9.1978          5.0487          5.0487
v  Pressure               -24.415          28.373          1.3538          1.3538
v  nu_tilda           4.4019e-007       0.0044641       0.0017861       0.0017861
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3025e-014       0.0052609       0.0020998       0.0020998
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2614:        0.22920E+01

===============================================================


 INSTANT    0.261500000E+04   TIME STEP NUMBER            2615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17487E-01 0.88956E+00
   Friction velocity        uk    :  0.17487E-01 0.88956E+00
   Dimensionless distance   yplus :  0.14079E+00 0.71616E+01
   Friction thermal sca.    tstar : -0.69607E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10504E+00 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10693E-01      33   0.21670E-03   0.46214E+01 0.19514E+03 
c  Velocity[X]                                      0.20053E+01 
c  Velocity[Y]                                      0.26161E+01 
c  Velocity[Z]                                      0.12356E-29 
c  Pressure     0.11410E-06     569   0.94215E-08   0.10929E+00 0.21278E+04 
c  nu_tilda     0.83409E-05      33   0.22611E-05   0.71661E-06 0.21387E+03 
c  TempC        0.43859E+02      27   0.29774E-03   0.51131E+01 0.24910E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2675          9.1944          4.5729          4.5729
v  Velocity[Y]            -2.9084          7.1871         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.6791e-015     -1.499e-017     -1.499e-017
v  ǁVelocityǁ         0.0021936          9.1964          5.0485          5.0485
v  Pressure               -24.362          28.621          1.4474          1.4474
v  nu_tilda           4.4016e-007       0.0044645       0.0017862       0.0017862
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3032e-014       0.0052614       0.0020999       0.0020999
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2615:        0.22860E+01

===============================================================


 INSTANT    0.261600000E+04   TIME STEP NUMBER            2616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10112E-01 0.89088E+00
   Friction velocity        uk    :  0.10112E-01 0.89088E+00
   Dimensionless distance   yplus :  0.81408E-01 0.71722E+01
   Friction thermal sca.    tstar : -0.67417E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60740E-01 0.53513E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10693E-01      33   0.23429E-03   0.46129E+01 0.19512E+03 
c  Velocity[X]                                      0.19809E+01 
c  Velocity[Y]                                      0.26320E+01 
c  Velocity[Z]                                      0.12208E-29 
c  Pressure     0.10431E-06     553   0.94553E-08   0.10025E+00 0.15396E+04 
c  nu_tilda     0.83420E-05      33   0.13493E-04   0.71666E-06 0.21386E+03 
c  TempC        0.43861E+02      26   0.26277E-03   0.48455E+01 0.25541E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2684          9.1929          4.5729          4.5729
v  Velocity[Y]            -2.9075          7.1933          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6569e-015    -1.4994e-017    -1.4994e-017
v  ǁVelocityǁ         0.0035123           9.195          5.0483          5.0483
v  Pressure               -24.433          28.487          1.3701          1.3701
v  nu_tilda           4.4005e-007       0.0044649       0.0017862       0.0017862
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3022e-014       0.0052619          0.0021          0.0021
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2616:        0.22640E+01

===============================================================


 INSTANT    0.261700000E+04   TIME STEP NUMBER            2617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.77518E-02 0.89044E+00
   Friction velocity        uk    :  0.77518E-02 0.89044E+00
   Dimensionless distance   yplus :  0.62407E-01 0.71687E+01
   Friction thermal sca.    tstar : -0.64673E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46563E-01 0.53486E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10693E-01      33   0.23303E-03   0.46208E+01 0.19499E+03 
c  Velocity[X]                                      0.20063E+01 
c  Velocity[Y]                                      0.26145E+01 
c  Velocity[Z]                                      0.18936E-29 
c  Pressure     0.13367E-06     504   0.98327E-08   0.13038E+00 0.64568E+03 
c  nu_tilda     0.83431E-05      33   0.22598E-05   0.71669E-06 0.21386E+03 
c  TempC        0.43863E+02      27   0.30377E-03   0.54142E+01 0.25768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2693          9.1915          4.5729          4.5729
v  Velocity[Y]            -2.9068          7.1633          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6403e-015    -1.5003e-017    -1.5003e-017
v  ǁVelocityǁ         0.0030638          9.1935          5.0481          5.0481
v  Pressure               -24.373          28.451          1.4006          1.4006
v  nu_tilda           4.4003e-007       0.0044653       0.0017864       0.0017864
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2991e-014       0.0052624       0.0021001       0.0021001
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2617:        0.21390E+01

===============================================================


 INSTANT    0.261800000E+04   TIME STEP NUMBER            2618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.68347E-02 0.88923E+00
   Friction velocity        uk    :  0.68347E-02 0.88923E+00
   Dimensionless distance   yplus :  0.55024E-01 0.71589E+01
   Friction thermal sca.    tstar : -0.65355E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41054E-01 0.53414E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10692E-01      33   0.24189E-03   0.46056E+01 0.19487E+03 
c  Velocity[X]                                      0.20053E+01 
c  Velocity[Y]                                      0.26004E+01 
c  Velocity[Z]                                      0.94189E-30 
c  Pressure     0.10241E-06     521   0.91858E-08   0.99058E-01 0.82008E+03 
c  nu_tilda     0.83442E-05      33   0.13486E-04   0.71670E-06 0.21385E+03 
c  TempC        0.43865E+02      27   0.29204E-03   0.53075E+01 0.25047E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2701            9.19          4.5729          4.5729
v  Velocity[Y]            -2.9061          7.1838          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6156e-015    -1.5007e-017    -1.5007e-017
v  ǁVelocityǁ         0.0020816          9.1921           5.048           5.048
v  Pressure               -24.452           28.46          1.3546          1.3546
v  nu_tilda           4.4003e-007       0.0044657       0.0017864       0.0017864
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2983e-014       0.0052628       0.0021001       0.0021001
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2618:        0.21840E+01

===============================================================


 INSTANT    0.261900000E+04   TIME STEP NUMBER            2619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13746E-01 0.89032E+00
   Friction velocity        uk    :  0.13746E-01 0.89032E+00
   Dimensionless distance   yplus :  0.11066E+00 0.71677E+01
   Friction thermal sca.    tstar : -0.60097E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82567E-01 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10692E-01      33   0.23841E-03   0.45967E+01 0.19480E+03 
c  Velocity[X]                                      0.19862E+01 
c  Velocity[Y]                                      0.26104E+01 
c  Velocity[Z]                                      0.18624E-29 
c  Pressure     0.11661E-06     490   0.98035E-08   0.11296E+00 0.70801E+03 
c  nu_tilda     0.83452E-05      33   0.22653E-05   0.71669E-06 0.21383E+03 
c  TempC        0.43867E+02      27   0.24753E-03   0.67783E+01 0.28060E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2711          9.1886          4.5729          4.5729
v  Velocity[Y]            -2.9053          7.1635          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6284e-015     -1.501e-017     -1.501e-017
v  ǁVelocityǁ         0.0015702          9.1906          5.0478          5.0478
v  Pressure               -24.392          28.453          1.3911          1.3911
v  nu_tilda           4.4009e-007       0.0044662       0.0017865       0.0017865
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2983e-014       0.0052633       0.0021002       0.0021002
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2619:        0.21180E+01

===============================================================


 INSTANT    0.262000000E+04   TIME STEP NUMBER            2620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.78080E-02 0.88946E+00
   Friction velocity        uk    :  0.78080E-02 0.88946E+00
   Dimensionless distance   yplus :  0.62860E-01 0.71608E+01
   Friction thermal sca.    tstar : -0.57915E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46901E-01 0.53427E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10691E-01      33   0.19409E-03   0.45985E+01 0.19506E+03 
c  Velocity[X]                                      0.19882E+01 
c  Velocity[Y]                                      0.26103E+01 
c  Velocity[Z]                                      0.10146E-29 
c  Pressure     0.11501E-06     521   0.96449E-08   0.10978E+00 0.84461E+03 
c  nu_tilda     0.83463E-05      33   0.13476E-04   0.71670E-06 0.21382E+03 
c  TempC        0.43869E+02      26   0.35285E-03   0.54614E+01 0.26789E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.272          9.1872          4.5729          4.5729
v  Velocity[Y]            -2.9045          7.1829          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6062e-015    -1.5013e-017    -1.5013e-017
v  ǁVelocityǁ         0.0026207          9.1892          5.0476          5.0476
v  Pressure               -24.469           28.43          1.3444          1.3444
v  nu_tilda           4.4013e-007       0.0044666       0.0017865       0.0017865
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3001e-014       0.0052639       0.0021003       0.0021003
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2620:        0.21930E+01

===============================================================


 INSTANT    0.262100000E+04   TIME STEP NUMBER            2621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17715E-01 0.89115E+00
   Friction velocity        uk    :  0.17715E-01 0.89115E+00
   Dimensionless distance   yplus :  0.14261E+00 0.71743E+01
   Friction thermal sca.    tstar : -0.57439E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10641E+00 0.53529E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10691E-01      33   0.26916E-03   0.45911E+01 0.19496E+03 
c  Velocity[X]                                      0.19887E+01 
c  Velocity[Y]                                      0.26025E+01 
c  Velocity[Z]                                      0.12151E-29 
c  Pressure     0.10864E-06     522   0.97643E-08   0.10476E+00 0.11314E+04 
c  nu_tilda     0.83474E-05      33   0.22651E-05   0.71669E-06 0.21381E+03 
c  TempC        0.43871E+02      27   0.26840E-03   0.77285E+01 0.30024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2729          9.1857          4.5729          4.5729
v  Velocity[Y]            -2.9037           7.195          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6145e-015    -1.5019e-017    -1.5019e-017
v  ǁVelocityǁ         0.0031702          9.1878          5.0475          5.0475
v  Pressure                -24.41          28.535          1.3998          1.3998
v  nu_tilda           4.4012e-007        0.004467       0.0017866       0.0017866
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3013e-014       0.0052644       0.0021003       0.0021003
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2621:        0.22030E+01

===============================================================


 INSTANT    0.262200000E+04   TIME STEP NUMBER            2622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13340E-01 0.89064E+00
   Friction velocity        uk    :  0.13340E-01 0.89064E+00
   Dimensionless distance   yplus :  0.10740E+00 0.71703E+01
   Friction thermal sca.    tstar : -0.57095E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80129E-01 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10690E-01      33   0.23661E-03   0.46318E+01 0.19515E+03 
c  Velocity[X]                                      0.20143E+01 
c  Velocity[Y]                                      0.26175E+01 
c  Velocity[Z]                                      0.18911E-29 
c  Pressure     0.12675E-06     585   0.95855E-08   0.12531E+00 0.19432E+04 
c  nu_tilda     0.83485E-05      33   0.13468E-04   0.71674E-06 0.21381E+03 
c  TempC        0.43872E+02      27   0.23717E-03   0.59224E+01 0.25725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2738          9.1843          4.5729          4.5729
v  Velocity[Y]            -2.9029          7.1668          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.5969e-015    -1.5025e-017    -1.5025e-017
v  ǁVelocityǁ         0.0024533          9.1863          5.0473          5.0473
v  Pressure               -24.482          28.317           1.309           1.309
v  nu_tilda           4.4017e-007       0.0044674       0.0017866       0.0017866
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3009e-014       0.0052648       0.0021004       0.0021004
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2622:        0.23350E+01

===============================================================


 INSTANT    0.262300000E+04   TIME STEP NUMBER            2623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10794E-01 0.88931E+00
   Friction velocity        uk    :  0.10794E-01 0.88931E+00
   Dimensionless distance   yplus :  0.86903E-01 0.71596E+01
   Friction thermal sca.    tstar : -0.61841E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64839E-01 0.53418E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10690E-01      33   0.23233E-03   0.45889E+01 0.19478E+03 
c  Velocity[X]                                      0.19953E+01 
c  Velocity[Y]                                      0.25936E+01 
c  Velocity[Z]                                      0.78619E-30 
c  Pressure     0.11747E-06     536   0.93425E-08   0.11125E+00 0.15297E+04 
c  nu_tilda     0.83495E-05      33   0.22684E-05   0.71674E-06 0.21380E+03 
c  TempC        0.43874E+02      27   0.30716E-03   0.41384E+01 0.22717E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2747          9.1829          4.5729          4.5729
v  Velocity[Y]            -2.9021          7.1835          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015      6.632e-015    -1.5028e-017    -1.5028e-017
v  ǁVelocityǁ         0.0017142          9.1849          5.0471          5.0471
v  Pressure               -24.428          28.482           1.379           1.379
v  nu_tilda            4.402e-007       0.0044678       0.0017867       0.0017867
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3025e-014       0.0052653       0.0021005       0.0021005
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2623:        0.22350E+01

===============================================================


 INSTANT    0.262400000E+04   TIME STEP NUMBER            2624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.45522E-02 0.89047E+00
   Friction velocity        uk    :  0.45522E-02 0.89047E+00
   Dimensionless distance   yplus :  0.36648E-01 0.71689E+01
   Friction thermal sca.    tstar : -0.58801E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27344E-01 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10689E-01      33   0.25103E-03   0.46026E+01 0.19481E+03 
c  Velocity[X]                                      0.20194E+01 
c  Velocity[Y]                                      0.25832E+01 
c  Velocity[Z]                                      0.17835E-29 
c  Pressure     0.11197E-06     537   0.96285E-08   0.10934E+00 0.16008E+04 
c  nu_tilda     0.83506E-05      33   0.13459E-04   0.71678E-06 0.21379E+03 
c  TempC        0.43876E+02      27   0.31952E-03   0.54648E+01 0.26911E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2756          9.1814          4.5729          4.5729
v  Velocity[Y]            -2.9014          7.1611          0.2433          0.2433
v  Velocity[Z]       -6.9287e-015     6.6719e-015    -1.5032e-017    -1.5032e-017
v  ǁVelocityǁ         0.0016192          9.1835          5.0469          5.0469
v  Pressure               -24.502          28.317          1.3008          1.3008
v  nu_tilda           4.4023e-007       0.0044683       0.0017867       0.0017867
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3035e-014       0.0052658       0.0021005       0.0021005
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2624:        0.22430E+01

===============================================================


 INSTANT    0.262500000E+04   TIME STEP NUMBER            2625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10711E-01 0.88963E+00
   Friction velocity        uk    :  0.10711E-01 0.88963E+00
   Dimensionless distance   yplus :  0.86232E-01 0.71621E+01
   Friction thermal sca.    tstar : -0.58311E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64338E-01 0.53437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10689E-01      33   0.23415E-03   0.46017E+01 0.19509E+03 
c  Velocity[X]                                      0.19900E+01 
c  Velocity[Y]                                      0.26117E+01 
c  Velocity[Z]                                      0.91234E-30 
c  Pressure     0.10484E-06     490   0.96450E-08   0.10082E+00 0.16129E+04 
c  nu_tilda     0.83516E-05      33   0.22707E-05   0.71673E-06 0.21377E+03 
c  TempC        0.43878E+02      26   0.31273E-03   0.53462E+01 0.26008E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2765            9.18          4.5729          4.5729
v  Velocity[Y]            -2.9006          7.1871         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.6925e-015    -1.5031e-017    -1.5031e-017
v  ǁVelocityǁ         0.0029495          9.1821          5.0468          5.0468
v  Pressure               -24.446          28.497          1.3744          1.3744
v  nu_tilda           4.4021e-007       0.0044687       0.0017868       0.0017868
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3043e-014       0.0052663       0.0021006       0.0021006
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2625:        0.21130E+01

===============================================================


 INSTANT    0.262600000E+04   TIME STEP NUMBER            2626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.65690E-02 0.89082E+00
   Friction velocity        uk    :  0.65690E-02 0.89082E+00
   Dimensionless distance   yplus :  0.52885E-01 0.71717E+01
   Friction thermal sca.    tstar : -0.57570E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39458E-01 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10689E-01      33   0.24460E-03   0.45706E+01 0.19489E+03 
c  Velocity[X]                                      0.19743E+01 
c  Velocity[Y]                                      0.25963E+01 
c  Velocity[Z]                                      0.12754E-29 
c  Pressure     0.12134E-06     522   0.99435E-08   0.11657E+00 0.14847E+04 
c  nu_tilda     0.83527E-05      33   0.13449E-04   0.71678E-06 0.21377E+03 
c  TempC        0.43880E+02      27   0.25947E-03   0.48316E+01 0.23955E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2773          9.1785          4.5729          4.5729
v  Velocity[Y]            -2.8998          7.1896         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015      6.744e-015    -1.5036e-017    -1.5036e-017
v  ǁVelocityǁ         0.0027584          9.1806          5.0466          5.0466
v  Pressure               -24.518          28.364          1.2998          1.2998
v  nu_tilda           4.4014e-007       0.0044691       0.0017868       0.0017868
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3038e-014       0.0052668       0.0021007       0.0021007
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2626:        0.22260E+01

===============================================================


 INSTANT    0.262700000E+04   TIME STEP NUMBER            2627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.89849E-02 0.89059E+00
   Friction velocity        uk    :  0.89849E-02 0.89059E+00
   Dimensionless distance   yplus :  0.72335E-01 0.71698E+01
   Friction thermal sca.    tstar : -0.57540E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53970E-01 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10688E-01      33   0.23066E-03   0.45877E+01 0.19487E+03 
c  Velocity[X]                                      0.20012E+01 
c  Velocity[Y]                                      0.25866E+01 
c  Velocity[Z]                                      0.19526E-29 
c  Pressure     0.12469E-06     488   0.98930E-08   0.12213E+00 0.75290E+03 
c  nu_tilda     0.83538E-05      33   0.22714E-05   0.71679E-06 0.21376E+03 
c  TempC        0.43881E+02      27   0.29061E-03   0.44086E+01 0.22200E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2781          9.1771          4.5729          4.5729
v  Velocity[Y]             -2.899           7.166         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.7625e-015    -1.5044e-017    -1.5044e-017
v  ǁVelocityǁ         0.0021238          9.1792          5.0464          5.0464
v  Pressure               -24.459          28.373          1.3391          1.3391
v  nu_tilda           4.4016e-007       0.0044695       0.0017869       0.0017869
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3016e-014       0.0052673       0.0021007       0.0021007
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2627:        0.21310E+01

===============================================================


 INSTANT    0.262800000E+04   TIME STEP NUMBER            2628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10370E-01 0.88912E+00
   Friction velocity        uk    :  0.10370E-01 0.88912E+00
   Dimensionless distance   yplus :  0.83484E-01 0.71580E+01
   Friction thermal sca.    tstar : -0.57972E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62289E-01 0.53407E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10688E-01      33   0.27033E-03   0.45750E+01 0.19480E+03 
c  Velocity[X]                                      0.19780E+01 
c  Velocity[Y]                                      0.25970E+01 
c  Velocity[Z]                                      0.76338E-30 
c  Pressure     0.97928E-07     506   0.96408E-08   0.94451E-01 0.82703E+03 
c  nu_tilda     0.83548E-05      33   0.13443E-04   0.71680E-06 0.21375E+03 
c  TempC        0.43883E+02      27   0.33030E-03   0.47728E+01 0.24994E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.279          9.1757          4.5729          4.5729
v  Velocity[Y]            -2.8981          7.1847         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.8029e-015    -1.5044e-017    -1.5044e-017
v  ǁVelocityǁ         0.0024069          9.1777          5.0463          5.0463
v  Pressure               -24.539          28.368          1.2923          1.2923
v  nu_tilda           4.4018e-007       0.0044699       0.0017869       0.0017869
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3022e-014       0.0052678       0.0021008       0.0021008
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2628:        0.22020E+01

===============================================================


 INSTANT    0.262900000E+04   TIME STEP NUMBER            2629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18681E-01 0.89028E+00
   Friction velocity        uk    :  0.18681E-01 0.89028E+00
   Dimensionless distance   yplus :  0.15039E+00 0.71673E+01
   Friction thermal sca.    tstar : -0.57148E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11221E+00 0.53476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10687E-01      33   0.23381E-03   0.46047E+01 0.19480E+03 
c  Velocity[X]                                      0.20265E+01 
c  Velocity[Y]                                      0.25782E+01 
c  Velocity[Z]                                      0.19511E-29 
c  Pressure     0.14285E-06     472   0.99274E-08   0.13673E+00 0.60744E+03 
c  nu_tilda     0.83558E-05      33   0.22769E-05   0.71682E-06 0.21374E+03 
c  TempC        0.43885E+02      26   0.27289E-03   0.68239E+01 0.29140E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2798          9.1743          4.5729          4.5729
v  Velocity[Y]            -2.8974          7.1608         0.24329         0.24329
v  Velocity[Z]       -6.9287e-015     6.8327e-015    -1.5046e-017    -1.5046e-017
v  ǁVelocityǁ         0.0017789          9.1763          5.0461          5.0461
v  Pressure               -24.478          28.314          1.3164          1.3164
v  nu_tilda           4.4023e-007       0.0044704        0.001787        0.001787
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc            3.303e-014       0.0052683       0.0021009       0.0021009
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2629:        0.20890E+01

===============================================================


 INSTANT    0.263000000E+04   TIME STEP NUMBER            2630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16627E-01 0.88977E+00
   Friction velocity        uk    :  0.16627E-01 0.88977E+00
   Dimensionless distance   yplus :  0.13386E+00 0.71633E+01
   Friction thermal sca.    tstar : -0.58557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99873E-01 0.53446E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10687E-01      33   0.19160E-03   0.45873E+01 0.19499E+03 
c  Velocity[X]                                      0.20042E+01 
c  Velocity[Y]                                      0.25831E+01 
c  Velocity[Z]                                      0.10424E-29 
c  Pressure     0.11534E-06     504   0.92273E-08   0.11329E+00 0.71238E+03 
c  nu_tilda     0.83569E-05      33   0.13434E-04   0.71684E-06 0.21373E+03 
c  TempC        0.43887E+02      26   0.29416E-03   0.62954E+01 0.27095E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2806          9.1729          4.5729          4.5729
v  Velocity[Y]            -2.8966           7.186         0.24328         0.24328
v  Velocity[Z]       -6.9287e-015     6.8702e-015    -1.5046e-017    -1.5046e-017
v  ǁVelocityǁ         0.0028508          9.1749          5.0459          5.0459
v  Pressure               -24.557          28.359          1.2808          1.2808
v  nu_tilda           4.4017e-007       0.0044708        0.001787        0.001787
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3043e-014       0.0052688       0.0021009       0.0021009
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2630:        0.21560E+01

===============================================================


 INSTANT    0.263100000E+04   TIME STEP NUMBER            2631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.58670E-02 0.89114E+00
   Friction velocity        uk    :  0.58670E-02 0.89114E+00
   Dimensionless distance   yplus :  0.47233E-01 0.71743E+01
   Friction thermal sca.    tstar : -0.61205E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35241E-01 0.53528E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10686E-01      33   0.24580E-03   0.45668E+01 0.19487E+03 
c  Velocity[X]                                      0.19681E+01 
c  Velocity[Y]                                      0.25987E+01 
c  Velocity[Z]                                      0.10463E-29 
c  Pressure     0.96294E-07     504   0.95695E-08   0.92710E-01 0.10129E+04 
c  nu_tilda     0.83579E-05      33   0.22776E-05   0.71682E-06 0.21372E+03 
c  TempC        0.43888E+02      26   0.28156E-03   0.48327E+01 0.25745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2814          9.1715          4.5729          4.5729
v  Velocity[Y]            -2.8958          7.1974         0.24328         0.24328
v  Velocity[Z]       -6.9287e-015     6.8862e-015    -1.5053e-017    -1.5053e-017
v  ǁVelocityǁ         0.0024057          9.1734          5.0458          5.0458
v  Pressure               -24.497          28.435          1.3324          1.3324
v  nu_tilda           4.4004e-007       0.0044712       0.0017871       0.0017871
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3026e-014       0.0052693        0.002101        0.002101
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2631:        0.21430E+01

===============================================================


 INSTANT    0.263200000E+04   TIME STEP NUMBER            2632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13053E-01 0.89070E+00
   Friction velocity        uk    :  0.13053E-01 0.89070E+00
   Dimensionless distance   yplus :  0.10508E+00 0.71707E+01
   Friction thermal sca.    tstar : -0.58287E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78405E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10686E-01      33   0.21269E-03   0.45914E+01 0.19491E+03 
c  Velocity[X]                                      0.20088E+01 
c  Velocity[Y]                                      0.25826E+01 
c  Velocity[Z]                                      0.18891E-29 
c  Pressure     0.12514E-06     568   0.94362E-08   0.12044E+00 0.20289E+04 
c  nu_tilda     0.83589E-05      33   0.13425E-04   0.71688E-06 0.21371E+03 
c  TempC        0.43890E+02      26   0.23634E-03   0.49949E+01 0.24773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2822          9.1701          4.5729          4.5729
v  Velocity[Y]             -2.895          7.1643         0.24328         0.24328
v  Velocity[Z]       -6.9287e-015      6.937e-015    -1.5057e-017    -1.5057e-017
v  ǁVelocityǁ         0.0025267           9.172          5.0456          5.0456
v  Pressure                -24.57          28.199          1.2387          1.2387
v  nu_tilda           4.4003e-007       0.0044716       0.0017871       0.0017871
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2986e-014       0.0052698        0.002101        0.002101
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2632:        0.23190E+01

===============================================================


 INSTANT    0.263300000E+04   TIME STEP NUMBER            2633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10987E-01 0.88953E+00
   Friction velocity        uk    :  0.10987E-01 0.88953E+00
   Dimensionless distance   yplus :  0.88451E-01 0.71613E+01
   Friction thermal sca.    tstar : -0.58568E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65995E-01 0.53431E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10685E-01      33   0.23689E-03   0.45557E+01 0.19465E+03 
c  Velocity[X]                                      0.19890E+01 
c  Velocity[Y]                                      0.25667E+01 
c  Velocity[Z]                                      0.95766E-30 
c  Pressure     0.99953E-07     586   0.95420E-08   0.96785E-01 0.18550E+04 
c  nu_tilda     0.83600E-05      33   0.22816E-05   0.71686E-06 0.21370E+03 
c  TempC        0.43892E+02      26   0.33061E-03   0.70250E+01 0.28211E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2831          9.1688          4.5729          4.5729
v  Velocity[Y]            -2.8941          7.1874         0.24327         0.24327
v  Velocity[Z]       -6.9287e-015      6.955e-015    -1.5058e-017    -1.5058e-017
v  ǁVelocityǁ         0.0023756          9.1706          5.0454          5.0454
v  Pressure               -24.516          28.423          1.3195          1.3195
v  nu_tilda           4.4005e-007        0.004472       0.0017872       0.0017872
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2983e-014       0.0052703       0.0021011       0.0021011
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2633:        0.23240E+01

===============================================================


 INSTANT    0.263400000E+04   TIME STEP NUMBER            2634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11362E-01 0.89029E+00
   Friction velocity        uk    :  0.11362E-01 0.89029E+00
   Dimensionless distance   yplus :  0.91471E-01 0.71674E+01
   Friction thermal sca.    tstar : -0.58939E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68248E-01 0.53477E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10685E-01      33   0.24629E-03   0.45722E+01 0.19473E+03 
c  Velocity[X]                                      0.19909E+01 
c  Velocity[Y]                                      0.25813E+01 
c  Velocity[Z]                                      0.16467E-29 
c  Pressure     0.10605E-06     552   0.94170E-08   0.10449E+00 0.20861E+04 
c  nu_tilda     0.83610E-05      33   0.13416E-04   0.71691E-06 0.21370E+03 
c  TempC        0.43894E+02      26   0.27134E-03   0.76438E+01 0.31222E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2839          9.1674          4.5729          4.5729
v  Velocity[Y]            -2.8934          7.1642         0.24327         0.24327
v  Velocity[Z]       -6.9287e-015     6.9892e-015    -1.5055e-017    -1.5055e-017
v  ǁVelocityǁ         0.0022531          9.1692          5.0452          5.0452
v  Pressure               -24.588          28.188           1.223           1.223
v  nu_tilda           4.4009e-007       0.0044724       0.0017872       0.0017872
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc            3.299e-014       0.0052707       0.0021012       0.0021012
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2634:        0.24250E+01

===============================================================


 INSTANT    0.263500000E+04   TIME STEP NUMBER            2635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90113E-02 0.88951E+00
   Friction velocity        uk    :  0.90113E-02 0.88951E+00
   Dimensionless distance   yplus :  0.72547E-01 0.71612E+01
   Friction thermal sca.    tstar : -0.74358E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54128E-01 0.53430E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10684E-01      33   0.21020E-03   0.45935E+01 0.19500E+03 
c  Velocity[X]                                      0.20167E+01 
c  Velocity[Y]                                      0.25768E+01 
c  Velocity[Z]                                      0.10571E-29 
c  Pressure     0.12739E-06     551   0.99067E-08   0.12089E+00 0.19238E+04 
c  nu_tilda     0.83620E-05      33   0.22818E-05   0.71689E-06 0.21369E+03 
c  TempC        0.43895E+02      26   0.30679E-03   0.50082E+01 0.24256E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2848           9.166          4.5729          4.5729
v  Velocity[Y]            -2.8926          7.1845         0.24326         0.24326
v  Velocity[Z]       -6.9287e-015     7.0164e-015    -1.5061e-017    -1.5061e-017
v  ǁVelocityǁ         0.0027994          9.1678          5.0451          5.0451
v  Pressure               -24.536          28.403          1.3089          1.3089
v  nu_tilda            4.401e-007       0.0044728       0.0017873       0.0017873
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3001e-014       0.0052712       0.0021012       0.0021012
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2635:        0.24980E+01

===============================================================


 INSTANT    0.263600000E+04   TIME STEP NUMBER            2636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.66688E-02 0.89086E+00
   Friction velocity        uk    :  0.66688E-02 0.89086E+00
   Dimensionless distance   yplus :  0.53688E-01 0.71720E+01
   Friction thermal sca.    tstar : -0.10046E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40058E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10684E-01      33   0.25254E-03   0.45859E+01 0.19495E+03 
c  Velocity[X]                                      0.20174E+01 
c  Velocity[Y]                                      0.25685E+01 
c  Velocity[Z]                                      0.12135E-29 
c  Pressure     0.11246E-06     567   0.99633E-08   0.10836E+00 0.14885E+04 
c  nu_tilda     0.83630E-05      33   0.13407E-04   0.71694E-06 0.21368E+03 
c  TempC        0.43897E+02      27   0.30715E-03   0.65551E+01 0.28485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2856          9.1646          4.5729          4.5729
v  Velocity[Y]            -2.8918          7.1924         0.24325         0.24325
v  Velocity[Z]       -7.0819e-015     7.0466e-015    -1.5061e-017    -1.5061e-017
v  ǁVelocityǁ         0.0024886          9.1664          5.0449          5.0449
v  Pressure               -24.607          28.278          1.2334          1.2334
v  nu_tilda           4.4007e-007       0.0044732       0.0017873       0.0017873
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3004e-014       0.0052717       0.0021013       0.0021013
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2636:        0.22960E+01

===============================================================


 INSTANT    0.263700000E+04   TIME STEP NUMBER            2637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.28205E-02 0.89049E+00
   Friction velocity        uk    :  0.28205E-02 0.89049E+00
   Dimensionless distance   yplus :  0.22707E-01 0.71690E+01
   Friction thermal sca.    tstar : -0.23733E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16942E-01 0.53489E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10683E-01      33   0.22661E-03   0.45803E+01 0.19481E+03 
c  Velocity[X]                                      0.20020E+01 
c  Velocity[Y]                                      0.25783E+01 
c  Velocity[Z]                                      0.18069E-29 
c  Pressure     0.11809E-06     504   0.93897E-08   0.11710E+00 0.72893E+03 
c  nu_tilda     0.83640E-05      33   0.22877E-05   0.71692E-06 0.21367E+03 
c  TempC        0.43899E+02      27   0.34768E-03   0.55471E+01 0.27443E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2863          9.1632          4.5729          4.5729
v  Velocity[Y]             -2.891          7.1667         0.24324         0.24324
v  Velocity[Z]        -7.193e-015     7.0616e-015     -1.507e-017     -1.507e-017
v  ǁVelocityǁ         0.0017344           9.165          5.0448          5.0448
v  Pressure               -24.549          28.277          1.2714          1.2714
v  nu_tilda           4.4009e-007       0.0044737       0.0017874       0.0017874
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.2994e-014       0.0052722       0.0021013       0.0021013
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2637:        0.21470E+01

===============================================================


 INSTANT    0.263800000E+04   TIME STEP NUMBER            2638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27823E-02 0.88908E+00
   Friction velocity        uk    :  0.27823E-02 0.88908E+00
   Dimensionless distance   yplus :  0.22399E-01 0.71577E+01
   Friction thermal sca.    tstar : -0.24059E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16712E-01 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10682E-01      33   0.22941E-03   0.45484E+01 0.19464E+03 
c  Velocity[X]                                      0.19887E+01 
c  Velocity[Y]                                      0.25597E+01 
c  Velocity[Z]                                      0.93429E-30 
c  Pressure     0.11256E-06     520   0.96915E-08   0.10737E+00 0.98561E+03 
c  nu_tilda     0.83650E-05      33   0.13400E-04   0.71695E-06 0.21366E+03 
c  TempC        0.43900E+02      27   0.30246E-03   0.61709E+01 0.27393E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2871          9.1618          4.5729          4.5729
v  Velocity[Y]            -2.8902          7.1809         0.24324         0.24324
v  Velocity[Z]       -7.3498e-015      7.108e-015    -1.5068e-017    -1.5068e-017
v  ǁVelocityǁ         0.0010824          9.1636          5.0446          5.0446
v  Pressure               -24.626          28.243          1.2161          1.2161
v  nu_tilda           4.4008e-007       0.0044741       0.0017874       0.0017874
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3001e-014       0.0052727       0.0021014       0.0021014
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2638:        0.21810E+01

===============================================================


 INSTANT    0.263900000E+04   TIME STEP NUMBER            2639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10197E-01 0.89032E+00
   Friction velocity        uk    :  0.10197E-01 0.89032E+00
   Dimensionless distance   yplus :  0.82092E-01 0.71677E+01
   Friction thermal sca.    tstar : -0.71260E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.61250E-01 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10682E-01      33   0.24443E-03   0.45588E+01 0.19457E+03 
c  Velocity[X]                                      0.20116E+01 
c  Velocity[Y]                                      0.25472E+01 
c  Velocity[Z]                                      0.16973E-29 
c  Pressure     0.12136E-06     536   0.93009E-08   0.11821E+00 0.87656E+03 
c  nu_tilda     0.83660E-05      33   0.22854E-05   0.71696E-06 0.21365E+03 
c  TempC        0.43902E+02      27   0.31354E-03   0.54474E+01 0.26854E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2879          9.1604          4.5729          4.5729
v  Velocity[Y]            -2.8893          7.1634         0.24323         0.24323
v  Velocity[Z]       -7.4273e-015     7.1208e-015    -1.5075e-017    -1.5075e-017
v  ǁVelocityǁ        0.00083925          9.1622          5.0444          5.0444
v  Pressure               -24.567          28.271          1.2624          1.2624
v  nu_tilda            4.401e-007       0.0044744       0.0017875       0.0017875
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2999e-014       0.0052731       0.0021014       0.0021014
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2639:        0.22280E+01

===============================================================


 INSTANT    0.264000000E+04   TIME STEP NUMBER            2640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.99447E-02 0.88951E+00
   Friction velocity        uk    :  0.99447E-02 0.88951E+00
   Dimensionless distance   yplus :  0.80061E-01 0.71612E+01
   Friction thermal sca.    tstar : -0.75313E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59735E-01 0.53430E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10681E-01      33   0.19154E-03   0.45657E+01 0.19487E+03 
c  Velocity[X]                                      0.19905E+01 
c  Velocity[Y]                                      0.25752E+01 
c  Velocity[Z]                                      0.95394E-30 
c  Pressure     0.11422E-06     521   0.98840E-08   0.11149E+00 0.10079E+04 
c  nu_tilda     0.83670E-05      33   0.13391E-04   0.71700E-06 0.21364E+03 
c  TempC        0.43903E+02      27   0.27737E-03   0.65878E+01 0.28648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2886           9.159          4.5729          4.5729
v  Velocity[Y]            -2.8885          7.1865         0.24322         0.24322
v  Velocity[Z]       -7.5415e-015     7.1497e-015    -1.5071e-017    -1.5071e-017
v  ǁVelocityǁ         0.0013505          9.1608          5.0443          5.0443
v  Pressure               -24.642          28.237          1.2065          1.2065
v  nu_tilda           4.4009e-007       0.0044748       0.0017875       0.0017875
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3004e-014       0.0052736       0.0021015       0.0021015
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2640:        0.22020E+01

===============================================================


 INSTANT    0.264100000E+04   TIME STEP NUMBER            2641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13240E-01 0.89099E+00
   Friction velocity        uk    :  0.13240E-01 0.89099E+00
   Dimensionless distance   yplus :  0.10659E+00 0.71731E+01
   Friction thermal sca.    tstar : -0.78748E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79528E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10681E-01      33   0.25480E-03   0.45428E+01 0.19466E+03 
c  Velocity[X]                                      0.19834E+01 
c  Velocity[Y]                                      0.25594E+01 
c  Velocity[Z]                                      0.12590E-29 
c  Pressure     0.11570E-06     520   0.89970E-08   0.11068E+00 0.11623E+04 
c  nu_tilda     0.83680E-05      33   0.22939E-05   0.71701E-06 0.21364E+03 
c  TempC        0.43905E+02      27   0.28656E-03   0.57625E+01 0.26212E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2894          9.1577          4.5729          4.5729
v  Velocity[Y]            -2.8877          7.1927         0.24321         0.24321
v  Velocity[Z]       -7.5773e-015     7.1753e-015    -1.5076e-017    -1.5076e-017
v  ǁVelocityǁ         0.0021834          9.1595          5.0441          5.0441
v  Pressure               -24.585          28.328          1.2646          1.2646
v  nu_tilda           4.4006e-007       0.0044752       0.0017876       0.0017876
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3002e-014        0.005274       0.0021015       0.0021015
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2641:        0.21740E+01

===============================================================


 INSTANT    0.264200000E+04   TIME STEP NUMBER            2642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13800E-01 0.89066E+00
   Friction velocity        uk    :  0.13800E-01 0.89066E+00
   Dimensionless distance   yplus :  0.11110E+00 0.71704E+01
   Friction thermal sca.    tstar : -0.84327E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82890E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10680E-01      33   0.24934E-03   0.45899E+01 0.19485E+03 
c  Velocity[X]                                      0.20378E+01 
c  Velocity[Y]                                      0.25521E+01 
c  Velocity[Z]                                      0.18064E-29 
c  Pressure     0.12787E-06     533   0.89186E-08   0.12491E+00 0.19458E+04 
c  nu_tilda     0.83690E-05      33   0.13384E-04   0.71704E-06 0.21363E+03 
c  TempC        0.43907E+02      27   0.23345E-03   0.50704E+01 0.23899E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2901          9.1563          4.5729          4.5729
v  Velocity[Y]            -2.8869          7.1664          0.2432          0.2432
v  Velocity[Z]       -7.6687e-015     7.2033e-015    -1.5081e-017    -1.5081e-017
v  ǁVelocityǁ         0.0016857          9.1581           5.044           5.044
v  Pressure               -24.658           28.12          1.1718          1.1718
v  nu_tilda           4.4011e-007       0.0044756       0.0017876       0.0017876
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2994e-014       0.0052745       0.0021016       0.0021016
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2642:        0.22100E+01

===============================================================


 INSTANT    0.264300000E+04   TIME STEP NUMBER            2643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15677E-01 0.88941E+00
   Friction velocity        uk    :  0.15677E-01 0.88941E+00
   Dimensionless distance   yplus :  0.12621E+00 0.71604E+01
   Friction thermal sca.    tstar : -0.90671E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94166E-01 0.53424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10680E-01      33   0.22966E-03   0.45520E+01 0.19462E+03 
c  Velocity[X]                                      0.19926E+01 
c  Velocity[Y]                                      0.25593E+01 
c  Velocity[Z]                                      0.77270E-30 
c  Pressure     0.10285E-06     568   0.89770E-08   0.99638E-01 0.18253E+04 
c  nu_tilda     0.83700E-05      33   0.22903E-05   0.71705E-06 0.21362E+03 
c  TempC        0.43908E+02      27   0.26505E-03   0.48790E+01 0.24715E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2908          9.1549          4.5729          4.5729
v  Velocity[Y]            -2.8861           7.187         0.24319         0.24319
v  Velocity[Z]       -7.5684e-015     7.2151e-015    -1.5081e-017    -1.5081e-017
v  ǁVelocityǁ         0.0010344          9.1567          5.0438          5.0438
v  Pressure               -24.604           28.33          1.2531          1.2531
v  nu_tilda           4.4013e-007        0.004476       0.0017877       0.0017877
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3006e-014        0.005275       0.0021016       0.0021016
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2643:        0.22940E+01

===============================================================


 INSTANT    0.264400000E+04   TIME STEP NUMBER            2644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94609E-02 0.89030E+00
   Friction velocity        uk    :  0.94609E-02 0.89030E+00
   Dimensionless distance   yplus :  0.76167E-01 0.71675E+01
   Friction thermal sca.    tstar : -0.99659E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56829E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10679E-01      33   0.24227E-03   0.45377E+01 0.19450E+03 
c  Velocity[X]                                      0.19958E+01 
c  Velocity[Y]                                      0.25419E+01 
c  Velocity[Z]                                      0.16479E-29 
c  Pressure     0.11319E-06     584   0.95063E-08   0.10928E+00 0.22287E+04 
c  nu_tilda     0.83710E-05      33   0.13374E-04   0.71710E-06 0.21361E+03 
c  TempC        0.43910E+02      27   0.34267E-03   0.51237E+01 0.25739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2916          9.1535          4.5729          4.5729
v  Velocity[Y]            -2.8853          7.1593         0.24319         0.24319
v  Velocity[Z]       -7.7532e-015     7.2516e-015    -1.5081e-017    -1.5081e-017
v  ǁVelocityǁ         0.0011961          9.1553          5.0436          5.0436
v  Pressure               -24.674          28.072           1.152           1.152
v  nu_tilda           4.4022e-007       0.0044764       0.0017877       0.0017877
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3014e-014       0.0052755       0.0021017       0.0021017
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2644:        0.23420E+01

===============================================================


 INSTANT    0.264500000E+04   TIME STEP NUMBER            2645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95921E-02 0.88964E+00
   Friction velocity        uk    :  0.95921E-02 0.88964E+00
   Dimensionless distance   yplus :  0.77223E-01 0.71622E+01
   Friction thermal sca.    tstar : -0.11100E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57617E-01 0.53438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10679E-01      33   0.24165E-03   0.45563E+01 0.19471E+03 
c  Velocity[X]                                      0.20128E+01 
c  Velocity[Y]                                      0.25435E+01 
c  Velocity[Z]                                      0.97212E-30 
c  Pressure     0.10317E-06     570   0.95976E-08   0.99661E-01 0.21746E+04 
c  nu_tilda     0.83719E-05      33   0.22963E-05   0.71708E-06 0.21360E+03 
c  TempC        0.43911E+02      27   0.28658E-03   0.78388E+01 0.29934E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2924          9.1521          4.5729          4.5729
v  Velocity[Y]            -2.8844          7.1866         0.24317         0.24317
v  Velocity[Z]       -7.6147e-015     7.2642e-015    -1.5079e-017    -1.5079e-017
v  ǁVelocityǁ         0.0027279           9.154          5.0435          5.0435
v  Pressure               -24.622           28.33          1.2461          1.2461
v  nu_tilda           4.4021e-007       0.0044768       0.0017878       0.0017878
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3041e-014       0.0052759       0.0021017       0.0021017
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2645:        0.23080E+01

===============================================================


 INSTANT    0.264600000E+04   TIME STEP NUMBER            2646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14065E-01 0.89076E+00
   Friction velocity        uk    :  0.14065E-01 0.89076E+00
   Dimensionless distance   yplus :  0.11323E+00 0.71712E+01
   Friction thermal sca.    tstar : -0.11961E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84484E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10678E-01      33   0.23281E-03   0.45315E+01 0.19459E+03 
c  Velocity[X]                                      0.19758E+01 
c  Velocity[Y]                                      0.25557E+01 
c  Velocity[Z]                                      0.11675E-29 
c  Pressure     0.10263E-06     520   0.91838E-08   0.10000E+00 0.16963E+04 
c  nu_tilda     0.83729E-05      33   0.13366E-04   0.71714E-06 0.21360E+03 
c  TempC        0.43913E+02      26   0.27582E-03   0.60042E+01 0.26365E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2931          9.1507          4.5729          4.5729
v  Velocity[Y]            -2.8836          7.1927         0.24317         0.24317
v  Velocity[Z]       -7.8183e-015     7.2907e-015    -1.5081e-017    -1.5081e-017
v  ǁVelocityǁ         0.0021725          9.1526          5.0433          5.0433
v  Pressure               -24.694          28.176          1.1614          1.1614
v  nu_tilda           4.4009e-007       0.0044772       0.0017878       0.0017878
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3036e-014       0.0052764       0.0021018       0.0021018
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2646:        0.21740E+01

===============================================================


 INSTANT    0.264700000E+04   TIME STEP NUMBER            2647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53737E-02 0.89033E+00
   Friction velocity        uk    :  0.53737E-02 0.89033E+00
   Dimensionless distance   yplus :  0.43262E-01 0.71678E+01
   Friction thermal sca.    tstar : -0.14437E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32278E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10677E-01      33   0.24431E-03   0.45451E+01 0.19450E+03 
c  Velocity[X]                                      0.20102E+01 
c  Velocity[Y]                                      0.25349E+01 
c  Velocity[Z]                                      0.15475E-29 
c  Pressure     0.12908E-06     490   0.97752E-08   0.12454E+00 0.69975E+03 
c  nu_tilda     0.83739E-05      33   0.22959E-05   0.71713E-06 0.21359E+03 
c  TempC        0.43914E+02      26   0.29139E-03   0.44614E+01 0.23090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2939          9.1494          4.5729          4.5729
v  Velocity[Y]            -2.8828           7.162         0.24315         0.24315
v  Velocity[Z]       -7.6571e-015     7.3119e-015    -1.5083e-017    -1.5083e-017
v  ǁVelocityǁ         0.0022829          9.1512          5.0432          5.0432
v  Pressure               -24.636          28.159          1.1975          1.1975
v  nu_tilda            4.401e-007       0.0044776       0.0017879       0.0017879
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3001e-014       0.0052768       0.0021018       0.0021018
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2647:        0.21210E+01

===============================================================


 INSTANT    0.264800000E+04   TIME STEP NUMBER            2648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13357E-01 0.88906E+00
   Friction velocity        uk    :  0.13357E-01 0.88906E+00
   Dimensionless distance   yplus :  0.10754E+00 0.71576E+01
   Friction thermal sca.    tstar : -0.20182E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80234E-01 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10677E-01      33   0.24741E-03   0.45512E+01 0.19458E+03 
c  Velocity[X]                                      0.20214E+01 
c  Velocity[Y]                                      0.25298E+01 
c  Velocity[Z]                                      0.11352E-29 
c  Pressure     0.11595E-06     504   0.96564E-08   0.11133E+00 0.87822E+03 
c  nu_tilda     0.83749E-05      33   0.13361E-04   0.71717E-06 0.21358E+03 
c  TempC        0.43916E+02      27   0.28632E-03   0.62818E+01 0.26872E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2946           9.148          4.5729          4.5729
v  Velocity[Y]             -2.882          7.1827         0.24314         0.24314
v  Velocity[Z]       -7.8995e-015     7.3344e-015    -1.5079e-017    -1.5079e-017
v  ǁVelocityǁ         0.0021902          9.1498           5.043           5.043
v  Pressure               -24.713          28.153          1.1479          1.1479
v  nu_tilda           4.4017e-007        0.004478       0.0017878       0.0017878
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3006e-014       0.0052773       0.0021019       0.0021019
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2648:        0.21580E+01

===============================================================


 INSTANT    0.264900000E+04   TIME STEP NUMBER            2649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42728E-02 0.89031E+00
   Friction velocity        uk    :  0.42728E-02 0.89031E+00
   Dimensionless distance   yplus :  0.34399E-01 0.71676E+01
   Friction thermal sca.    tstar : -0.31760E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25666E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10676E-01      33   0.24062E-03   0.45428E+01 0.19450E+03 
c  Velocity[X]                                      0.20005E+01 
c  Velocity[Y]                                      0.25423E+01 
c  Velocity[Z]                                      0.17475E-29 
c  Pressure     0.11264E-06     472   0.99210E-08   0.11097E+00 0.69947E+03 
c  nu_tilda     0.83758E-05      33   0.22993E-05   0.71720E-06 0.21357E+03 
c  TempC        0.43917E+02      26   0.32899E-03   0.60326E+01 0.27283E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2953          9.1466          4.5729          4.5729
v  Velocity[Y]            -2.8812          7.1625         0.24313         0.24313
v  Velocity[Z]       -7.7099e-015     7.3441e-015    -1.5072e-017    -1.5072e-017
v  ǁVelocityǁ         0.0026789          9.1484          5.0429          5.0429
v  Pressure               -24.652          28.148          1.1843          1.1843
v  nu_tilda           4.4024e-007       0.0044784       0.0017879       0.0017879
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3025e-014       0.0052778       0.0021019       0.0021019
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2649:        0.20840E+01

===============================================================


 INSTANT    0.265000000E+04   TIME STEP NUMBER            2650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11467E-01 0.88945E+00
   Friction velocity        uk    :  0.11467E-01 0.88945E+00
   Dimensionless distance   yplus :  0.92319E-01 0.71607E+01
   Friction thermal sca.    tstar : -0.23503E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68880E-01 0.53427E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10676E-01      33   0.17999E-03   0.45291E+01 0.19452E+03 
c  Velocity[X]                                      0.19951E+01 
c  Velocity[Y]                                      0.25340E+01 
c  Velocity[Z]                                      0.10796E-29 
c  Pressure     0.11688E-06     504   0.88776E-08   0.11180E+00 0.82243E+03 
c  nu_tilda     0.83768E-05      33   0.13350E-04   0.71724E-06 0.21357E+03 
c  TempC        0.43919E+02      26   0.27543E-03   0.63363E+01 0.28582E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.296          9.1452          4.5729          4.5729
v  Velocity[Y]            -2.8804          7.1814         0.24312         0.24312
v  Velocity[Z]       -7.9691e-015     7.3813e-015    -1.5072e-017    -1.5072e-017
v  ǁVelocityǁ         0.0033732           9.147          5.0427          5.0427
v  Pressure               -24.733          28.141           1.138           1.138
v  nu_tilda           4.4022e-007       0.0044788       0.0017879       0.0017879
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3046e-014       0.0052782        0.002102        0.002102
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2650:        0.21410E+01

===============================================================


 INSTANT    0.265100000E+04   TIME STEP NUMBER            2651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.75319E-02 0.89106E+00
   Friction velocity        uk    :  0.75319E-02 0.89106E+00
   Dimensionless distance   yplus :  0.60637E-01 0.71737E+01
   Friction thermal sca.    tstar : -0.22489E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45242E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10675E-01      33   0.24393E-03   0.45119E+01 0.19422E+03 
c  Velocity[X]                                      0.19957E+01 
c  Velocity[Y]                                      0.25163E+01 
c  Velocity[Z]                                      0.13058E-29 
c  Pressure     0.10449E-06     520   0.90203E-08   0.10054E+00 0.10122E+04 
c  nu_tilda     0.83777E-05      33   0.23015E-05   0.71724E-06 0.21356E+03 
c  TempC        0.43920E+02      26   0.25430E-03   0.75457E+01 0.28408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2967          9.1438          4.5729          4.5729
v  Velocity[Y]            -2.8795          7.1948         0.24311         0.24311
v  Velocity[Z]       -7.7425e-015     7.3874e-015    -1.5075e-017    -1.5075e-017
v  ǁVelocityǁ         0.0024381          9.1457          5.0425          5.0425
v  Pressure               -24.676          28.227          1.1876          1.1876
v  nu_tilda           4.4017e-007       0.0044791        0.001788        0.001788
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc            3.304e-014       0.0052787        0.002102        0.002102
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2651:        0.21910E+01

===============================================================


 INSTANT    0.265200000E+04   TIME STEP NUMBER            2652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12510E-01 0.89063E+00
   Friction velocity        uk    :  0.12510E-01 0.89063E+00
   Dimensionless distance   yplus :  0.10071E+00 0.71702E+01
   Friction thermal sca.    tstar : -0.14378E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75143E-01 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10675E-01      33   0.23559E-03   0.45373E+01 0.19448E+03 
c  Velocity[X]                                      0.20026E+01 
c  Velocity[Y]                                      0.25347E+01 
c  Velocity[Z]                                      0.14938E-29 
c  Pressure     0.11381E-06     552   0.89487E-08   0.11222E+00 0.19401E+04 
c  nu_tilda     0.83787E-05      33   0.13344E-04   0.71727E-06 0.21355E+03 
c  TempC        0.43922E+02      26   0.31224E-03   0.48248E+01 0.24368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2974          9.1424          4.5729          4.5729
v  Velocity[Y]            -2.8787          7.1652         0.24309         0.24309
v  Velocity[Z]       -8.0412e-015     7.4078e-015    -1.5072e-017    -1.5072e-017
v  ǁVelocityǁ          0.002364          9.1443          5.0424          5.0424
v  Pressure                -24.75          28.013          1.0959          1.0959
v  nu_tilda           4.4019e-007       0.0044795        0.001788        0.001788
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3025e-014       0.0052791       0.0021021       0.0021021
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2652:        0.22570E+01

===============================================================


 INSTANT    0.265300000E+04   TIME STEP NUMBER            2653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10110E-01 0.88921E+00
   Friction velocity        uk    :  0.10110E-01 0.88921E+00
   Dimensionless distance   yplus :  0.81390E-01 0.71587E+01
   Friction thermal sca.    tstar : -0.12406E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60726E-01 0.53412E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10674E-01      33   0.23484E-03   0.45147E+01 0.19429E+03 
c  Velocity[X]                                      0.19971E+01 
c  Velocity[Y]                                      0.25176E+01 
c  Velocity[Z]                                      0.10891E-29 
c  Pressure     0.10042E-06     553   0.98968E-08   0.96208E-01 0.15998E+04 
c  nu_tilda     0.83796E-05      33   0.23028E-05   0.71728E-06 0.21354E+03 
c  TempC        0.43923E+02      27   0.28380E-03   0.61991E+01 0.27318E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2981           9.141          4.5729          4.5729
v  Velocity[Y]            -2.8779          7.1829         0.24308         0.24308
v  Velocity[Z]       -7.7891e-015      7.428e-015    -1.5071e-017    -1.5071e-017
v  ǁVelocityǁ         0.0011272          9.1429          5.0422          5.0422
v  Pressure               -24.694          28.185          1.1695          1.1695
v  nu_tilda           4.4019e-007       0.0044799       0.0017881       0.0017881
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3033e-014       0.0052795       0.0021021       0.0021021
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2653:        0.22470E+01

===============================================================


 INSTANT    0.265400000E+04   TIME STEP NUMBER            2654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13943E-01 0.89028E+00
   Friction velocity        uk    :  0.13943E-01 0.89028E+00
   Dimensionless distance   yplus :  0.11225E+00 0.71673E+01
   Friction thermal sca.    tstar : -0.10673E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83753E-01 0.53476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10673E-01      33   0.27805E-03   0.45282E+01 0.19456E+03 
c  Velocity[X]                                      0.20095E+01 
c  Velocity[Y]                                      0.25187E+01 
c  Velocity[Z]                                      0.15565E-29 
c  Pressure     0.10891E-06     536   0.94437E-08   0.10759E+00 0.18217E+04 
c  nu_tilda     0.83805E-05      33   0.13335E-04   0.71735E-06 0.21354E+03 
c  TempC        0.43925E+02      26   0.31448E-03   0.69356E+01 0.27885E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2987          9.1397          4.5729          4.5729
v  Velocity[Y]            -2.8771          7.1604         0.24307         0.24307
v  Velocity[Z]       -7.7748e-015     7.4493e-015    -1.5068e-017    -1.5068e-017
v  ǁVelocityǁ         0.0015472          9.1415          5.0421          5.0421
v  Pressure               -24.768          27.992          1.0819          1.0819
v  nu_tilda           4.4018e-007       0.0044803       0.0017881       0.0017881
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3032e-014         0.00528       0.0021022       0.0021022
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2654:        0.22100E+01

===============================================================


 INSTANT    0.265500000E+04   TIME STEP NUMBER            2655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11155E-01 0.88957E+00
   Friction velocity        uk    :  0.11155E-01 0.88957E+00
   Dimensionless distance   yplus :  0.89804E-01 0.71617E+01
   Friction thermal sca.    tstar : -0.98680E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67004E-01 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10673E-01      33   0.23349E-03   0.45500E+01 0.19438E+03 
c  Velocity[X]                                      0.20256E+01 
c  Velocity[Y]                                      0.25244E+01 
c  Velocity[Z]                                      0.99800E-30 
c  Pressure     0.12497E-06     553   0.92842E-08   0.11970E+00 0.17479E+04 
c  nu_tilda     0.83815E-05      33   0.23073E-05   0.71735E-06 0.21353E+03 
c  TempC        0.43926E+02      27   0.26913E-03   0.52340E+01 0.25665E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2994          9.1383          4.5729          4.5729
v  Velocity[Y]            -2.8763          7.1862         0.24305         0.24305
v  Velocity[Z]       -7.7374e-015     7.4565e-015     -1.507e-017     -1.507e-017
v  ǁVelocityǁ         0.0020093          9.1401          5.0419          5.0419
v  Pressure               -24.715          28.193          1.1592          1.1592
v  nu_tilda           4.4014e-007       0.0044807       0.0017882       0.0017882
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3028e-014       0.0052805       0.0021022       0.0021022
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2655:        0.22500E+01

===============================================================


 INSTANT    0.265600000E+04   TIME STEP NUMBER            2656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11700E-01 0.89081E+00
   Friction velocity        uk    :  0.11700E-01 0.89081E+00
   Dimensionless distance   yplus :  0.94194E-01 0.71717E+01
   Friction thermal sca.    tstar : -0.90427E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.70279E-01 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10672E-01      33   0.21700E-03   0.45080E+01 0.19433E+03 
c  Velocity[X]                                      0.19948E+01 
c  Velocity[Y]                                      0.25133E+01 
c  Velocity[Z]                                      0.13730E-29 
c  Pressure     0.11411E-06     552   0.91183E-08   0.10958E+00 0.15918E+04 
c  nu_tilda     0.83824E-05      33   0.13326E-04   0.71738E-06 0.21352E+03 
c  TempC        0.43927E+02      27   0.28960E-03   0.39427E+01 0.22624E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3001          9.1369          4.5729          4.5729
v  Velocity[Y]            -2.8754          7.1879         0.24304         0.24304
v  Velocity[Z]       -7.7872e-015     7.4891e-015    -1.5069e-017    -1.5069e-017
v  ǁVelocityǁ         0.0025174          9.1387          5.0418          5.0418
v  Pressure                -24.79          28.043          1.0795          1.0795
v  nu_tilda           4.4012e-007        0.004481       0.0017881       0.0017881
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3018e-014       0.0052809       0.0021023       0.0021023
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2656:        0.22550E+01

===============================================================


 INSTANT    0.265700000E+04   TIME STEP NUMBER            2657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24677E-02 0.89064E+00
   Friction velocity        uk    :  0.24677E-02 0.89064E+00
   Dimensionless distance   yplus :  0.19866E-01 0.71702E+01
   Friction thermal sca.    tstar : -0.85327E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14823E-01 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10672E-01      33   0.23605E-03   0.45080E+01 0.19427E+03 
c  Velocity[X]                                      0.20043E+01 
c  Velocity[Y]                                      0.25037E+01 
c  Velocity[Z]                                      0.16663E-29 
c  Pressure     0.11460E-06     489   0.91976E-08   0.11274E+00 0.82582E+03 
c  nu_tilda     0.83833E-05      33   0.23068E-05   0.71738E-06 0.21351E+03 
c  TempC        0.43929E+02      27   0.29506E-03   0.55873E+01 0.25889E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3008          9.1355          4.5729          4.5729
v  Velocity[Y]            -2.8745          7.1646         0.24302         0.24302
v  Velocity[Z]       -7.7812e-015     7.4966e-015    -1.5072e-017    -1.5072e-017
v  ǁVelocityǁ         0.0018975          9.1374          5.0416          5.0416
v  Pressure               -24.731          28.073          1.1229          1.1229
v  nu_tilda           4.4014e-007       0.0044814       0.0017882       0.0017882
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3012e-014       0.0052814       0.0021023       0.0021023
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2657:        0.21010E+01

===============================================================


 INSTANT    0.265800000E+04   TIME STEP NUMBER            2658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12517E-02 0.88922E+00
   Friction velocity        uk    :  0.12517E-02 0.88922E+00
   Dimensionless distance   yplus :  0.10077E-01 0.71589E+01
   Friction thermal sca.    tstar : -0.78287E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75183E-02 0.53413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10671E-01      33   0.25685E-03   0.45025E+01 0.19427E+03 
c  Velocity[X]                                      0.19853E+01 
c  Velocity[Y]                                      0.25173E+01 
c  Velocity[Z]                                      0.10237E-29 
c  Pressure     0.10888E-06     506   0.98928E-08   0.10491E+00 0.84168E+03 
c  nu_tilda     0.83843E-05      33   0.13320E-04   0.71744E-06 0.21350E+03 
c  TempC        0.43930E+02      26   0.31714E-03   0.61365E+01 0.26371E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3015          9.1341          4.5729          4.5729
v  Velocity[Y]            -2.8737           7.183           0.243           0.243
v  Velocity[Z]       -8.1849e-015     7.5154e-015     -1.507e-017     -1.507e-017
v  ǁVelocityǁ         0.0015163           9.136          5.0415          5.0415
v  Pressure                -24.81          28.062          1.0754          1.0754
v  nu_tilda           4.4014e-007       0.0044817       0.0017882       0.0017882
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3016e-014       0.0052818       0.0021023       0.0021023
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2658:        0.21570E+01

===============================================================


 INSTANT    0.265900000E+04   TIME STEP NUMBER            2659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13738E-01 0.89034E+00
   Friction velocity        uk    :  0.13738E-01 0.89034E+00
   Dimensionless distance   yplus :  0.11060E+00 0.71679E+01
   Friction thermal sca.    tstar : -0.76687E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82521E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10670E-01      33   0.24313E-03   0.45471E+01 0.19457E+03 
c  Velocity[X]                                      0.20279E+01 
c  Velocity[Y]                                      0.25193E+01 
c  Velocity[Z]                                      0.13870E-29 
c  Pressure     0.14041E-06     409   0.93580E-08   0.13508E+00 0.62440E+03 
c  nu_tilda     0.83852E-05      33   0.23136E-05   0.71746E-06 0.21350E+03 
c  TempC        0.43932E+02      26   0.27197E-03   0.62283E+01 0.27498E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3021          9.1328          4.5729          4.5729
v  Velocity[Y]            -2.8729          7.1592         0.24299         0.24299
v  Velocity[Z]       -7.8689e-015     7.5262e-015    -1.5068e-017    -1.5068e-017
v  ǁVelocityǁ         0.0011367          9.1346          5.0413          5.0413
v  Pressure               -24.746          27.982          1.0916          1.0916
v  nu_tilda           4.4022e-007       0.0044821       0.0017883       0.0017883
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3016e-014       0.0052822       0.0021024       0.0021024
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2659:        0.19200E+01

===============================================================


 INSTANT    0.266000000E+04   TIME STEP NUMBER            2660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.30039E-02 0.88991E+00
   Friction velocity        uk    :  0.30039E-02 0.88991E+00
   Dimensionless distance   yplus :  0.24184E-01 0.71644E+01
   Friction thermal sca.    tstar : -0.69955E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18044E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10670E-01      33   0.19385E-03   0.45200E+01 0.19429E+03 
c  Velocity[X]                                      0.20190E+01 
c  Velocity[Y]                                      0.25010E+01 
c  Velocity[Z]                                      0.10531E-29 
c  Pressure     0.10658E-06     458   0.94525E-08   0.10343E+00 0.72729E+03 
c  nu_tilda     0.83861E-05      33   0.13311E-04   0.71754E-06 0.21350E+03 
c  TempC        0.43933E+02      26   0.26276E-03   0.59947E+01 0.27157E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3028          9.1314          4.5729          4.5729
v  Velocity[Y]            -2.8721          7.1846         0.24297         0.24297
v  Velocity[Z]       -7.8454e-015     7.5472e-015     -1.507e-017     -1.507e-017
v  ǁVelocityǁ         0.0009534          9.1332          5.0412          5.0412
v  Pressure               -24.831          28.057          1.0623          1.0623
v  nu_tilda           4.4021e-007       0.0044825       0.0017883       0.0017883
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3041e-014       0.0052826       0.0021024       0.0021024
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2660:        0.20420E+01

===============================================================


 INSTANT    0.266100000E+04   TIME STEP NUMBER            2661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13577E-01 0.89133E+00
   Friction velocity        uk    :  0.13577E-01 0.89133E+00
   Dimensionless distance   yplus :  0.10931E+00 0.71758E+01
   Friction thermal sca.    tstar : -0.69887E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81554E-01 0.53539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10669E-01      33   0.22669E-03   0.44890E+01 0.19420E+03 
c  Velocity[X]                                      0.19756E+01 
c  Velocity[Y]                                      0.25135E+01 
c  Velocity[Z]                                      0.15828E-29 
c  Pressure     0.89979E-07     520   0.92481E-08   0.87681E-01 0.80055E+03 
c  nu_tilda     0.83870E-05      33   0.23129E-05   0.71751E-06 0.21349E+03 
c  TempC        0.43934E+02      26   0.34907E-03   0.55279E+01 0.26443E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3034            9.13          4.5729          4.5729
v  Velocity[Y]            -2.8712          7.1968         0.24296         0.24296
v  Velocity[Z]       -7.8076e-015     7.5519e-015    -1.5071e-017    -1.5071e-017
v  ǁVelocityǁ         0.0011689          9.1318           5.041           5.041
v  Pressure                -24.77          28.103          1.1034          1.1034
v  nu_tilda           4.4009e-007       0.0044829       0.0017884       0.0017884
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3037e-014       0.0052831       0.0021024       0.0021024
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2661:        0.21780E+01

===============================================================


 INSTANT    0.266200000E+04   TIME STEP NUMBER            2662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.86446E-02 0.89089E+00
   Friction velocity        uk    :  0.86446E-02 0.89089E+00
   Dimensionless distance   yplus :  0.69595E-01 0.71723E+01
   Friction thermal sca.    tstar : -0.65100E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51926E-01 0.53513E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10668E-01      33   0.24592E-03   0.45049E+01 0.19423E+03 
c  Velocity[X]                                      0.20063E+01 
c  Velocity[Y]                                      0.24986E+01 
c  Velocity[Z]                                      0.94393E-30 
c  Pressure     0.11760E-06     554   0.95582E-08   0.11393E+00 0.18253E+04 
c  nu_tilda     0.83879E-05      33   0.13302E-04   0.71756E-06 0.21348E+03 
c  TempC        0.43936E+02      26   0.28093E-03   0.67631E+01 0.30038E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3041          9.1286          4.5729          4.5729
v  Velocity[Y]            -2.8703          7.1631         0.24294         0.24294
v  Velocity[Z]       -7.8445e-015     7.5804e-015    -1.5071e-017    -1.5071e-017
v  ǁVelocityǁ         0.0019811          9.1305          5.0409          5.0409
v  Pressure               -24.846          27.901          1.0166          1.0166
v  nu_tilda           4.4006e-007       0.0044833       0.0017883       0.0017883
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3002e-014       0.0052835       0.0021025       0.0021025
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2662:        0.22650E+01

===============================================================


 INSTANT    0.266300000E+04   TIME STEP NUMBER            2663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.66141E-02 0.88956E+00
   Friction velocity        uk    :  0.66141E-02 0.88956E+00
   Dimensionless distance   yplus :  0.53248E-01 0.71616E+01
   Friction thermal sca.    tstar : -0.63546E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39729E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10668E-01      33   0.26639E-03   0.45198E+01 0.19430E+03 
c  Velocity[X]                                      0.20285E+01 
c  Velocity[Y]                                      0.24913E+01 
c  Velocity[Z]                                      0.15050E-29 
c  Pressure     0.11226E-06     537   0.92629E-08   0.10890E+00 0.15632E+04 
c  nu_tilda     0.83888E-05      33   0.23184E-05   0.71758E-06 0.21347E+03 
c  TempC        0.43937E+02      26   0.27310E-03   0.68870E+01 0.28491E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3047          9.1272          4.5729          4.5729
v  Velocity[Y]            -2.8695          7.1867         0.24292         0.24292
v  Velocity[Z]        -7.817e-015      7.585e-015    -1.5068e-017    -1.5068e-017
v  ǁVelocityǁ         0.0020366          9.1291          5.0407          5.0407
v  Pressure               -24.788          28.078          1.0873          1.0873
v  nu_tilda           4.4008e-007       0.0044836       0.0017884       0.0017884
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2993e-014        0.005284       0.0021025       0.0021025
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2663:        0.25250E+01

===============================================================


 INSTANT    0.266400000E+04   TIME STEP NUMBER            2664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13341E-01 0.89054E+00
   Friction velocity        uk    :  0.13341E-01 0.89054E+00
   Dimensionless distance   yplus :  0.10740E+00 0.71695E+01
   Friction thermal sca.    tstar : -0.60111E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80133E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10667E-01      33   0.24447E-03   0.45221E+01 0.19454E+03 
c  Velocity[X]                                      0.20025E+01 
c  Velocity[Y]                                      0.25196E+01 
c  Velocity[Z]                                      0.86762E-30 
c  Pressure     0.10773E-06     569   0.97995E-08   0.10513E+00 0.17823E+04 
c  nu_tilda     0.83897E-05      33   0.13295E-04   0.71765E-06 0.21347E+03 
c  TempC        0.43938E+02      26   0.29503E-03   0.53785E+01 0.25370E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3053          9.1258          4.5729          4.5729
v  Velocity[Y]            -2.8687          7.1629          0.2429          0.2429
v  Velocity[Z]       -7.8597e-015     7.6037e-015    -1.5063e-017    -1.5063e-017
v  ǁVelocityǁ         0.0013319          9.1277          5.0406          5.0406
v  Pressure               -24.862          27.885          1.0025          1.0025
v  nu_tilda           4.4015e-007       0.0044839       0.0017884       0.0017884
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2999e-014       0.0052844       0.0021026       0.0021026
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2664:        0.24520E+01

===============================================================


 INSTANT    0.266500000E+04   TIME STEP NUMBER            2665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11312E-01 0.88969E+00
   Friction velocity        uk    :  0.11312E-01 0.88969E+00
   Dimensionless distance   yplus :  0.91068E-01 0.71626E+01
   Friction thermal sca.    tstar : -0.59140E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67947E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10667E-01      33   0.24516E-03   0.45051E+01 0.19427E+03 
c  Velocity[X]                                      0.20068E+01 
c  Velocity[Y]                                      0.24983E+01 
c  Velocity[Z]                                      0.12256E-29 
c  Pressure     0.11803E-06     553   0.92571E-08   0.11356E+00 0.17064E+04 
c  nu_tilda     0.83906E-05      33   0.23172E-05   0.71766E-06 0.21346E+03 
c  TempC        0.43940E+02      26   0.23713E-03   0.49069E+01 0.25185E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3059          9.1245          4.5729          4.5729
v  Velocity[Y]            -2.8679          7.1843         0.24288         0.24288
v  Velocity[Z]       -7.8282e-015     7.6172e-015    -1.5066e-017    -1.5066e-017
v  ǁVelocityǁ         0.0013701          9.1263          5.0405          5.0405
v  Pressure               -24.808          28.074          1.0791          1.0791
v  nu_tilda           4.4014e-007       0.0044843       0.0017885       0.0017885
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3019e-014       0.0052848       0.0021026       0.0021026
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2665:        0.22730E+01

===============================================================


 INSTANT    0.266600000E+04   TIME STEP NUMBER            2666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.37374E-02 0.89096E+00
   Friction velocity        uk    :  0.37374E-02 0.89096E+00
   Dimensionless distance   yplus :  0.30089E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.17493E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.22449E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10666E-01      33   0.24356E-03   0.44902E+01 0.19421E+03 
c  Velocity[X]                                      0.20002E+01 
c  Velocity[Y]                                      0.24900E+01 
c  Velocity[Z]                                      0.15164E-29 
c  Pressure     0.95520E-07     538   0.97267E-08   0.92705E-01 0.13513E+04 
c  nu_tilda     0.83915E-05      33   0.13286E-04   0.71771E-06 0.21346E+03 
c  TempC        0.43941E+02      26   0.30964E-03   0.44943E+01 0.23906E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3065          9.1231          4.5729          4.5729
v  Velocity[Y]             -2.867           7.193         0.24286         0.24286
v  Velocity[Z]       -7.8835e-015     7.6331e-015    -1.5065e-017    -1.5065e-017
v  ǁVelocityǁ         0.0031242           9.125          5.0403          5.0403
v  Pressure               -24.882          27.969          1.0083          1.0083
v  nu_tilda           4.4007e-007       0.0044847       0.0017884       0.0017884
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3017e-014       0.0052852       0.0021026       0.0021026
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2666:        0.22350E+01

===============================================================


 INSTANT    0.266700000E+04   TIME STEP NUMBER            2667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.25281E-02 0.89054E+00
   Friction velocity        uk    :  0.25281E-02 0.89054E+00
   Dimensionless distance   yplus :  0.20353E-01 0.71695E+01
   Friction thermal sca.    tstar : -0.14685E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15186E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10665E-01      33   0.23403E-03   0.45080E+01 0.19429E+03 
c  Velocity[X]                                      0.20045E+01 
c  Velocity[Y]                                      0.25034E+01 
c  Velocity[Z]                                      0.10479E-29 
c  Pressure     0.12083E-06     474   0.96069E-08   0.11926E+00 0.67264E+03 
c  nu_tilda     0.83924E-05      33   0.23245E-05   0.71772E-06 0.21345E+03 
c  TempC        0.43942E+02      27   0.29608E-03   0.48516E+01 0.24360E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3071          9.1217          4.5729          4.5729
v  Velocity[Y]            -2.8661          7.1666         0.24284         0.24284
v  Velocity[Z]       -7.8552e-015     7.6351e-015    -1.5065e-017    -1.5065e-017
v  ǁVelocityǁ         0.0031063          9.1236          5.0402          5.0402
v  Pressure               -24.823          27.961          1.0431          1.0431
v  nu_tilda           4.4009e-007       0.0044851       0.0017885       0.0017885
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2995e-014       0.0052857       0.0021027       0.0021027
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2667:        0.21030E+01

===============================================================


 INSTANT    0.266800000E+04   TIME STEP NUMBER            2668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12004E-01 0.88907E+00
   Friction velocity        uk    :  0.12004E-01 0.88907E+00
   Dimensionless distance   yplus :  0.96639E-01 0.71577E+01
   Friction thermal sca.    tstar : -0.57937E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72103E-01 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10665E-01      33   0.24849E-03   0.44787E+01 0.19411E+03 
c  Velocity[X]                                      0.19941E+01 
c  Velocity[Y]                                      0.24846E+01 
c  Velocity[Z]                                      0.14780E-29 
c  Pressure     0.11000E-06     520   0.90197E-08   0.10490E+00 0.97711E+03 
c  nu_tilda     0.83932E-05      33   0.13281E-04   0.71778E-06 0.21344E+03 
c  TempC        0.43943E+02      26   0.22857E-03   0.45967E+01 0.24104E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3077          9.1203          4.5729          4.5729
v  Velocity[Y]            -2.8652          7.1811         0.24282         0.24282
v  Velocity[Z]        -7.898e-015     7.6594e-015    -1.5059e-017    -1.5059e-017
v  ǁVelocityǁ         0.0032916          9.1222            5.04            5.04
v  Pressure               -24.899          27.923         0.98867         0.98867
v  nu_tilda            4.401e-007       0.0044854       0.0017885       0.0017885
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3003e-014       0.0052861       0.0021027       0.0021027
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2668:        0.22090E+01

===============================================================


 INSTANT    0.266900000E+04   TIME STEP NUMBER            2669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17993E-01 0.89036E+00
   Friction velocity        uk    :  0.17993E-01 0.89036E+00
   Dimensionless distance   yplus :  0.14485E+00 0.71680E+01
   Friction thermal sca.    tstar : -0.57369E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10808E+00 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10664E-01      33   0.25234E-03   0.45148E+01 0.19440E+03 
c  Velocity[X]                                      0.20280E+01 
c  Velocity[Y]                                      0.24868E+01 
c  Velocity[Z]                                      0.12242E-29 
c  Pressure     0.12270E-06     537   0.92678E-08   0.12137E+00 0.80309E+03 
c  nu_tilda     0.83941E-05      33   0.23207E-05   0.71779E-06 0.21343E+03 
c  TempC        0.43945E+02      26   0.33243E-03   0.66855E+01 0.26879E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3083          9.1189          4.5729          4.5729
v  Velocity[Y]            -2.8644          7.1638         0.24279         0.24279
v  Velocity[Z]       -7.8748e-015     7.6625e-015    -1.5064e-017    -1.5064e-017
v  ǁVelocityǁ          0.002221          9.1208          5.0399          5.0399
v  Pressure               -24.839          27.945          1.0313          1.0313
v  nu_tilda            4.401e-007       0.0044858       0.0017886       0.0017886
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3006e-014       0.0052865       0.0021027       0.0021027
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2669:        0.22520E+01

===============================================================


 INSTANT    0.267000000E+04   TIME STEP NUMBER            2670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12506E-01 0.88958E+00
   Friction velocity        uk    :  0.12506E-01 0.88958E+00
   Dimensionless distance   yplus :  0.10068E+00 0.71617E+01
   Friction thermal sca.    tstar : -0.58201E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.75117E-01 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10663E-01      33   0.18667E-03   0.45043E+01 0.19436E+03 
c  Velocity[X]                                      0.19994E+01 
c  Velocity[Y]                                      0.25049E+01 
c  Velocity[Z]                                      0.15665E-29 
c  Pressure     0.10713E-06     489   0.99135E-08   0.10381E+00 0.84255E+03 
c  nu_tilda     0.83950E-05      33   0.13271E-04   0.71786E-06 0.21343E+03 
c  TempC        0.43946E+02      26   0.25552E-03   0.74162E+01 0.29833E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3089          9.1176          4.5729          4.5729
v  Velocity[Y]            -2.8636           7.186         0.24277         0.24277
v  Velocity[Z]       -7.9205e-015     7.6786e-015    -1.5064e-017    -1.5064e-017
v  ǁVelocityǁ         0.0016261          9.1195          5.0398          5.0398
v  Pressure               -24.916          27.942          0.9837          0.9837
v  nu_tilda           4.4006e-007       0.0044861       0.0017886       0.0017886
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3004e-014       0.0052869       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2670:        0.21230E+01

===============================================================


 INSTANT    0.267100000E+04   TIME STEP NUMBER            2671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18965E-01 0.89090E+00
   Friction velocity        uk    :  0.18965E-01 0.89090E+00
   Dimensionless distance   yplus :  0.15268E+00 0.71724E+01
   Friction thermal sca.    tstar : -0.61077E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11391E+00 0.53514E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10663E-01      33   0.23877E-03   0.44724E+01 0.19412E+03 
c  Velocity[X]                                      0.19874E+01 
c  Velocity[Y]                                      0.24850E+01 
c  Velocity[Z]                                      0.83127E-30 
c  Pressure     0.11617E-06     505   0.96797E-08   0.11163E+00 0.89249E+03 
c  nu_tilda     0.83958E-05      33   0.23292E-05   0.71786E-06 0.21342E+03 
c  TempC        0.43947E+02      26   0.31191E-03   0.44072E+01 0.24383E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3095          9.1162          4.5729          4.5729
v  Velocity[Y]            -2.8627          7.1922         0.24275         0.24275
v  Velocity[Z]       -7.9014e-015     7.6882e-015    -1.5061e-017    -1.5061e-017
v  ǁVelocityǁ         0.0026417          9.1181          5.0396          5.0396
v  Pressure               -24.859          27.997          1.0293          1.0293
v  nu_tilda           4.4002e-007       0.0044865       0.0017886       0.0017886
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.2992e-014       0.0052873       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2671:        0.21650E+01

===============================================================


 INSTANT    0.267200000E+04   TIME STEP NUMBER            2672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18458E-01 0.89061E+00
   Friction velocity        uk    :  0.18458E-01 0.89061E+00
   Dimensionless distance   yplus :  0.14860E+00 0.71700E+01
   Friction thermal sca.    tstar : -0.58487E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11087E+00 0.53497E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10662E-01      33   0.23519E-03   0.45044E+01 0.19420E+03 
c  Velocity[X]                                      0.20301E+01 
c  Velocity[Y]                                      0.24743E+01 
c  Velocity[Z]                                      0.14709E-29 
c  Pressure     0.10725E-06     554   0.97279E-08   0.10531E+00 0.18046E+04 
c  nu_tilda     0.83967E-05      33   0.13265E-04   0.71793E-06 0.21342E+03 
c  TempC        0.43948E+02      27   0.28769E-03   0.59103E+01 0.26514E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3101          9.1148          4.5729          4.5729
v  Velocity[Y]            -2.8619          7.1656         0.24273         0.24273
v  Velocity[Z]       -7.9429e-015     7.7022e-015    -1.5064e-017    -1.5064e-017
v  ǁVelocityǁ         0.0017273          9.1167          5.0395          5.0395
v  Pressure               -24.932          27.805         0.94264         0.94264
v  nu_tilda           4.4006e-007       0.0044868       0.0017886       0.0017886
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2981e-014       0.0052878       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2672:        0.23830E+01

===============================================================


 INSTANT    0.267300000E+04   TIME STEP NUMBER            2673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17594E-01 0.88929E+00
   Friction velocity        uk    :  0.17594E-01 0.88929E+00
   Dimensionless distance   yplus :  0.14164E+00 0.71594E+01
   Friction thermal sca.    tstar : -0.58256E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10568E+00 0.53417E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10661E-01      33   0.23239E-03   0.44738E+01 0.19402E+03 
c  Velocity[X]                                      0.19903E+01 
c  Velocity[Y]                                      0.24835E+01 
c  Velocity[Z]                                      0.88554E-30 
c  Pressure     0.93806E-07     538   0.96949E-08   0.91528E-01 0.17523E+04 
c  nu_tilda     0.83976E-05      33   0.23261E-05   0.71792E-06 0.21341E+03 
c  TempC        0.43949E+02      27   0.25617E-03   0.42991E+01 0.24165E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3106          9.1134          4.5729          4.5729
v  Velocity[Y]             -2.861           7.186          0.2427          0.2427
v  Velocity[Z]       -7.9244e-015      7.704e-015    -1.5062e-017    -1.5062e-017
v  ǁVelocityǁ         0.0013482          9.1153          5.0394          5.0394
v  Pressure               -24.878          28.005          1.0206          1.0206
v  nu_tilda           4.4008e-007       0.0044872       0.0017887       0.0017887
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2993e-014       0.0052882       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2673:        0.24970E+01

===============================================================


 INSTANT    0.267400000E+04   TIME STEP NUMBER            2674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.49162E-02 0.89014E+00
   Friction velocity        uk    :  0.49162E-02 0.89014E+00
   Dimensionless distance   yplus :  0.39579E-01 0.71663E+01
   Friction thermal sca.    tstar : -0.57443E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29530E-01 0.53468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10661E-01      33   0.25476E-03   0.44801E+01 0.19421E+03 
c  Velocity[X]                                      0.20010E+01 
c  Velocity[Y]                                      0.24791E+01 
c  Velocity[Z]                                      0.11242E-29 
c  Pressure     0.11218E-06     554   0.98579E-08   0.10839E+00 0.21596E+04 
c  nu_tilda     0.83984E-05      33   0.13256E-04   0.71797E-06 0.21340E+03 
c  TempC        0.43951E+02      26   0.33723E-03   0.41052E+01 0.22171E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3112           9.112          4.5729          4.5729
v  Velocity[Y]            -2.8601           7.158         0.24268         0.24268
v  Velocity[Z]       -7.9564e-015     7.7237e-015    -1.5067e-017    -1.5067e-017
v  ǁVelocityǁ         0.0014272           9.114          5.0392          5.0392
v  Pressure               -24.949          27.759         0.92172         0.92172
v  nu_tilda           4.4015e-007       0.0044875       0.0017886       0.0017886
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2999e-014       0.0052886       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2674:        0.24780E+01

===============================================================


 INSTANT    0.267500000E+04   TIME STEP NUMBER            2675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17448E-01 0.88950E+00
   Friction velocity        uk    :  0.17448E-01 0.88950E+00
   Dimensionless distance   yplus :  0.14047E+00 0.71611E+01
   Friction thermal sca.    tstar : -0.58600E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10481E+00 0.53430E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10660E-01      33   0.24659E-03   0.44999E+01 0.19423E+03 
c  Velocity[X]                                      0.20267E+01 
c  Velocity[Y]                                      0.24733E+01 
c  Velocity[Z]                                      0.15852E-29 
c  Pressure     0.11684E-06     553   0.97314E-08   0.11313E+00 0.19974E+04 
c  nu_tilda     0.83993E-05      33   0.23298E-05   0.71798E-06 0.21340E+03 
c  TempC        0.43952E+02      27   0.27063E-03   0.54887E+01 0.25613E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3118          9.1107          4.5729          4.5729
v  Velocity[Y]            -2.8592          7.1857         0.24266         0.24266
v  Velocity[Z]       -7.9285e-015     7.7263e-015     -1.507e-017     -1.507e-017
v  ǁVelocityǁ         0.0014878          9.1126          5.0391          5.0391
v  Pressure               -24.896          27.993          1.0086          1.0086
v  nu_tilda           4.4014e-007       0.0044879       0.0017887       0.0017887
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3019e-014        0.005289       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2675:        0.24610E+01

===============================================================


 INSTANT    0.267600000E+04   TIME STEP NUMBER            2676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18399E-01 0.89078E+00
   Friction velocity        uk    :  0.18399E-01 0.89078E+00
   Dimensionless distance   yplus :  0.14813E+00 0.71714E+01
   Friction thermal sca.    tstar : -0.57347E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11052E+00 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10659E-01      33   0.23394E-03   0.44687E+01 0.19410E+03 
c  Velocity[X]                                      0.19835E+01 
c  Velocity[Y]                                      0.24852E+01 
c  Velocity[Z]                                      0.77135E-30 
c  Pressure     0.96061E-07     522   0.95233E-08   0.92639E-01 0.14484E+04 
c  nu_tilda     0.84001E-05      33   0.13248E-04   0.71807E-06 0.21340E+03 
c  TempC        0.43953E+02      27   0.26755E-03   0.30231E+01 0.21568E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3124          9.1093          4.5729          4.5729
v  Velocity[Y]            -2.8584          7.1917         0.24263         0.24263
v  Velocity[Z]       -7.9611e-015     7.7386e-015    -1.5073e-017    -1.5073e-017
v  ǁVelocityǁ          0.001748          9.1112           5.039           5.039
v  Pressure               -24.971          27.875         0.93326         0.93326
v  nu_tilda           4.4005e-007       0.0044882       0.0017887       0.0017887
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3016e-014       0.0052894       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2676:        0.22700E+01

===============================================================


 INSTANT    0.267700000E+04   TIME STEP NUMBER            2677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.65236E-02 0.89031E+00
   Friction velocity        uk    :  0.65236E-02 0.89031E+00
   Dimensionless distance   yplus :  0.52519E-01 0.71676E+01
   Friction thermal sca.    tstar : -0.56725E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39185E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10658E-01      33   0.22880E-03   0.44785E+01 0.19399E+03 
c  Velocity[X]                                      0.20128E+01 
c  Velocity[Y]                                      0.24656E+01 
c  Velocity[Z]                                      0.14905E-29 
c  Pressure     0.12140E-06     473   0.97722E-08   0.11848E+00 0.60757E+03 
c  nu_tilda     0.84009E-05      33   0.23325E-05   0.71810E-06 0.21339E+03 
c  TempC        0.43954E+02      27   0.34469E-03   0.34599E+01 0.21724E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3129          9.1079          4.5729          4.5729
v  Velocity[Y]            -2.8576          7.1619         0.24261         0.24261
v  Velocity[Z]       -7.9302e-015      7.746e-015    -1.5071e-017    -1.5071e-017
v  ǁVelocityǁ         0.0014095          9.1098          5.0388          5.0388
v  Pressure               -24.911          27.831         0.96131         0.96131
v  nu_tilda           4.4006e-007       0.0044886       0.0017888       0.0017888
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.2991e-014       0.0052898       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2677:        0.21800E+01

===============================================================


 INSTANT    0.267800000E+04   TIME STEP NUMBER            2678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85110E-02 0.88912E+00
   Friction velocity        uk    :  0.85110E-02 0.88912E+00
   Dimensionless distance   yplus :  0.68520E-01 0.71580E+01
   Friction thermal sca.    tstar : -0.58182E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51123E-01 0.53407E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10658E-01      33   0.23660E-03   0.44707E+01 0.19395E+03 
c  Velocity[X]                                      0.20142E+01 
c  Velocity[Y]                                      0.24565E+01 
c  Velocity[Z]                                      0.96167E-30 
c  Pressure     0.99266E-07     505   0.93637E-08   0.95923E-01 0.81068E+03 
c  nu_tilda     0.84018E-05      33   0.13243E-04   0.71813E-06 0.21338E+03 
c  TempC        0.43955E+02      27   0.33767E-03   0.57520E+01 0.25290E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3135          9.1065          4.5729          4.5729
v  Velocity[Y]            -2.8567          7.1818         0.24258         0.24258
v  Velocity[Z]       -7.9587e-015     7.7585e-015    -1.5073e-017    -1.5073e-017
v  ǁVelocityǁ         0.0025549          9.1085          5.0387          5.0387
v  Pressure                -24.99          27.844         0.91579         0.91579
v  nu_tilda           4.4008e-007        0.004489       0.0017887       0.0017887
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2991e-014       0.0052903        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2678:        0.21810E+01

===============================================================


 INSTANT    0.267900000E+04   TIME STEP NUMBER            2679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18878E-01 0.89018E+00
   Friction velocity        uk    :  0.18878E-01 0.89018E+00
   Dimensionless distance   yplus :  0.15198E+00 0.71665E+01
   Friction thermal sca.    tstar : -0.61096E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11339E+00 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10657E-01      33   0.24143E-03   0.44762E+01 0.19415E+03 
c  Velocity[X]                                      0.19977E+01 
c  Velocity[Y]                                      0.24785E+01 
c  Velocity[Z]                                      0.94580E-30 
c  Pressure     0.11023E-06     504   0.89968E-08   0.10799E+00 0.62371E+03 
c  nu_tilda     0.84026E-05      33   0.23334E-05   0.71815E-06 0.21338E+03 
c  TempC        0.43956E+02      26   0.23115E-03   0.64634E+01 0.27786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.314          9.1052          4.5729          4.5729
v  Velocity[Y]            -2.8558          7.1612         0.24255         0.24255
v  Velocity[Z]       -7.9314e-015     7.7569e-015     -1.507e-017     -1.507e-017
v  ǁVelocityǁ         0.0030672          9.1071          5.0386          5.0386
v  Pressure               -24.927          27.819         0.94638         0.94638
v  nu_tilda           4.4016e-007       0.0044893       0.0017888       0.0017888
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2997e-014       0.0052907        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2679:        0.21360E+01

===============================================================


 INSTANT    0.268000000E+04   TIME STEP NUMBER            2680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17173E-01 0.88934E+00
   Friction velocity        uk    :  0.17173E-01 0.88934E+00
   Dimensionless distance   yplus :  0.13826E+00 0.71598E+01
   Friction thermal sca.    tstar : -0.59529E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10315E+00 0.53420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10656E-01      33   0.20555E-03   0.44660E+01 0.19405E+03 
c  Velocity[X]                                      0.20001E+01 
c  Velocity[Y]                                      0.24659E+01 
c  Velocity[Z]                                      0.14661E-29 
c  Pressure     0.11450E-06     521   0.96485E-08   0.10936E+00 0.83140E+03 
c  nu_tilda     0.84034E-05      33   0.13233E-04   0.71824E-06 0.21337E+03 
c  TempC        0.43957E+02      27   0.28887E-03   0.39289E+01 0.23677E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3145          9.1038          4.5729          4.5729
v  Velocity[Y]            -2.8549          7.1809         0.24253         0.24253
v  Velocity[Z]        -7.949e-015     7.7757e-015    -1.5072e-017    -1.5072e-017
v  ǁVelocityǁ         0.0033023          9.1057          5.0384          5.0384
v  Pressure               -25.009           27.81         0.89933         0.89933
v  nu_tilda           4.4019e-007       0.0044897       0.0017888       0.0017888
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3023e-014       0.0052911        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2680:        0.22020E+01

===============================================================


 INSTANT    0.268100000E+04   TIME STEP NUMBER            2681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18403E-01 0.89109E+00
   Friction velocity        uk    :  0.18403E-01 0.89109E+00
   Dimensionless distance   yplus :  0.14816E+00 0.71739E+01
   Friction thermal sca.    tstar : -0.59584E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11054E+00 0.53525E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10656E-01      33   0.25172E-03   0.44656E+01 0.19403E+03 
c  Velocity[X]                                      0.20090E+01 
c  Velocity[Y]                                      0.24566E+01 
c  Velocity[Z]                                      0.89159E-30 
c  Pressure     0.10672E-06     490   0.98580E-08   0.10408E+00 0.10177E+04 
c  nu_tilda     0.84043E-05      33   0.23381E-05   0.71828E-06 0.21337E+03 
c  TempC        0.43958E+02      27   0.32585E-03   0.54037E+01 0.24897E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.315          9.1024          4.5729          4.5729
v  Velocity[Y]             -2.854          7.1954          0.2425          0.2425
v  Velocity[Z]       -7.9198e-015     7.7752e-015    -1.5069e-017    -1.5069e-017
v  ǁVelocityǁ         0.0023409          9.1043          5.0383          5.0383
v  Pressure                -24.95          27.896         0.94969         0.94969
v  nu_tilda           4.4014e-007       0.0044901       0.0017889       0.0017889
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3033e-014       0.0052916        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2681:        0.21380E+01

===============================================================


 INSTANT    0.268200000E+04   TIME STEP NUMBER            2682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13120E-01 0.89078E+00
   Friction velocity        uk    :  0.13120E-01 0.89078E+00
   Dimensionless distance   yplus :  0.10562E+00 0.71714E+01
   Friction thermal sca.    tstar : -0.62990E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78805E-01 0.53506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10655E-01      33   0.22998E-03   0.44766E+01 0.19402E+03 
c  Velocity[X]                                      0.20084E+01 
c  Velocity[Y]                                      0.24682E+01 
c  Velocity[Z]                                      0.13184E-29 
c  Pressure     0.10912E-06     536   0.92986E-08   0.10684E+00 0.17246E+04 
c  nu_tilda     0.84051E-05      33   0.13226E-04   0.71833E-06 0.21337E+03 
c  TempC        0.43960E+02      26   0.27979E-03   0.71216E+01 0.29755E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3155           9.101          4.5729          4.5729
v  Velocity[Y]            -2.8532          7.1652         0.24247         0.24247
v  Velocity[Z]       -7.9362e-015     7.7861e-015    -1.5065e-017    -1.5065e-017
v  ǁVelocityǁ         0.0016873           9.103          5.0382          5.0382
v  Pressure               -25.026          27.714         0.86568         0.86568
v  nu_tilda           4.4015e-007       0.0044905       0.0017888       0.0017888
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3018e-014        0.005292       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2682:        0.22350E+01

===============================================================


 INSTANT    0.268300000E+04   TIME STEP NUMBER            2683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11041E-01 0.88924E+00
   Friction velocity        uk    :  0.11041E-01 0.88924E+00
   Dimensionless distance   yplus :  0.88886E-01 0.71590E+01
   Friction thermal sca.    tstar : -0.64371E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66319E-01 0.53414E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10654E-01      33   0.23519E-03   0.44507E+01 0.19379E+03 
c  Velocity[X]                                      0.20018E+01 
c  Velocity[Y]                                      0.24489E+01 
c  Velocity[Z]                                      0.99569E-30 
c  Pressure     0.11230E-06     553   0.98489E-08   0.10720E+00 0.13078E+04 
c  nu_tilda     0.84059E-05      33   0.23383E-05   0.71834E-06 0.21336E+03 
c  TempC        0.43961E+02      27   0.23786E-03   0.59262E+01 0.27295E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.316          9.0997          4.5729          4.5729
v  Velocity[Y]            -2.8523          7.1822         0.24244         0.24244
v  Velocity[Z]       -7.9023e-015      7.785e-015    -1.5059e-017    -1.5059e-017
v  ǁVelocityǁ         0.0013465          9.1016          5.0381          5.0381
v  Pressure               -24.967          27.847         0.92751         0.92751
v  nu_tilda           4.4015e-007       0.0044908       0.0017889       0.0017889
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3018e-014       0.0052925       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2683:        0.22630E+01

===============================================================


 INSTANT    0.268400000E+04   TIME STEP NUMBER            2684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.88745E-02 0.89039E+00
   Friction velocity        uk    :  0.88745E-02 0.89039E+00
   Dimensionless distance   yplus :  0.71446E-01 0.71682E+01
   Friction thermal sca.    tstar : -0.68509E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53307E-01 0.53483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10654E-01      33   0.25159E-03   0.44808E+01 0.19410E+03 
c  Velocity[X]                                      0.20303E+01 
c  Velocity[Y]                                      0.24504E+01 
c  Velocity[Z]                                      0.98410E-30 
c  Pressure     0.10647E-06     538   0.92738E-08   0.10419E+00 0.15588E+04 
c  nu_tilda     0.84067E-05      33   0.13218E-04   0.71839E-06 0.21335E+03 
c  TempC        0.43962E+02      27   0.32248E-03   0.39570E+01 0.22971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3166          9.0984          4.5729          4.5729
v  Velocity[Y]            -2.8514          7.1605         0.24241         0.24241
v  Velocity[Z]       -7.9233e-015     7.7972e-015    -1.5059e-017    -1.5059e-017
v  ǁVelocityǁ         0.0014171          9.1002          5.0379          5.0379
v  Pressure               -25.044          27.691         0.84981         0.84981
v  nu_tilda           4.4015e-007       0.0044912       0.0017888       0.0017888
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3021e-014       0.0052929       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2684:        0.22150E+01

===============================================================


 INSTANT    0.268500000E+04   TIME STEP NUMBER            2685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17575E-01 0.88956E+00
   Friction velocity        uk    :  0.17575E-01 0.88956E+00
   Dimensionless distance   yplus :  0.14149E+00 0.71615E+01
   Friction thermal sca.    tstar : -0.70064E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10557E+00 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10653E-01      33   0.18320E-03   0.44646E+01 0.19400E+03 
c  Velocity[X]                                      0.19990E+01 
c  Velocity[Y]                                      0.24657E+01 
c  Velocity[Z]                                      0.14177E-29 
c  Pressure     0.10269E-06     536   0.98966E-08   0.99693E-01 0.15471E+04 
c  nu_tilda     0.84075E-05      33   0.23439E-05   0.71845E-06 0.21335E+03 
c  TempC        0.43963E+02      27   0.27353E-03   0.57505E+01 0.27977E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3171          9.0971          4.5729          4.5729
v  Velocity[Y]            -2.8505          7.1861         0.24238         0.24238
v  Velocity[Z]       -7.8773e-015     7.7965e-015    -1.5055e-017    -1.5055e-017
v  ǁVelocityǁ        0.00056714          9.0989          5.0378          5.0378
v  Pressure               -24.987          27.866         0.91994         0.91994
v  nu_tilda           4.4007e-007       0.0044915       0.0017889       0.0017889
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3018e-014       0.0052933       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2685:        0.22390E+01

===============================================================


 INSTANT    0.268600000E+04   TIME STEP NUMBER            2686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16422E-01 0.89075E+00
   Friction velocity        uk    :  0.16422E-01 0.89075E+00
   Dimensionless distance   yplus :  0.13220E+00 0.71712E+01
   Friction thermal sca.    tstar : -0.74269E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98640E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10652E-01      33   0.24906E-03   0.44286E+01 0.19380E+03 
c  Velocity[X]                                      0.19799E+01 
c  Velocity[Y]                                      0.24487E+01 
c  Velocity[Z]                                      0.88882E-30 
c  Pressure     0.11065E-06     536   0.93071E-08   0.10551E+00 0.14220E+04 
c  nu_tilda     0.84083E-05      33   0.13210E-04   0.71853E-06 0.21335E+03 
c  TempC        0.43964E+02      26   0.29393E-03   0.58055E+01 0.27111E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3176          9.0957          4.5729          4.5729
v  Velocity[Y]            -2.8496          7.1883         0.24235         0.24235
v  Velocity[Z]       -7.8943e-015     7.8057e-015    -1.5052e-017    -1.5052e-017
v  ǁVelocityǁ        0.00023074          9.0975          5.0377          5.0377
v  Pressure               -25.064          27.737         0.84636         0.84636
v  nu_tilda           4.3997e-007       0.0044919       0.0017889       0.0017889
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2995e-014       0.0052937       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2686:        0.22280E+01

===============================================================


 INSTANT    0.268700000E+04   TIME STEP NUMBER            2687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13125E-01 0.89053E+00
   Friction velocity        uk    :  0.13125E-01 0.89053E+00
   Dimensionless distance   yplus :  0.10566E+00 0.71694E+01
   Friction thermal sca.    tstar : -0.76290E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78836E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10651E-01      33   0.24386E-03   0.44612E+01 0.19386E+03 
c  Velocity[X]                                      0.20230E+01 
c  Velocity[Y]                                      0.24382E+01 
c  Velocity[Z]                                      0.13419E-29 
c  Pressure     0.12283E-06     474   0.92740E-08   0.12110E+00 0.68262E+03 
c  nu_tilda     0.84091E-05      33   0.23421E-05   0.71855E-06 0.21334E+03 
c  TempC        0.43965E+02      27   0.27084E-03   0.39650E+01 0.23778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3181          9.0944          4.5729          4.5729
v  Velocity[Y]            -2.8488          7.1643         0.24232         0.24232
v  Velocity[Z]       -7.8441e-015      7.806e-015    -1.5046e-017    -1.5046e-017
v  ǁVelocityǁ         0.0010379          9.0961          5.0376          5.0376
v  Pressure               -25.003          27.744         0.88202         0.88202
v  nu_tilda           4.3997e-007       0.0044923        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2966e-014       0.0052941       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2687:        0.20680E+01

===============================================================


 INSTANT    0.268800000E+04   TIME STEP NUMBER            2688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11570E-01 0.88908E+00
   Friction velocity        uk    :  0.11570E-01 0.88908E+00
   Dimensionless distance   yplus :  0.93144E-01 0.71577E+01
   Friction thermal sca.    tstar : -0.84226E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69496E-01 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10651E-01      33   0.25909E-03   0.44457E+01 0.19381E+03 
c  Velocity[X]                                      0.19924E+01 
c  Velocity[Y]                                      0.24533E+01 
c  Velocity[Z]                                      0.81585E-30 
c  Pressure     0.99354E-07     537   0.93658E-08   0.95778E-01 0.84990E+03 
c  nu_tilda     0.84099E-05      33   0.13204E-04   0.71860E-06 0.21334E+03 
c  TempC        0.43966E+02      26   0.24718E-03   0.37195E+01 0.22614E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3186          9.0931          4.5729          4.5729
v  Velocity[Y]            -2.8479          7.1836         0.24229         0.24229
v  Velocity[Z]       -7.8544e-015     7.8171e-015    -1.5039e-017    -1.5039e-017
v  ǁVelocityǁ         0.0010658          9.0947          5.0374          5.0374
v  Pressure               -25.085          27.738         0.83351         0.83351
v  nu_tilda              4.4e-007       0.0044926       0.0017889       0.0017889
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2966e-014       0.0052946       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2688:        0.22170E+01

===============================================================


 INSTANT    0.268900000E+04   TIME STEP NUMBER            2689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52958E-02 0.89024E+00
   Friction velocity        uk    :  0.52958E-02 0.89024E+00
   Dimensionless distance   yplus :  0.42635E-01 0.71670E+01
   Friction thermal sca.    tstar : -0.86443E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31810E-01 0.53474E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10650E-01      33   0.24254E-03   0.44681E+01 0.19394E+03 
c  Velocity[X]                                      0.20254E+01 
c  Velocity[Y]                                      0.24426E+01 
c  Velocity[Z]                                      0.11357E-29 
c  Pressure     0.13309E-06     441   0.95373E-08   0.12890E+00 0.59588E+03 
c  nu_tilda     0.84107E-05      33   0.23499E-05   0.71860E-06 0.21333E+03 
c  TempC        0.43967E+02      26   0.31725E-03   0.65153E+01 0.27473E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3191          9.0918          4.5729          4.5729
v  Velocity[Y]             -2.847          7.1604         0.24226         0.24226
v  Velocity[Z]       -7.8166e-015     7.8146e-015    -1.5035e-017    -1.5035e-017
v  ǁVelocityǁ        0.00096656          9.0934          5.0373          5.0373
v  Pressure               -25.021          27.673         0.85383         0.85383
v  nu_tilda           4.4006e-007        0.004493        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2974e-014        0.005295       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2689:        0.20060E+01

===============================================================


 INSTANT    0.269000000E+04   TIME STEP NUMBER            2690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52147E-02 0.88972E+00
   Friction velocity        uk    :  0.52147E-02 0.88972E+00
   Dimensionless distance   yplus :  0.41982E-01 0.71628E+01
   Friction thermal sca.    tstar : -0.99007E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31323E-01 0.53443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10649E-01      33   0.18545E-03   0.44457E+01 0.19382E+03 
c  Velocity[X]                                      0.20095E+01 
c  Velocity[Y]                                      0.24362E+01 
c  Velocity[Z]                                      0.14273E-29 
c  Pressure     0.10905E-06     521   0.97947E-08   0.10588E+00 0.73050E+03 
c  nu_tilda     0.84115E-05      33   0.13197E-04   0.71871E-06 0.21333E+03 
c  TempC        0.43968E+02      26   0.27336E-03   0.62822E+01 0.28959E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3195          9.0905          4.5729          4.5729
v  Velocity[Y]            -2.8461           7.185         0.24223         0.24223
v  Velocity[Z]        -7.826e-015     7.8266e-015    -1.5027e-017    -1.5027e-017
v  ǁVelocityǁ         0.0020584          9.0921          5.0372          5.0372
v  Pressure               -25.102          27.713         0.81624         0.81624
v  nu_tilda           4.4004e-007       0.0044933       0.0017889       0.0017889
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2994e-014       0.0052954       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2690:        0.22980E+01

===============================================================


 INSTANT    0.269100000E+04   TIME STEP NUMBER            2691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46590E-02 0.89101E+00
   Friction velocity        uk    :  0.46590E-02 0.89101E+00
   Dimensionless distance   yplus :  0.37508E-01 0.71732E+01
   Friction thermal sca.    tstar : -0.10161E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27985E-01 0.53520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10648E-01      33   0.24926E-03   0.44254E+01 0.19373E+03 
c  Velocity[X]                                      0.19744E+01 
c  Velocity[Y]                                      0.24510E+01 
c  Velocity[Z]                                      0.72763E-30 
c  Pressure     0.90650E-07     522   0.99886E-08   0.88026E-01 0.11152E+04 
c  nu_tilda     0.84122E-05      33   0.23480E-05   0.71877E-06 0.21333E+03 
c  TempC        0.43969E+02      26   0.30059E-03   0.53601E+01 0.24768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.32          9.0892          4.5729          4.5729
v  Velocity[Y]            -2.8452           7.195         0.24219         0.24219
v  Velocity[Z]       -7.7747e-015     7.8271e-015    -1.5019e-017    -1.5019e-017
v  ǁVelocityǁ         0.0021019          9.0908          5.0371          5.0371
v  Pressure               -25.044          27.808         0.87154         0.87154
v  nu_tilda           4.3996e-007       0.0044937        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2988e-014       0.0052959       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2691:        0.27220E+01

===============================================================


 INSTANT    0.269200000E+04   TIME STEP NUMBER            2692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.61130E-02 0.89049E+00
   Friction velocity        uk    :  0.61130E-02 0.89049E+00
   Dimensionless distance   yplus :  0.49214E-01 0.71690E+01
   Friction thermal sca.    tstar : -0.11551E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36719E-01 0.53489E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10648E-01      33   0.23106E-03   0.44502E+01 0.19377E+03 
c  Velocity[X]                                      0.20164E+01 
c  Velocity[Y]                                      0.24337E+01 
c  Velocity[Z]                                      0.13632E-29 
c  Pressure     0.11705E-06     585   0.96319E-08   0.11280E+00 0.22853E+04 
c  nu_tilda     0.84130E-05      33   0.13188E-04   0.71882E-06 0.21332E+03 
c  TempC        0.43970E+02      26   0.29887E-03   0.55445E+01 0.26698E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3205          9.0878          4.5729          4.5729
v  Velocity[Y]            -2.8443          7.1631         0.24216         0.24216
v  Velocity[Z]       -7.7804e-015     7.8327e-015    -1.5014e-017    -1.5014e-017
v  ǁVelocityǁ         0.0025616          9.0895           5.037           5.037
v  Pressure               -25.119          27.542         0.76623         0.76623
v  nu_tilda              4.4e-007        0.004494        0.001789        0.001789
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2962e-014       0.0052963       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2692:        0.25300E+01

===============================================================


 INSTANT    0.269300000E+04   TIME STEP NUMBER            2693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.70529E-02 0.88944E+00
   Friction velocity        uk    :  0.70529E-02 0.88944E+00
   Dimensionless distance   yplus :  0.56781E-01 0.71606E+01
   Friction thermal sca.    tstar : -0.13257E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42365E-01 0.53426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10647E-01      33   0.23817E-03   0.44187E+01 0.19357E+03 
c  Velocity[X]                                      0.19978E+01 
c  Velocity[Y]                                      0.24209E+01 
c  Velocity[Z]                                      0.93879E-30 
c  Pressure     0.97662E-07     569   0.92299E-08   0.95704E-01 0.20292E+04 
c  nu_tilda     0.84138E-05      33   0.23537E-05   0.71884E-06 0.21332E+03 
c  TempC        0.43971E+02      26   0.35815E-03   0.52590E+01 0.27081E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3209          9.0865          4.5729          4.5729
v  Velocity[Y]            -2.8435           7.186         0.24213         0.24213
v  Velocity[Z]       -7.7408e-015     7.8326e-015    -1.5003e-017    -1.5003e-017
v  ǁVelocityǁ         0.0023324          9.0882          5.0368          5.0368
v  Pressure               -25.065          27.787         0.85345         0.85345
v  nu_tilda           4.4004e-007       0.0044944        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2974e-014       0.0052966       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2693:        0.23090E+01

===============================================================


 INSTANT    0.269400000E+04   TIME STEP NUMBER            2694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46774E-02 0.89020E+00
   Friction velocity        uk    :  0.46774E-02 0.89020E+00
   Dimensionless distance   yplus :  0.37657E-01 0.71667E+01
   Friction thermal sca.    tstar : -0.16440E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28096E-01 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10646E-01      33   0.25976E-03   0.44424E+01 0.19383E+03 
c  Velocity[X]                                      0.19970E+01 
c  Velocity[Y]                                      0.24455E+01 
c  Velocity[Z]                                      0.94807E-30 
c  Pressure     0.95009E-07     554   0.91789E-08   0.92853E-01 0.20891E+04 
c  nu_tilda     0.84145E-05      33   0.13181E-04   0.71890E-06 0.21331E+03 
c  TempC        0.43971E+02      27   0.31936E-03   0.64799E+01 0.28691E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3213          9.0852          4.5729          4.5729
v  Velocity[Y]            -2.8426          7.1621         0.24209         0.24209
v  Velocity[Z]       -7.7456e-015     7.8401e-015       -1.5e-017       -1.5e-017
v  ǁVelocityǁ         0.0013022          9.0869          5.0367          5.0367
v  Pressure               -25.138          27.553         0.75607         0.75607
v  nu_tilda           4.4009e-007       0.0044947        0.001789        0.001789
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.2985e-014       0.0052971       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2694:        0.22620E+01

===============================================================


 INSTANT    0.269500000E+04   TIME STEP NUMBER            2695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.26319E-02 0.88940E+00
   Friction velocity        uk    :  0.26319E-02 0.88940E+00
   Dimensionless distance   yplus :  0.21189E-01 0.71602E+01
   Friction thermal sca.    tstar : -0.22224E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15809E-01 0.53423E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10645E-01      33   0.25228E-03   0.44523E+01 0.19377E+03 
c  Velocity[X]                                      0.20226E+01 
c  Velocity[Y]                                      0.24297E+01 
c  Velocity[Z]                                      0.13655E-29 
c  Pressure     0.12355E-06     569   0.93380E-08   0.11804E+00 0.17367E+04 
c  nu_tilda     0.84153E-05      33   0.23518E-05   0.71895E-06 0.21331E+03 
c  TempC        0.43972E+02      27   0.18797E-03   0.50766E+01 0.25993E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3217          9.0839          4.5729          4.5729
v  Velocity[Y]            -2.8417          7.1826         0.24206         0.24206
v  Velocity[Z]       -7.7065e-015     7.8383e-015    -1.4991e-017    -1.4991e-017
v  ǁVelocityǁ        0.00091972          9.0855          5.0366          5.0366
v  Pressure               -25.082          27.746         0.83453         0.83453
v  nu_tilda           4.4011e-007       0.0044951       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc              3.3e-014       0.0052975       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2695:        0.22880E+01

===============================================================


 INSTANT    0.269600000E+04   TIME STEP NUMBER            2696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42432E-02 0.89069E+00
   Friction velocity        uk    :  0.42432E-02 0.89069E+00
   Dimensionless distance   yplus :  0.34160E-01 0.71707E+01
   Friction thermal sca.    tstar : -0.48416E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25488E-01 0.53501E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10644E-01      33   0.25074E-03   0.44417E+01 0.19371E+03 
c  Velocity[X]                                      0.20241E+01 
c  Velocity[Y]                                      0.24177E+01 
c  Velocity[Z]                                      0.82235E-30 
c  Pressure     0.10745E-06     537   0.98021E-08   0.10365E+00 0.14254E+04 
c  nu_tilda     0.84161E-05      33   0.13173E-04   0.71903E-06 0.21331E+03 
c  TempC        0.43973E+02      26   0.37311E-03   0.33277E+01 0.21992E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3222          9.0826          4.5729          4.5729
v  Velocity[Y]            -2.8408          7.1916         0.24202         0.24202
v  Velocity[Z]       -7.7261e-015      7.847e-015    -1.4985e-017    -1.4985e-017
v  ǁVelocityǁ         0.0016142          9.0842          5.0365          5.0365
v  Pressure               -25.159           27.63         0.75944         0.75944
v  nu_tilda           4.4009e-007       0.0044954        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3008e-014       0.0052979       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2696:        0.22340E+01

===============================================================


 INSTANT    0.269700000E+04   TIME STEP NUMBER            2697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.80890E-02 0.89041E+00
   Friction velocity        uk    :  0.80890E-02 0.89041E+00
   Dimensionless distance   yplus :  0.65122E-01 0.71684E+01
   Friction thermal sca.    tstar : -0.30732E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48589E-01 0.53485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10644E-01      33   0.22804E-03   0.44382E+01 0.19365E+03 
c  Velocity[X]                                      0.20065E+01 
c  Velocity[Y]                                      0.24317E+01 
c  Velocity[Z]                                      0.13010E-29 
c  Pressure     0.10873E-06     489   0.95856E-08   0.10753E+00 0.70400E+03 
c  nu_tilda     0.84168E-05      33   0.23576E-05   0.71908E-06 0.21331E+03 
c  TempC        0.43974E+02      27   0.31270E-03   0.65301E+01 0.30302E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3227          9.0813          4.5729          4.5729
v  Velocity[Y]            -2.8398          7.1655         0.24199         0.24199
v  Velocity[Z]       -7.6866e-015     7.8485e-015    -1.4975e-017    -1.4975e-017
v  ǁVelocityǁ           0.00183          9.0829          5.0364          5.0364
v  Pressure               -25.099          27.632          0.7966          0.7966
v  nu_tilda            4.401e-007       0.0044958       0.0017891       0.0017891
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3003e-014       0.0052983       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2697:        0.21140E+01

===============================================================


 INSTANT    0.269800000E+04   TIME STEP NUMBER            2698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.31043E-02 0.88898E+00
   Friction velocity        uk    :  0.31043E-02 0.88898E+00
   Dimensionless distance   yplus :  0.24992E-01 0.71569E+01
   Friction thermal sca.    tstar : -0.16751E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18647E-01 0.53399E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10643E-01      33   0.23109E-03   0.44056E+01 0.19345E+03 
c  Velocity[X]                                      0.19923E+01 
c  Velocity[Y]                                      0.24133E+01 
c  Velocity[Z]                                      0.95823E-30 
c  Pressure     0.10548E-06     522   0.99921E-08   0.10047E+00 0.10287E+04 
c  nu_tilda     0.84176E-05      33   0.13168E-04   0.71914E-06 0.21330E+03 
c  TempC        0.43975E+02      27   0.30118E-03   0.54183E+01 0.25779E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3231            9.08          4.5729          4.5729
v  Velocity[Y]             -2.839          7.1798         0.24195         0.24195
v  Velocity[Z]       -7.7011e-015     7.8595e-015    -1.4966e-017    -1.4966e-017
v  ǁVelocityǁ         0.0020357          9.0816          5.0363          5.0363
v  Pressure               -25.177          27.592          0.7385          0.7385
v  nu_tilda           4.4008e-007       0.0044961        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3004e-014       0.0052987       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2698:        0.21950E+01

===============================================================


 INSTANT    0.269900000E+04   TIME STEP NUMBER            2699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.28757E-02 0.89023E+00
   Friction velocity        uk    :  0.28757E-02 0.89023E+00
   Dimensionless distance   yplus :  0.23152E-01 0.71669E+01
   Friction thermal sca.    tstar : -0.14205E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.17274E-01 0.53473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10642E-01      33   0.24988E-03   0.44296E+01 0.19362E+03 
c  Velocity[X]                                      0.20183E+01 
c  Velocity[Y]                                      0.24113E+01 
c  Velocity[Z]                                      0.95209E-30 
c  Pressure     0.11135E-06     504   0.95359E-08   0.10942E+00 0.77093E+03 
c  nu_tilda     0.84183E-05      33   0.23564E-05   0.71917E-06 0.21330E+03 
c  TempC        0.43976E+02      26   0.29714E-03   0.53913E+01 0.26572E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3236          9.0787          4.5729          4.5729
v  Velocity[Y]            -2.8381          7.1616         0.24191         0.24191
v  Velocity[Z]       -7.6824e-015     7.8565e-015    -1.4959e-017    -1.4959e-017
v  ǁVelocityǁ          0.001266          9.0803          5.0362          5.0362
v  Pressure               -25.117          27.605         0.77966         0.77966
v  nu_tilda           4.4011e-007       0.0044965       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2999e-014       0.0052991       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2699:        0.21580E+01

===============================================================


 INSTANT    0.270000000E+04   TIME STEP NUMBER            2700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17489E-02 0.88943E+00
   Friction velocity        uk    :  0.17489E-02 0.88943E+00
   Dimensionless distance   yplus :  0.14079E-01 0.71605E+01
   Friction thermal sca.    tstar : -0.13235E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10505E-01 0.53426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10641E-01      33   0.18933E-03   0.44264E+01 0.19363E+03 
c  Velocity[X]                                      0.19975E+01 
c  Velocity[Y]                                      0.24288E+01 
c  Velocity[Z]                                      0.12436E-29 
c  Pressure     0.10729E-06     506   0.94154E-08   0.10353E+00 0.86203E+03 
c  nu_tilda     0.84190E-05      33   0.13160E-04   0.71926E-06 0.21329E+03 
c  TempC        0.43977E+02      26   0.25271E-03   0.50363E+01 0.25517E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.324          9.0774          4.5729          4.5729
v  Velocity[Y]            -2.8372          7.1853         0.24187         0.24187
v  Velocity[Z]       -7.7164e-015     7.8594e-015    -1.4951e-017    -1.4951e-017
v  ǁVelocityǁ        0.00073271           9.079          5.0361          5.0361
v  Pressure               -25.196            27.6         0.73046         0.73046
v  nu_tilda            4.401e-007       0.0044968        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3007e-014       0.0052995       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2700:        0.21650E+01

===============================================================


 INSTANT    0.270100000E+04   TIME STEP NUMBER            2701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27143E-02 0.89097E+00
   Friction velocity        uk    :  0.27143E-02 0.89097E+00
   Dimensionless distance   yplus :  0.21852E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.11279E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16304E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10641E-01      33   0.25119E-03   0.43980E+01 0.19340E+03 
c  Velocity[X]                                      0.19871E+01 
c  Velocity[Y]                                      0.24109E+01 
c  Velocity[Z]                                      0.97253E-30 
c  Pressure     0.10959E-06     552   0.93730E-08   0.10547E+00 0.96231E+03 
c  nu_tilda     0.84198E-05      33   0.23606E-05   0.71930E-06 0.21329E+03 
c  TempC        0.43978E+02      27   0.29813E-03   0.41306E+01 0.22590E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3244          9.0761          4.5729          4.5729
v  Velocity[Y]            -2.8363          7.1921         0.24183         0.24183
v  Velocity[Z]        -7.687e-015     7.8565e-015    -1.4938e-017    -1.4938e-017
v  ǁVelocityǁ         0.0015489          9.0777           5.036           5.036
v  Pressure               -25.138          27.671         0.77924         0.77924
v  nu_tilda           4.4007e-007       0.0044972       0.0017891       0.0017891
v  TempC                       21          73.053           22.06           22.06
v  TurbVisc           3.3005e-014          0.0053       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2701:        0.22600E+01

===============================================================


 INSTANT    0.270200000E+04   TIME STEP NUMBER            2702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54752E-02 0.89062E+00
   Friction velocity        uk    :  0.54752E-02 0.89062E+00
   Dimensionless distance   yplus :  0.44079E-01 0.71701E+01
   Friction thermal sca.    tstar : -0.98704E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32888E-01 0.53497E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10640E-01      33   0.24566E-03   0.44427E+01 0.19358E+03 
c  Velocity[X]                                      0.20395E+01 
c  Velocity[Y]                                      0.24033E+01 
c  Velocity[Z]                                      0.11401E-29 
c  Pressure     0.11760E-06     552   0.99986E-08   0.11642E+00 0.20040E+04 
c  nu_tilda     0.84205E-05      33   0.13153E-04   0.71938E-06 0.21329E+03 
c  TempC        0.43978E+02      27   0.32846E-03   0.48082E+01 0.23928E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3248          9.0747          4.5729          4.5729
v  Velocity[Y]            -2.8353          7.1656          0.2418          0.2418
v  Velocity[Z]       -7.7208e-015      7.862e-015    -1.4931e-017    -1.4931e-017
v  ǁVelocityǁ         0.0023428          9.0764          5.0359          5.0359
v  Pressure               -25.212          27.449         0.68385         0.68385
v  nu_tilda            4.401e-007       0.0044975        0.001789        0.001789
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2996e-014       0.0053004       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2702:        0.23800E+01

===============================================================


 INSTANT    0.270300000E+04   TIME STEP NUMBER            2703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.40515E-02 0.88933E+00
   Friction velocity        uk    :  0.40515E-02 0.88933E+00
   Dimensionless distance   yplus :  0.32618E-01 0.71597E+01
   Friction thermal sca.    tstar : -0.12252E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.24336E-01 0.53420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10639E-01      33   0.23061E-03   0.44121E+01 0.19343E+03 
c  Velocity[X]                                      0.19979E+01 
c  Velocity[Y]                                      0.24141E+01 
c  Velocity[Z]                                      0.82569E-30 
c  Pressure     0.10807E-06     569   0.97363E-08   0.10307E+00 0.19769E+04 
c  nu_tilda     0.84212E-05      33   0.23632E-05   0.71942E-06 0.21329E+03 
c  TempC        0.43979E+02      27   0.31012E-03   0.53522E+01 0.24667E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3253          9.0734          4.5729          4.5729
v  Velocity[Y]            -2.8344          7.1851         0.24175         0.24175
v  Velocity[Z]       -7.7001e-015     7.8619e-015    -1.4916e-017    -1.4916e-017
v  ǁVelocityǁ        0.00058943          9.0751          5.0358          5.0358
v  Pressure               -25.158          27.685         0.77002         0.77002
v  nu_tilda            4.401e-007       0.0044978       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3004e-014       0.0053008       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2703:        0.24430E+01

===============================================================


 INSTANT    0.270400000E+04   TIME STEP NUMBER            2704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.27239E-02 0.89011E+00
   Friction velocity        uk    :  0.27239E-02 0.89011E+00
   Dimensionless distance   yplus :  0.21930E-01 0.71660E+01
   Friction thermal sca.    tstar : -0.84893E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.16362E-01 0.53466E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10638E-01      33   0.23942E-03   0.44069E+01 0.19348E+03 
c  Velocity[X]                                      0.20009E+01 
c  Velocity[Y]                                      0.24059E+01 
c  Velocity[Z]                                      0.11859E-29 
c  Pressure     0.11186E-06     554   0.92907E-08   0.10818E+00 0.20929E+04 
c  nu_tilda     0.84219E-05      33   0.13145E-04   0.71950E-06 0.21329E+03 
c  TempC        0.43980E+02      27   0.23303E-03   0.41090E+01 0.23487E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3257          9.0721          4.5729          4.5729
v  Velocity[Y]            -2.8336          7.1585         0.24172         0.24172
v  Velocity[Z]       -7.7399e-015     7.8721e-015    -1.4911e-017    -1.4911e-017
v  ǁVelocityǁ        0.00081608          9.0738          5.0357          5.0357
v  Pressure               -25.233          27.441         0.67304         0.67304
v  nu_tilda           4.4016e-007       0.0044981       0.0017891       0.0017891
v  TempC                       21          73.051           22.06           22.06
v  TurbVisc           3.3005e-014       0.0053011       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2704:        0.22750E+01

===============================================================


 INSTANT    0.270500000E+04   TIME STEP NUMBER            2705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.76181E-02 0.88954E+00
   Friction velocity        uk    :  0.76181E-02 0.88954E+00
   Dimensionless distance   yplus :  0.61331E-01 0.71614E+01
   Friction thermal sca.    tstar : -0.83224E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45760E-01 0.53432E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10637E-01      33   0.18968E-03   0.44124E+01 0.19345E+03 
c  Velocity[X]                                      0.20139E+01 
c  Velocity[Y]                                      0.23985E+01 
c  Velocity[Z]                                      0.12144E-29 
c  Pressure     0.90127E-07     554   0.91799E-08   0.87272E-01 0.16931E+04 
c  nu_tilda     0.84227E-05      33   0.23628E-05   0.71956E-06 0.21328E+03 
c  TempC        0.43981E+02      26   0.24403E-03   0.34224E+01 0.22791E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.326          9.0708          4.5729          4.5729
v  Velocity[Y]            -2.8327          7.1858         0.24167         0.24167
v  Velocity[Z]       -7.7293e-015     7.8663e-015    -1.4896e-017    -1.4896e-017
v  ǁVelocityǁ         0.0012226          9.0725          5.0355          5.0355
v  Pressure               -25.175          27.643         0.74792         0.74792
v  nu_tilda           4.4011e-007       0.0044985       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3022e-014       0.0053015       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2705:        0.22560E+01

===============================================================


 INSTANT    0.270600000E+04   TIME STEP NUMBER            2706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.63084E-02 0.89074E+00
   Friction velocity        uk    :  0.63084E-02 0.89074E+00
   Dimensionless distance   yplus :  0.50787E-01 0.71711E+01
   Friction thermal sca.    tstar : -0.76658E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.37893E-01 0.53504E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10636E-01      33   0.23695E-03   0.43886E+01 0.19337E+03 
c  Velocity[X]                                      0.19764E+01 
c  Velocity[Y]                                      0.24122E+01 
c  Velocity[Z]                                      0.93503E-30 
c  Pressure     0.93118E-07     538   0.98417E-08   0.90322E-01 0.12857E+04 
c  nu_tilda     0.84234E-05      33   0.13136E-04   0.71963E-06 0.21328E+03 
c  TempC        0.43982E+02      26   0.30540E-03   0.40534E+01 0.22224E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3264          9.0695          4.5729          4.5729
v  Velocity[Y]            -2.8318           7.191         0.24163         0.24163
v  Velocity[Z]       -7.7587e-015     7.8712e-015    -1.4883e-017    -1.4883e-017
v  ǁVelocityǁ         0.0010414          9.0712          5.0355          5.0355
v  Pressure               -25.254          27.544         0.67882         0.67882
v  nu_tilda           4.3998e-007       0.0044988       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.3008e-014       0.0053019       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2706:        0.22280E+01

===============================================================


 INSTANT    0.270700000E+04   TIME STEP NUMBER            2707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.67454E-02 0.89023E+00
   Friction velocity        uk    :  0.67454E-02 0.89023E+00
   Dimensionless distance   yplus :  0.54305E-01 0.71669E+01
   Friction thermal sca.    tstar : -0.74662E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40518E-01 0.53473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10636E-01      33   0.25223E-03   0.44109E+01 0.19333E+03 
c  Velocity[X]                                      0.20164E+01 
c  Velocity[Y]                                      0.23944E+01 
c  Velocity[Z]                                      0.11959E-29 
c  Pressure     0.12192E-06     458   0.92588E-08   0.11769E+00 0.57041E+03 
c  nu_tilda     0.84241E-05      33   0.23694E-05   0.71966E-06 0.21328E+03 
c  TempC        0.43982E+02      26   0.26412E-03   0.36399E+01 0.23394E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3267          9.0682          4.5729          4.5729
v  Velocity[Y]            -2.8308          7.1613         0.24159         0.24159
v  Velocity[Z]       -7.7489e-015     7.8662e-015    -1.4868e-017    -1.4868e-017
v  ǁVelocityǁ         0.0010892          9.0699          5.0353          5.0353
v  Pressure               -25.192          27.489         0.70135         0.70135
v  nu_tilda           4.4001e-007       0.0044992       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc            3.297e-014       0.0053023       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2707:        0.20460E+01

===============================================================


 INSTANT    0.270800000E+04   TIME STEP NUMBER            2708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85418E-02 0.88906E+00
   Friction velocity        uk    :  0.85418E-02 0.88906E+00
   Dimensionless distance   yplus :  0.68768E-01 0.71575E+01
   Friction thermal sca.    tstar : -0.69076E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51308E-01 0.53403E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10635E-01      33   0.24626E-03   0.44106E+01 0.19335E+03 
c  Velocity[X]                                      0.20250E+01 
c  Velocity[Y]                                      0.23856E+01 
c  Velocity[Z]                                      0.99411E-30 
c  Pressure     0.10718E-06     521   0.99279E-08   0.10380E+00 0.77123E+03 
c  nu_tilda     0.84248E-05      33   0.13132E-04   0.71974E-06 0.21328E+03 
c  TempC        0.43983E+02      27   0.28312E-03   0.35957E+01 0.22999E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3271          9.0669          4.5729          4.5729
v  Velocity[Y]            -2.8299          7.1824         0.24155         0.24155
v  Velocity[Z]       -7.7913e-015      7.875e-015    -1.4857e-017    -1.4857e-017
v  ǁVelocityǁ          0.001048          9.0686          5.0353          5.0353
v  Pressure               -25.273          27.508         0.65874         0.65874
v  nu_tilda           4.4005e-007       0.0044995       0.0017891       0.0017891
v  TempC                       21          73.052           22.06           22.06
v  TurbVisc           3.2976e-014       0.0053027       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2708:        0.22060E+01

===============================================================


 INSTANT    0.270900000E+04   TIME STEP NUMBER            2709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11386E-01 0.89030E+00
   Friction velocity        uk    :  0.11386E-01 0.89030E+00
   Dimensionless distance   yplus :  0.91665E-01 0.71676E+01
   Friction thermal sca.    tstar : -0.67938E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68392E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10634E-01      33   0.23466E-03   0.44057E+01 0.19341E+03 
c  Velocity[X]                                      0.20005E+01 
c  Velocity[Y]                                      0.24052E+01 
c  Velocity[Z]                                      0.11660E-29 
c  Pressure     0.11020E-06     504   0.98968E-08   0.10831E+00 0.64122E+03 
c  nu_tilda     0.84255E-05      33   0.23680E-05   0.71980E-06 0.21328E+03 
c  TempC        0.43984E+02      26   0.33987E-03   0.60160E+01 0.26543E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3275          9.0656          4.5729          4.5729
v  Velocity[Y]             -2.829          7.1615          0.2415          0.2415
v  Velocity[Z]       -7.7792e-015     7.8701e-015    -1.4845e-017    -1.4845e-017
v  ǁVelocityǁ        0.00046041          9.0673          5.0352          5.0352
v  Pressure               -25.213          27.501         0.69191         0.69191
v  nu_tilda            4.401e-007       0.0044998       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2989e-014       0.0053031       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2709:        0.21550E+01

===============================================================


 INSTANT    0.271000000E+04   TIME STEP NUMBER            2710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10894E-01 0.88935E+00
   Friction velocity        uk    :  0.10894E-01 0.88935E+00
   Dimensionless distance   yplus :  0.87708E-01 0.71599E+01
   Friction thermal sca.    tstar : -0.64670E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65440E-01 0.53421E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10633E-01      33   0.18464E-03   0.43865E+01 0.19327E+03 
c  Velocity[X]                                      0.19959E+01 
c  Velocity[Y]                                      0.23906E+01 
c  Velocity[Z]                                      0.12413E-29 
c  Pressure     0.10779E-06     537   0.93903E-08   0.10357E+00 0.97517E+03 
c  nu_tilda     0.84262E-05      33   0.13123E-04   0.71991E-06 0.21327E+03 
c  TempC        0.43985E+02      26   0.24433E-03   0.71246E+01 0.29107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3279          9.0643          4.5729          4.5729
v  Velocity[Y]            -2.8281          7.1807         0.24146         0.24146
v  Velocity[Z]       -7.8299e-015     7.8754e-015    -1.4835e-017    -1.4835e-017
v  ǁVelocityǁ        0.00058103           9.066          5.0351          5.0351
v  Pressure               -25.291          27.464         0.63666         0.63666
v  nu_tilda           4.4011e-007       0.0045001       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3003e-014       0.0053035       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2710:        0.22390E+01

===============================================================


 INSTANT    0.271100000E+04   TIME STEP NUMBER            2711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12126E-01 0.89097E+00
   Friction velocity        uk    :  0.12126E-01 0.89097E+00
   Dimensionless distance   yplus :  0.97621E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.64060E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72836E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10632E-01      33   0.24871E-03   0.43831E+01 0.19322E+03 
c  Velocity[X]                                      0.20007E+01 
c  Velocity[Y]                                      0.23824E+01 
c  Velocity[Z]                                      0.88979E-30 
c  Pressure     0.95503E-07     505   0.95338E-08   0.92440E-01 0.10523E+04 
c  nu_tilda     0.84269E-05      33   0.23747E-05   0.71994E-06 0.21327E+03 
c  TempC        0.43985E+02      26   0.31822E-03   0.41609E+01 0.23641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3283           9.063          4.5729          4.5729
v  Velocity[Y]            -2.8272          7.1938         0.24142         0.24142
v  Velocity[Z]       -7.8136e-015     7.8706e-015    -1.4821e-017    -1.4821e-017
v  ǁVelocityǁ        0.00010331          9.0647           5.035           5.035
v  Pressure               -25.233          27.556         0.68835         0.68835
v  nu_tilda           4.4008e-007       0.0045005       0.0017891       0.0017891
v  TempC                       21          73.053          22.059          22.059
v  TurbVisc           3.3007e-014       0.0053038       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2711:        0.21590E+01

===============================================================


 INSTANT    0.271200000E+04   TIME STEP NUMBER            2712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10873E-01 0.89056E+00
   Friction velocity        uk    :  0.10873E-01 0.89056E+00
   Dimensionless distance   yplus :  0.87538E-01 0.71696E+01
   Friction thermal sca.    tstar : -0.60605E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65313E-01 0.53493E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10632E-01      33   0.23219E-03   0.43988E+01 0.19328E+03 
c  Velocity[X]                                      0.20031E+01 
c  Velocity[Y]                                      0.23957E+01 
c  Velocity[Z]                                      0.11516E-29 
c  Pressure     0.10240E-06     554   0.92735E-08   0.10058E+00 0.19550E+04 
c  nu_tilda     0.84275E-05      33   0.13117E-04   0.71999E-06 0.21327E+03 
c  TempC        0.43986E+02      26   0.31094E-03   0.61593E+01 0.27253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3286          9.0617          4.5729          4.5729
v  Velocity[Y]            -2.8263          7.1644         0.24137         0.24137
v  Velocity[Z]       -7.8641e-015     7.8745e-015    -1.4805e-017    -1.4805e-017
v  ǁVelocityǁ         0.0009901          9.0634          5.0349          5.0349
v  Pressure               -25.308          27.342         0.59464         0.59464
v  nu_tilda           4.4009e-007       0.0045008       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc              3.3e-014       0.0053042       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2712:        0.22910E+01

===============================================================


 INSTANT    0.271300000E+04   TIME STEP NUMBER            2713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15176E-01 0.88914E+00
   Friction velocity        uk    :  0.15176E-01 0.88914E+00
   Dimensionless distance   yplus :  0.12218E+00 0.71582E+01
   Friction thermal sca.    tstar : -0.58659E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91161E-01 0.53408E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10631E-01      33   0.22933E-03   0.43754E+01 0.19306E+03 
c  Velocity[X]                                      0.19970E+01 
c  Velocity[Y]                                      0.23784E+01 
c  Velocity[Z]                                      0.99425E-30 
c  Pressure     0.96914E-07     536   0.99410E-08   0.93459E-01 0.17684E+04 
c  nu_tilda     0.84282E-05      33   0.23728E-05   0.72005E-06 0.21327E+03 
c  TempC        0.43987E+02      26   0.28907E-03   0.59247E+01 0.26221E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.329          9.0604          4.5729          4.5729
v  Velocity[Y]            -2.8253          7.1816         0.24133         0.24133
v  Velocity[Z]       -7.8665e-015     7.8735e-015    -1.4795e-017    -1.4795e-017
v  ǁVelocityǁ        0.00037976           9.062          5.0348          5.0348
v  Pressure               -25.256          27.538         0.67338         0.67338
v  nu_tilda           4.4008e-007       0.0045011       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc              3.3e-014       0.0053046       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2713:        0.22810E+01

===============================================================


 INSTANT    0.271400000E+04   TIME STEP NUMBER            2714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15825E-01 0.89015E+00
   Friction velocity        uk    :  0.15825E-01 0.89015E+00
   Dimensionless distance   yplus :  0.12740E+00 0.71663E+01
   Friction thermal sca.    tstar : -0.57622E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95057E-01 0.53469E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10630E-01      33   0.28100E-03   0.43836E+01 0.19323E+03 
c  Velocity[X]                                      0.20087E+01 
c  Velocity[Y]                                      0.23749E+01 
c  Velocity[Z]                                      0.99392E-30 
c  Pressure     0.97249E-07     553   0.96322E-08   0.95518E-01 0.21029E+04 
c  nu_tilda     0.84289E-05      33   0.13109E-04   0.72017E-06 0.21327E+03 
c  TempC        0.43987E+02      26   0.29147E-03   0.53099E+01 0.25593E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3294          9.0591          4.5729          4.5729
v  Velocity[Y]            -2.8244          7.1598         0.24128         0.24128
v  Velocity[Z]        -7.912e-015     7.8766e-015    -1.4784e-017    -1.4784e-017
v  ǁVelocityǁ        0.00029525          9.0608          5.0347          5.0347
v  Pressure               -25.328          27.306         0.57424         0.57424
v  nu_tilda           4.4011e-007       0.0045014       0.0017891       0.0017891
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.2999e-014        0.005305       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2714:        0.22770E+01

===============================================================


 INSTANT    0.271500000E+04   TIME STEP NUMBER            2715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11411E-01 0.88957E+00
   Friction velocity        uk    :  0.11411E-01 0.88957E+00
   Dimensionless distance   yplus :  0.91866E-01 0.71616E+01
   Friction thermal sca.    tstar : -0.58888E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68542E-01 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10629E-01      33   0.24027E-03   0.44213E+01 0.19338E+03 
c  Velocity[X]                                      0.20286E+01 
c  Velocity[Y]                                      0.23927E+01 
c  Velocity[Z]                                      0.11664E-29 
c  Pressure     0.11983E-06     554   0.97085E-08   0.11529E+00 0.19844E+04 
c  nu_tilda     0.84296E-05      33   0.23798E-05   0.72024E-06 0.21327E+03 
c  TempC        0.43988E+02      26   0.28874E-03   0.64545E+01 0.28788E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3297          9.0578          4.5729          4.5729
v  Velocity[Y]            -2.8235           7.185         0.24123         0.24123
v  Velocity[Z]       -7.9183e-015     7.8699e-015    -1.4775e-017    -1.4775e-017
v  ǁVelocityǁ        0.00081003          9.0595          5.0346          5.0346
v  Pressure               -25.274          27.543         0.66083         0.66083
v  nu_tilda           4.4011e-007       0.0045017       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3007e-014       0.0053054       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2715:        0.22730E+01

===============================================================


 INSTANT    0.271600000E+04   TIME STEP NUMBER            2716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96028E-02 0.89072E+00
   Friction velocity        uk    :  0.96028E-02 0.89072E+00
   Dimensionless distance   yplus :  0.77309E-01 0.71709E+01
   Friction thermal sca.    tstar : -0.57301E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57681E-01 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10628E-01      33   0.21736E-03   0.43695E+01 0.19307E+03 
c  Velocity[X]                                      0.19962E+01 
c  Velocity[Y]                                      0.23733E+01 
c  Velocity[Z]                                      0.11158E-29 
c  Pressure     0.10720E-06     537   0.90626E-08   0.10236E+00 0.17824E+04 
c  nu_tilda     0.84302E-05      33   0.13101E-04   0.72030E-06 0.21326E+03 
c  TempC        0.43989E+02      27   0.32462E-03   0.50433E+01 0.24647E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.33          9.0565          4.5729          4.5729
v  Velocity[Y]            -2.8226          7.1868         0.24119         0.24119
v  Velocity[Z]       -7.9845e-015     7.8744e-015    -1.4763e-017    -1.4763e-017
v  ǁVelocityǁ         0.0011843          9.0581          5.0345          5.0345
v  Pressure               -25.349          27.367         0.57218         0.57218
v  nu_tilda           4.4009e-007        0.004502       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3008e-014       0.0053058       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2716:        0.22460E+01

===============================================================


 INSTANT    0.271700000E+04   TIME STEP NUMBER            2717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18510E-01 0.89056E+00
   Friction velocity        uk    :  0.18510E-01 0.89056E+00
   Dimensionless distance   yplus :  0.14901E+00 0.71696E+01
   Friction thermal sca.    tstar : -0.57297E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11118E+00 0.53493E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10627E-01      33   0.23701E-03   0.43644E+01 0.19297E+03 
c  Velocity[X]                                      0.20022E+01 
c  Velocity[Y]                                      0.23622E+01 
c  Velocity[Z]                                      0.12943E-29 
c  Pressure     0.10726E-06     537   0.91170E-08   0.10613E+00 0.86280E+03 
c  nu_tilda     0.84309E-05      33   0.23761E-05   0.72033E-06 0.21326E+03 
c  TempC        0.43989E+02      27   0.27722E-03   0.41031E+01 0.24071E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3303          9.0552          4.5729          4.5729
v  Velocity[Y]            -2.8217          7.1634         0.24114         0.24114
v  Velocity[Z]        -7.987e-015     7.8692e-015    -1.4751e-017    -1.4751e-017
v  ǁVelocityǁ        0.00054927          9.0569          5.0344          5.0344
v  Pressure               -25.291          27.401         0.61754         0.61754
v  nu_tilda           4.4012e-007       0.0045024       0.0017891       0.0017891
v  TempC                       21          73.053          22.059          22.059
v  TurbVisc           3.3003e-014       0.0053061       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2717:        0.22430E+01

===============================================================


 INSTANT    0.271800000E+04   TIME STEP NUMBER            2718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11331E-01 0.88919E+00
   Friction velocity        uk    :  0.11331E-01 0.88919E+00
   Dimensionless distance   yplus :  0.91221E-01 0.71586E+01
   Friction thermal sca.    tstar : -0.58282E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68061E-01 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10626E-01      33   0.25608E-03   0.43649E+01 0.19300E+03 
c  Velocity[X]                                      0.19848E+01 
c  Velocity[Y]                                      0.23801E+01 
c  Velocity[Z]                                      0.96513E-30 
c  Pressure     0.10071E-06     505   0.97526E-08   0.97516E-01 0.93806E+03 
c  nu_tilda     0.84316E-05      33   0.13096E-04   0.72044E-06 0.21326E+03 
c  TempC        0.43990E+02      27   0.27467E-03   0.56618E+01 0.25676E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3307          9.0539          4.5729          4.5729
v  Velocity[Y]            -2.8207          7.1816         0.24109         0.24109
v  Velocity[Z]       -8.0582e-015      7.875e-015     -1.474e-017     -1.474e-017
v  ǁVelocityǁ         0.0002455          9.0556          5.0343          5.0343
v  Pressure               -25.372          27.384         0.56345         0.56345
v  nu_tilda           4.4012e-007       0.0045027       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3009e-014       0.0053065       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2718:        0.21440E+01

===============================================================


 INSTANT    0.271900000E+04   TIME STEP NUMBER            2719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13011E-01 0.89030E+00
   Friction velocity        uk    :  0.13011E-01 0.89030E+00
   Dimensionless distance   yplus :  0.10475E+00 0.71675E+01
   Friction thermal sca.    tstar : -0.61241E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78153E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10625E-01      33   0.24250E-03   0.43903E+01 0.19300E+03 
c  Velocity[X]                                      0.20276E+01 
c  Velocity[Y]                                      0.23627E+01 
c  Velocity[Z]                                      0.10036E-29 
c  Pressure     0.13241E-06     458   0.91142E-08   0.12712E+00 0.58365E+03 
c  nu_tilda     0.84322E-05      33   0.23842E-05   0.72051E-06 0.21326E+03 
c  TempC        0.43991E+02      26   0.34507E-03   0.57510E+01 0.26591E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3309          9.0526          4.5729          4.5729
v  Velocity[Y]            -2.8198          7.1586         0.24104         0.24104
v  Velocity[Z]       -8.0763e-015     7.8697e-015    -1.4731e-017    -1.4731e-017
v  ǁVelocityǁ        0.00081131          9.0543          5.0342          5.0342
v  Pressure                -25.31          27.336         0.58921         0.58921
v  nu_tilda            4.402e-007        0.004503       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3011e-014       0.0053069       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2719:        0.22180E+01

===============================================================


 INSTANT    0.272000000E+04   TIME STEP NUMBER            2720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.35070E-02 0.88984E+00
   Friction velocity        uk    :  0.35070E-02 0.88984E+00
   Dimensionless distance   yplus :  0.28234E-01 0.71638E+01
   Friction thermal sca.    tstar : -0.59895E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21065E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10625E-01      33   0.19499E-03   0.43769E+01 0.19305E+03 
c  Velocity[X]                                      0.20183E+01 
c  Velocity[Y]                                      0.23585E+01 
c  Velocity[Z]                                      0.10976E-29 
c  Pressure     0.97321E-07     506   0.90803E-08   0.94595E-01 0.86829E+03 
c  nu_tilda     0.84329E-05      33   0.13089E-04   0.72060E-06 0.21326E+03 
c  TempC        0.43991E+02      27   0.25102E-03   0.61488E+01 0.28923E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3312          9.0513          4.5729          4.5729
v  Velocity[Y]            -2.8188          7.1841         0.24099         0.24099
v  Velocity[Z]       -8.1463e-015     7.8703e-015    -1.4717e-017    -1.4717e-017
v  ǁVelocityǁ         0.0015917           9.053          5.0341          5.0341
v  Pressure               -25.388          27.343         0.53956         0.53956
v  nu_tilda           4.4017e-007       0.0045033        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3035e-014       0.0053073       0.0021034       0.0021034
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2720:        0.24160E+01

===============================================================


 INSTANT    0.272100000E+04   TIME STEP NUMBER            2721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18273E-01 0.89126E+00
   Friction velocity        uk    :  0.18273E-01 0.89126E+00
   Dimensionless distance   yplus :  0.14711E+00 0.71753E+01
   Friction thermal sca.    tstar : -0.57969E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10976E+00 0.53535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10624E-01      33   0.22505E-03   0.43502E+01 0.19294E+03 
c  Velocity[X]                                      0.19739E+01 
c  Velocity[Y]                                      0.23763E+01 
c  Velocity[Z]                                      0.98485E-30 
c  Pressure     0.79259E-07     537   0.99122E-08   0.76852E-01 0.11801E+04 
c  nu_tilda     0.84335E-05      33   0.23819E-05   0.72066E-06 0.21326E+03 
c  TempC        0.43992E+02      26   0.29201E-03   0.45801E+01 0.23810E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3315            9.05          4.5729          4.5729
v  Velocity[Y]             -2.818          7.1949         0.24094         0.24094
v  Velocity[Z]       -8.1591e-015     7.8652e-015    -1.4706e-017    -1.4706e-017
v  ǁVelocityǁ         0.0021543          9.0517          5.0341          5.0341
v  Pressure               -25.331          27.445         0.59768         0.59768
v  nu_tilda           4.4004e-007       0.0045036       0.0017891       0.0017891
v  TempC                       21          73.053          22.059          22.059
v  TurbVisc           3.3024e-014       0.0053076       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2721:        0.22270E+01

===============================================================


 INSTANT    0.272200000E+04   TIME STEP NUMBER            2722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18463E-01 0.89075E+00
   Friction velocity        uk    :  0.18463E-01 0.89075E+00
   Dimensionless distance   yplus :  0.14864E+00 0.71711E+01
   Friction thermal sca.    tstar : -0.57511E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11090E+00 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10623E-01      33   0.24517E-03   0.43623E+01 0.19292E+03 
c  Velocity[X]                                      0.20032E+01 
c  Velocity[Y]                                      0.23591E+01 
c  Velocity[Z]                                      0.11523E-29 
c  Pressure     0.11290E-06     585   0.91681E-08   0.10991E+00 0.20527E+04 
c  nu_tilda     0.84341E-05      33   0.13081E-04   0.72074E-06 0.21326E+03 
c  TempC        0.43992E+02      26   0.30208E-03   0.53737E+01 0.25410E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3318          9.0487          4.5729          4.5729
v  Velocity[Y]             -2.817           7.163         0.24089         0.24089
v  Velocity[Z]        -8.249e-015     7.8677e-015    -1.4696e-017    -1.4696e-017
v  ǁVelocityǁ        0.00095403          9.0504           5.034           5.034
v  Pressure               -25.408          27.214          0.4999          0.4999
v  nu_tilda           4.4003e-007       0.0045039        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2986e-014        0.005308       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2722:        0.23470E+01

===============================================================


 INSTANT    0.272300000E+04   TIME STEP NUMBER            2723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17344E-01 0.88953E+00
   Friction velocity        uk    :  0.17344E-01 0.88953E+00
   Dimensionless distance   yplus :  0.13963E+00 0.71613E+01
   Friction thermal sca.    tstar : -0.58740E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10418E+00 0.53431E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10622E-01      33   0.26651E-03   0.43741E+01 0.19293E+03 
c  Velocity[X]                                      0.20250E+01 
c  Velocity[Y]                                      0.23491E+01 
c  Velocity[Z]                                      0.91981E-30 
c  Pressure     0.11244E-06     586   0.97019E-08   0.10863E+00 0.17665E+04 
c  nu_tilda     0.84348E-05      33   0.23853E-05   0.72080E-06 0.21326E+03 
c  TempC        0.43993E+02      26   0.28420E-03   0.45756E+01 0.24896E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3322          9.0475          4.5729          4.5729
v  Velocity[Y]            -2.8161          7.1863         0.24084         0.24084
v  Velocity[Z]       -8.2661e-015     7.8645e-015    -1.4684e-017    -1.4684e-017
v  ǁVelocityǁ         0.0011138          9.0491          5.0339          5.0339
v  Pressure               -25.352           27.42         0.57799         0.57799
v  nu_tilda           4.4004e-007       0.0045042       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2983e-014       0.0053083       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2723:        0.23320E+01

===============================================================


 INSTANT    0.272400000E+04   TIME STEP NUMBER            2724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10970E-01 0.89049E+00
   Friction velocity        uk    :  0.10970E-01 0.89049E+00
   Dimensionless distance   yplus :  0.88318E-01 0.71691E+01
   Friction thermal sca.    tstar : -0.57567E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65895E-01 0.53489E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10621E-01      33   0.24269E-03   0.43630E+01 0.19288E+03 
c  Velocity[X]                                      0.19996E+01 
c  Velocity[Y]                                      0.23634E+01 
c  Velocity[Z]                                      0.91830E-30 
c  Pressure     0.10294E-06     552   0.94728E-08   0.10112E+00 0.19048E+04 
c  nu_tilda     0.84354E-05      33   0.13074E-04   0.72091E-06 0.21326E+03 
c  TempC        0.43994E+02      27   0.35157E-03   0.44197E+01 0.24055E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3325          9.0462          4.5729          4.5729
v  Velocity[Y]            -2.8151           7.162         0.24079         0.24079
v  Velocity[Z]       -8.3686e-015     7.8662e-015    -1.4677e-017    -1.4677e-017
v  ǁVelocityǁ        0.00081394          9.0478          5.0338          5.0338
v  Pressure               -25.427          27.215         0.48613         0.48613
v  nu_tilda           4.4007e-007       0.0045046        0.001789        0.001789
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.2985e-014       0.0053087       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2724:        0.22540E+01

===============================================================


 INSTANT    0.272500000E+04   TIME STEP NUMBER            2725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17389E-01 0.88957E+00
   Friction velocity        uk    :  0.17389E-01 0.88957E+00
   Dimensionless distance   yplus :  0.13999E+00 0.71617E+01
   Friction thermal sca.    tstar : -0.58050E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10445E+00 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10620E-01      33   0.24545E-03   0.43547E+01 0.19282E+03 
c  Velocity[X]                                      0.20034E+01 
c  Velocity[Y]                                      0.23513E+01 
c  Velocity[Z]                                      0.10609E-29 
c  Pressure     0.10667E-06     521   0.97139E-08   0.10185E+00 0.14840E+04 
c  nu_tilda     0.84360E-05      33   0.23876E-05   0.72096E-06 0.21326E+03 
c  TempC        0.43994E+02      27   0.28636E-03   0.56994E+01 0.28751E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3328          9.0449          4.5729          4.5729
v  Velocity[Y]            -2.8141          7.1836         0.24073         0.24073
v  Velocity[Z]       -8.3884e-015     7.8572e-015    -1.4668e-017    -1.4668e-017
v  ǁVelocityǁ         0.0016965          9.0465          5.0337          5.0337
v  Pressure               -25.369          27.375          0.5548          0.5548
v  nu_tilda           4.4007e-007       0.0045049       0.0017891       0.0017891
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2995e-014       0.0053091       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2725:        0.21870E+01

===============================================================


 INSTANT    0.272600000E+04   TIME STEP NUMBER            2726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94075E-02 0.89091E+00
   Friction velocity        uk    :  0.94075E-02 0.89091E+00
   Dimensionless distance   yplus :  0.75737E-01 0.71724E+01
   Friction thermal sca.    tstar : -0.57707E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56508E-01 0.53514E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10619E-01      33   0.24593E-03   0.43389E+01 0.19272E+03 
c  Velocity[X]                                      0.19969E+01 
c  Velocity[Y]                                      0.23420E+01 
c  Velocity[Z]                                      0.87488E-30 
c  Pressure     0.87433E-07     522   0.95737E-08   0.85100E-01 0.12069E+04 
c  nu_tilda     0.84367E-05      33   0.13067E-04   0.72104E-06 0.21326E+03 
c  TempC        0.43995E+02      27   0.31458E-03   0.51116E+01 0.25844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3331          9.0436          4.5729          4.5729
v  Velocity[Y]            -2.8132          7.1925         0.24068         0.24068
v  Velocity[Z]       -8.5005e-015     7.8591e-015     -1.466e-017     -1.466e-017
v  ǁVelocityǁ         0.0016355          9.0452          5.0337          5.0337
v  Pressure                -25.45          27.292         0.48788         0.48788
v  nu_tilda           4.4001e-007       0.0045052        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2995e-014       0.0053095       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2726:        0.21930E+01

===============================================================


 INSTANT    0.272700000E+04   TIME STEP NUMBER            2727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18957E-01 0.89054E+00
   Friction velocity        uk    :  0.18957E-01 0.89054E+00
   Dimensionless distance   yplus :  0.15261E+00 0.71694E+01
   Friction thermal sca.    tstar : -0.61186E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11387E+00 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10618E-01      33   0.23518E-03   0.43558E+01 0.19276E+03 
c  Velocity[X]                                      0.20007E+01 
c  Velocity[Y]                                      0.23551E+01 
c  Velocity[Z]                                      0.11306E-29 
c  Pressure     0.11209E-06     490   0.92085E-08   0.10982E+00 0.60602E+03 
c  nu_tilda     0.84373E-05      33   0.23885E-05   0.72111E-06 0.21326E+03 
c  TempC        0.43995E+02      27   0.26470E-03   0.50273E+01 0.26132E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3334          9.0423          4.5729          4.5729
v  Velocity[Y]            -2.8124          7.1655         0.24062         0.24062
v  Velocity[Z]         -8.52e-015     7.8518e-015    -1.4647e-017    -1.4647e-017
v  ǁVelocityǁ         0.0017447          9.0439          5.0336          5.0336
v  Pressure               -25.388           27.28         0.51856         0.51856
v  nu_tilda           4.3999e-007       0.0045055       0.0017891       0.0017891
v  TempC                       21          73.053          22.059          22.059
v  TurbVisc           3.2978e-014       0.0053098       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2727:        0.21080E+01

===============================================================


 INSTANT    0.272800000E+04   TIME STEP NUMBER            2728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15171E-01 0.88898E+00
   Friction velocity        uk    :  0.15171E-01 0.88898E+00
   Dimensionless distance   yplus :  0.12214E+00 0.71569E+01
   Friction thermal sca.    tstar : -0.59148E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91127E-01 0.53399E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10618E-01      33   0.24433E-03   0.43329E+01 0.19265E+03 
c  Velocity[X]                                      0.19912E+01 
c  Velocity[Y]                                      0.23416E+01 
c  Velocity[Z]                                      0.97193E-30 
c  Pressure     0.10375E-06     521   0.94955E-08   0.99516E-01 0.91707E+03 
c  nu_tilda     0.84379E-05      33   0.13062E-04   0.72124E-06 0.21326E+03 
c  TempC        0.43996E+02      26   0.26490E-03   0.48752E+01 0.25283E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3337           9.041          4.5729          4.5729
v  Velocity[Y]            -2.8114          7.1804         0.24057         0.24057
v  Velocity[Z]       -8.6513e-015     7.8575e-015    -1.4641e-017    -1.4641e-017
v  ǁVelocityǁ         0.0014883          9.0426          5.0335          5.0335
v  Pressure                -25.47          27.251         0.46594         0.46594
v  nu_tilda           4.3998e-007       0.0045057        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2972e-014       0.0053101       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2728:        0.22150E+01

===============================================================


 INSTANT    0.272900000E+04   TIME STEP NUMBER            2729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16948E-01 0.89031E+00
   Friction velocity        uk    :  0.16948E-01 0.89031E+00
   Dimensionless distance   yplus :  0.13644E+00 0.71676E+01
   Friction thermal sca.    tstar : -0.58936E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10180E+00 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10617E-01      33   0.25150E-03   0.43567E+01 0.19272E+03 
c  Velocity[X]                                      0.20237E+01 
c  Velocity[Y]                                      0.23331E+01 
c  Velocity[Z]                                      0.10197E-29 
c  Pressure     0.11336E-06     490   0.97081E-08   0.11160E+00 0.60764E+03 
c  nu_tilda     0.84385E-05      33   0.23929E-05   0.72129E-06 0.21326E+03 
c  TempC        0.43996E+02      27   0.34164E-03   0.50877E+01 0.24559E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3339          9.0397          4.5729          4.5729
v  Velocity[Y]            -2.8105          7.1632         0.24051         0.24051
v  Velocity[Z]       -8.6736e-015     7.8494e-015    -1.4632e-017    -1.4632e-017
v  ǁVelocityǁ         0.0017337          9.0413          5.0334          5.0334
v  Pressure               -25.408          27.241          0.4968          0.4968
v  nu_tilda           4.3999e-007       0.0045061        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2967e-014       0.0053105       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2729:        0.21180E+01

===============================================================


 INSTANT    0.273000000E+04   TIME STEP NUMBER            2730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12112E-01 0.88953E+00
   Friction velocity        uk    :  0.12112E-01 0.88953E+00
   Dimensionless distance   yplus :  0.97512E-01 0.71613E+01
   Friction thermal sca.    tstar : -0.62498E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.72755E-01 0.53432E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10616E-01      33   0.18687E-03   0.43448E+01 0.19275E+03 
c  Velocity[X]                                      0.19933E+01 
c  Velocity[Y]                                      0.23515E+01 
c  Velocity[Z]                                      0.10894E-29 
c  Pressure     0.95210E-07     505   0.93701E-08   0.92344E-01 0.89946E+03 
c  nu_tilda     0.84391E-05      33   0.13054E-04   0.72137E-06 0.21326E+03 
c  TempC        0.43997E+02      26   0.24629E-03   0.63018E+01 0.29549E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3342          9.0384          4.5729          4.5729
v  Velocity[Y]            -2.8095          7.1855         0.24046         0.24046
v  Velocity[Z]       -8.8199e-015     7.8527e-015    -1.4624e-017    -1.4624e-017
v  ǁVelocityǁ         0.0016938            9.04          5.0334          5.0334
v  Pressure               -25.488          27.236         0.44483         0.44483
v  nu_tilda           4.3999e-007       0.0045064        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2971e-014       0.0053109       0.0021033       0.0021033
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2730:        0.21400E+01

===============================================================


 INSTANT    0.273100000E+04   TIME STEP NUMBER            2731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18795E-01 0.89091E+00
   Friction velocity        uk    :  0.18795E-01 0.89091E+00
   Dimensionless distance   yplus :  0.15131E+00 0.71724E+01
   Friction thermal sca.    tstar : -0.64246E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11290E+00 0.53514E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10615E-01      33   0.24050E-03   0.43174E+01 0.19251E+03 
c  Velocity[X]                                      0.19833E+01 
c  Velocity[Y]                                      0.23341E+01 
c  Velocity[Z]                                      0.91174E-30 
c  Pressure     0.11277E-06     522   0.92509E-08   0.10773E+00 0.11125E+04 
c  nu_tilda     0.84397E-05      33   0.23939E-05   0.72143E-06 0.21326E+03 
c  TempC        0.43997E+02      26   0.26004E-03   0.42812E+01 0.23755E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3344          9.0372          4.5729          4.5729
v  Velocity[Y]            -2.8085          7.1915          0.2404          0.2404
v  Velocity[Z]       -8.8421e-015     7.8462e-015    -1.4617e-017    -1.4617e-017
v  ǁVelocityǁ         0.0011855          9.0388          5.0333          5.0333
v  Pressure               -25.432          27.321         0.50057         0.50057
v  nu_tilda           4.3996e-007       0.0045067        0.001789        0.001789
v  TempC                       21          73.053          22.059          22.059
v  TurbVisc            3.297e-014       0.0053112       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2731:        0.21880E+01

===============================================================


 INSTANT    0.273200000E+04   TIME STEP NUMBER            2732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16844E-01 0.89057E+00
   Friction velocity        uk    :  0.16844E-01 0.89057E+00
   Dimensionless distance   yplus :  0.13560E+00 0.71697E+01
   Friction thermal sca.    tstar : -0.66650E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10118E+00 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10614E-01      33   0.23619E-03   0.43535E+01 0.19266E+03 
c  Velocity[X]                                      0.20249E+01 
c  Velocity[Y]                                      0.23287E+01 
c  Velocity[Z]                                      0.10134E-29 
c  Pressure     0.98094E-07     586   0.96287E-08   0.96744E-01 0.20044E+04 
c  nu_tilda     0.84403E-05      33   0.13047E-04   0.72155E-06 0.21326E+03 
c  TempC        0.43998E+02      27   0.34063E-03   0.40006E+01 0.22210E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3346           9.036          4.5729          4.5729
v  Velocity[Y]            -2.8076           7.165         0.24034         0.24034
v  Velocity[Z]       -9.0107e-015      7.842e-015    -1.4605e-017    -1.4605e-017
v  ǁVelocityǁ        0.00030586          9.0375          5.0332          5.0332
v  Pressure               -25.506          27.104         0.40403         0.40403
v  nu_tilda              4.4e-007        0.004507       0.0017889       0.0017889
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2962e-014       0.0053116       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2732:        0.23440E+01

===============================================================


 INSTANT    0.273300000E+04   TIME STEP NUMBER            2733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13001E-01 0.88924E+00
   Friction velocity        uk    :  0.13001E-01 0.88924E+00
   Dimensionless distance   yplus :  0.10466E+00 0.71590E+01
   Friction thermal sca.    tstar : -0.69207E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78090E-01 0.53414E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10613E-01      33   0.23202E-03   0.43293E+01 0.19256E+03 
c  Velocity[X]                                      0.19866E+01 
c  Velocity[Y]                                      0.23428E+01 
c  Velocity[Z]                                      0.96117E-30 
c  Pressure     0.84834E-07     570   0.93338E-08   0.82563E-01 0.19291E+04 
c  nu_tilda     0.84409E-05      33   0.23991E-05   0.72165E-06 0.21327E+03 
c  TempC        0.43998E+02      27   0.25929E-03   0.56013E+01 0.26079E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3349          9.0347          4.5729          4.5729
v  Velocity[Y]            -2.8067           7.185         0.24028         0.24028
v  Velocity[Z]       -9.0321e-015     7.8352e-015    -1.4599e-017    -1.4599e-017
v  ǁVelocityǁ        0.00049769          9.0362          5.0331          5.0331
v  Pressure               -25.454          27.329         0.48816         0.48816
v  nu_tilda           4.4002e-007       0.0045072        0.001789        0.001789
v  TempC                       21          73.053          22.059          22.059
v  TurbVisc           3.2976e-014       0.0053119       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2733:        0.22890E+01

===============================================================


 INSTANT    0.273400000E+04   TIME STEP NUMBER            2734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.78587E-02 0.89004E+00
   Friction velocity        uk    :  0.78587E-02 0.89004E+00
   Dimensionless distance   yplus :  0.63268E-01 0.71654E+01
   Friction thermal sca.    tstar : -0.70919E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47205E-01 0.53462E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10612E-01      33   0.25492E-03   0.43219E+01 0.19249E+03 
c  Velocity[X]                                      0.19955E+01 
c  Velocity[Y]                                      0.23263E+01 
c  Velocity[Z]                                      0.10819E-29 
c  Pressure     0.10811E-06     569   0.92979E-08   0.10487E+00 0.23886E+04 
c  nu_tilda     0.84415E-05      33   0.13040E-04   0.72175E-06 0.21327E+03 
c  TempC        0.43999E+02      27   0.24613E-03   0.46692E+01 0.22698E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3351          9.0335          4.5729          4.5729
v  Velocity[Y]            -2.8058          7.1573         0.24023         0.24023
v  Velocity[Z]       -9.2221e-015     7.8351e-015    -1.4594e-017    -1.4594e-017
v  ǁVelocityǁ         0.0014605          9.0349          5.0331          5.0331
v  Pressure               -25.526          27.055         0.37854         0.37854
v  nu_tilda           4.4007e-007       0.0045075       0.0017889       0.0017889
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc            3.298e-014       0.0053122       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2734:        0.22990E+01

===============================================================


 INSTANT    0.273500000E+04   TIME STEP NUMBER            2735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11235E-01 0.88944E+00
   Friction velocity        uk    :  0.11235E-01 0.88944E+00
   Dimensionless distance   yplus :  0.90450E-01 0.71606E+01
   Friction thermal sca.    tstar : -0.75144E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67486E-01 0.53426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10611E-01      33   0.20409E-03   0.43413E+01 0.19259E+03 
c  Velocity[X]                                      0.20201E+01 
c  Velocity[Y]                                      0.23212E+01 
c  Velocity[Z]                                      0.11219E-29 
c  Pressure     0.11201E-06     554   0.92165E-08   0.10790E+00 0.19755E+04 
c  nu_tilda     0.84420E-05      33   0.23969E-05   0.72180E-06 0.21327E+03 
c  TempC        0.43999E+02      26   0.36442E-03   0.47882E+01 0.25670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3354          9.0323          4.5729          4.5729
v  Velocity[Y]            -2.8048           7.185         0.24017         0.24017
v  Velocity[Z]       -9.2335e-015     7.8318e-015     -1.459e-017     -1.459e-017
v  ǁVelocityǁ        0.00082157          9.0336           5.033           5.033
v  Pressure               -25.472          27.289         0.46404         0.46404
v  nu_tilda           4.4005e-007       0.0045078        0.001789        0.001789
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2996e-014       0.0053126       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2735:        0.22720E+01

===============================================================


 INSTANT    0.273600000E+04   TIME STEP NUMBER            2736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18274E-01 0.89077E+00
   Friction velocity        uk    :  0.18274E-01 0.89077E+00
   Dimensionless distance   yplus :  0.14712E+00 0.71713E+01
   Friction thermal sca.    tstar : -0.79631E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10977E+00 0.53506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10610E-01      33   0.23534E-03   0.43137E+01 0.19249E+03 
c  Velocity[X]                                      0.19779E+01 
c  Velocity[Y]                                      0.23357E+01 
c  Velocity[Z]                                      0.89327E-30 
c  Pressure     0.90137E-07     553   0.92861E-08   0.87133E-01 0.14628E+04 
c  nu_tilda     0.84426E-05      33   0.13032E-04   0.72188E-06 0.21327E+03 
c  TempC        0.43999E+02      26   0.30223E-03   0.73626E+01 0.31288E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3356          9.0311          4.5729          4.5729
v  Velocity[Y]            -2.8038          7.1909         0.24011         0.24011
v  Velocity[Z]       -9.4458e-015     7.8321e-015    -1.4581e-017    -1.4581e-017
v  ǁVelocityǁ         0.0010235          9.0324          5.0329          5.0329
v  Pressure               -25.549           27.17         0.38698         0.38698
v  nu_tilda           4.3995e-007       0.0045081       0.0017889       0.0017889
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc            3.299e-014       0.0053129       0.0021032       0.0021032
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2736:        0.22790E+01

===============================================================


 INSTANT    0.273700000E+04   TIME STEP NUMBER            2737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.88938E-02 0.89030E+00
   Friction velocity        uk    :  0.88938E-02 0.89030E+00
   Dimensionless distance   yplus :  0.71601E-01 0.71676E+01
   Friction thermal sca.    tstar : -0.83704E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53423E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10609E-01      33   0.23229E-03   0.43296E+01 0.19243E+03 
c  Velocity[X]                                      0.20084E+01 
c  Velocity[Y]                                      0.23212E+01 
c  Velocity[Z]                                      0.11051E-29 
c  Pressure     0.11392E-06     488   0.94056E-08   0.11047E+00 0.59078E+03 
c  nu_tilda     0.84432E-05      33   0.24048E-05   0.72197E-06 0.21327E+03 
c  TempC        0.44000E+02      26   0.29286E-03   0.50468E+01 0.25223E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3358          9.0299          4.5729          4.5729
v  Velocity[Y]            -2.8029           7.161         0.24005         0.24005
v  Velocity[Z]       -9.4533e-015     7.8265e-015     -1.457e-017     -1.457e-017
v  ǁVelocityǁ         0.0011379          9.0312          5.0329          5.0329
v  Pressure               -25.487          27.127         0.41456         0.41456
v  nu_tilda           4.3996e-007       0.0045084       0.0017889       0.0017889
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc            3.296e-014       0.0053133       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2737:        0.21230E+01

===============================================================


 INSTANT    0.273800000E+04   TIME STEP NUMBER            2738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16962E-01 0.88910E+00
   Friction velocity        uk    :  0.16962E-01 0.88910E+00
   Dimensionless distance   yplus :  0.13656E+00 0.71578E+01
   Friction thermal sca.    tstar : -0.93234E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10189E+00 0.53405E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10608E-01      33   0.23707E-03   0.43244E+01 0.19242E+03 
c  Velocity[X]                                      0.20094E+01 
c  Velocity[Y]                                      0.23150E+01 
c  Velocity[Z]                                      0.91896E-30 
c  Pressure     0.91350E-07     522   0.93479E-08   0.88845E-01 0.77531E+03 
c  nu_tilda     0.84437E-05      33   0.13029E-04   0.72211E-06 0.21327E+03 
c  TempC        0.44000E+02      26   0.27578E-03   0.52226E+01 0.25089E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3361          9.0286          4.5729          4.5729
v  Velocity[Y]             -2.802          7.1818         0.23999         0.23999
v  Velocity[Z]       -9.7016e-015     7.8279e-015     -1.457e-017     -1.457e-017
v  ǁVelocityǁ         0.0013787            9.03          5.0328          5.0328
v  Pressure               -25.571          27.152         0.37199         0.37199
v  nu_tilda           4.4001e-007       0.0045087       0.0017888       0.0017888
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2962e-014       0.0053136       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2738:        0.21800E+01

===============================================================


 INSTANT    0.273900000E+04   TIME STEP NUMBER            2739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18753E-01 0.89027E+00
   Friction velocity        uk    :  0.18753E-01 0.89027E+00
   Dimensionless distance   yplus :  0.15097E+00 0.71672E+01
   Friction thermal sca.    tstar : -0.92557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11264E+00 0.53476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10607E-01      33   0.24598E-03   0.43191E+01 0.19239E+03 
c  Velocity[X]                                      0.19917E+01 
c  Velocity[Y]                                      0.23274E+01 
c  Velocity[Z]                                      0.88097E-30 
c  Pressure     0.10572E-06     506   0.92795E-08   0.10323E+00 0.58799E+03 
c  nu_tilda     0.84443E-05      33   0.24015E-05   0.72218E-06 0.21328E+03 
c  TempC        0.44001E+02      27   0.29495E-03   0.48980E+01 0.24325E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3363          9.0274          4.5729          4.5729
v  Velocity[Y]             -2.801          7.1611         0.23992         0.23992
v  Velocity[Z]         -9.69e-015     7.8158e-015    -1.4564e-017    -1.4564e-017
v  ǁVelocityǁ         0.0023138          9.0288          5.0327          5.0327
v  Pressure               -25.509          27.137         0.40129         0.40129
v  nu_tilda           4.4007e-007       0.0045091       0.0017889       0.0017889
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2976e-014        0.005314       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2739:        0.21690E+01

===============================================================


 INSTANT    0.274000000E+04   TIME STEP NUMBER            2740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17327E-01 0.88931E+00
   Friction velocity        uk    :  0.17327E-01 0.88931E+00
   Dimensionless distance   yplus :  0.13950E+00 0.71595E+01
   Friction thermal sca.    tstar : -0.10673E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10408E+00 0.53418E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10606E-01      33   0.20526E-03   0.43069E+01 0.19236E+03 
c  Velocity[X]                                      0.19927E+01 
c  Velocity[Y]                                      0.23142E+01 
c  Velocity[Z]                                      0.10659E-29 
c  Pressure     0.10785E-06     538   0.94025E-08   0.10329E+00 0.10288E+04 
c  nu_tilda     0.84449E-05      33   0.13020E-04   0.72228E-06 0.21328E+03 
c  TempC        0.44001E+02      27   0.27964E-03   0.44913E+01 0.23284E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3365          9.0262          4.5729          4.5729
v  Velocity[Y]            -2.8001          7.1805         0.23986         0.23986
v  Velocity[Z]       -9.9611e-015     7.8172e-015    -1.4561e-017    -1.4561e-017
v  ǁVelocityǁ         0.0021334          9.0275          5.0327          5.0327
v  Pressure               -25.589          27.087         0.34276         0.34276
v  nu_tilda            4.401e-007       0.0045094       0.0017888       0.0017888
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.2994e-014       0.0053144       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2740:        0.22350E+01

===============================================================


 INSTANT    0.274100000E+04   TIME STEP NUMBER            2741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24129E-02 0.89101E+00
   Friction velocity        uk    :  0.24129E-02 0.89101E+00
   Dimensionless distance   yplus :  0.19426E-01 0.71732E+01
   Friction thermal sca.    tstar : -0.11207E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14494E-01 0.53520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10605E-01      33   0.25501E-03   0.43101E+01 0.19235E+03 
c  Velocity[X]                                      0.20025E+01 
c  Velocity[Y]                                      0.23076E+01 
c  Velocity[Z]                                      0.87458E-30 
c  Pressure     0.10089E-06     521   0.92120E-08   0.97924E-01 0.11422E+04 
c  nu_tilda     0.84454E-05      33   0.24085E-05   0.72233E-06 0.21328E+03 
c  TempC        0.44001E+02      27   0.23950E-03   0.58463E+01 0.25176E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3367           9.025          4.5729          4.5729
v  Velocity[Y]            -2.7991          7.1937         0.23979         0.23979
v  Velocity[Z]       -9.9375e-015     7.8098e-015    -1.4553e-017    -1.4553e-017
v  ǁVelocityǁ         0.0018317          9.0263          5.0326          5.0326
v  Pressure               -25.529          27.192         0.39875         0.39875
v  nu_tilda           4.4008e-007       0.0045097       0.0017889       0.0017889
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3004e-014       0.0053148       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2741:        0.21850E+01

===============================================================


 INSTANT    0.274200000E+04   TIME STEP NUMBER            2742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18391E-01 0.89064E+00
   Friction velocity        uk    :  0.18391E-01 0.89064E+00
   Dimensionless distance   yplus :  0.14806E+00 0.71703E+01
   Friction thermal sca.    tstar : -0.13683E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11047E+00 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10604E-01      33   0.23078E-03   0.43252E+01 0.19241E+03 
c  Velocity[X]                                      0.20017E+01 
c  Velocity[Y]                                      0.23235E+01 
c  Velocity[Z]                                      0.99548E-30 
c  Pressure     0.10006E-06     554   0.95767E-08   0.98433E-01 0.17787E+04 
c  nu_tilda     0.84460E-05      33   0.13014E-04   0.72246E-06 0.21328E+03 
c  TempC        0.44002E+02      26   0.34584E-03   0.60179E+01 0.26531E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3369          9.0238          4.5729          4.5729
v  Velocity[Y]            -2.7981          7.1646         0.23973         0.23973
v  Velocity[Z]        -1.024e-014      7.813e-015    -1.4553e-017    -1.4553e-017
v  ǁVelocityǁ         0.0018356          9.0251          5.0326          5.0326
v  Pressure               -25.607          27.004          0.3112          0.3112
v  nu_tilda           4.4006e-007         0.00451       0.0017888       0.0017888
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2999e-014       0.0053151       0.0021031       0.0021031
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2742:        0.22710E+01

===============================================================


 INSTANT    0.274300000E+04   TIME STEP NUMBER            2743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17666E-01 0.88920E+00
   Friction velocity        uk    :  0.17666E-01 0.88920E+00
   Dimensionless distance   yplus :  0.14222E+00 0.71586E+01
   Friction thermal sca.    tstar : -0.14993E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10611E+00 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10603E-01      33   0.23556E-03   0.43005E+01 0.19218E+03 
c  Velocity[X]                                      0.19947E+01 
c  Velocity[Y]                                      0.23058E+01 
c  Velocity[Z]                                      0.79908E-30 
c  Pressure     0.11262E-06     554   0.93004E-08   0.10706E+00 0.13897E+04 
c  nu_tilda     0.84465E-05      33   0.24062E-05   0.72254E-06 0.21328E+03 
c  TempC        0.44002E+02      27   0.26179E-03   0.62506E+01 0.29432E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3371          9.0226          4.5729          4.5729
v  Velocity[Y]            -2.7972          7.1814         0.23967         0.23967
v  Velocity[Z]         -1.02e-014     7.8068e-015    -1.4545e-017    -1.4545e-017
v  ǁVelocityǁ         0.0019145          9.0239          5.0325          5.0325
v  Pressure               -25.551           27.15         0.37539         0.37539
v  nu_tilda           4.4003e-007       0.0045103       0.0017888       0.0017888
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2993e-014       0.0053155        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2743:        0.22740E+01

===============================================================


 INSTANT    0.274400000E+04   TIME STEP NUMBER            2744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13170E-01 0.89034E+00
   Friction velocity        uk    :  0.13170E-01 0.89034E+00
   Dimensionless distance   yplus :  0.10602E+00 0.71678E+01
   Friction thermal sca.    tstar : -0.20111E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79106E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10603E-01      33   0.25173E-03   0.43202E+01 0.19228E+03 
c  Velocity[X]                                      0.20214E+01 
c  Velocity[Y]                                      0.22988E+01 
c  Velocity[Z]                                      0.95273E-30 
c  Pressure     0.10033E-06     584   0.98240E-08   0.98463E-01 0.19519E+04 
c  nu_tilda     0.84470E-05      33   0.13008E-04   0.72265E-06 0.21329E+03 
c  TempC        0.44002E+02      27   0.24501E-03   0.49882E+01 0.24850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3373          9.0213          4.5729          4.5729
v  Velocity[Y]            -2.7962          7.1593          0.2396          0.2396
v  Velocity[Z]       -1.0522e-014       7.81e-015    -1.4542e-017    -1.4542e-017
v  ǁVelocityǁ         0.0021574          9.0227          5.0324          5.0324
v  Pressure               -25.625          26.944         0.28072         0.28072
v  nu_tilda           4.4006e-007       0.0045106       0.0017887       0.0017887
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.2983e-014       0.0053158        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2744:        0.23360E+01

===============================================================


 INSTANT    0.274500000E+04   TIME STEP NUMBER            2745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55783E-02 0.88951E+00
   Friction velocity        uk    :  0.55783E-02 0.88951E+00
   Dimensionless distance   yplus :  0.44909E-01 0.71612E+01
   Friction thermal sca.    tstar : -0.47475E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33507E-01 0.53430E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10602E-01      33   0.23035E-03   0.43059E+01 0.19225E+03 
c  Velocity[X]                                      0.19914E+01 
c  Velocity[Y]                                      0.23145E+01 
c  Velocity[Z]                                      0.10814E-29 
c  Pressure     0.91971E-07     538   0.94527E-08   0.88920E-01 0.19054E+04 
c  nu_tilda     0.84476E-05      33   0.24106E-05   0.72273E-06 0.21329E+03 
c  TempC        0.44003E+02      26   0.30159E-03   0.47655E+01 0.23301E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3375          9.0201          4.5729          4.5729
v  Velocity[Y]            -2.7953          7.1851         0.23953         0.23953
v  Velocity[Z]         -1.05e-014     7.8041e-015    -1.4539e-017    -1.4539e-017
v  ǁVelocityǁ         0.0021225          9.0215          5.0324          5.0324
v  Pressure               -25.571          27.162         0.36454         0.36454
v  nu_tilda           4.4009e-007       0.0045109       0.0017888       0.0017888
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2992e-014       0.0053162        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2745:        0.22230E+01

===============================================================


 INSTANT    0.274600000E+04   TIME STEP NUMBER            2746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.88724E-02 0.89070E+00
   Friction velocity        uk    :  0.88724E-02 0.89070E+00
   Dimensionless distance   yplus :  0.71429E-01 0.71708E+01
   Friction thermal sca.    tstar : -0.29847E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.53294E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10601E-01      33   0.23218E-03   0.42694E+01 0.19205E+03 
c  Velocity[X]                                      0.19703E+01 
c  Velocity[Y]                                      0.22991E+01 
c  Velocity[Z]                                      0.91833E-30 
c  Pressure     0.94990E-07     554   0.93227E-08   0.91340E-01 0.16033E+04 
c  nu_tilda     0.84481E-05      33   0.12999E-04   0.72285E-06 0.21329E+03 
c  TempC        0.44003E+02      27   0.25529E-03   0.46528E+01 0.24219E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3376          9.0189          4.5729          4.5729
v  Velocity[Y]            -2.7943          7.1881         0.23947         0.23947
v  Velocity[Z]       -1.0868e-014      7.805e-015    -1.4537e-017    -1.4537e-017
v  ǁVelocityǁ        0.00095616          9.0202          5.0323          5.0323
v  Pressure               -25.647           27.02         0.28229         0.28229
v  nu_tilda           4.4009e-007       0.0045112       0.0017887       0.0017887
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3001e-014       0.0053166        0.002103        0.002103
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2746:        0.22660E+01

===============================================================


 INSTANT    0.274700000E+04   TIME STEP NUMBER            2747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13440E-01 0.89034E+00
   Friction velocity        uk    :  0.13440E-01 0.89034E+00
   Dimensionless distance   yplus :  0.10820E+00 0.71678E+01
   Friction thermal sca.    tstar : -0.19702E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80729E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10600E-01      33   0.27082E-03   0.42995E+01 0.19214E+03 
c  Velocity[X]                                      0.20067E+01 
c  Velocity[Y]                                      0.22928E+01 
c  Velocity[Z]                                      0.92359E-30 
c  Pressure     0.10766E-06     505   0.98036E-08   0.10554E+00 0.77364E+03 
c  nu_tilda     0.84486E-05      33   0.24112E-05   0.72293E-06 0.21329E+03 
c  TempC        0.44003E+02      27   0.29016E-03   0.35684E+01 0.22122E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3378          9.0177          4.5729          4.5729
v  Velocity[Y]            -2.7933          7.1632          0.2394          0.2394
v  Velocity[Z]       -1.0832e-014     7.7964e-015    -1.4534e-017    -1.4534e-017
v  ǁVelocityǁ         0.0019048           9.019          5.0323          5.0323
v  Pressure               -25.589          27.031          0.3235          0.3235
v  nu_tilda           4.4011e-007       0.0045115       0.0017887       0.0017887
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3001e-014        0.005317       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2747:        0.22490E+01

===============================================================


 INSTANT    0.274800000E+04   TIME STEP NUMBER            2748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16881E-01 0.88907E+00
   Friction velocity        uk    :  0.16881E-01 0.88907E+00
   Dimensionless distance   yplus :  0.13591E+00 0.71576E+01
   Friction thermal sca.    tstar : -0.15686E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10140E+00 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10599E-01      33   0.24426E-03   0.43283E+01 0.19230E+03 
c  Velocity[X]                                      0.20187E+01 
c  Velocity[Y]                                      0.23096E+01 
c  Velocity[Z]                                      0.89101E-30 
c  Pressure     0.11945E-06     538   0.97190E-08   0.11541E+00 0.10459E+04 
c  nu_tilda     0.84492E-05      33   0.12996E-04   0.72304E-06 0.21329E+03 
c  TempC        0.44004E+02      27   0.33999E-03   0.53789E+01 0.26273E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.338          9.0165          4.5729          4.5729
v  Velocity[Y]            -2.7923          7.1826         0.23933         0.23933
v  Velocity[Z]       -1.1159e-014      7.792e-015    -1.4533e-017    -1.4533e-017
v  ǁVelocityǁ         0.0019962          9.0178          5.0322          5.0322
v  Pressure               -25.667              27         0.26322         0.26322
v  nu_tilda           4.4011e-007       0.0045118       0.0017887       0.0017887
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3008e-014       0.0053173       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2748:        0.25320E+01

===============================================================


 INSTANT    0.274900000E+04   TIME STEP NUMBER            2749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10432E-01 0.89026E+00
   Friction velocity        uk    :  0.10432E-01 0.89026E+00
   Dimensionless distance   yplus :  0.83983E-01 0.71672E+01
   Friction thermal sca.    tstar : -0.13256E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.62661E-01 0.53475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10598E-01      33   0.21818E-03   0.43088E+01 0.19207E+03 
c  Velocity[X]                                      0.20184E+01 
c  Velocity[Y]                                      0.22904E+01 
c  Velocity[Z]                                      0.10166E-29 
c  Pressure     0.11442E-06     490   0.96702E-08   0.11087E+00 0.64223E+03 
c  nu_tilda     0.84497E-05      33   0.24131E-05   0.72311E-06 0.21330E+03 
c  TempC        0.44004E+02      26   0.27469E-03   0.60285E+01 0.29324E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3381          9.0153          4.5729          4.5729
v  Velocity[Y]            -2.7914          7.1574         0.23926         0.23926
v  Velocity[Z]       -1.1012e-014      7.784e-015    -1.4529e-017    -1.4529e-017
v  ǁVelocityǁ         0.0021372          9.0166          5.0322          5.0322
v  Pressure               -25.608          26.982          0.2966          0.2966
v  nu_tilda           4.4015e-007       0.0045121       0.0017887       0.0017887
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3008e-014       0.0053176       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2749:        0.21370E+01

===============================================================


 INSTANT    0.275000000E+04   TIME STEP NUMBER            2750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16575E-01 0.88956E+00
   Friction velocity        uk    :  0.16575E-01 0.88956E+00
   Dimensionless distance   yplus :  0.13344E+00 0.71615E+01
   Friction thermal sca.    tstar : -0.11253E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99560E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10597E-01      33   0.19015E-03   0.42730E+01 0.19191E+03 
c  Velocity[X]                                      0.19918E+01 
c  Velocity[Y]                                      0.22812E+01 
c  Velocity[Z]                                      0.89518E-30 
c  Pressure     0.89856E-07     536   0.99283E-08   0.87435E-01 0.92063E+03 
c  nu_tilda     0.84502E-05      33   0.12988E-04   0.72324E-06 0.21330E+03 
c  TempC        0.44004E+02      26   0.26992E-03   0.61372E+01 0.27285E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3383          9.0141          4.5729          4.5729
v  Velocity[Y]            -2.7905          7.1829         0.23919         0.23919
v  Velocity[Z]       -1.1358e-014     7.7849e-015    -1.4535e-017    -1.4535e-017
v  ǁVelocityǁ         0.0012366          9.0154          5.0321          5.0321
v  Pressure               -25.685          26.972         0.24337         0.24337
v  nu_tilda           4.4016e-007       0.0045124       0.0017886       0.0017886
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3021e-014        0.005318       0.0021029       0.0021029
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2750:        0.22110E+01

===============================================================


 INSTANT    0.275100000E+04   TIME STEP NUMBER            2751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18379E-01 0.89112E+00
   Friction velocity        uk    :  0.18379E-01 0.89112E+00
   Dimensionless distance   yplus :  0.14796E+00 0.71741E+01
   Friction thermal sca.    tstar : -0.10292E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11040E+00 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10596E-01      33   0.25704E-03   0.42646E+01 0.19195E+03 
c  Velocity[X]                                      0.19648E+01 
c  Velocity[Y]                                      0.22998E+01 
c  Velocity[Z]                                      0.81312E-30 
c  Pressure     0.90287E-07     538   0.91536E-08   0.86943E-01 0.11818E+04 
c  nu_tilda     0.84507E-05      33   0.24180E-05   0.72335E-06 0.21331E+03 
c  TempC        0.44004E+02      26   0.30905E-03   0.46846E+01 0.24402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3385          9.0129          4.5729          4.5729
v  Velocity[Y]            -2.7895          7.1942         0.23912         0.23912
v  Velocity[Z]       -1.1205e-014     7.7812e-015    -1.4527e-017    -1.4527e-017
v  ǁVelocityǁ         0.0010951          9.0142          5.0321          5.0321
v  Pressure               -25.629          27.077         0.30123         0.30123
v  nu_tilda           4.4009e-007       0.0045127       0.0017887       0.0017887
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3021e-014       0.0053183       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2751:        0.22220E+01

===============================================================


 INSTANT    0.275200000E+04   TIME STEP NUMBER            2752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18394E-01 0.89072E+00
   Friction velocity        uk    :  0.18394E-01 0.89072E+00
   Dimensionless distance   yplus :  0.14809E+00 0.71709E+01
   Friction thermal sca.    tstar : -0.93334E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11049E+00 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10595E-01      33   0.23533E-03   0.43077E+01 0.19210E+03 
c  Velocity[X]                                      0.20178E+01 
c  Velocity[Y]                                      0.22899E+01 
c  Velocity[Z]                                      0.10844E-29 
c  Pressure     0.12652E-06     570   0.91487E-08   0.12234E+00 0.20673E+04 
c  nu_tilda     0.84512E-05      33   0.12981E-04   0.72349E-06 0.21331E+03 
c  TempC        0.44005E+02      26   0.25359E-03   0.56280E+01 0.26516E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3387          9.0117          4.5729          4.5729
v  Velocity[Y]            -2.7885          7.1616         0.23905         0.23905
v  Velocity[Z]       -1.1505e-014     7.7817e-015    -1.4535e-017    -1.4535e-017
v  ǁVelocityǁ         0.0017482           9.013           5.032           5.032
v  Pressure               -25.705          26.838         0.20379         0.20379
v  nu_tilda           4.4013e-007        0.004513       0.0017886       0.0017886
v  TempC                       21           73.05          22.059          22.059
v  TurbVisc           3.3002e-014       0.0053187       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2752:        0.23070E+01

===============================================================


 INSTANT    0.275300000E+04   TIME STEP NUMBER            2753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13158E-01 0.88964E+00
   Friction velocity        uk    :  0.13158E-01 0.88964E+00
   Dimensionless distance   yplus :  0.10593E+00 0.71622E+01
   Friction thermal sca.    tstar : -0.91357E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79037E-01 0.53438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10594E-01      33   0.24190E-03   0.42802E+01 0.19195E+03 
c  Velocity[X]                                      0.20024E+01 
c  Velocity[Y]                                      0.22777E+01 
c  Velocity[Z]                                      0.10954E-29 
c  Pressure     0.91872E-07     568   0.96236E-08   0.89396E-01 0.17650E+04 
c  nu_tilda     0.84517E-05      33   0.24162E-05   0.72353E-06 0.21331E+03 
c  TempC        0.44005E+02      26   0.28697E-03   0.56681E+01 0.24943E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3388          9.0105          4.5729          4.5729
v  Velocity[Y]            -2.7875          7.1855         0.23898         0.23898
v  Velocity[Z]       -1.1244e-014     7.7759e-015    -1.4525e-017    -1.4525e-017
v  ǁVelocityǁ         0.0025897          9.0118           5.032           5.032
v  Pressure               -25.649          27.053         0.28024         0.28024
v  nu_tilda           4.4013e-007       0.0045133       0.0017886       0.0017886
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3014e-014       0.0053191       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2753:        0.23030E+01

===============================================================


 INSTANT    0.275400000E+04   TIME STEP NUMBER            2754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17990E-01 0.89050E+00
   Friction velocity        uk    :  0.17990E-01 0.89050E+00
   Dimensionless distance   yplus :  0.14483E+00 0.71691E+01
   Friction thermal sca.    tstar : -0.83141E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10806E+00 0.53490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10593E-01      33   0.24339E-03   0.42835E+01 0.19195E+03 
c  Velocity[X]                                      0.19894E+01 
c  Velocity[Y]                                      0.22941E+01 
c  Velocity[Z]                                      0.10062E-29 
c  Pressure     0.94959E-07     554   0.91709E-08   0.93207E-01 0.18873E+04 
c  nu_tilda     0.84522E-05      33   0.12974E-04   0.72363E-06 0.21331E+03 
c  TempC        0.44005E+02      27   0.32306E-03   0.51257E+01 0.24038E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.339          9.0093          4.5729          4.5729
v  Velocity[Y]            -2.7866          7.1623         0.23891         0.23891
v  Velocity[Z]       -1.1515e-014     7.8011e-015    -1.4538e-017    -1.4538e-017
v  ǁVelocityǁ         0.0018715          9.0106          5.0319          5.0319
v  Pressure               -25.725          26.848         0.18872         0.18872
v  nu_tilda            4.401e-007       0.0045136       0.0017885       0.0017885
v  TempC                       21          73.051          22.059          22.059
v  TurbVisc           3.3015e-014       0.0053194       0.0021028       0.0021028
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2754:        0.22740E+01

===============================================================


 INSTANT    0.275500000E+04   TIME STEP NUMBER            2755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17497E-01 0.88964E+00
   Friction velocity        uk    :  0.17497E-01 0.88964E+00
   Dimensionless distance   yplus :  0.14086E+00 0.71622E+01
   Friction thermal sca.    tstar : -0.80128E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10510E+00 0.53438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10592E-01      33   0.20401E-03   0.42759E+01 0.19181E+03 
c  Velocity[X]                                      0.19986E+01 
c  Velocity[Y]                                      0.22773E+01 
c  Velocity[Z]                                      0.91197E-30 
c  Pressure     0.11098E-06     522   0.92230E-08   0.10522E+00 0.13726E+04 
c  nu_tilda     0.84527E-05      33   0.24237E-05   0.72372E-06 0.21332E+03 
c  TempC        0.44005E+02      27   0.27622E-03   0.52154E+01 0.24794E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3391          9.0081          4.5729          4.5729
v  Velocity[Y]            -2.7856          7.1834         0.23883         0.23883
v  Velocity[Z]       -1.1275e-014     7.7913e-015    -1.4535e-017    -1.4535e-017
v  ǁVelocityǁ        0.00080776          9.0094          5.0319          5.0319
v  Pressure               -25.669          26.996         0.25185         0.25185
v  nu_tilda           4.4008e-007       0.0045139       0.0017886       0.0017886
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.3004e-014       0.0053197       0.0021027       0.0021027
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2755:        0.22040E+01

===============================================================


 INSTANT    0.275600000E+04   TIME STEP NUMBER            2756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17348E-01 0.89101E+00
   Friction velocity        uk    :  0.17348E-01 0.89101E+00
   Dimensionless distance   yplus :  0.13966E+00 0.71733E+01
   Friction thermal sca.    tstar : -0.74296E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10421E+00 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10591E-01      33   0.26839E-03   0.42812E+01 0.19189E+03 
c  Velocity[X]                                      0.20107E+01 
c  Velocity[Y]                                      0.22705E+01 
c  Velocity[Z]                                      0.95880E-30 
c  Pressure     0.10299E-06     521   0.98578E-08   0.99837E-01 0.11127E+04 
c  nu_tilda     0.84531E-05      33   0.12968E-04   0.72390E-06 0.21333E+03 
c  TempC        0.44006E+02      27   0.34264E-03   0.46208E+01 0.24852E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3392          9.0069          4.5729          4.5729
v  Velocity[Y]            -2.7847          7.1909         0.23876         0.23876
v  Velocity[Z]       -1.1538e-014      7.832e-015    -1.4546e-017    -1.4546e-017
v  ǁVelocityǁ        0.00076547          9.0081          5.0318          5.0318
v  Pressure               -25.748          26.927         0.18961         0.18961
v  nu_tilda           4.4005e-007       0.0045142       0.0017885       0.0017885
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2999e-014         0.00532       0.0021027       0.0021027
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2756:        0.21790E+01

===============================================================


 INSTANT    0.275700000E+04   TIME STEP NUMBER            2757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16311E-01 0.89055E+00
   Friction velocity        uk    :  0.16311E-01 0.89055E+00
   Dimensionless distance   yplus :  0.13132E+00 0.71696E+01
   Friction thermal sca.    tstar : -0.73080E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97978E-01 0.53493E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10590E-01      33   0.22769E-03   0.42832E+01 0.19186E+03 
c  Velocity[X]                                      0.19967E+01 
c  Velocity[Y]                                      0.22865E+01 
c  Velocity[Z]                                      0.10399E-29 
c  Pressure     0.11106E-06     473   0.95176E-08   0.10914E+00 0.60121E+03 
c  nu_tilda     0.84536E-05      33   0.24216E-05   0.72399E-06 0.21333E+03 
c  TempC        0.44006E+02      27   0.28208E-03   0.56220E+01 0.28526E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3394          9.0057          4.5729          4.5729
v  Velocity[Y]            -2.7837          7.1654         0.23868         0.23868
v  Velocity[Z]       -1.1279e-014      7.822e-015    -1.4541e-017    -1.4541e-017
v  ǁVelocityǁ         0.0019693           9.007          5.0318          5.0318
v  Pressure               -25.688          26.904         0.22013         0.22013
v  nu_tilda           4.4002e-007       0.0045145       0.0017885       0.0017885
v  TempC                       21          73.052          22.059          22.059
v  TurbVisc           3.2989e-014       0.0053204       0.0021027       0.0021027
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2757:        0.20790E+01

===============================================================


 INSTANT    0.275800000E+04   TIME STEP NUMBER            2758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16961E-01 0.88912E+00
   Friction velocity        uk    :  0.16961E-01 0.88912E+00
   Dimensionless distance   yplus :  0.13655E+00 0.71580E+01
   Friction thermal sca.    tstar : -0.69447E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10188E+00 0.53407E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10589E-01      33   0.24708E-03   0.42512E+01 0.19168E+03 
c  Velocity[X]                                      0.19817E+01 
c  Velocity[Y]                                      0.22695E+01 
c  Velocity[Z]                                      0.76220E-30 
c  Pressure     0.10149E-06     506   0.94597E-08   0.97229E-01 0.10020E+04 
c  nu_tilda     0.84541E-05      33   0.12962E-04   0.72407E-06 0.21333E+03 
c  TempC        0.44006E+02      26   0.29667E-03   0.55350E+01 0.25093E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3395          9.0045          4.5729          4.5729
v  Velocity[Y]            -2.7827          7.1801         0.23861         0.23861
v  Velocity[Z]       -1.1542e-014     7.8586e-015     -1.455e-017     -1.455e-017
v  ǁVelocityǁ        0.00056609          9.0057          5.0318          5.0318
v  Pressure               -25.768          26.872         0.16232         0.16232
v  nu_tilda           4.3994e-007       0.0045148       0.0017884       0.0017884
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.2979e-014       0.0053208       0.0021026       0.0021026
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2758:        0.21480E+01

===============================================================


 INSTANT    0.275900000E+04   TIME STEP NUMBER            2759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18348E-01 0.89037E+00
   Friction velocity        uk    :  0.18348E-01 0.89037E+00
   Dimensionless distance   yplus :  0.14772E+00 0.71680E+01
   Friction thermal sca.    tstar : -0.67661E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11021E+00 0.53482E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10588E-01      33   0.24705E-03   0.42684E+01 0.19170E+03 
c  Velocity[X]                                      0.20068E+01 
c  Velocity[Y]                                      0.22616E+01 
c  Velocity[Z]                                      0.80267E-30 
c  Pressure     0.10370E-06     489   0.98078E-08   0.10141E+00 0.62395E+03 
c  nu_tilda     0.84546E-05      33   0.24282E-05   0.72412E-06 0.21333E+03 
c  TempC        0.44006E+02      26   0.26086E-03   0.48812E+01 0.25076E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3396          9.0033          4.5729          4.5729
v  Velocity[Y]            -2.7817          7.1628         0.23853         0.23853
v  Velocity[Z]       -1.1277e-014     7.8484e-015    -1.4553e-017    -1.4553e-017
v  ǁVelocityǁ         0.0010974          9.0046          5.0317          5.0317
v  Pressure               -25.706          26.867         0.19481         0.19481
v  nu_tilda           4.3992e-007        0.004515       0.0017885       0.0017885
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2957e-014       0.0053211       0.0021026       0.0021026
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2759:        0.21230E+01

===============================================================


 INSTANT    0.276000000E+04   TIME STEP NUMBER            2760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16499E-01 0.88956E+00
   Friction velocity        uk    :  0.16499E-01 0.88956E+00
   Dimensionless distance   yplus :  0.13283E+00 0.71616E+01
   Friction thermal sca.    tstar : -0.64076E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99104E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10587E-01      33   0.19515E-03   0.42622E+01 0.19171E+03 
c  Velocity[X]                                      0.19841E+01 
c  Velocity[Y]                                      0.22780E+01 
c  Velocity[Z]                                      0.94418E-30 
c  Pressure     0.91234E-07     506   0.99081E-08   0.88142E-01 0.91333E+03 
c  nu_tilda     0.84550E-05      33   0.12956E-04   0.72426E-06 0.21334E+03 
c  TempC        0.44006E+02      26   0.25525E-03   0.43657E+01 0.24155E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3396          9.0021          4.5729          4.5729
v  Velocity[Y]            -2.7807          7.1855         0.23846         0.23846
v  Velocity[Z]       -1.1569e-014     7.8857e-015    -1.4558e-017    -1.4558e-017
v  ǁVelocityǁ         0.0013768          9.0034          5.0317          5.0317
v  Pressure               -25.787          26.857         0.14167         0.14167
v  nu_tilda           4.3989e-007       0.0045153       0.0017884       0.0017884
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2951e-014       0.0053214       0.0021026       0.0021026
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2760:        0.21580E+01

===============================================================


 INSTANT    0.276100000E+04   TIME STEP NUMBER            2761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17851E-01 0.89097E+00
   Friction velocity        uk    :  0.17851E-01 0.89097E+00
   Dimensionless distance   yplus :  0.14371E+00 0.71730E+01
   Friction thermal sca.    tstar : -0.62607E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10723E+00 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10585E-01      33   0.25139E-03   0.42393E+01 0.19153E+03 
c  Velocity[X]                                      0.19764E+01 
c  Velocity[Y]                                      0.22629E+01 
c  Velocity[Z]                                      0.10445E-29 
c  Pressure     0.10324E-06     506   0.98909E-08   0.98962E-01 0.11209E+04 
c  nu_tilda     0.84555E-05      33   0.24263E-05   0.72439E-06 0.21335E+03 
c  TempC        0.44006E+02      27   0.31728E-03   0.45409E+01 0.23773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3398          9.0009          4.5729          4.5729
v  Velocity[Y]            -2.7798          7.1922         0.23838         0.23838
v  Velocity[Z]       -1.1267e-014     7.8791e-015    -1.4565e-017    -1.4565e-017
v  ǁVelocityǁ        0.00047149          9.0022          5.0316          5.0316
v  Pressure               -25.731          26.944         0.19753         0.19753
v  nu_tilda           4.3988e-007       0.0045156       0.0017884       0.0017884
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2942e-014       0.0053218       0.0021025       0.0021025
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2761:        0.21690E+01

===============================================================


 INSTANT    0.276200000E+04   TIME STEP NUMBER            2762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17078E-01 0.89066E+00
   Friction velocity        uk    :  0.17078E-01 0.89066E+00
   Dimensionless distance   yplus :  0.13749E+00 0.71704E+01
   Friction thermal sca.    tstar : -0.61261E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10258E+00 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10584E-01      33   0.24752E-03   0.42855E+01 0.19174E+03 
c  Velocity[X]                                      0.20281E+01 
c  Velocity[Y]                                      0.22573E+01 
c  Velocity[Z]                                      0.10194E-29 
c  Pressure     0.11210E-06     569   0.95384E-08   0.10998E+00 0.19633E+04 
c  nu_tilda     0.84560E-05      33   0.12949E-04   0.72452E-06 0.21336E+03 
c  TempC        0.44007E+02      27   0.28320E-03   0.47721E+01 0.25012E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3399          8.9997          4.5729          4.5729
v  Velocity[Y]            -2.7788          7.1652          0.2383          0.2383
v  Velocity[Z]       -1.1534e-014     7.9151e-015    -1.4571e-017    -1.4571e-017
v  ǁVelocityǁ         0.0030989           9.001          5.0316          5.0316
v  Pressure               -25.805          26.738           0.102           0.102
v  nu_tilda           4.3993e-007       0.0045159       0.0017883       0.0017883
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.2938e-014       0.0053221       0.0021025       0.0021025
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2762:        0.22940E+01

===============================================================


 INSTANT    0.276300000E+04   TIME STEP NUMBER            2763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17557E-01 0.88932E+00
   Friction velocity        uk    :  0.17557E-01 0.88932E+00
   Dimensionless distance   yplus :  0.14135E+00 0.71596E+01
   Friction thermal sca.    tstar : -0.59179E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10546E+00 0.53419E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10583E-01      33   0.23151E-03   0.42536E+01 0.19159E+03 
c  Velocity[X]                                      0.19841E+01 
c  Velocity[Y]                                      0.22695E+01 
c  Velocity[Z]                                      0.94625E-30 
c  Pressure     0.92176E-07     553   0.99920E-08   0.88794E-01 0.17929E+04 
c  nu_tilda     0.84564E-05      33   0.24331E-05   0.72459E-06 0.21336E+03 
c  TempC        0.44007E+02      27   0.23638E-03   0.46068E+01 0.22489E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.34          8.9985          4.5729          4.5729
v  Velocity[Y]            -2.7778          7.1859         0.23822         0.23822
v  Velocity[Z]       -1.1292e-014     7.9098e-015    -1.4579e-017    -1.4579e-017
v  ǁVelocityǁ         0.0024756          8.9998          5.0316          5.0316
v  Pressure               -25.752          26.946          0.1804          0.1804
v  nu_tilda           4.3993e-007       0.0045162       0.0017883       0.0017883
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2952e-014       0.0053224       0.0021025       0.0021025
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2763:        0.22790E+01

===============================================================


 INSTANT    0.276400000E+04   TIME STEP NUMBER            2764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14613E-01 0.89018E+00
   Friction velocity        uk    :  0.14613E-01 0.89018E+00
   Dimensionless distance   yplus :  0.11765E+00 0.71665E+01
   Friction thermal sca.    tstar : -0.57450E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87778E-01 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10582E-01      33   0.24362E-03   0.42430E+01 0.19150E+03 
c  Velocity[X]                                      0.19879E+01 
c  Velocity[Y]                                      0.22551E+01 
c  Velocity[Z]                                      0.94093E-30 
c  Pressure     0.10410E-06     569   0.94177E-08   0.10051E+00 0.23698E+04 
c  nu_tilda     0.84569E-05      33   0.12943E-04   0.72472E-06 0.21336E+03 
c  TempC        0.44007E+02      26   0.33289E-03   0.54023E+01 0.26145E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3401          8.9973          4.5729          4.5729
v  Velocity[Y]            -2.7768          7.1585         0.23814         0.23814
v  Velocity[Z]       -1.1591e-014      7.946e-015    -1.4596e-017    -1.4596e-017
v  ǁVelocityǁ        0.00074725          8.9986          5.0315          5.0315
v  Pressure               -25.826          26.672        0.070621        0.070621
v  nu_tilda           4.3996e-007       0.0045165       0.0017882       0.0017882
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2954e-014       0.0053228       0.0021024       0.0021024
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2764:        0.22990E+01

===============================================================


 INSTANT    0.276500000E+04   TIME STEP NUMBER            2765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16862E-01 0.88959E+00
   Friction velocity        uk    :  0.16862E-01 0.88959E+00
   Dimensionless distance   yplus :  0.13575E+00 0.71618E+01
   Friction thermal sca.    tstar : -0.58412E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10128E+00 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10581E-01      33   0.24271E-03   0.42515E+01 0.19149E+03 
c  Velocity[X]                                      0.20042E+01 
c  Velocity[Y]                                      0.22474E+01 
c  Velocity[Z]                                      0.88966E-30 
c  Pressure     0.90678E-07     537   0.93136E-08   0.87829E-01 0.21550E+04 
c  nu_tilda     0.84573E-05      33   0.24292E-05   0.72482E-06 0.21337E+03 
c  TempC        0.44007E+02      27   0.25415E-03   0.68105E+01 0.29590E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3402          8.9962          4.5729          4.5729
v  Velocity[Y]            -2.7758          7.1852         0.23806         0.23806
v  Velocity[Z]       -1.1317e-014     7.9434e-015    -1.4602e-017    -1.4602e-017
v  ǁVelocityǁ          0.001785          8.9974          5.0315          5.0315
v  Pressure               -25.773          26.933          0.1626          0.1626
v  nu_tilda           4.3992e-007       0.0045167       0.0017883       0.0017883
v  TempC                       21          73.053          22.058          22.058
v  TurbVisc           3.2961e-014       0.0053231       0.0021024       0.0021024
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2765:        0.22150E+01

===============================================================


 INSTANT    0.276600000E+04   TIME STEP NUMBER            2766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11421E-01 0.89063E+00
   Friction velocity        uk    :  0.11421E-01 0.89063E+00
   Dimensionless distance   yplus :  0.91946E-01 0.71702E+01
   Friction thermal sca.    tstar : -0.57417E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68602E-01 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10580E-01      33   0.23385E-03   0.42316E+01 0.19147E+03 
c  Velocity[X]                                      0.19666E+01 
c  Velocity[Y]                                      0.22650E+01 
c  Velocity[Z]                                      0.86543E-30 
c  Pressure     0.93468E-07     537   0.98910E-08   0.90374E-01 0.15441E+04 
c  nu_tilda     0.84577E-05      33   0.12936E-04   0.72496E-06 0.21337E+03 
c  TempC        0.44007E+02      26   0.31204E-03   0.48041E+01 0.23764E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3403           8.995          4.5729          4.5729
v  Velocity[Y]            -2.7749          7.1914         0.23798         0.23798
v  Velocity[Z]       -1.1578e-014     7.9813e-015    -1.4615e-017    -1.4615e-017
v  ǁVelocityǁ         0.0021831          8.9962          5.0315          5.0315
v  Pressure                -25.85          26.796        0.082039        0.082039
v  nu_tilda           4.3985e-007        0.004517       0.0017882       0.0017882
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc            3.295e-014       0.0053234       0.0021024       0.0021024
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2766:        0.22300E+01

===============================================================


 INSTANT    0.276700000E+04   TIME STEP NUMBER            2767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18381E-01 0.89021E+00
   Friction velocity        uk    :  0.18381E-01 0.89021E+00
   Dimensionless distance   yplus :  0.14798E+00 0.71668E+01
   Friction thermal sca.    tstar : -0.60946E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11041E+00 0.53472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10579E-01      33   0.24435E-03   0.42494E+01 0.19143E+03 
c  Velocity[X]                                      0.20002E+01 
c  Velocity[Y]                                      0.22492E+01 
c  Velocity[Z]                                      0.80040E-30 
c  Pressure     0.11781E-06     456   0.96566E-08   0.11361E+00 0.55910E+03 
c  nu_tilda     0.84582E-05      33   0.24355E-05   0.72504E-06 0.21338E+03 
c  TempC        0.44007E+02      26   0.31156E-03   0.69293E+01 0.29712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3404          8.9938          4.5729          4.5729
v  Velocity[Y]            -2.7739          7.1614          0.2379          0.2379
v  Velocity[Z]       -1.1402e-014     7.9743e-015    -1.4621e-017    -1.4621e-017
v  ǁVelocityǁ          0.001358           8.995          5.0314          5.0314
v  Pressure               -25.787          26.735         0.10312         0.10312
v  nu_tilda           4.3995e-007       0.0045172       0.0017882       0.0017882
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc            3.293e-014       0.0053237       0.0021023       0.0021023
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2767:        0.20420E+01

===============================================================


 INSTANT    0.276800000E+04   TIME STEP NUMBER            2768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11940E-01 0.88903E+00
   Friction velocity        uk    :  0.11940E-01 0.88903E+00
   Dimensionless distance   yplus :  0.96122E-01 0.71573E+01
   Friction thermal sca.    tstar : -0.59694E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.71718E-01 0.53402E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10578E-01      33   0.24859E-03   0.42534E+01 0.19147E+03 
c  Velocity[X]                                      0.20118E+01 
c  Velocity[Y]                                      0.22416E+01 
c  Velocity[Z]                                      0.90984E-30 
c  Pressure     0.10503E-06     505   0.96204E-08   0.10149E+00 0.77248E+03 
c  nu_tilda     0.84586E-05      33   0.12933E-04   0.72520E-06 0.21339E+03 
c  TempC        0.44007E+02      26   0.32152E-03   0.55559E+01 0.27611E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3405          8.9926          4.5729          4.5729
v  Velocity[Y]            -2.7729          7.1815         0.23782         0.23782
v  Velocity[Z]       -1.1699e-014     8.0165e-015    -1.4641e-017    -1.4641e-017
v  ǁVelocityǁ        0.00050756          8.9938          5.0314          5.0314
v  Pressure               -25.871          26.771        0.061424        0.061424
v  nu_tilda              4.4e-007       0.0045175       0.0017881       0.0017881
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2958e-014        0.005324       0.0021023       0.0021023
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2768:        0.21500E+01

===============================================================


 INSTANT    0.276900000E+04   TIME STEP NUMBER            2769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14141E-01 0.89019E+00
   Friction velocity        uk    :  0.14141E-01 0.89019E+00
   Dimensionless distance   yplus :  0.11384E+00 0.71667E+01
   Friction thermal sca.    tstar : -0.57718E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84939E-01 0.53471E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10577E-01      33   0.24135E-03   0.42469E+01 0.19143E+03 
c  Velocity[X]                                      0.19907E+01 
c  Velocity[Y]                                      0.22563E+01 
c  Velocity[Z]                                      0.11240E-29 
c  Pressure     0.98603E-07     472   0.97409E-08   0.96506E-01 0.57053E+03 
c  nu_tilda     0.84590E-05      33   0.24350E-05   0.72532E-06 0.21339E+03 
c  TempC        0.44007E+02      27   0.28048E-03   0.53259E+01 0.27221E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3405          8.9914          4.5729          4.5729
v  Velocity[Y]            -2.7719          7.1612         0.23773         0.23773
v  Velocity[Z]       -1.1459e-014     8.0093e-015    -1.4643e-017    -1.4643e-017
v  ǁVelocityǁ         0.0012901          8.9926          5.0314          5.0314
v  Pressure               -25.809          26.743        0.089216        0.089216
v  nu_tilda           4.4002e-007       0.0045178       0.0017881       0.0017881
v  TempC                       21          73.053          22.058          22.058
v  TurbVisc           3.2973e-014       0.0053244       0.0021022       0.0021022
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2769:        0.20850E+01

===============================================================


 INSTANT    0.277000000E+04   TIME STEP NUMBER            2770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.32128E-02 0.88934E+00
   Friction velocity        uk    :  0.32128E-02 0.88934E+00
   Dimensionless distance   yplus :  0.25865E-01 0.71598E+01
   Friction thermal sca.    tstar : -0.58555E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.19298E-01 0.53420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10576E-01      33   0.18062E-03   0.42251E+01 0.19128E+03 
c  Velocity[X]                                      0.19837E+01 
c  Velocity[Y]                                      0.22414E+01 
c  Velocity[Z]                                      0.91124E-30 
c  Pressure     0.10472E-06     537   0.94941E-08   0.10017E+00 0.91257E+03 
c  nu_tilda     0.84594E-05      33   0.12925E-04   0.72546E-06 0.21340E+03 
c  TempC        0.44007E+02      27   0.23385E-03   0.56840E+01 0.27175E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3406          8.9903          4.5729          4.5729
v  Velocity[Y]            -2.7709          7.1802         0.23765         0.23765
v  Velocity[Z]       -1.1698e-014      8.051e-015    -1.4664e-017    -1.4664e-017
v  ǁVelocityǁ        0.00098914          8.9914          5.0313          5.0313
v  Pressure                -25.89          26.724        0.036315        0.036315
v  nu_tilda           4.4003e-007       0.0045181        0.001788        0.001788
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2981e-014       0.0053247       0.0021022       0.0021022
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2770:        0.22150E+01

===============================================================


 INSTANT    0.277100000E+04   TIME STEP NUMBER            2771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.39358E-02 0.89096E+00
   Friction velocity        uk    :  0.39358E-02 0.89096E+00
   Dimensionless distance   yplus :  0.31686E-01 0.71728E+01
   Friction thermal sca.    tstar : -0.58088E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23641E-01 0.53517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10575E-01      33   0.24490E-03   0.42217E+01 0.19125E+03 
c  Velocity[X]                                      0.19860E+01 
c  Velocity[Y]                                      0.22357E+01 
c  Velocity[Z]                                      0.72582E-30 
c  Pressure     0.96830E-07     536   0.95027E-08   0.93437E-01 0.11637E+04 
c  nu_tilda     0.84599E-05      33   0.24367E-05   0.72554E-06 0.21340E+03 
c  TempC        0.44007E+02      26   0.33968E-03   0.44894E+01 0.25390E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3406          8.9892          4.5729          4.5729
v  Velocity[Y]            -2.7699          7.1935         0.23756         0.23756
v  Velocity[Z]        -1.153e-014     8.0459e-015    -1.4668e-017    -1.4668e-017
v  ǁVelocityǁ        0.00041323          8.9902          5.0313          5.0313
v  Pressure               -25.832           26.83         0.09311         0.09311
v  nu_tilda           4.4003e-007       0.0045183       0.0017881       0.0017881
v  TempC                       21          73.053          22.058          22.058
v  TurbVisc           3.2985e-014        0.005325       0.0021022       0.0021022
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2771:        0.22130E+01

===============================================================


 INSTANT    0.277200000E+04   TIME STEP NUMBER            2772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13331E-01 0.89053E+00
   Friction velocity        uk    :  0.13331E-01 0.89053E+00
   Dimensionless distance   yplus :  0.10732E+00 0.71694E+01
   Friction thermal sca.    tstar : -0.57331E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.80075E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10574E-01      33   0.23662E-03   0.42422E+01 0.19135E+03 
c  Velocity[X]                                      0.19911E+01 
c  Velocity[Y]                                      0.22511E+01 
c  Velocity[Z]                                      0.92909E-30 
c  Pressure     0.98847E-07     522   0.97652E-08   0.96955E-01 0.19672E+04 
c  nu_tilda     0.84603E-05      33   0.12919E-04   0.72566E-06 0.21341E+03 
c  TempC        0.44007E+02      27   0.26490E-03   0.66442E+01 0.30004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3407          8.9882          4.5729          4.5729
v  Velocity[Y]             -2.769          7.1643         0.23748         0.23748
v  Velocity[Z]       -1.1835e-014     8.0841e-015    -1.4679e-017    -1.4679e-017
v  ǁVelocityǁ         0.0013859           8.989          5.0313          5.0313
v  Pressure               -25.908          26.613      -0.0017536      -0.0017536
v  nu_tilda           4.4004e-007       0.0045186        0.001788        0.001788
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.2984e-014       0.0053253       0.0021021       0.0021021
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2772:        0.21900E+01

===============================================================


 INSTANT    0.277300000E+04   TIME STEP NUMBER            2773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15856E-01 0.88916E+00
   Friction velocity        uk    :  0.15856E-01 0.88916E+00
   Dimensionless distance   yplus :  0.12766E+00 0.71583E+01
   Friction thermal sca.    tstar : -0.58073E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95245E-01 0.53409E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10573E-01      33   0.23534E-03   0.42196E+01 0.19117E+03 
c  Velocity[X]                                      0.19853E+01 
c  Velocity[Y]                                      0.22344E+01 
c  Velocity[Z]                                      0.84586E-30 
c  Pressure     0.88911E-07     521   0.92594E-08   0.85289E-01 0.13989E+04 
c  nu_tilda     0.84607E-05      33   0.24414E-05   0.72576E-06 0.21342E+03 
c  TempC        0.44007E+02      26   0.31428E-03   0.54285E+01 0.24907E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3407          8.9885          4.5729          4.5729
v  Velocity[Y]             -2.768          7.1817         0.23739         0.23739
v  Velocity[Z]       -1.1577e-014     8.0783e-015    -1.4684e-017    -1.4684e-017
v  ǁVelocityǁ         0.0013928          8.9888          5.0313          5.0313
v  Pressure                -25.85          26.766         0.06261         0.06261
v  nu_tilda              4.4e-007       0.0045188        0.001788        0.001788
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2986e-014       0.0053256       0.0021021       0.0021021
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2773:        0.21920E+01

===============================================================


 INSTANT    0.277400000E+04   TIME STEP NUMBER            2774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15001E-01 0.89019E+00
   Friction velocity        uk    :  0.15001E-01 0.89019E+00
   Dimensionless distance   yplus :  0.12077E+00 0.71666E+01
   Friction thermal sca.    tstar : -0.57791E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90106E-01 0.53471E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10572E-01      33   0.27943E-03   0.42224E+01 0.19121E+03 
c  Velocity[X]                                      0.19956E+01 
c  Velocity[Y]                                      0.22268E+01 
c  Velocity[Z]                                      0.80151E-30 
c  Pressure     0.93076E-07     569   0.96157E-08   0.91079E-01 0.18850E+04 
c  nu_tilda     0.84611E-05      33   0.12913E-04   0.72595E-06 0.21343E+03 
c  TempC        0.44007E+02      26   0.29844E-03   0.78817E+01 0.29725E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3408          8.9888          4.5729          4.5729
v  Velocity[Y]             -2.767          7.1595         0.23731         0.23731
v  Velocity[Z]       -1.1768e-014      8.117e-015    -1.4692e-017    -1.4692e-017
v  ǁVelocityǁ         0.0014152           8.989          5.0312          5.0312
v  Pressure               -25.925          26.564       -0.029323       -0.029323
v  nu_tilda           4.4001e-007       0.0045191       0.0017879       0.0017879
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2974e-014       0.0053259        0.002102        0.002102
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2774:        0.22780E+01

===============================================================


 INSTANT    0.277500000E+04   TIME STEP NUMBER            2775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17118E-01 0.88952E+00
   Friction velocity        uk    :  0.17118E-01 0.88952E+00
   Dimensionless distance   yplus :  0.13781E+00 0.71612E+01
   Friction thermal sca.    tstar : -0.62462E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10282E+00 0.53431E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10571E-01      33   0.23427E-03   0.42589E+01 0.19134E+03 
c  Velocity[X]                                      0.20142E+01 
c  Velocity[Y]                                      0.22447E+01 
c  Velocity[Z]                                      0.89650E-30 
c  Pressure     0.11599E-06     568   0.97974E-08   0.11139E+00 0.19743E+04 
c  nu_tilda     0.84615E-05      33   0.24408E-05   0.72603E-06 0.21343E+03 
c  TempC        0.44007E+02      26   0.29106E-03   0.54491E+01 0.27008E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3408          8.9891          4.5729          4.5729
v  Velocity[Y]             -2.766          7.1853         0.23722         0.23722
v  Velocity[Z]       -1.1423e-014     8.1138e-015    -1.4699e-017    -1.4699e-017
v  ǁVelocityǁ         0.0012152          8.9893          5.0312          5.0312
v  Pressure               -25.873          26.794        0.056465        0.056465
v  nu_tilda           4.4002e-007       0.0045194       0.0017879       0.0017879
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2977e-014       0.0053263        0.002102        0.002102
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2775:        0.23080E+01

===============================================================


 INSTANT    0.277600000E+04   TIME STEP NUMBER            2776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15892E-01 0.89076E+00
   Friction velocity        uk    :  0.15892E-01 0.89076E+00
   Dimensionless distance   yplus :  0.12794E+00 0.71712E+01
   Friction thermal sca.    tstar : -0.58885E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95457E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10570E-01      33   0.21731E-03   0.42087E+01 0.19109E+03 
c  Velocity[X]                                      0.19808E+01 
c  Velocity[Y]                                      0.22279E+01 
c  Velocity[Z]                                      0.10032E-29 
c  Pressure     0.10168E-06     568   0.94148E-08   0.96812E-01 0.17716E+04 
c  nu_tilda     0.84619E-05      33   0.12905E-04   0.72614E-06 0.21344E+03 
c  TempC        0.44007E+02      26   0.31513E-03   0.43419E+01 0.24395E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3409          8.9893          4.5729          4.5729
v  Velocity[Y]             -2.765          7.1867         0.23713         0.23713
v  Velocity[Z]       -1.1799e-014     8.1507e-015    -1.4706e-017    -1.4706e-017
v  ǁVelocityǁ        0.00050963          8.9896          5.0312          5.0312
v  Pressure               -25.947          26.624       -0.032488       -0.032488
v  nu_tilda           4.4004e-007       0.0045197       0.0017878       0.0017878
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2981e-014       0.0053266        0.002102        0.002102
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2776:        0.26200E+01

===============================================================


 INSTANT    0.277700000E+04   TIME STEP NUMBER            2777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15717E-01 0.89055E+00
   Friction velocity        uk    :  0.15717E-01 0.89055E+00
   Dimensionless distance   yplus :  0.12653E+00 0.71696E+01
   Friction thermal sca.    tstar : -0.57933E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94405E-01 0.53493E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10568E-01      33   0.23680E-03   0.42084E+01 0.19102E+03 
c  Velocity[X]                                      0.19904E+01 
c  Velocity[Y]                                      0.22180E+01 
c  Velocity[Z]                                      0.10465E-29 
c  Pressure     0.10514E-06     522   0.97310E-08   0.10370E+00 0.85999E+03 
c  nu_tilda     0.84622E-05      33   0.24464E-05   0.72623E-06 0.21344E+03 
c  TempC        0.44007E+02      27   0.24145E-03   0.47979E+01 0.25508E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3409          8.9896          4.5729          4.5729
v  Velocity[Y]             -2.764          7.1638         0.23704         0.23704
v  Velocity[Z]       -1.1363e-014     8.1451e-015    -1.4711e-017    -1.4711e-017
v  ǁVelocityǁ        0.00085215          8.9899          5.0312          5.0312
v  Pressure               -25.888          26.662        0.012832        0.012832
v  nu_tilda           4.4008e-007       0.0045199       0.0017879       0.0017879
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2986e-014       0.0053269       0.0021019       0.0021019
v  total_pressure      1.013e+005     1.0135e+005     1.0133e+005     1.0133e+005


 TIME FOR THE TIME STEP             2777:        0.23250E+01

===============================================================


 INSTANT    0.277800000E+04   TIME STEP NUMBER            2778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13810E-01 0.88918E+00
   Friction velocity        uk    :  0.13810E-01 0.88918E+00
   Dimensionless distance   yplus :  0.11118E+00 0.71585E+01
   Friction thermal sca.    tstar : -0.58474E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82951E-01 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10567E-01      33   0.25784E-03   0.42076E+01 0.19107E+03 
c  Velocity[X]                                      0.19717E+01 
c  Velocity[Y]                                      0.22359E+01 
c  Velocity[Z]                                      0.10842E-29 
c  Pressure     0.92680E-07     489   0.99168E-08   0.89517E-01 0.10648E+04 
c  nu_tilda     0.84626E-05      33   0.12902E-04   0.72640E-06 0.21345E+03 
c  TempC        0.44007E+02      26   0.35578E-03   0.41343E+01 0.25111E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9899          4.5729          4.5729
v  Velocity[Y]            -2.7631          7.1822         0.23695         0.23695
v  Velocity[Z]       -1.1419e-014      8.184e-015    -1.4713e-017    -1.4713e-017
v  ǁVelocityǁ        0.00055067          8.9901          5.0312          5.0312
v  Pressure               -25.966          26.619       -0.048134       -0.048134
v  nu_tilda           4.4008e-007       0.0045202       0.0017878       0.0017878
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2997e-014       0.0053272       0.0021019       0.0021019
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2778:        0.21220E+01

===============================================================


 INSTANT    0.277900000E+04   TIME STEP NUMBER            2779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18387E-01 0.89032E+00
   Friction velocity        uk    :  0.18387E-01 0.89032E+00
   Dimensionless distance   yplus :  0.14803E+00 0.71677E+01
   Friction thermal sca.    tstar : -0.58473E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11044E+00 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10566E-01      33   0.24452E-03   0.42340E+01 0.19108E+03 
c  Velocity[X]                                      0.20114E+01 
c  Velocity[Y]                                      0.22226E+01 
c  Velocity[Z]                                      0.88084E-30 
c  Pressure     0.13525E-06     474   0.95784E-08   0.12955E+00 0.61921E+03 
c  nu_tilda     0.84630E-05      33   0.24456E-05   0.72652E-06 0.21346E+03 
c  TempC        0.44007E+02      26   0.25574E-03   0.79423E+01 0.33413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9901          4.5729          4.5729
v  Velocity[Y]            -2.7621          7.1582         0.23686         0.23686
v  Velocity[Z]        -1.087e-014     8.1775e-015    -1.4719e-017    -1.4719e-017
v  ǁVelocityǁ         0.0014954          8.9904          5.0311          5.0311
v  Pressure               -25.907          26.592       -0.016367       -0.016367
v  nu_tilda           4.4008e-007       0.0045204       0.0017878       0.0017878
v  TempC                       21          73.053          22.058          22.058
v  TurbVisc           3.2997e-014       0.0053275       0.0021018       0.0021018
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2779:        0.20830E+01

===============================================================


 INSTANT    0.278000000E+04   TIME STEP NUMBER            2780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16152E-01 0.88983E+00
   Friction velocity        uk    :  0.16152E-01 0.88983E+00
   Dimensionless distance   yplus :  0.13004E+00 0.71637E+01
   Friction thermal sca.    tstar : -0.60558E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97022E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10565E-01      33   0.19424E-03   0.42179E+01 0.19102E+03 
c  Velocity[X]                                      0.20035E+01 
c  Velocity[Y]                                      0.22144E+01 
c  Velocity[Z]                                      0.91352E-30 
c  Pressure     0.10302E-06     489   0.93948E-08   0.99756E-01 0.82868E+03 
c  nu_tilda     0.84634E-05      33   0.12894E-04   0.72662E-06 0.21346E+03 
c  TempC        0.44007E+02      26   0.30870E-03   0.38089E+01 0.24572E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9904          4.5729          4.5729
v  Velocity[Y]             -2.761          7.1838         0.23677         0.23677
v  Velocity[Z]       -1.1145e-014     8.2173e-015    -1.4724e-017    -1.4724e-017
v  ǁVelocityǁ         0.0024404          8.9907          5.0311          5.0311
v  Pressure               -25.987          26.614       -0.063666       -0.063666
v  nu_tilda           4.4001e-007       0.0045207       0.0017877       0.0017877
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2997e-014       0.0053278       0.0021018       0.0021018
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2780:        0.21040E+01

===============================================================


 INSTANT    0.278100000E+04   TIME STEP NUMBER            2781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11039E-01 0.89130E+00
   Friction velocity        uk    :  0.11039E-01 0.89130E+00
   Dimensionless distance   yplus :  0.88874E-01 0.71756E+01
   Friction thermal sca.    tstar : -0.61186E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66310E-01 0.53538E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10564E-01      33   0.22768E-03   0.41884E+01 0.19089E+03 
c  Velocity[X]                                      0.19588E+01 
c  Velocity[Y]                                      0.22295E+01 
c  Velocity[Z]                                      0.99471E-30 
c  Pressure     0.74674E-07     504   0.97541E-08   0.72234E-01 0.93014E+03 
c  nu_tilda     0.84637E-05      33   0.24528E-05   0.72669E-06 0.21347E+03 
c  TempC        0.44007E+02      27   0.25215E-03   0.46161E+01 0.26322E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9907          4.5729          4.5729
v  Velocity[Y]              -2.76           7.196         0.23667         0.23667
v  Velocity[Z]        -1.057e-014     8.2102e-015    -1.4723e-017    -1.4723e-017
v  ǁVelocityǁ         0.0020562          8.9909          5.0311          5.0311
v  Pressure               -25.927          26.684        -0.01625        -0.01625
v  nu_tilda           4.3993e-007       0.0045209       0.0017877       0.0017877
v  TempC                       21          73.053          22.058          22.058
v  TurbVisc           3.2978e-014       0.0053281       0.0021017       0.0021017
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2781:        0.21510E+01

===============================================================


 INSTANT    0.278200000E+04   TIME STEP NUMBER            2782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13148E-01 0.89086E+00
   Friction velocity        uk    :  0.13148E-01 0.89086E+00
   Dimensionless distance   yplus :  0.10585E+00 0.71720E+01
   Friction thermal sca.    tstar : -0.64815E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78977E-01 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10563E-01      33   0.24382E-03   0.42048E+01 0.19092E+03 
c  Velocity[X]                                      0.19888E+01 
c  Velocity[Y]                                      0.22160E+01 
c  Velocity[Z]                                      0.82056E-30 
c  Pressure     0.10864E-06     521   0.95806E-08   0.10548E+00 0.19243E+04 
c  nu_tilda     0.84641E-05      33   0.12888E-04   0.72685E-06 0.21347E+03 
c  TempC        0.44007E+02      27   0.24471E-03   0.43514E+01 0.24905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9909          4.5729          4.5729
v  Velocity[Y]             -2.759          7.1627         0.23658         0.23658
v  Velocity[Z]       -1.0445e-014     8.2485e-015    -1.4727e-017    -1.4727e-017
v  ǁVelocityǁ         0.0020807          8.9912          5.0311          5.0311
v  Pressure               -26.003          26.469        -0.10872        -0.10872
v  nu_tilda           4.3994e-007       0.0045212       0.0017876       0.0017876
v  TempC                       21          73.051          22.058          22.058
v  TurbVisc           3.2952e-014       0.0053284       0.0021017       0.0021017
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2782:        0.21680E+01

===============================================================


 INSTANT    0.278300000E+04   TIME STEP NUMBER            2783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17141E-01 0.88948E+00
   Friction velocity        uk    :  0.17141E-01 0.88948E+00
   Dimensionless distance   yplus :  0.13800E+00 0.71610E+01
   Friction thermal sca.    tstar : -0.66158E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10296E+00 0.53429E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10562E-01      33   0.26841E-03   0.42169E+01 0.19095E+03 
c  Velocity[X]                                      0.20104E+01 
c  Velocity[Y]                                      0.22065E+01 
c  Velocity[Z]                                      0.84626E-30 
c  Pressure     0.99536E-07     553   0.89475E-08   0.95806E-01 0.16623E+04 
c  nu_tilda     0.84645E-05      33   0.24488E-05   0.72696E-06 0.21348E+03 
c  TempC        0.44007E+02      26   0.33928E-03   0.41200E+01 0.24878E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9912          4.5729          4.5729
v  Velocity[Y]            -2.7581          7.1861         0.23649         0.23649
v  Velocity[Z]       -9.9786e-015     8.2428e-015    -1.4727e-017    -1.4727e-017
v  ǁVelocityǁ         0.0023506          8.9914          5.0311          5.0311
v  Pressure               -25.947          26.661       -0.034966       -0.034966
v  nu_tilda           4.3994e-007       0.0045214       0.0017876       0.0017876
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2957e-014       0.0053287       0.0021016       0.0021016
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2783:        0.22660E+01

===============================================================


 INSTANT    0.278400000E+04   TIME STEP NUMBER            2784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17739E-01 0.89045E+00
   Friction velocity        uk    :  0.17739E-01 0.89045E+00
   Dimensionless distance   yplus :  0.14281E+00 0.71687E+01
   Friction thermal sca.    tstar : -0.69677E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10655E+00 0.53486E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10561E-01      33   0.24540E-03   0.42072E+01 0.19091E+03 
c  Velocity[X]                                      0.19851E+01 
c  Velocity[Y]                                      0.22221E+01 
c  Velocity[Z]                                      0.92457E-30 
c  Pressure     0.99023E-07     553   0.95492E-08   0.96998E-01 0.18030E+04 
c  nu_tilda     0.84648E-05      33   0.12882E-04   0.72709E-06 0.21349E+03 
c  TempC        0.44007E+02      26   0.26854E-03   0.53596E+01 0.29310E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9915          4.5729          4.5729
v  Velocity[Y]            -2.7571          7.1623         0.23639         0.23639
v  Velocity[Z]       -9.9274e-015      8.281e-015    -1.4732e-017    -1.4732e-017
v  ǁVelocityǁ         0.0025351          8.9917          5.0311          5.0311
v  Pressure               -26.024          26.468        -0.12395        -0.12395
v  nu_tilda           4.3992e-007       0.0045217       0.0017875       0.0017875
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2958e-014        0.005329       0.0021016       0.0021016
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2784:        0.22520E+01

===============================================================


 INSTANT    0.278500000E+04   TIME STEP NUMBER            2785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54744E-02 0.88959E+00
   Friction velocity        uk    :  0.54744E-02 0.88959E+00
   Dimensionless distance   yplus :  0.44073E-01 0.71618E+01
   Friction thermal sca.    tstar : -0.70919E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32883E-01 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10560E-01      33   0.20293E-03   0.41952E+01 0.19075E+03 
c  Velocity[X]                                      0.19875E+01 
c  Velocity[Y]                                      0.22077E+01 
c  Velocity[Z]                                      0.83265E-30 
c  Pressure     0.10901E-06     522   0.94873E-08   0.10377E+00 0.15216E+04 
c  nu_tilda     0.84652E-05      33   0.24572E-05   0.72713E-06 0.21349E+03 
c  TempC        0.44007E+02      27   0.24694E-03   0.58778E+01 0.27754E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9917          4.5729          4.5729
v  Velocity[Y]            -2.7561          7.1839          0.2363          0.2363
v  Velocity[Z]       -9.5094e-015     8.2746e-015    -1.4733e-017    -1.4733e-017
v  ǁVelocityǁ         0.0016158          8.9919          5.0311          5.0311
v  Pressure               -25.968          26.638        -0.05506        -0.05506
v  nu_tilda            4.399e-007       0.0045219       0.0017875       0.0017875
v  TempC                       21          73.053          22.058          22.058
v  TurbVisc           3.2951e-014       0.0053293       0.0021015       0.0021015
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2785:        0.21760E+01

===============================================================


 INSTANT    0.278600000E+04   TIME STEP NUMBER            2786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13197E-01 0.89096E+00
   Friction velocity        uk    :  0.13197E-01 0.89096E+00
   Dimensionless distance   yplus :  0.10624E+00 0.71728E+01
   Friction thermal sca.    tstar : -0.73889E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79268E-01 0.53517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10558E-01      33   0.24624E-03   0.41817E+01 0.19070E+03 
c  Velocity[X]                                      0.19821E+01 
c  Velocity[Y]                                      0.21996E+01 
c  Velocity[Z]                                      0.78104E-30 
c  Pressure     0.85139E-07     552   0.97365E-08   0.82590E-01 0.12657E+04 
c  nu_tilda     0.84655E-05      33   0.12876E-04   0.72724E-06 0.21350E+03 
c  TempC        0.44007E+02      27   0.32125E-03   0.40630E+01 0.23448E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341           8.992          4.5729          4.5729
v  Velocity[Y]             -2.755          7.1927          0.2362          0.2362
v  Velocity[Z]       -9.3743e-015     8.3119e-015    -1.4735e-017    -1.4735e-017
v  ǁVelocityǁ         0.0018948          8.9922          5.0311          5.0311
v  Pressure               -26.046          26.546        -0.12463        -0.12463
v  nu_tilda           4.3986e-007       0.0045222       0.0017874       0.0017874
v  TempC                       21          73.052          22.058          22.058
v  TurbVisc           3.2944e-014       0.0053295       0.0021015       0.0021015
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2786:        0.22670E+01

===============================================================


 INSTANT    0.278700000E+04   TIME STEP NUMBER            2787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18031E-01 0.89056E+00
   Friction velocity        uk    :  0.18031E-01 0.89056E+00
   Dimensionless distance   yplus :  0.14516E+00 0.71696E+01
   Friction thermal sca.    tstar : -0.75757E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10831E+00 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10557E-01      33   0.23876E-03   0.42021E+01 0.19078E+03 
c  Velocity[X]                                      0.19876E+01 
c  Velocity[Y]                                      0.22145E+01 
c  Velocity[Z]                                      0.93780E-30 
c  Pressure     0.11243E-06     522   0.95821E-08   0.10973E+00 0.58959E+03 
c  nu_tilda     0.84658E-05      33   0.24534E-05   0.72738E-06 0.21351E+03 
c  TempC        0.44007E+02      27   0.27446E-03   0.51265E+01 0.26773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9922          4.5729          4.5729
v  Velocity[Y]             -2.754          7.1655          0.2361          0.2361
v  Velocity[Z]       -9.0507e-015     8.3034e-015    -1.4735e-017    -1.4735e-017
v  ǁVelocityǁ         0.0030592          8.9925          5.0311          5.0311
v  Pressure               -25.984          26.533       -0.094405       -0.094405
v  nu_tilda           4.3985e-007       0.0045224       0.0017875       0.0017875
v  TempC                       21          73.053          22.057          22.057
v  TurbVisc           3.2932e-014       0.0053299       0.0021014       0.0021014
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2787:        0.21940E+01

===============================================================


 INSTANT    0.278800000E+04   TIME STEP NUMBER            2788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17122E-01 0.88900E+00
   Friction velocity        uk    :  0.17122E-01 0.88900E+00
   Dimensionless distance   yplus :  0.13784E+00 0.71571E+01
   Friction thermal sca.    tstar : -0.83229E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10285E+00 0.53400E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10556E-01      33   0.24551E-03   0.41749E+01 0.19064E+03 
c  Velocity[X]                                      0.19751E+01 
c  Velocity[Y]                                      0.21998E+01 
c  Velocity[Z]                                      0.96442E-30 
c  Pressure     0.99625E-07     474   0.94165E-08   0.94979E-01 0.11157E+04 
c  nu_tilda     0.84662E-05      33   0.12872E-04   0.72756E-06 0.21352E+03 
c  TempC        0.44006E+02      26   0.23233E-03   0.63139E+01 0.28248E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9925          4.5729          4.5729
v  Velocity[Y]             -2.753          7.1808         0.23601         0.23601
v  Velocity[Z]       -8.8942e-015     8.3415e-015    -1.4733e-017    -1.4733e-017
v  ǁVelocityǁ         0.0031908          8.9928          5.0311          5.0311
v  Pressure               -26.063          26.473        -0.15797        -0.15797
v  nu_tilda           4.3984e-007       0.0045227       0.0017874       0.0017874
v  TempC                       21          73.055          22.057          22.057
v  TurbVisc            3.293e-014       0.0053302       0.0021014       0.0021014
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2788:        0.20740E+01

===============================================================


 INSTANT    0.278900000E+04   TIME STEP NUMBER            2789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14378E-01 0.89035E+00
   Friction velocity        uk    :  0.14378E-01 0.89035E+00
   Dimensionless distance   yplus :  0.11575E+00 0.71679E+01
   Friction thermal sca.    tstar : -0.87265E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.86366E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10555E-01      33   0.25316E-03   0.42023E+01 0.19071E+03 
c  Velocity[X]                                      0.20087E+01 
c  Velocity[Y]                                      0.21936E+01 
c  Velocity[Z]                                      0.10003E-29 
c  Pressure     0.11291E-06     505   0.96440E-08   0.11101E+00 0.93484E+03 
c  nu_tilda     0.84665E-05      33   0.24587E-05   0.72762E-06 0.21352E+03 
c  TempC        0.44006E+02      26   0.36662E-03   0.54704E+01 0.26176E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9928          4.5729          4.5729
v  Velocity[Y]            -2.7521          7.1629         0.23591         0.23591
v  Velocity[Z]       -8.6636e-015     8.3345e-015    -1.4739e-017    -1.4739e-017
v  ǁVelocityǁ         0.0021248          8.9931          5.0311          5.0311
v  Pressure               -26.007          26.525        -0.10949        -0.10949
v  nu_tilda           4.3985e-007       0.0045229       0.0017874       0.0017874
v  TempC                       21          73.055          22.057          22.057
v  TurbVisc           3.2927e-014       0.0053304       0.0021013       0.0021013
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2789:        0.21580E+01

===============================================================


 INSTANT    0.279000000E+04   TIME STEP NUMBER            2790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13801E-01 0.88948E+00
   Friction velocity        uk    :  0.13801E-01 0.88948E+00
   Dimensionless distance   yplus :  0.11111E+00 0.71609E+01
   Friction thermal sca.    tstar : -0.91333E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82899E-01 0.53428E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10554E-01      33   0.18695E-03   0.41872E+01 0.19066E+03 
c  Velocity[X]                                      0.19784E+01 
c  Velocity[Y]                                      0.22087E+01 
c  Velocity[Z]                                      0.91752E-30 
c  Pressure     0.88859E-07     522   0.93394E-08   0.86156E-01 0.11235E+04 
c  nu_tilda     0.84668E-05      33   0.12865E-04   0.72771E-06 0.21352E+03 
c  TempC        0.44006E+02      27   0.26778E-03   0.79503E+01 0.31736E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9931          4.5729          4.5729
v  Velocity[Y]            -2.7511          7.1855         0.23581         0.23581
v  Velocity[Z]       -8.6139e-015     8.3716e-015    -1.4742e-017    -1.4742e-017
v  ǁVelocityǁ         0.0033227          8.9934          5.0311          5.0311
v  Pressure               -26.084          26.476         -0.1738         -0.1738
v  nu_tilda           4.3984e-007       0.0045231       0.0017873       0.0017873
v  TempC                       21          73.055          22.057          22.057
v  TurbVisc           3.2929e-014       0.0053307       0.0021013       0.0021013
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2790:        0.22000E+01

===============================================================


 INSTANT    0.279100000E+04   TIME STEP NUMBER            2791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18503E-01 0.89084E+00
   Friction velocity        uk    :  0.18503E-01 0.89084E+00
   Dimensionless distance   yplus :  0.14896E+00 0.71719E+01
   Friction thermal sca.    tstar : -0.98140E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11114E+00 0.53510E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10553E-01      33   0.23976E-03   0.41592E+01 0.19044E+03 
c  Velocity[X]                                      0.19670E+01 
c  Velocity[Y]                                      0.21921E+01 
c  Velocity[Z]                                      0.77021E-30 
c  Pressure     0.10942E-06     488   0.94246E-08   0.10433E+00 0.10530E+04 
c  nu_tilda     0.84671E-05      33   0.24594E-05   0.72780E-06 0.21353E+03 
c  TempC        0.44006E+02      26   0.22905E-03   0.65148E+01 0.26695E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.341          8.9933          4.5729          4.5729
v  Velocity[Y]            -2.7501          7.1916         0.23571         0.23571
v  Velocity[Z]       -8.3543e-015     8.3652e-015    -1.4747e-017    -1.4747e-017
v  ǁVelocityǁ         0.0031052          8.9936          5.0311          5.0311
v  Pressure               -26.028          26.557        -0.12125        -0.12125
v  nu_tilda           4.3984e-007       0.0045234       0.0017873       0.0017873
v  TempC                       21          73.055          22.057          22.057
v  TurbVisc           3.2926e-014        0.005331       0.0021012       0.0021012
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2791:        0.21050E+01

===============================================================


 INSTANT    0.279200000E+04   TIME STEP NUMBER            2792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18091E-01 0.89056E+00
   Friction velocity        uk    :  0.18091E-01 0.89056E+00
   Dimensionless distance   yplus :  0.14564E+00 0.71696E+01
   Friction thermal sca.    tstar : -0.10807E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10867E+00 0.53493E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10552E-01      33   0.23673E-03   0.41958E+01 0.19060E+03 
c  Velocity[X]                                      0.20094E+01 
c  Velocity[Y]                                      0.21864E+01 
c  Velocity[Z]                                      0.86634E-30 
c  Pressure     0.99134E-07     552   0.97133E-08   0.97490E-01 0.19534E+04 
c  nu_tilda     0.84675E-05      33   0.12860E-04   0.72798E-06 0.21354E+03 
c  TempC        0.44006E+02      27   0.36637E-03   0.40405E+01 0.22595E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3409          8.9936          4.5729          4.5729
v  Velocity[Y]            -2.7491          7.1647         0.23561         0.23561
v  Velocity[Z]       -8.2977e-015     8.3996e-015    -1.4751e-017    -1.4751e-017
v  ǁVelocityǁ         0.0021799          8.9939          5.0311          5.0311
v  Pressure               -26.102           26.35        -0.21685        -0.21685
v  nu_tilda           4.3992e-007       0.0045236       0.0017872       0.0017872
v  TempC                       21          73.055          22.057          22.057
v  TurbVisc           3.2927e-014       0.0053313       0.0021012       0.0021012
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2792:        0.22350E+01

===============================================================


 INSTANT    0.279300000E+04   TIME STEP NUMBER            2793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96244E-02 0.88919E+00
   Friction velocity        uk    :  0.96244E-02 0.88919E+00
   Dimensionless distance   yplus :  0.77483E-01 0.71586E+01
   Friction thermal sca.    tstar : -0.12100E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57811E-01 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10550E-01      33   0.23353E-03   0.41699E+01 0.19049E+03 
c  Velocity[X]                                      0.19699E+01 
c  Velocity[Y]                                      0.22000E+01 
c  Velocity[Z]                                      0.10099E-29 
c  Pressure     0.87110E-07     570   0.97792E-08   0.84294E-01 0.18558E+04 
c  nu_tilda     0.84678E-05      33   0.24603E-05   0.72808E-06 0.21355E+03 
c  TempC        0.44006E+02      28   0.30505E-03   0.55960E+01 0.26287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3409          8.9939          4.5729          4.5729
v  Velocity[Y]             -2.748          7.1852         0.23551         0.23551
v  Velocity[Z]       -8.0933e-015     8.3929e-015    -1.4754e-017    -1.4754e-017
v  ǁVelocityǁ         0.0020417          8.9942          5.0311          5.0311
v  Pressure                -26.05          26.562        -0.13529        -0.13529
v  nu_tilda           4.3997e-007       0.0045239       0.0017872       0.0017872
v  TempC                       21          73.056          22.057          22.057
v  TurbVisc            3.295e-014       0.0053316       0.0021011       0.0021011
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2793:        0.22970E+01

===============================================================


 INSTANT    0.279400000E+04   TIME STEP NUMBER            2794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12841E-01 0.89010E+00
   Friction velocity        uk    :  0.12841E-01 0.89010E+00
   Dimensionless distance   yplus :  0.10338E+00 0.71659E+01
   Friction thermal sca.    tstar : -0.13451E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77131E-01 0.53466E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10549E-01      33   0.25232E-03   0.41667E+01 0.19043E+03 
c  Velocity[X]                                      0.19796E+01 
c  Velocity[Y]                                      0.21871E+01 
c  Velocity[Z]                                      0.10608E-29 
c  Pressure     0.10816E-06     538   0.91790E-08   0.10459E+00 0.22321E+04 
c  nu_tilda     0.84681E-05      33   0.12853E-04   0.72820E-06 0.21355E+03 
c  TempC        0.44005E+02      27   0.27882E-03   0.55973E+01 0.24812E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3409          8.9942          4.5729          4.5729
v  Velocity[Y]            -2.7471          7.1571          0.2354          0.2354
v  Velocity[Z]       -8.0737e-015     8.4266e-015    -1.4754e-017    -1.4754e-017
v  ǁVelocityǁ         0.0024422          8.9945          5.0311          5.0311
v  Pressure               -26.123           26.31        -0.24036        -0.24036
v  nu_tilda           4.4002e-007       0.0045241       0.0017871       0.0017871
v  TempC                       21          73.056          22.057          22.057
v  TurbVisc           3.2966e-014       0.0053319       0.0021011       0.0021011
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2794:        0.22260E+01

===============================================================


 INSTANT    0.279500000E+04   TIME STEP NUMBER            2795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17051E-01 0.88943E+00
   Friction velocity        uk    :  0.17051E-01 0.88943E+00
   Dimensionless distance   yplus :  0.13727E+00 0.71605E+01
   Friction thermal sca.    tstar : -0.15029E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10242E+00 0.53425E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10548E-01      33   0.24755E-03   0.41827E+01 0.19047E+03 
c  Velocity[X]                                      0.20029E+01 
c  Velocity[Y]                                      0.21798E+01 
c  Velocity[Z]                                      0.95765E-30 
c  Pressure     0.10444E-06     506   0.99373E-08   0.10006E+00 0.16558E+04 
c  nu_tilda     0.84684E-05      33   0.24642E-05   0.72828E-06 0.21356E+03 
c  TempC        0.44005E+02      26   0.29944E-03   0.39769E+01 0.22913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3408          8.9945          4.5729          4.5729
v  Velocity[Y]            -2.7461          7.1851          0.2353          0.2353
v  Velocity[Z]       -7.8334e-015     8.4171e-015    -1.4754e-017    -1.4754e-017
v  ǁVelocityǁ         0.0021381          8.9948          5.0311          5.0311
v  Pressure               -26.067          26.503        -0.16732        -0.16732
v  nu_tilda           4.4001e-007       0.0045243       0.0017871       0.0017871
v  TempC                       21          73.057          22.057          22.057
v  TurbVisc            3.298e-014       0.0053321        0.002101        0.002101
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2795:        0.21570E+01

===============================================================


 INSTANT    0.279600000E+04   TIME STEP NUMBER            2796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10753E-01 0.89076E+00
   Friction velocity        uk    :  0.10753E-01 0.89076E+00
   Dimensionless distance   yplus :  0.86567E-01 0.71712E+01
   Friction thermal sca.    tstar : -0.24487E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64589E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10547E-01      33   0.23508E-03   0.41554E+01 0.19038E+03 
c  Velocity[X]                                      0.19613E+01 
c  Velocity[Y]                                      0.21942E+01 
c  Velocity[Z]                                      0.90386E-30 
c  Pressure     0.89517E-07     522   0.93059E-08   0.86508E-01 0.11704E+04 
c  nu_tilda     0.84687E-05      33   0.12847E-04   0.72841E-06 0.21356E+03 
c  TempC        0.44005E+02      26   0.27413E-03   0.45185E+01 0.24039E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3408          8.9948          4.5729          4.5729
v  Velocity[Y]            -2.7451          7.1909          0.2352          0.2352
v  Velocity[Z]        -7.815e-015     8.4529e-015     -1.476e-017     -1.476e-017
v  ǁVelocityǁ         0.0018815          8.9951          5.0311          5.0311
v  Pressure               -26.147          26.428        -0.23277        -0.23277
v  nu_tilda           4.3993e-007       0.0045246        0.001787        0.001787
v  TempC                       21          73.058          22.057          22.057
v  TurbVisc           3.2978e-014       0.0053324        0.002101        0.002101
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2796:        0.21900E+01

===============================================================


 INSTANT    0.279700000E+04   TIME STEP NUMBER            2797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.87585E-02 0.89026E+00
   Friction velocity        uk    :  0.87585E-02 0.89026E+00
   Dimensionless distance   yplus :  0.70512E-01 0.71672E+01
   Friction thermal sca.    tstar : -0.30062E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52610E-01 0.53475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10546E-01      33   0.22973E-03   0.41701E+01 0.19032E+03 
c  Velocity[X]                                      0.19908E+01 
c  Velocity[Y]                                      0.21793E+01 
c  Velocity[Z]                                      0.92189E-30 
c  Pressure     0.11284E-06     457   0.90736E-08   0.10921E+00 0.57341E+03 
c  nu_tilda     0.84690E-05      33   0.24646E-05   0.72852E-06 0.21357E+03 
c  TempC        0.44005E+02      27   0.30228E-03   0.49985E+01 0.24511E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3407          8.9951          4.5729          4.5729
v  Velocity[Y]            -2.7441          7.1615         0.23509         0.23509
v  Velocity[Z]       -7.7524e-015     8.4426e-015    -1.4764e-017    -1.4764e-017
v  ǁVelocityǁ         0.0013162          8.9954          5.0311          5.0311
v  Pressure               -26.084          26.358        -0.21191        -0.21191
v  nu_tilda           4.3997e-007       0.0045248        0.001787        0.001787
v  TempC                       21          73.059          22.057          22.057
v  TurbVisc           3.2954e-014       0.0053326       0.0021009       0.0021009
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2797:        0.20320E+01

===============================================================


 INSTANT    0.279800000E+04   TIME STEP NUMBER            2798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.81568E-02 0.88909E+00
   Friction velocity        uk    :  0.81568E-02 0.88909E+00
   Dimensionless distance   yplus :  0.65668E-01 0.71577E+01
   Friction thermal sca.    tstar : -0.24447E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48995E-01 0.53405E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10545E-01      33   0.23813E-03   0.41652E+01 0.19030E+03 
c  Velocity[X]                                      0.19917E+01 
c  Velocity[Y]                                      0.21735E+01 
c  Velocity[Z]                                      0.82824E-30 
c  Pressure     0.89077E-07     473   0.97019E-08   0.86474E-01 0.75882E+03 
c  nu_tilda     0.84692E-05      33   0.12843E-04   0.72866E-06 0.21358E+03 
c  TempC        0.44004E+02      26   0.31698E-03   0.60466E+01 0.27141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3406          8.9954          4.5729          4.5729
v  Velocity[Y]            -2.7431          7.1816         0.23499         0.23499
v  Velocity[Z]       -7.8525e-015     8.4813e-015    -1.4768e-017    -1.4768e-017
v  ǁVelocityǁ        0.00033797          8.9957          5.0311          5.0311
v  Pressure               -26.166          26.398        -0.25245        -0.25245
v  nu_tilda           4.4004e-007       0.0045251       0.0017869       0.0017869
v  TempC                       21          73.059          22.057          22.057
v  TurbVisc           3.2965e-014        0.005333       0.0021009       0.0021009
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2798:        0.21100E+01

===============================================================


 INSTANT    0.279900000E+04   TIME STEP NUMBER            2799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.98144E-02 0.89017E+00
   Friction velocity        uk    :  0.98144E-02 0.89017E+00
   Dimensionless distance   yplus :  0.79013E-01 0.71665E+01
   Friction thermal sca.    tstar : -0.26827E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58952E-01 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10543E-01      33   0.24694E-03   0.41628E+01 0.19029E+03 
c  Velocity[X]                                      0.19752E+01 
c  Velocity[Y]                                      0.21875E+01 
c  Velocity[Z]                                      0.82349E-30 
c  Pressure     0.10139E-06     457   0.95368E-08   0.98630E-01 0.53928E+03 
c  nu_tilda     0.84695E-05      33   0.24706E-05   0.72874E-06 0.21359E+03 
c  TempC        0.44004E+02      26   0.25148E-03   0.51455E+01 0.25979E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3405          8.9957          4.5729          4.5729
v  Velocity[Y]             -2.742          7.1611         0.23488         0.23488
v  Velocity[Z]       -7.8887e-015     8.4685e-015    -1.4767e-017    -1.4767e-017
v  ǁVelocityǁ         0.0012557          8.9959          5.0311          5.0311
v  Pressure               -26.104          26.358         -0.2287         -0.2287
v  nu_tilda           4.4011e-007       0.0045253       0.0017869       0.0017869
v  TempC                       21           73.06          22.057          22.057
v  TurbVisc           3.2986e-014       0.0053333       0.0021008       0.0021008
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2799:        0.20380E+01

===============================================================


 INSTANT    0.280000000E+04   TIME STEP NUMBER            2800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16715E-01 0.88935E+00
   Friction velocity        uk    :  0.16715E-01 0.88935E+00
   Dimensionless distance   yplus :  0.13456E+00 0.71598E+01
   Friction thermal sca.    tstar : -0.15017E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10040E+00 0.53420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10542E-01      33   0.20645E-03   0.41480E+01 0.19019E+03 
c  Velocity[X]                                      0.19754E+01 
c  Velocity[Y]                                      0.21726E+01 
c  Velocity[Z]                                      0.10234E-29 
c  Pressure     0.10425E-06     472   0.96427E-08   0.99587E-01 0.91069E+03 
c  nu_tilda     0.84698E-05      33   0.12836E-04   0.72886E-06 0.21359E+03 
c  TempC        0.44004E+02      26   0.35282E-03   0.60136E+01 0.26941E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3405          8.9959          4.5729          4.5729
v  Velocity[Y]            -2.7411          7.1807         0.23478         0.23478
v  Velocity[Z]       -8.0071e-015     8.5017e-015    -1.4768e-017    -1.4768e-017
v  ǁVelocityǁ          0.001436          8.9962          5.0311          5.0311
v  Pressure               -26.184          26.337        -0.28167        -0.28167
v  nu_tilda           4.4014e-007       0.0045255       0.0017868       0.0017868
v  TempC                       21          73.061          22.057          22.057
v  TurbVisc           3.3009e-014       0.0053335       0.0021008       0.0021008
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2800:        0.20780E+01

===============================================================


 INSTANT    0.280100000E+04   TIME STEP NUMBER            2801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17047E-01 0.89108E+00
   Friction velocity        uk    :  0.17047E-01 0.89108E+00
   Dimensionless distance   yplus :  0.13724E+00 0.71738E+01
   Friction thermal sca.    tstar : -0.14093E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10240E+00 0.53525E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10541E-01      33   0.25159E-03   0.41508E+01 0.19019E+03 
c  Velocity[X]                                      0.19854E+01 
c  Velocity[Y]                                      0.21654E+01 
c  Velocity[Z]                                      0.96643E-30 
c  Pressure     0.97363E-07     474   0.91168E-08   0.94234E-01 0.10731E+04 
c  nu_tilda     0.84701E-05      33   0.24686E-05   0.72894E-06 0.21360E+03 
c  TempC        0.44004E+02      26   0.25131E-03   0.75194E+01 0.30730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3404          8.9962          4.5729          4.5729
v  Velocity[Y]            -2.7401          7.1951         0.23467         0.23467
v  Velocity[Z]       -8.0457e-015     8.4915e-015    -1.4765e-017    -1.4765e-017
v  ǁVelocityǁ         0.0012458          8.9965          5.0311          5.0311
v  Pressure               -26.125          26.433        -0.22876        -0.22876
v  nu_tilda           4.4012e-007       0.0045258       0.0017868       0.0017868
v  TempC                       21          73.061          22.057          22.057
v  TurbVisc           3.3017e-014       0.0053338       0.0021007       0.0021007
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2801:        0.20770E+01

===============================================================


 INSTANT    0.280200000E+04   TIME STEP NUMBER            2802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11038E-01 0.89075E+00
   Friction velocity        uk    :  0.11038E-01 0.89075E+00
   Dimensionless distance   yplus :  0.88862E-01 0.71712E+01
   Friction thermal sca.    tstar : -0.11532E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66301E-01 0.53505E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10540E-01      33   0.23190E-03   0.41645E+01 0.19024E+03 
c  Velocity[X]                                      0.19829E+01 
c  Velocity[Y]                                      0.21815E+01 
c  Velocity[Z]                                      0.88157E-30 
c  Pressure     0.10139E-06     521   0.97287E-08   0.99251E-01 0.18641E+04 
c  nu_tilda     0.84703E-05      33   0.12830E-04   0.72910E-06 0.21361E+03 
c  TempC        0.44003E+02      26   0.32245E-03   0.47594E+01 0.24121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3403          8.9965          4.5729          4.5729
v  Velocity[Y]            -2.7391          7.1647         0.23456         0.23456
v  Velocity[Z]       -8.1753e-015     8.5249e-015    -1.4764e-017    -1.4764e-017
v  ǁVelocityǁ        0.00097242          8.9968          5.0311          5.0311
v  Pressure               -26.199          26.235        -0.31996        -0.31996
v  nu_tilda           4.4009e-007       0.0045261       0.0017867       0.0017867
v  TempC                       21          73.061          22.057          22.057
v  TurbVisc           3.3011e-014       0.0053341       0.0021007       0.0021007
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2802:        0.21930E+01

===============================================================


 INSTANT    0.280300000E+04   TIME STEP NUMBER            2803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16639E-01 0.88918E+00
   Friction velocity        uk    :  0.16639E-01 0.88918E+00
   Dimensionless distance   yplus :  0.13395E+00 0.71585E+01
   Friction thermal sca.    tstar : -0.10574E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99945E-01 0.53411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10539E-01      33   0.23620E-03   0.41446E+01 0.19004E+03 
c  Velocity[X]                                      0.19785E+01 
c  Velocity[Y]                                      0.21661E+01 
c  Velocity[Z]                                      0.85219E-30 
c  Pressure     0.10696E-06     553   0.97400E-08   0.10168E+00 0.16143E+04 
c  nu_tilda     0.84706E-05      33   0.24765E-05   0.72922E-06 0.21362E+03 
c  TempC        0.44003E+02      26   0.33881E-03   0.75282E+01 0.30530E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3403          8.9968          4.5729          4.5729
v  Velocity[Y]            -2.7381          7.1817         0.23445         0.23445
v  Velocity[Z]       -8.2258e-015     8.5156e-015    -1.4763e-017    -1.4763e-017
v  ǁVelocityǁ        0.00083602          8.9971          5.0311          5.0311
v  Pressure               -26.145          26.407        -0.24663        -0.24663
v  nu_tilda           4.4006e-007       0.0045263       0.0017867       0.0017867
v  TempC                       21           73.06          22.057          22.057
v  TurbVisc           3.3002e-014       0.0053345       0.0021006       0.0021006
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2803:        0.22570E+01

===============================================================


 INSTANT    0.280400000E+04   TIME STEP NUMBER            2804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16865E-01 0.89032E+00
   Friction velocity        uk    :  0.16865E-01 0.89032E+00
   Dimensionless distance   yplus :  0.13577E+00 0.71677E+01
   Friction thermal sca.    tstar : -0.10110E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10130E+00 0.53479E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10537E-01      33   0.25292E-03   0.41642E+01 0.19015E+03 
c  Velocity[X]                                      0.20048E+01 
c  Velocity[Y]                                      0.21593E+01 
c  Velocity[Z]                                      0.89101E-30 
c  Pressure     0.95031E-07     521   0.91355E-08   0.93043E-01 0.20294E+04 
c  nu_tilda     0.84708E-05      33   0.12826E-04   0.72936E-06 0.21363E+03 
c  TempC        0.44003E+02      26   0.29231E-03   0.74022E+01 0.29033E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3402           8.997          4.5729          4.5729
v  Velocity[Y]             -2.737          7.1607         0.23434         0.23434
v  Velocity[Z]       -8.3685e-015     8.5445e-015    -1.4763e-017    -1.4763e-017
v  ǁVelocityǁ        0.00031235          8.9973          5.0312          5.0312
v  Pressure               -26.217          26.189        -0.34451        -0.34451
v  nu_tilda           4.4007e-007       0.0045266       0.0017866       0.0017866
v  TempC                       21           73.06          22.057          22.057
v  TurbVisc           3.2992e-014       0.0053348       0.0021005       0.0021005
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2804:        0.21960E+01

===============================================================


 INSTANT    0.280500000E+04   TIME STEP NUMBER            2805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14515E-01 0.88959E+00
   Friction velocity        uk    :  0.14515E-01 0.88959E+00
   Dimensionless distance   yplus :  0.11685E+00 0.71618E+01
   Friction thermal sca.    tstar : -0.92558E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87187E-01 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10536E-01      33   0.18369E-03   0.41470E+01 0.19007E+03 
c  Velocity[X]                                      0.19732E+01 
c  Velocity[Y]                                      0.21738E+01 
c  Velocity[Z]                                      0.90181E-30 
c  Pressure     0.88370E-07     505   0.99294E-08   0.85205E-01 0.19115E+04 
c  nu_tilda     0.84711E-05      33   0.24729E-05   0.72945E-06 0.21364E+03 
c  TempC        0.44002E+02      26   0.25409E-03   0.56898E+01 0.25854E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3401          8.9973          4.5729          4.5729
v  Velocity[Y]             -2.736          7.1857         0.23423         0.23423
v  Velocity[Z]       -8.4088e-015     8.5358e-015    -1.4759e-017    -1.4759e-017
v  ǁVelocityǁ        0.00080532          8.9976          5.0312          5.0312
v  Pressure               -26.163          26.416        -0.26111        -0.26111
v  nu_tilda           4.3999e-007       0.0045268       0.0017866       0.0017866
v  TempC                       21           73.06          22.057          22.057
v  TurbVisc           3.2995e-014        0.005335       0.0021005       0.0021005
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2805:        0.24110E+01

===============================================================


 INSTANT    0.280600000E+04   TIME STEP NUMBER            2806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.99887E-02 0.89074E+00
   Friction velocity        uk    :  0.99887E-02 0.89074E+00
   Dimensionless distance   yplus :  0.80416E-01 0.71711E+01
   Friction thermal sca.    tstar : -0.86930E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59999E-01 0.53504E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10535E-01      33   0.25071E-03   0.41122E+01 0.18989E+03 
c  Velocity[X]                                      0.19537E+01 
c  Velocity[Y]                                      0.21586E+01 
c  Velocity[Z]                                      0.88522E-30 
c  Pressure     0.10081E-06     520   0.95971E-08   0.96226E-01 0.17251E+04 
c  nu_tilda     0.84713E-05      33   0.12818E-04   0.72958E-06 0.21364E+03 
c  TempC        0.44002E+02      26   0.23509E-03   0.49370E+01 0.24426E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.34          8.9976          4.5729          4.5729
v  Velocity[Y]            -2.7351          7.1882         0.23412         0.23412
v  Velocity[Z]       -8.5872e-015     8.5671e-015    -1.4762e-017    -1.4762e-017
v  ǁVelocityǁ         0.0017143          8.9978          5.0312          5.0312
v  Pressure               -26.236          26.248        -0.34804        -0.34804
v  nu_tilda           4.3992e-007        0.004527       0.0017865       0.0017865
v  TempC                       21          73.061          22.057          22.057
v  TurbVisc           3.2973e-014       0.0053353       0.0021004       0.0021004
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2806:        0.23430E+01

===============================================================


 INSTANT    0.280700000E+04   TIME STEP NUMBER            2807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.26147E-02 0.89051E+00
   Friction velocity        uk    :  0.26147E-02 0.89051E+00
   Dimensionless distance   yplus :  0.21050E-01 0.71692E+01
   Friction thermal sca.    tstar : -0.11612E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15706E-01 0.53490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10534E-01      33   0.24573E-03   0.41492E+01 0.19000E+03 
c  Velocity[X]                                      0.19968E+01 
c  Velocity[Y]                                      0.21524E+01 
c  Velocity[Z]                                      0.79313E-30 
c  Pressure     0.12211E-06     458   0.92122E-08   0.11943E+00 0.91677E+03 
c  nu_tilda     0.84716E-05      33   0.24805E-05   0.72967E-06 0.21365E+03 
c  TempC        0.44002E+02      26   0.40244E-03   0.41474E+01 0.23595E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.34          8.9978          4.5729          4.5729
v  Velocity[Y]            -2.7341          7.1642           0.234           0.234
v  Velocity[Z]       -8.6221e-015     8.5574e-015    -1.4755e-017    -1.4755e-017
v  ǁVelocityǁ         0.0020971          8.9981          5.0312          5.0312
v  Pressure               -26.179          26.295        -0.30018        -0.30018
v  nu_tilda           4.3991e-007       0.0045273       0.0017865       0.0017865
v  TempC                       21          73.061          22.057          22.057
v  TurbVisc            3.295e-014       0.0053356       0.0021004       0.0021004
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2807:        0.20500E+01

===============================================================


 INSTANT    0.280800000E+04   TIME STEP NUMBER            2808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16965E-01 0.88907E+00
   Friction velocity        uk    :  0.16965E-01 0.88907E+00
   Dimensionless distance   yplus :  0.13658E+00 0.71576E+01
   Friction thermal sca.    tstar : -0.78257E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10191E+00 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10533E-01      33   0.25993E-03   0.41376E+01 0.18998E+03 
c  Velocity[X]                                      0.19666E+01 
c  Velocity[Y]                                      0.21710E+01 
c  Velocity[Z]                                      0.85188E-30 
c  Pressure     0.96172E-07     537   0.94811E-08   0.92763E-01 0.10478E+04 
c  nu_tilda     0.84718E-05      33   0.12816E-04   0.72982E-06 0.21366E+03 
c  TempC        0.44001E+02      27   0.30310E-03   0.68861E+01 0.31777E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3399          8.9981          4.5729          4.5729
v  Velocity[Y]             -2.733          7.1835         0.23389         0.23389
v  Velocity[Z]       -8.8174e-015     8.5881e-015    -1.4756e-017    -1.4756e-017
v  ǁVelocityǁ         0.0014355          8.9984          5.0312          5.0312
v  Pressure               -26.257          26.255        -0.36083        -0.36083
v  nu_tilda           4.3992e-007       0.0045276       0.0017864       0.0017864
v  TempC                       21          73.062          22.057          22.057
v  TurbVisc           3.2948e-014       0.0053359       0.0021003       0.0021003
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2808:        0.22260E+01

===============================================================


 INSTANT    0.280900000E+04   TIME STEP NUMBER            2809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.35645E-02 0.89025E+00
   Friction velocity        uk    :  0.35645E-02 0.89025E+00
   Dimensionless distance   yplus :  0.28696E-01 0.71671E+01
   Friction thermal sca.    tstar : -0.57870E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21411E-01 0.53475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10531E-01      33   0.24315E-03   0.41519E+01 0.18992E+03 
c  Velocity[X]                                      0.19985E+01 
c  Velocity[Y]                                      0.21534E+01 
c  Velocity[Z]                                      0.10092E-29 
c  Pressure     0.12792E-06     473   0.94150E-08   0.12322E+00 0.58292E+03 
c  nu_tilda     0.84720E-05      33   0.24774E-05   0.72993E-06 0.21367E+03 
c  TempC        0.44001E+02      27   0.29946E-03   0.52566E+01 0.26348E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3398          8.9984          4.5729          4.5729
v  Velocity[Y]             -2.732          7.1601         0.23378         0.23378
v  Velocity[Z]       -8.8454e-015     8.5766e-015    -1.4748e-017    -1.4748e-017
v  ǁVelocityǁ         0.0028964          8.9987          5.0313          5.0313
v  Pressure               -26.196          26.223        -0.33185        -0.33185
v  nu_tilda           4.3995e-007       0.0045278       0.0017864       0.0017864
v  TempC                       21          73.062          22.056          22.056
v  TurbVisc           3.2949e-014       0.0053362       0.0021002       0.0021002
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2809:        0.20570E+01

===============================================================


 INSTANT    0.281000000E+04   TIME STEP NUMBER            2810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14676E-01 0.88969E+00
   Friction velocity        uk    :  0.14676E-01 0.88969E+00
   Dimensionless distance   yplus :  0.11815E+00 0.71626E+01
   Friction thermal sca.    tstar : -0.14035E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88156E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10530E-01      33   0.18569E-03   0.41285E+01 0.18982E+03 
c  Velocity[X]                                      0.19828E+01 
c  Velocity[Y]                                      0.21457E+01 
c  Velocity[Z]                                      0.82939E-30 
c  Pressure     0.92004E-07     520   0.99019E-08   0.89517E-01 0.89145E+03 
c  nu_tilda     0.84723E-05      33   0.12809E-04   0.73007E-06 0.21368E+03 
c  TempC        0.44001E+02      26   0.27427E-03   0.56655E+01 0.26642E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3396          8.9986          4.5729          4.5729
v  Velocity[Y]             -2.731           7.185         0.23366         0.23366
v  Velocity[Z]       -9.0847e-015     8.6078e-015     -1.475e-017     -1.475e-017
v  ǁVelocityǁ         0.0032608          8.9989          5.0313          5.0313
v  Pressure               -26.273          26.223        -0.38386        -0.38386
v  nu_tilda            4.399e-007        0.004528       0.0017863       0.0017863
v  TempC                       21          73.063          22.056          22.056
v  TurbVisc           3.2961e-014       0.0053365       0.0021002       0.0021002
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2810:        0.22660E+01

===============================================================


 INSTANT    0.281100000E+04   TIME STEP NUMBER            2811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14649E-01 0.89100E+00
   Friction velocity        uk    :  0.14649E-01 0.89100E+00
   Dimensionless distance   yplus :  0.11794E+00 0.71731E+01
   Friction thermal sca.    tstar : -0.95459E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87993E-01 0.53519E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10529E-01      33   0.25233E-03   0.41074E+01 0.18974E+03 
c  Velocity[X]                                      0.19451E+01 
c  Velocity[Y]                                      0.21623E+01 
c  Velocity[Z]                                      0.95625E-30 
c  Pressure     0.76125E-07     538   0.90827E-08   0.73297E-01 0.10871E+04 
c  nu_tilda     0.84725E-05      33   0.24846E-05   0.73016E-06 0.21369E+03 
c  TempC        0.44000E+02      27   0.27990E-03   0.44530E+01 0.24656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3395          8.9989          4.5729          4.5729
v  Velocity[Y]              -2.73          7.1949         0.23355         0.23355
v  Velocity[Z]       -9.1022e-015     8.5969e-015    -1.4738e-017    -1.4738e-017
v  ǁVelocityǁ         0.0032978          8.9992          5.0313          5.0313
v  Pressure               -26.215          26.315        -0.32975        -0.32975
v  nu_tilda            4.398e-007       0.0045283       0.0017863       0.0017863
v  TempC                       21          73.063          22.056          22.056
v  TurbVisc           3.2946e-014       0.0053368       0.0021001       0.0021001
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2811:        0.24320E+01

===============================================================


 INSTANT    0.281200000E+04   TIME STEP NUMBER            2812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.83287E-02 0.89047E+00
   Friction velocity        uk    :  0.83287E-02 0.89047E+00
   Dimensionless distance   yplus :  0.67051E-01 0.71689E+01
   Friction thermal sca.    tstar : -0.24883E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.50028E-01 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10528E-01      33   0.23295E-03   0.41400E+01 0.18983E+03 
c  Velocity[X]                                      0.19897E+01 
c  Velocity[Y]                                      0.21503E+01 
c  Velocity[Z]                                      0.10928E-29 
c  Pressure     0.11365E-06     554   0.98687E-08   0.10993E+00 0.20112E+04 
c  nu_tilda     0.84727E-05      33   0.12804E-04   0.73031E-06 0.21369E+03 
c  TempC        0.44000E+02      26   0.36966E-03   0.49493E+01 0.25475E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3394          8.9992          4.5729          4.5729
v  Velocity[Y]             -2.729          7.1629         0.23343         0.23343
v  Velocity[Z]       -9.3637e-015      8.625e-015    -1.4741e-017    -1.4741e-017
v  ǁVelocityǁ         0.0018669          8.9994          5.0314          5.0314
v  Pressure               -26.291          26.082        -0.42572        -0.42572
v  nu_tilda           4.3986e-007       0.0045285       0.0017862       0.0017862
v  TempC                       21          73.063          22.056          22.056
v  TurbVisc           3.2916e-014        0.005337       0.0021001       0.0021001
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2812:        0.24610E+01

===============================================================


 INSTANT    0.281300000E+04   TIME STEP NUMBER            2813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42812E-03 0.88942E+00
   Friction velocity        uk    :  0.42812E-03 0.88942E+00
   Dimensionless distance   yplus :  0.34466E-02 0.71605E+01
   Friction thermal sca.    tstar : -0.66036E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25716E-02 0.53425E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10526E-01      33   0.23864E-03   0.41078E+01 0.18964E+03 
c  Velocity[X]                                      0.19694E+01 
c  Velocity[Y]                                      0.21384E+01 
c  Velocity[Z]                                      0.94326E-30 
c  Pressure     0.87448E-07     552   0.96228E-08   0.84964E-01 0.17731E+04 
c  nu_tilda     0.84729E-05      33   0.24812E-05   0.73042E-06 0.21370E+03 
c  TempC        0.44000E+02      27   0.27391E-03   0.61359E+01 0.30083E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3392          8.9994          4.5729          4.5729
v  Velocity[Y]             -2.728          7.1856         0.23331         0.23331
v  Velocity[Z]       -9.3718e-015     8.6149e-015    -1.4731e-017    -1.4731e-017
v  ǁVelocityǁ         0.0032324          8.9997          5.0314          5.0314
v  Pressure               -26.235          26.301        -0.34875        -0.34875
v  nu_tilda           4.3993e-007       0.0045287       0.0017862       0.0017862
v  TempC                       21          73.063          22.056          22.056
v  TurbVisc           3.2932e-014       0.0053373          0.0021          0.0021
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2813:        0.24540E+01

===============================================================


 INSTANT    0.281400000E+04   TIME STEP NUMBER            2814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17886E-01 0.89016E+00
   Friction velocity        uk    :  0.17886E-01 0.89016E+00
   Dimensionless distance   yplus :  0.14400E+00 0.71664E+01
   Friction thermal sca.    tstar : -0.10945E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10744E+00 0.53469E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10525E-01      33   0.26179E-03   0.41256E+01 0.18975E+03 
c  Velocity[X]                                      0.19683E+01 
c  Velocity[Y]                                      0.21572E+01 
c  Velocity[Z]                                      0.80253E-30 
c  Pressure     0.94157E-07     552   0.97213E-08   0.92242E-01 0.19211E+04 
c  nu_tilda     0.84731E-05      33   0.12798E-04   0.73058E-06 0.21372E+03 
c  TempC        0.43999E+02      27   0.25047E-03   0.44371E+01 0.23132E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3391          8.9997          4.5729          4.5729
v  Velocity[Y]             -2.727          7.1619          0.2332          0.2332
v  Velocity[Z]        -9.677e-015     8.6441e-015    -1.4734e-017    -1.4734e-017
v  ǁVelocityǁ         0.0030067               9          5.0314          5.0314
v  Pressure                -26.31          26.084         -0.4416         -0.4416
v  nu_tilda           4.3999e-007        0.004529       0.0017861       0.0017861
v  TempC                       21          73.063          22.056          22.056
v  TurbVisc           3.2953e-014       0.0053376       0.0020999       0.0020999
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2814:        0.23510E+01

===============================================================


 INSTANT    0.281500000E+04   TIME STEP NUMBER            2815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16745E-01 0.88937E+00
   Friction velocity        uk    :  0.16745E-01 0.88937E+00
   Dimensionless distance   yplus :  0.13481E+00 0.71601E+01
   Friction thermal sca.    tstar : -0.12323E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10058E+00 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10524E-01      33   0.25286E-03   0.41327E+01 0.18969E+03 
c  Velocity[X]                                      0.19928E+01 
c  Velocity[Y]                                      0.21399E+01 
c  Velocity[Z]                                      0.84079E-30 
c  Pressure     0.11658E-06     537   0.90432E-08   0.11046E+00 0.14123E+04 
c  nu_tilda     0.84733E-05      33   0.24852E-05   0.73066E-06 0.21373E+03 
c  TempC        0.43999E+02      26   0.30308E-03   0.44738E+01 0.22807E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.339               9          4.5729          4.5729
v  Velocity[Y]            -2.7259          7.1832         0.23308         0.23308
v  Velocity[Z]        -9.678e-015     8.6327e-015    -1.4727e-017    -1.4727e-017
v  ǁVelocityǁ          0.003125          9.0002          5.0315          5.0315
v  Pressure               -26.252           26.24        -0.37674        -0.37674
v  nu_tilda           4.4002e-007       0.0045292       0.0017861       0.0017861
v  TempC                       21          73.064          22.056          22.056
v  TurbVisc           3.2971e-014       0.0053379       0.0020999       0.0020999
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2815:        0.22890E+01

===============================================================


 INSTANT    0.281600000E+04   TIME STEP NUMBER            2816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.25250E-02 0.89077E+00
   Friction velocity        uk    :  0.25250E-02 0.89077E+00
   Dimensionless distance   yplus :  0.20328E-01 0.71713E+01
   Friction thermal sca.    tstar : -0.71243E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.15167E-01 0.53506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10523E-01      33   0.25235E-03   0.41268E+01 0.18968E+03 
c  Velocity[X]                                      0.19947E+01 
c  Velocity[Y]                                      0.21321E+01 
c  Velocity[Z]                                      0.99208E-30 
c  Pressure     0.10518E-06     504   0.98076E-08   0.10163E+00 0.10811E+04 
c  nu_tilda     0.84735E-05      33   0.12792E-04   0.73080E-06 0.21373E+03 
c  TempC        0.43998E+02      27   0.26525E-03   0.52171E+01 0.24810E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3389          9.0002          4.5729          4.5729
v  Velocity[Y]            -2.7249          7.1915         0.23296         0.23296
v  Velocity[Z]       -1.0022e-014     8.6599e-015    -1.4727e-017    -1.4727e-017
v  ǁVelocityǁ         0.0021416          9.0005          5.0315          5.0315
v  Pressure               -26.332          26.179        -0.43833        -0.43833
v  nu_tilda           4.3996e-007       0.0045295        0.001786        0.001786
v  TempC                       21          73.064          22.056          22.056
v  TurbVisc           3.2981e-014       0.0053382       0.0020998       0.0020998
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2816:        0.21640E+01

===============================================================


 INSTANT    0.281700000E+04   TIME STEP NUMBER            2817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11563E-01 0.89040E+00
   Friction velocity        uk    :  0.11563E-01 0.89040E+00
   Dimensionless distance   yplus :  0.93094E-01 0.71683E+01
   Friction thermal sca.    tstar : -0.74343E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.69458E-01 0.53484E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10521E-01      33   0.22950E-03   0.41259E+01 0.18963E+03 
c  Velocity[X]                                      0.19775E+01 
c  Velocity[Y]                                      0.21483E+01 
c  Velocity[Z]                                      0.10854E-29 
c  Pressure     0.11196E-06     440   0.97122E-08   0.10989E+00 0.56040E+03 
c  nu_tilda     0.84737E-05      33   0.24880E-05   0.73089E-06 0.21374E+03 
c  TempC        0.43998E+02      27   0.33324E-03   0.53325E+01 0.25094E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3387          9.0005          4.5729          4.5729
v  Velocity[Y]            -2.7239          7.1654         0.23284         0.23284
v  Velocity[Z]       -1.0002e-014     8.6473e-015    -1.4725e-017    -1.4725e-017
v  ǁVelocityǁ         0.0029886          9.0008          5.0315          5.0315
v  Pressure                -26.27          26.146        -0.41121        -0.41121
v  nu_tilda           4.3992e-007       0.0045297        0.001786        0.001786
v  TempC                       21          73.066          22.056          22.056
v  TurbVisc           3.2961e-014       0.0053384       0.0020997       0.0020997
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2817:        0.20010E+01

===============================================================


 INSTANT    0.281800000E+04   TIME STEP NUMBER            2818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16755E-01 0.88897E+00
   Friction velocity        uk    :  0.16755E-01 0.88897E+00
   Dimensionless distance   yplus :  0.13489E+00 0.71568E+01
   Friction thermal sca.    tstar : -0.12195E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10064E+00 0.53398E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10520E-01      33   0.23204E-03   0.40953E+01 0.18946E+03 
c  Velocity[X]                                      0.19631E+01 
c  Velocity[Y]                                      0.21322E+01 
c  Velocity[Z]                                      0.91295E-30 
c  Pressure     0.99836E-07     505   0.94335E-08   0.95389E-01 0.97037E+03 
c  nu_tilda     0.84739E-05      33   0.12789E-04   0.73104E-06 0.21375E+03 
c  TempC        0.43997E+02      26   0.28963E-03   0.70082E+01 0.29739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3386          9.0007          4.5729          4.5729
v  Velocity[Y]            -2.7229          7.1804         0.23272         0.23272
v  Velocity[Z]       -1.0387e-014     8.6764e-015    -1.4725e-017    -1.4725e-017
v  ǁVelocityǁ         0.0029657           9.001          5.0316          5.0316
v  Pressure               -26.349          26.113        -0.46767        -0.46767
v  nu_tilda           4.3992e-007       0.0045299       0.0017859       0.0017859
v  TempC                       21          73.068          22.056          22.056
v  TurbVisc           3.2952e-014       0.0053387       0.0020997       0.0020997
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2818:        0.21290E+01

===============================================================


 INSTANT    0.281900000E+04   TIME STEP NUMBER            2819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18005E-01 0.89031E+00
   Friction velocity        uk    :  0.18005E-01 0.89031E+00
   Dimensionless distance   yplus :  0.14495E+00 0.71676E+01
   Friction thermal sca.    tstar : -0.82852E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10815E+00 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10519E-01      33   0.24493E-03   0.41126E+01 0.18948E+03 
c  Velocity[X]                                      0.19874E+01 
c  Velocity[Y]                                      0.21252E+01 
c  Velocity[Z]                                      0.74040E-30 
c  Pressure     0.10371E-06     489   0.96445E-08   0.10108E+00 0.62653E+03 
c  nu_tilda     0.84741E-05      33   0.24877E-05   0.73115E-06 0.21376E+03 
c  TempC        0.43997E+02      26   0.21025E-03   0.50635E+01 0.24706E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3385           9.001          4.5729          4.5729
v  Velocity[Y]            -2.7219           7.162         0.23259         0.23259
v  Velocity[Z]       -1.0336e-014     8.6629e-015    -1.4722e-017    -1.4722e-017
v  ǁVelocityǁ         0.0021969          9.0013          5.0316          5.0316
v  Pressure               -26.289          26.119        -0.43456        -0.43456
v  nu_tilda           4.3997e-007       0.0045301       0.0017859       0.0017859
v  TempC                       21          73.069          22.056          22.056
v  TurbVisc           3.2951e-014       0.0053389       0.0020996       0.0020996
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2819:        0.21140E+01

===============================================================


 INSTANT    0.282000000E+04   TIME STEP NUMBER            2820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60990E-02 0.88943E+00
   Friction velocity        uk    :  0.60990E-02 0.88943E+00
   Dimensionless distance   yplus :  0.49101E-01 0.71605E+01
   Friction thermal sca.    tstar : -0.30994E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36635E-01 0.53426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10518E-01      33   0.19485E-03   0.41045E+01 0.18947E+03 
c  Velocity[X]                                      0.19633E+01 
c  Velocity[Y]                                      0.21412E+01 
c  Velocity[Z]                                      0.92944E-30 
c  Pressure     0.90820E-07     505   0.95295E-08   0.87715E-01 0.96610E+03 
c  nu_tilda     0.84743E-05      33   0.12782E-04   0.73132E-06 0.21377E+03 
c  TempC        0.43996E+02      27   0.29611E-03   0.37039E+01 0.20766E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3383          9.0012          4.5729          4.5729
v  Velocity[Y]            -2.7208          7.1854         0.23247         0.23247
v  Velocity[Z]       -1.0682e-014      8.689e-015    -1.4723e-017    -1.4723e-017
v  ǁVelocityǁ         0.0030009          9.0015          5.0317          5.0317
v  Pressure               -26.367           26.09        -0.49096        -0.49096
v  nu_tilda           4.3998e-007       0.0045304       0.0017858       0.0017858
v  TempC                       21           73.07          22.056          22.056
v  TurbVisc           3.2964e-014       0.0053392       0.0020996       0.0020996
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2820:        0.21470E+01

===============================================================


 INSTANT    0.282100000E+04   TIME STEP NUMBER            2821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15876E-01 0.89093E+00
   Friction velocity        uk    :  0.15876E-01 0.89093E+00
   Dimensionless distance   yplus :  0.12781E+00 0.71726E+01
   Friction thermal sca.    tstar : -0.99668E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95361E-01 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10516E-01      33   0.25775E-03   0.40845E+01 0.18928E+03 
c  Velocity[X]                                      0.19589E+01 
c  Velocity[Y]                                      0.21255E+01 
c  Velocity[Z]                                      0.10672E-29 
c  Pressure     0.10335E-06     520   0.98952E-08   0.99043E-01 0.11934E+04 
c  nu_tilda     0.84744E-05      33   0.24948E-05   0.73142E-06 0.21378E+03 
c  TempC        0.43996E+02      27   0.29210E-03   0.45393E+01 0.23825E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3382          9.0015          4.5729          4.5729
v  Velocity[Y]            -2.7198          7.1917         0.23235         0.23235
v  Velocity[Z]        -1.055e-014     8.6787e-015    -1.4714e-017    -1.4714e-017
v  ǁVelocityǁ         0.0032513          9.0018          5.0317          5.0317
v  Pressure               -26.312          26.194        -0.43262        -0.43262
v  nu_tilda           4.3991e-007       0.0045306       0.0017858       0.0017858
v  TempC                       21          73.071          22.056          22.056
v  TurbVisc           3.2968e-014       0.0053395       0.0020995       0.0020995
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2821:        0.21860E+01

===============================================================


 INSTANT    0.282200000E+04   TIME STEP NUMBER            2822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90211E-02 0.89058E+00
   Friction velocity        uk    :  0.90211E-02 0.89058E+00
   Dimensionless distance   yplus :  0.72626E-01 0.71698E+01
   Friction thermal sca.    tstar : -0.81192E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54187E-01 0.53494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10515E-01      33   0.24595E-03   0.41289E+01 0.18950E+03 
c  Velocity[X]                                      0.20088E+01 
c  Velocity[Y]                                      0.21201E+01 
c  Velocity[Z]                                      0.96637E-30 
c  Pressure     0.11002E-06     521   0.94611E-08   0.10792E+00 0.21036E+04 
c  nu_tilda     0.84746E-05      33   0.12777E-04   0.73157E-06 0.21379E+03 
c  TempC        0.43996E+02      27   0.35396E-03   0.50709E+01 0.24876E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.338          9.0017          4.5729          4.5729
v  Velocity[Y]            -2.7188          7.1658         0.23222         0.23222
v  Velocity[Z]       -1.0908e-014     8.7029e-015    -1.4718e-017    -1.4718e-017
v  ǁVelocityǁ         0.0029778           9.002          5.0318          5.0318
v  Pressure               -26.383          25.962        -0.53327        -0.53327
v  nu_tilda           4.3988e-007       0.0045308       0.0017857       0.0017857
v  TempC                       21          73.073          22.056          22.056
v  TurbVisc           3.2947e-014       0.0053398       0.0020994       0.0020994
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2822:        0.21990E+01

===============================================================


 INSTANT    0.282300000E+04   TIME STEP NUMBER            2823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17004E-01 0.88934E+00
   Friction velocity        uk    :  0.17004E-01 0.88934E+00
   Dimensionless distance   yplus :  0.13689E+00 0.71598E+01
   Friction thermal sca.    tstar : -0.10755E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10214E+00 0.53420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10514E-01      33   0.23066E-03   0.40975E+01 0.18934E+03 
c  Velocity[X]                                      0.19647E+01 
c  Velocity[Y]                                      0.21329E+01 
c  Velocity[Z]                                      0.81125E-30 
c  Pressure     0.91116E-07     506   0.98890E-08   0.87644E-01 0.18996E+04 
c  nu_tilda     0.84748E-05      33   0.24927E-05   0.73168E-06 0.21380E+03 
c  TempC        0.43995E+02      27   0.24210E-03   0.65389E+01 0.29109E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3378           9.002          4.5729          4.5729
v  Velocity[Y]            -2.7178          7.1859          0.2321          0.2321
v  Velocity[Z]       -1.0693e-014     8.6931e-015    -1.4712e-017    -1.4712e-017
v  ǁVelocityǁ         0.0017103          9.0023          5.0318          5.0318
v  Pressure               -26.331          26.188        -0.45069        -0.45069
v  nu_tilda           4.3987e-007        0.004531       0.0017857       0.0017857
v  TempC                       21          73.075          22.056          22.056
v  TurbVisc            3.294e-014         0.00534       0.0020994       0.0020994
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2823:        0.21690E+01

===============================================================


 INSTANT    0.282400000E+04   TIME STEP NUMBER            2824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10134E-01 0.89018E+00
   Friction velocity        uk    :  0.10134E-01 0.89018E+00
   Dimensionless distance   yplus :  0.81582E-01 0.71665E+01
   Friction thermal sca.    tstar : -0.11336E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60869E-01 0.53470E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10513E-01      33   0.24400E-03   0.40881E+01 0.18925E+03 
c  Velocity[X]                                      0.19688E+01 
c  Velocity[Y]                                      0.21193E+01 
c  Velocity[Z]                                      0.10505E-29 
c  Pressure     0.10264E-06     538   0.93897E-08   0.98881E-01 0.23270E+04 
c  nu_tilda     0.84749E-05      33   0.12771E-04   0.73184E-06 0.21382E+03 
c  TempC        0.43994E+02      26   0.25433E-03   0.36904E+01 0.23678E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3376          9.0022          4.5729          4.5729
v  Velocity[Y]            -2.7168          7.1581         0.23197         0.23197
v  Velocity[Z]       -1.0944e-014     8.7141e-015    -1.4714e-017    -1.4714e-017
v  ǁVelocityǁ         0.0028855          9.0025          5.0319          5.0319
v  Pressure               -26.403          25.919        -0.55963        -0.55963
v  nu_tilda           4.3988e-007       0.0045312       0.0017856       0.0017856
v  TempC                       21          73.077          22.056          22.056
v  TurbVisc           3.2936e-014       0.0053403       0.0020993       0.0020993
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2824:        0.22150E+01

===============================================================


 INSTANT    0.282500000E+04   TIME STEP NUMBER            2825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10832E-01 0.88955E+00
   Friction velocity        uk    :  0.10832E-01 0.88955E+00
   Dimensionless distance   yplus :  0.87202E-01 0.71615E+01
   Friction thermal sca.    tstar : -0.59072E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65062E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10511E-01      33   0.19858E-03   0.40948E+01 0.18922E+03 
c  Velocity[X]                                      0.19834E+01 
c  Velocity[Y]                                      0.21114E+01 
c  Velocity[Z]                                      0.93926E-30 
c  Pressure     0.87580E-07     521   0.90060E-08   0.84267E-01 0.19161E+04 
c  nu_tilda     0.84751E-05      33   0.24990E-05   0.73192E-06 0.21382E+03 
c  TempC        0.43994E+02      27   0.33986E-03   0.35293E+01 0.22624E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3375          9.0025          4.5729          4.5729
v  Velocity[Y]            -2.7158          7.1856         0.23184         0.23184
v  Velocity[Z]       -1.0638e-014     8.7037e-015    -1.4704e-017    -1.4704e-017
v  ǁVelocityǁ         0.0032104          9.0027          5.0319          5.0319
v  Pressure                -26.35          26.151        -0.47729        -0.47729
v  nu_tilda           4.3983e-007       0.0045315       0.0017856       0.0017856
v  TempC                       21          73.078          22.056          22.056
v  TurbVisc           3.2938e-014       0.0053405       0.0020992       0.0020992
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2825:        0.21940E+01

===============================================================


 INSTANT    0.282600000E+04   TIME STEP NUMBER            2826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17787E-01 0.89074E+00
   Friction velocity        uk    :  0.17787E-01 0.89074E+00
   Dimensionless distance   yplus :  0.14320E+00 0.71711E+01
   Friction thermal sca.    tstar : -0.57963E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10684E+00 0.53504E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10510E-01      33   0.24014E-03   0.40749E+01 0.18916E+03 
c  Velocity[X]                                      0.19479E+01 
c  Velocity[Y]                                      0.21269E+01 
c  Velocity[Z]                                      0.92840E-30 
c  Pressure     0.89411E-07     474   0.90956E-08   0.86439E-01 0.12724E+04 
c  nu_tilda     0.84752E-05      33   0.12765E-04   0.73208E-06 0.21384E+03 
c  TempC        0.43993E+02      27   0.27272E-03   0.52549E+01 0.24885E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3373          9.0027          4.5729          4.5729
v  Velocity[Y]            -2.7147           7.192         0.23172         0.23172
v  Velocity[Z]       -1.0884e-014     8.7296e-015    -1.4704e-017    -1.4704e-017
v  ǁVelocityǁ         0.0034089           9.003           5.032           5.032
v  Pressure               -26.427          26.051        -0.54693        -0.54693
v  nu_tilda           4.3978e-007       0.0045317       0.0017854       0.0017854
v  TempC                       21          73.078          22.056          22.056
v  TurbVisc           3.2925e-014       0.0053408       0.0020992       0.0020992
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2826:        0.20710E+01

===============================================================


 INSTANT    0.282700000E+04   TIME STEP NUMBER            2827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16652E-01 0.89031E+00
   Friction velocity        uk    :  0.16652E-01 0.89031E+00
   Dimensionless distance   yplus :  0.13406E+00 0.71676E+01
   Friction thermal sca.    tstar : -0.57793E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10002E+00 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10509E-01      33   0.24560E-03   0.40925E+01 0.18911E+03 
c  Velocity[X]                                      0.19817E+01 
c  Velocity[Y]                                      0.21108E+01 
c  Velocity[Z]                                      0.93297E-30 
c  Pressure     0.11687E-06     456   0.99939E-08   0.11238E+00 0.55073E+03 
c  nu_tilda     0.84754E-05      33   0.24979E-05   0.73219E-06 0.21385E+03 
c  TempC        0.43993E+02      27   0.29634E-03   0.42242E+01 0.22206E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3371           9.003          4.5729          4.5729
v  Velocity[Y]            -2.7137          7.1618         0.23159         0.23159
v  Velocity[Z]       -1.0583e-014     8.7153e-015      -1.47e-017      -1.47e-017
v  ǁVelocityǁ         0.0016937          9.0032           5.032           5.032
v  Pressure               -26.365          25.989        -0.52651        -0.52651
v  nu_tilda           4.3984e-007       0.0045319       0.0017855       0.0017855
v  TempC                       21          73.079          22.056          22.056
v  TurbVisc           3.2908e-014       0.0053411       0.0020991       0.0020991
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2827:        0.20380E+01

===============================================================


 INSTANT    0.282800000E+04   TIME STEP NUMBER            2828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10075E-01 0.88907E+00
   Friction velocity        uk    :  0.10075E-01 0.88907E+00
   Dimensionless distance   yplus :  0.81112E-01 0.71576E+01
   Friction thermal sca.    tstar : -0.58656E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60519E-01 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10507E-01      33   0.24980E-03   0.40961E+01 0.18917E+03 
c  Velocity[X]                                      0.19920E+01 
c  Velocity[Y]                                      0.21041E+01 
c  Velocity[Z]                                      0.82774E-30 
c  Pressure     0.10720E-06     474   0.92962E-08   0.10333E+00 0.79336E+03 
c  nu_tilda     0.84755E-05      33   0.12762E-04   0.73234E-06 0.21386E+03 
c  TempC        0.43992E+02      27   0.30011E-03   0.50293E+01 0.25410E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3369          9.0032          4.5729          4.5729
v  Velocity[Y]            -2.7127          7.1824         0.23146         0.23146
v  Velocity[Z]       -1.0867e-014      8.738e-015    -1.4702e-017    -1.4702e-017
v  ǁVelocityǁ         0.0032286          9.0034          5.0321          5.0321
v  Pressure               -26.445          26.012        -0.57147        -0.57147
v  nu_tilda           4.3987e-007       0.0045321       0.0017853       0.0017853
v  TempC                       21           73.08          22.055          22.055
v  TurbVisc           3.2926e-014       0.0053413        0.002099        0.002099
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2828:        0.20740E+01

===============================================================


 INSTANT    0.282900000E+04   TIME STEP NUMBER            2829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18092E-01 0.89025E+00
   Friction velocity        uk    :  0.18092E-01 0.89025E+00
   Dimensionless distance   yplus :  0.14565E+00 0.71671E+01
   Friction thermal sca.    tstar : -0.57620E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10867E+00 0.53475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10506E-01      33   0.24222E-03   0.40903E+01 0.18912E+03 
c  Velocity[X]                                      0.19712E+01 
c  Velocity[Y]                                      0.21191E+01 
c  Velocity[Z]                                      0.11570E-29 
c  Pressure     0.10157E-06     441   0.90163E-08   0.99056E-01 0.54393E+03 
c  nu_tilda     0.84756E-05      33   0.25050E-05   0.73245E-06 0.21387E+03 
c  TempC        0.43992E+02      26   0.33258E-03   0.49896E+01 0.26186E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3367          9.0034          4.5729          4.5729
v  Velocity[Y]            -2.7117          7.1619         0.23133         0.23133
v  Velocity[Z]       -1.0546e-014     8.7235e-015    -1.4695e-017    -1.4695e-017
v  ǁVelocityǁ          0.002948          9.0037          5.0321          5.0321
v  Pressure               -26.384          25.985        -0.54507        -0.54507
v  nu_tilda           4.3993e-007       0.0045323       0.0017853       0.0017853
v  TempC                       21          73.081          22.055          22.055
v  TurbVisc           3.2936e-014       0.0053416       0.0020989       0.0020989
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2829:        0.19900E+01

===============================================================


 INSTANT    0.283000000E+04   TIME STEP NUMBER            2830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60233E-02 0.88938E+00
   Friction velocity        uk    :  0.60233E-02 0.88938E+00
   Dimensionless distance   yplus :  0.48491E-01 0.71601E+01
   Friction thermal sca.    tstar : -0.58631E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36180E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10505E-01      33   0.18223E-03   0.40690E+01 0.18898E+03 
c  Velocity[X]                                      0.19637E+01 
c  Velocity[Y]                                      0.21053E+01 
c  Velocity[Z]                                      0.10875E-29 
c  Pressure     0.10702E-06     521   0.95583E-08   0.10191E+00 0.89232E+03 
c  nu_tilda     0.84757E-05      33   0.12756E-04   0.73262E-06 0.21388E+03 
c  TempC        0.43991E+02      26   0.25966E-03   0.63984E+01 0.27661E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3366          9.0037          4.5729          4.5729
v  Velocity[Y]            -2.7107          7.1814          0.2312          0.2312
v  Velocity[Z]       -1.0857e-014       8.75e-015    -1.4693e-017    -1.4693e-017
v  ǁVelocityǁ         0.0031914          9.0039          5.0322          5.0322
v  Pressure               -26.464          25.965        -0.59733        -0.59733
v  nu_tilda           4.4001e-007       0.0045325       0.0017852       0.0017852
v  TempC                       21          73.081          22.055          22.055
v  TurbVisc           3.2953e-014       0.0053418       0.0020989       0.0020989
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2830:        0.21780E+01

===============================================================


 INSTANT    0.283100000E+04   TIME STEP NUMBER            2831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17593E-01 0.89109E+00
   Friction velocity        uk    :  0.17593E-01 0.89109E+00
   Dimensionless distance   yplus :  0.14164E+00 0.71739E+01
   Friction thermal sca.    tstar : -0.61996E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10568E+00 0.53525E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10503E-01      33   0.24724E-03   0.40655E+01 0.18892E+03 
c  Velocity[X]                                      0.19675E+01 
c  Velocity[Y]                                      0.20980E+01 
c  Velocity[Z]                                      0.87052E-30 
c  Pressure     0.10199E-06     506   0.92790E-08   0.98121E-01 0.11318E+04 
c  nu_tilda     0.84759E-05      33   0.25018E-05   0.73273E-06 0.21389E+03 
c  TempC        0.43991E+02      26   0.28220E-03   0.47421E+01 0.24410E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3364          9.0039          4.5729          4.5729
v  Velocity[Y]            -2.7096          7.1942         0.23106         0.23106
v  Velocity[Z]       -1.0582e-014      8.737e-015    -1.4682e-017    -1.4682e-017
v  ǁVelocityǁ          0.002786          9.0042          5.0322          5.0322
v  Pressure               -26.408          26.075        -0.54259        -0.54259
v  nu_tilda           4.4001e-007       0.0045328       0.0017852       0.0017852
v  TempC                       21          73.082          22.055          22.055
v  TurbVisc           3.2978e-014        0.005342       0.0020988       0.0020988
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2831:        0.21570E+01

===============================================================


 INSTANT    0.283200000E+04   TIME STEP NUMBER            2832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17301E-01 0.89059E+00
   Friction velocity        uk    :  0.17301E-01 0.89059E+00
   Dimensionless distance   yplus :  0.13929E+00 0.71698E+01
   Friction thermal sca.    tstar : -0.58756E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10392E+00 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10502E-01      33   0.24075E-03   0.40868E+01 0.18901E+03 
c  Velocity[X]                                      0.19735E+01 
c  Velocity[Y]                                      0.21133E+01 
c  Velocity[Z]                                      0.83423E-30 
c  Pressure     0.10339E-06     538   0.95629E-08   0.10106E+00 0.19211E+04 
c  nu_tilda     0.84760E-05      33   0.12751E-04   0.73291E-06 0.21391E+03 
c  TempC        0.43990E+02      27   0.35408E-03   0.50177E+01 0.24074E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3362          9.0042          4.5729          4.5729
v  Velocity[Y]            -2.7086          7.1651         0.23093         0.23093
v  Velocity[Z]       -1.0871e-014      8.761e-015    -1.4681e-017    -1.4681e-017
v  ǁVelocityǁ         0.0029971          9.0044          5.0323          5.0323
v  Pressure               -26.481          25.859        -0.63586        -0.63586
v  nu_tilda           4.4002e-007        0.004533       0.0017851       0.0017851
v  TempC                       21          73.083          22.055          22.055
v  TurbVisc           3.2979e-014       0.0053423       0.0020987       0.0020987
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2832:        0.22230E+01

===============================================================


 INSTANT    0.283300000E+04   TIME STEP NUMBER            2833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17065E-01 0.88923E+00
   Friction velocity        uk    :  0.17065E-01 0.88923E+00
   Dimensionless distance   yplus :  0.13738E+00 0.71589E+01
   Friction thermal sca.    tstar : -0.58794E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10250E+00 0.53414E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10501E-01      33   0.23662E-03   0.40641E+01 0.18883E+03 
c  Velocity[X]                                      0.19665E+01 
c  Velocity[Y]                                      0.20976E+01 
c  Velocity[Z]                                      0.88776E-30 
c  Pressure     0.90481E-07     521   0.95553E-08   0.86514E-01 0.13820E+04 
c  nu_tilda     0.84761E-05      33   0.25096E-05   0.73303E-06 0.21392E+03 
c  TempC        0.43989E+02      27   0.25160E-03   0.57187E+01 0.26191E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.336          9.0044          4.5729          4.5729
v  Velocity[Y]            -2.7076          7.1826          0.2308          0.2308
v  Velocity[Z]       -1.0582e-014     8.7503e-015    -1.4672e-017    -1.4672e-017
v  ǁVelocityǁ         0.0031576          9.0047          5.0323          5.0323
v  Pressure               -26.424          26.015        -0.57263        -0.57263
v  nu_tilda           4.4001e-007       0.0045332       0.0017851       0.0017851
v  TempC                       21          73.083          22.055          22.055
v  TurbVisc            3.298e-014       0.0053426       0.0020987       0.0020987
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2833:        0.22060E+01

===============================================================


 INSTANT    0.283400000E+04   TIME STEP NUMBER            2834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17548E-01 0.89022E+00
   Friction velocity        uk    :  0.17548E-01 0.89022E+00
   Dimensionless distance   yplus :  0.14127E+00 0.71669E+01
   Friction thermal sca.    tstar : -0.63089E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10540E+00 0.53473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10499E-01      33   0.28119E-03   0.40671E+01 0.18888E+03 
c  Velocity[X]                                      0.19760E+01 
c  Velocity[Y]                                      0.20911E+01 
c  Velocity[Z]                                      0.93807E-30 
c  Pressure     0.93946E-07     537   0.99634E-08   0.91488E-01 0.19081E+04 
c  nu_tilda     0.84762E-05      33   0.12746E-04   0.73318E-06 0.21393E+03 
c  TempC        0.43989E+02      27   0.22978E-03   0.41961E+01 0.22211E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3358          9.0046          4.5729          4.5729
v  Velocity[Y]            -2.7066          7.1605         0.23066         0.23066
v  Velocity[Z]       -1.0907e-014     8.7747e-015    -1.4668e-017    -1.4668e-017
v  ǁVelocityǁ         0.0020522          9.0049          5.0324          5.0324
v  Pressure               -26.498          25.804        -0.66558        -0.66558
v  nu_tilda           4.4004e-007       0.0045334        0.001785        0.001785
v  TempC                       21          73.084          22.055          22.055
v  TurbVisc           3.2978e-014       0.0053428       0.0020986       0.0020986
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2834:        0.25390E+01

===============================================================


 INSTANT    0.283500000E+04   TIME STEP NUMBER            2835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.99032E-02 0.88959E+00
   Friction velocity        uk    :  0.99032E-02 0.88959E+00
   Dimensionless distance   yplus :  0.79727E-01 0.71618E+01
   Friction thermal sca.    tstar : -0.61778E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.59486E-01 0.53435E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10498E-01      33   0.23535E-03   0.41037E+01 0.18901E+03 
c  Velocity[X]                                      0.19952E+01 
c  Velocity[Y]                                      0.21085E+01 
c  Velocity[Z]                                      0.93713E-30 
c  Pressure     0.11846E-06     552   0.98613E-08   0.11341E+00 0.19175E+04 
c  nu_tilda     0.84763E-05      33   0.25056E-05   0.73331E-06 0.21394E+03 
c  TempC        0.43988E+02      26   0.35056E-03   0.40980E+01 0.24066E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3356          9.0049          4.5729          4.5729
v  Velocity[Y]            -2.7055          7.1862         0.23053         0.23053
v  Velocity[Z]        -1.065e-014      8.762e-015     -1.466e-017     -1.466e-017
v  ǁVelocityǁ         0.0031924          9.0051          5.0324          5.0324
v  Pressure               -26.448          26.032        -0.58303        -0.58303
v  nu_tilda           4.4002e-007       0.0045336        0.001785        0.001785
v  TempC                       21          73.084          22.055          22.055
v  TurbVisc           3.2985e-014        0.005343       0.0020985       0.0020985
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2835:        0.23260E+01

===============================================================


 INSTANT    0.283600000E+04   TIME STEP NUMBER            2836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13658E-01 0.89079E+00
   Friction velocity        uk    :  0.13658E-01 0.89079E+00
   Dimensionless distance   yplus :  0.10996E+00 0.71715E+01
   Friction thermal sca.    tstar : -0.62472E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.82039E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10497E-01      33   0.21807E-03   0.40525E+01 0.18873E+03 
c  Velocity[X]                                      0.19618E+01 
c  Velocity[Y]                                      0.20907E+01 
c  Velocity[Z]                                      0.96884E-30 
c  Pressure     0.10243E-06     538   0.98437E-08   0.97133E-01 0.17487E+04 
c  nu_tilda     0.84764E-05      33   0.12740E-04   0.73347E-06 0.21395E+03 
c  TempC        0.43987E+02      26   0.31381E-03   0.69534E+01 0.30868E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3354          9.0051          4.5729          4.5729
v  Velocity[Y]            -2.7045          7.1873         0.23039         0.23039
v  Velocity[Z]       -1.0907e-014     8.7785e-015    -1.4657e-017    -1.4657e-017
v  ǁVelocityǁ          0.003197          9.0054          5.0325          5.0325
v  Pressure                -26.52          25.863        -0.67135        -0.67135
v  nu_tilda           4.3999e-007       0.0045338       0.0017848       0.0017848
v  TempC                       21          73.085          22.055          22.055
v  TurbVisc            3.298e-014       0.0053433       0.0020985       0.0020985
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2836:        0.22300E+01

===============================================================


 INSTANT    0.283700000E+04   TIME STEP NUMBER            2837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17955E-01 0.89058E+00
   Friction velocity        uk    :  0.17955E-01 0.89058E+00
   Dimensionless distance   yplus :  0.14455E+00 0.71698E+01
   Friction thermal sca.    tstar : -0.95900E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10785E+00 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10495E-01      33   0.23831E-03   0.40518E+01 0.18865E+03 
c  Velocity[X]                                      0.19710E+01 
c  Velocity[Y]                                      0.20808E+01 
c  Velocity[Z]                                      0.95614E-30 
c  Pressure     0.10658E-06     456   0.98207E-08   0.10468E+00 0.82029E+03 
c  nu_tilda     0.84765E-05      33   0.25113E-05   0.73358E-06 0.21396E+03 
c  TempC        0.43987E+02      26   0.29743E-03   0.52532E+01 0.25977E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3351          9.0053          4.5729          4.5729
v  Velocity[Y]            -2.7034          7.1644         0.23025         0.23025
v  Velocity[Z]       -1.0632e-014     8.7613e-015    -1.4647e-017    -1.4647e-017
v  ǁVelocityǁ         0.0029367          9.0056          5.0325          5.0325
v  Pressure               -26.463          25.896        -0.62797        -0.62797
v  nu_tilda           4.4002e-007        0.004534       0.0017849       0.0017849
v  TempC                       21          73.085          22.055          22.055
v  TurbVisc           3.2971e-014       0.0053435       0.0020984       0.0020984
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2837:        0.20470E+01

===============================================================


 INSTANT    0.283800000E+04   TIME STEP NUMBER            2838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16499E-01 0.88921E+00
   Friction velocity        uk    :  0.16499E-01 0.88921E+00
   Dimensionless distance   yplus :  0.13283E+00 0.71588E+01
   Friction thermal sca.    tstar : -0.70721E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99106E-01 0.53413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10494E-01      33   0.25833E-03   0.40508E+01 0.18868E+03 
c  Velocity[X]                                      0.19523E+01 
c  Velocity[Y]                                      0.20984E+01 
c  Velocity[Z]                                      0.94585E-30 
c  Pressure     0.94823E-07     490   0.93193E-08   0.91139E-01 0.99700E+03 
c  nu_tilda     0.84766E-05      33   0.12738E-04   0.73375E-06 0.21398E+03 
c  TempC        0.43986E+02      26   0.27386E-03   0.49411E+01 0.25307E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3349          9.0055          4.5729          4.5729
v  Velocity[Y]            -2.7024          7.1827         0.23012         0.23012
v  Velocity[Z]       -1.0933e-014      8.782e-015    -1.4649e-017    -1.4649e-017
v  ǁVelocityǁ         0.0019864          9.0058          5.0326          5.0326
v  Pressure               -26.538          25.863        -0.68593        -0.68593
v  nu_tilda           4.3998e-007       0.0045342       0.0017847       0.0017847
v  TempC                       21          73.085          22.055          22.055
v  TurbVisc           3.2981e-014       0.0053438       0.0020983       0.0020983
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2838:        0.21400E+01

===============================================================


 INSTANT    0.283900000E+04   TIME STEP NUMBER            2839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10939E-01 0.89033E+00
   Friction velocity        uk    :  0.10939E-01 0.89033E+00
   Dimensionless distance   yplus :  0.88064E-01 0.71678E+01
   Friction thermal sca.    tstar : -0.13695E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65706E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10493E-01      33   0.24554E-03   0.40790E+01 0.18871E+03 
c  Velocity[X]                                      0.19920E+01 
c  Velocity[Y]                                      0.20871E+01 
c  Velocity[Z]                                      0.91625E-30 
c  Pressure     0.13034E-06     457   0.99866E-08   0.12397E+00 0.53820E+03 
c  nu_tilda     0.84766E-05      33   0.25114E-05   0.73389E-06 0.21399E+03 
c  TempC        0.43985E+02      26   0.26937E-03   0.58738E+01 0.27883E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3346          9.0058          4.5729          4.5729
v  Velocity[Y]            -2.7014          7.1585         0.22998         0.22998
v  Velocity[Z]       -1.0715e-014     8.7673e-015    -1.4639e-017    -1.4639e-017
v  ǁVelocityǁ         0.0027674           9.006          5.0326          5.0326
v  Pressure               -26.478           25.81        -0.66314        -0.66314
v  nu_tilda           4.3996e-007       0.0045344       0.0017847       0.0017847
v  TempC                       21          73.086          22.055          22.055
v  TurbVisc           3.2969e-014        0.005344       0.0020982       0.0020982
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2839:        0.22530E+01

===============================================================


 INSTANT    0.284000000E+04   TIME STEP NUMBER            2840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.90367E-02 0.88986E+00
   Friction velocity        uk    :  0.90367E-02 0.88986E+00
   Dimensionless distance   yplus :  0.72751E-01 0.71640E+01
   Friction thermal sca.    tstar : -0.74477E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54281E-01 0.53451E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10491E-01      33   0.19446E-03   0.40645E+01 0.18865E+03 
c  Velocity[X]                                      0.19860E+01 
c  Velocity[Y]                                      0.20786E+01 
c  Velocity[Z]                                      0.83916E-30 
c  Pressure     0.98918E-07     473   0.91773E-08   0.95771E-01 0.73799E+03 
c  nu_tilda     0.84767E-05      33   0.12732E-04   0.73404E-06 0.21401E+03 
c  TempC        0.43985E+02      26   0.33704E-03   0.63089E+01 0.27020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3344           9.006          4.5729          4.5729
v  Velocity[Y]            -2.7004          7.1844         0.22984         0.22984
v  Velocity[Z]       -1.0917e-014     8.7949e-015    -1.4637e-017    -1.4637e-017
v  ǁVelocityǁ         0.0031484          9.0063          5.0327          5.0327
v  Pressure               -26.559           25.86        -0.70094        -0.70094
v  nu_tilda           4.3993e-007       0.0045346       0.0017846       0.0017846
v  TempC                       21          73.086          22.055          22.055
v  TurbVisc           3.2962e-014       0.0053442       0.0020982       0.0020982
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2840:        0.20630E+01

===============================================================


 INSTANT    0.284100000E+04   TIME STEP NUMBER            2841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57575E-02 0.89130E+00
   Friction velocity        uk    :  0.57575E-02 0.89130E+00
   Dimensionless distance   yplus :  0.46352E-01 0.71756E+01
   Friction thermal sca.    tstar : -0.10200E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34583E-01 0.53538E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10490E-01      33   0.22765E-03   0.40350E+01 0.18854E+03 
c  Velocity[X]                                      0.19406E+01 
c  Velocity[Y]                                      0.20944E+01 
c  Velocity[Z]                                      0.10379E-29 
c  Pressure     0.73406E-07     506   0.98494E-08   0.70781E-01 0.88213E+03 
c  nu_tilda     0.84768E-05      33   0.25135E-05   0.73416E-06 0.21402E+03 
c  TempC        0.43984E+02      26   0.28417E-03   0.61214E+01 0.29078E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3342          9.0062          4.5729          4.5729
v  Velocity[Y]            -2.6993           7.196          0.2297          0.2297
v  Velocity[Z]       -1.0689e-014     8.7879e-015    -1.4626e-017    -1.4626e-017
v  ǁVelocityǁ         0.0021131          9.0065          5.0327          5.0327
v  Pressure                 -26.5          25.929        -0.65614        -0.65614
v  nu_tilda           4.3989e-007       0.0045347       0.0017846       0.0017846
v  TempC                       21          73.087          22.055          22.055
v  TurbVisc           3.2953e-014       0.0053445       0.0020981       0.0020981
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2841:        0.21580E+01

===============================================================


 INSTANT    0.284200000E+04   TIME STEP NUMBER            2842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14111E-01 0.89081E+00
   Friction velocity        uk    :  0.14111E-01 0.89081E+00
   Dimensionless distance   yplus :  0.11360E+00 0.71716E+01
   Friction thermal sca.    tstar : -0.15581E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84759E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10489E-01      33   0.24529E-03   0.40485E+01 0.18852E+03 
c  Velocity[X]                                      0.19696E+01 
c  Velocity[Y]                                      0.20789E+01 
c  Velocity[Z]                                      0.90598E-30 
c  Pressure     0.11108E-06     569   0.95395E-08   0.10731E+00 0.20028E+04 
c  nu_tilda     0.84768E-05      33   0.12727E-04   0.73433E-06 0.21403E+03 
c  TempC        0.43983E+02      26   0.26276E-03   0.62007E+01 0.27228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3339          9.0064          4.5729          4.5729
v  Velocity[Y]            -2.6983          7.1633         0.22956         0.22956
v  Velocity[Z]       -1.1065e-014     8.8977e-015    -1.4626e-017    -1.4626e-017
v  ǁVelocityǁ         0.0028873          9.0067          5.0328          5.0328
v  Pressure               -26.573          25.697        -0.75176        -0.75176
v  nu_tilda           4.3993e-007       0.0045349       0.0017845       0.0017845
v  TempC                       21          73.088          22.055          22.055
v  TurbVisc            3.294e-014       0.0053447        0.002098        0.002098
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2842:        0.23100E+01

===============================================================


 INSTANT    0.284300000E+04   TIME STEP NUMBER            2843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10000E-01 0.88957E+00
   Friction velocity        uk    :  0.10000E-01 0.88957E+00
   Dimensionless distance   yplus :  0.80509E-01 0.71616E+01
   Friction thermal sca.    tstar : -0.24178E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60068E-01 0.53434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10487E-01      33   0.26882E-03   0.40626E+01 0.18856E+03 
c  Velocity[X]                                      0.19918E+01 
c  Velocity[Y]                                      0.20708E+01 
c  Velocity[Z]                                      0.94770E-30 
c  Pressure     0.10710E-06     554   0.92526E-08   0.10252E+00 0.17493E+04 
c  nu_tilda     0.84769E-05      33   0.25167E-05   0.73447E-06 0.21404E+03 
c  TempC        0.43982E+02      26   0.31266E-03   0.41648E+01 0.23520E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3337          9.0067          4.5729          4.5729
v  Velocity[Y]            -2.6973          7.1869         0.22941         0.22941
v  Velocity[Z]       -1.0767e-014     8.9298e-015    -1.4618e-017    -1.4618e-017
v  ǁVelocityǁ         0.0031166          9.0069          5.0328          5.0328
v  Pressure               -26.517          25.906        -0.67445        -0.67445
v  nu_tilda           4.3993e-007       0.0045352       0.0017845       0.0017845
v  TempC                       21          73.089          22.055          22.055
v  TurbVisc           3.2954e-014       0.0053449       0.0020979       0.0020979
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2843:        0.22700E+01

===============================================================


 INSTANT    0.284400000E+04   TIME STEP NUMBER            2844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17390E-01 0.89054E+00
   Friction velocity        uk    :  0.17390E-01 0.89054E+00
   Dimensionless distance   yplus :  0.14000E+00 0.71695E+01
   Friction thermal sca.    tstar : -0.11208E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10445E+00 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10486E-01      33   0.24699E-03   0.40518E+01 0.18853E+03 
c  Velocity[X]                                      0.19646E+01 
c  Velocity[Y]                                      0.20871E+01 
c  Velocity[Z]                                      0.93038E-30 
c  Pressure     0.98170E-07     552   0.93793E-08   0.95392E-01 0.19987E+04 
c  nu_tilda     0.84770E-05      33   0.12722E-04   0.73464E-06 0.21406E+03 
c  TempC        0.43982E+02      26   0.29145E-03   0.52125E+01 0.26773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3335          9.0069          4.5729          4.5729
v  Velocity[Y]            -2.6963           7.163         0.22927         0.22927
v  Velocity[Z]       -1.0998e-014     9.0558e-015    -1.4612e-017    -1.4612e-017
v  ǁVelocityǁ         0.0028793          9.0071          5.0329          5.0329
v  Pressure                -26.59          25.686        -0.77115        -0.77115
v  nu_tilda           4.3993e-007       0.0045354       0.0017843       0.0017843
v  TempC                       21           73.09          22.055          22.055
v  TurbVisc           3.2953e-014       0.0053452       0.0020979       0.0020979
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2844:        0.22990E+01

===============================================================


 INSTANT    0.284500000E+04   TIME STEP NUMBER            2845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10868E-01 0.88969E+00
   Friction velocity        uk    :  0.10868E-01 0.88969E+00
   Dimensionless distance   yplus :  0.87495E-01 0.71626E+01
   Friction thermal sca.    tstar : -0.12800E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65281E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10485E-01      33   0.24761E-03   0.40434E+01 0.18837E+03 
c  Velocity[X]                                      0.19698E+01 
c  Velocity[Y]                                      0.20736E+01 
c  Velocity[Z]                                      0.86458E-30 
c  Pressure     0.10698E-06     537   0.99711E-08   0.10173E+00 0.17827E+04 
c  nu_tilda     0.84770E-05      33   0.25174E-05   0.73477E-06 0.21407E+03 
c  TempC        0.43981E+02      26   0.32381E-03   0.65469E+01 0.27579E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3332          9.0071          4.5729          4.5729
v  Velocity[Y]            -2.6952          7.1844         0.22913         0.22913
v  Velocity[Z]       -1.0429e-014     9.1159e-015    -1.4599e-017    -1.4599e-017
v  ǁVelocityǁ         0.0016532          9.0073           5.033           5.033
v  Pressure               -26.537           25.89        -0.69235        -0.69235
v  nu_tilda           4.3995e-007       0.0045355       0.0017843       0.0017843
v  TempC                       21           73.09          22.054          22.054
v  TurbVisc           3.2954e-014       0.0053454       0.0020978       0.0020978
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2845:        0.22680E+01

===============================================================


 INSTANT    0.284600000E+04   TIME STEP NUMBER            2846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10588E-01 0.89097E+00
   Friction velocity        uk    :  0.10588E-01 0.89097E+00
   Dimensionless distance   yplus :  0.85239E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.10515E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.63598E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10483E-01      33   0.24618E-03   0.40252E+01 0.18828E+03 
c  Velocity[X]                                      0.19624E+01 
c  Velocity[Y]                                      0.20628E+01 
c  Velocity[Z]                                      0.92406E-30 
c  Pressure     0.85969E-07     520   0.99694E-08   0.83096E-01 0.14745E+04 
c  nu_tilda     0.84770E-05      33   0.12716E-04   0.73495E-06 0.21409E+03 
c  TempC        0.43980E+02      27   0.25367E-03   0.53534E+01 0.25128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.333          9.0073          4.5729          4.5729
v  Velocity[Y]            -2.6942          7.1935         0.22898         0.22898
v  Velocity[Z]       -1.0869e-014     9.2554e-015    -1.4594e-017    -1.4594e-017
v  ǁVelocityǁ         0.0032832          9.0075           5.033           5.033
v  Pressure                -26.61          25.768        -0.77069        -0.77069
v  nu_tilda           4.3991e-007       0.0045357       0.0017842       0.0017842
v  TempC                       21          73.091          22.054          22.054
v  TurbVisc           3.2958e-014       0.0053456       0.0020977       0.0020977
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2846:        0.22740E+01

===============================================================


 INSTANT    0.284700000E+04   TIME STEP NUMBER            2847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.18331E-01 0.89059E+00
   Friction velocity        uk    :  0.18331E-01 0.89059E+00
   Dimensionless distance   yplus :  0.14758E+00 0.71698E+01
   Friction thermal sca.    tstar : -0.10372E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.11011E+00 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10482E-01      33   0.23649E-03   0.40458E+01 0.18835E+03 
c  Velocity[X]                                      0.19668E+01 
c  Velocity[Y]                                      0.20790E+01 
c  Velocity[Z]                                      0.95318E-30 
c  Pressure     0.11310E-06     472   0.99541E-08   0.11012E+00 0.74498E+03 
c  nu_tilda     0.84771E-05      33   0.25235E-05   0.73507E-06 0.21410E+03 
c  TempC        0.43979E+02      27   0.26597E-03   0.32693E+01 0.21768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3327          9.0075          4.5729          4.5729
v  Velocity[Y]            -2.6931          7.1667         0.22884         0.22884
v  Velocity[Z]       -1.0485e-014     9.2851e-015    -1.4582e-017    -1.4582e-017
v  ǁVelocityǁ         0.0029549          9.0078          5.0331          5.0331
v  Pressure               -26.551          25.781        -0.73033        -0.73033
v  nu_tilda           4.3989e-007       0.0045359       0.0017842       0.0017842
v  TempC                       21          73.092          22.054          22.054
v  TurbVisc           3.2946e-014       0.0053458       0.0020976       0.0020976
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2847:        0.20810E+01

===============================================================


 INSTANT    0.284800000E+04   TIME STEP NUMBER            2848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14608E-01 0.88907E+00
   Friction velocity        uk    :  0.14608E-01 0.88907E+00
   Dimensionless distance   yplus :  0.11760E+00 0.71577E+01
   Friction thermal sca.    tstar : -0.11595E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87744E-01 0.53404E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10481E-01      33   0.25126E-03   0.40221E+01 0.18824E+03 
c  Velocity[X]                                      0.19567E+01 
c  Velocity[Y]                                      0.20654E+01 
c  Velocity[Z]                                      0.99190E-30 
c  Pressure     0.10003E-06     536   0.93334E-08   0.94931E-01 0.11338E+04 
c  nu_tilda     0.84771E-05      33   0.12713E-04   0.73522E-06 0.21411E+03 
c  TempC        0.43979E+02      26   0.32586E-03   0.46015E+01 0.25546E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3325          9.0078          4.5729          4.5729
v  Velocity[Y]            -2.6921          7.1816         0.22869         0.22869
v  Velocity[Z]       -1.0618e-014     9.4526e-015    -1.4575e-017    -1.4575e-017
v  ǁVelocityǁ         0.0025415           9.008          5.0331          5.0331
v  Pressure               -26.626           25.72        -0.79472        -0.79472
v  nu_tilda           4.3991e-007       0.0045361       0.0017841       0.0017841
v  TempC                       21          73.093          22.054          22.054
v  TurbVisc           3.2942e-014        0.005346       0.0020976       0.0020976
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2848:        0.22180E+01

===============================================================


 INSTANT    0.284900000E+04   TIME STEP NUMBER            2849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14804E-01 0.89039E+00
   Friction velocity        uk    :  0.14804E-01 0.89039E+00
   Dimensionless distance   yplus :  0.11919E+00 0.71683E+01
   Friction thermal sca.    tstar : -0.12647E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88925E-01 0.53483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10479E-01      33   0.25527E-03   0.40477E+01 0.18831E+03 
c  Velocity[X]                                      0.19896E+01 
c  Velocity[Y]                                      0.20581E+01 
c  Velocity[Z]                                      0.10750E-29 
c  Pressure     0.11397E-06     490   0.96487E-08   0.11136E+00 0.82468E+03 
c  nu_tilda     0.84771E-05      33   0.25218E-05   0.73535E-06 0.21413E+03 
c  TempC        0.43978E+02      26   0.31287E-03   0.61004E+01 0.28648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3322           9.008          4.5729          4.5729
v  Velocity[Y]            -2.6911          7.1638         0.22854         0.22854
v  Velocity[Z]       -1.0102e-014     9.5038e-015    -1.4562e-017    -1.4562e-017
v  ǁVelocityǁ         0.0029119          9.0082          5.0332          5.0332
v  Pressure               -26.569          25.757        -0.75141        -0.75141
v  nu_tilda           4.3991e-007       0.0045363       0.0017841       0.0017841
v  TempC                       21          73.094          22.054          22.054
v  TurbVisc           3.2946e-014       0.0053462       0.0020975       0.0020975
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2849:        0.21120E+01

===============================================================


 INSTANT    0.285000000E+04   TIME STEP NUMBER            2850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52115E-02 0.88953E+00
   Friction velocity        uk    :  0.52115E-02 0.88953E+00
   Dimensionless distance   yplus :  0.41956E-01 0.71613E+01
   Friction thermal sca.    tstar : -0.14752E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31304E-01 0.53432E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10478E-01      33   0.18813E-03   0.40320E+01 0.18821E+03 
c  Velocity[X]                                      0.19600E+01 
c  Velocity[Y]                                      0.20721E+01 
c  Velocity[Z]                                      0.97157E-30 
c  Pressure     0.10529E-06     538   0.94818E-08   0.10157E+00 0.97884E+03 
c  nu_tilda     0.84772E-05      33   0.12707E-04   0.73555E-06 0.21415E+03 
c  TempC        0.43977E+02      26   0.24560E-03   0.54127E+01 0.25554E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3319          9.0082          4.5729          4.5729
v  Velocity[Y]            -2.6901          7.1865         0.22839         0.22839
v  Velocity[Z]       -1.0408e-014     9.6691e-015    -1.4557e-017    -1.4557e-017
v  ǁVelocityǁ         0.0032321          9.0084          5.0332          5.0332
v  Pressure               -26.646           25.73        -0.80866        -0.80866
v  nu_tilda           4.3987e-007       0.0045365       0.0017839       0.0017839
v  TempC                       21          73.095          22.054          22.054
v  TurbVisc           3.2947e-014       0.0053465       0.0020974       0.0020974
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2850:        0.22310E+01

===============================================================


 INSTANT    0.285100000E+04   TIME STEP NUMBER            2851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.24916E-02 0.89097E+00
   Friction velocity        uk    :  0.24916E-02 0.89097E+00
   Dimensionless distance   yplus :  0.20059E-01 0.71729E+01
   Friction thermal sca.    tstar : -0.15746E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.14966E-01 0.53518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10476E-01      33   0.24260E-03   0.40041E+01 0.18799E+03 
c  Velocity[X]                                      0.19484E+01 
c  Velocity[Y]                                      0.20557E+01 
c  Velocity[Z]                                      0.94597E-30 
c  Pressure     0.11051E-06     506   0.94305E-08   0.10491E+00 0.10160E+04 
c  nu_tilda     0.84772E-05      33   0.25298E-05   0.73568E-06 0.21416E+03 
c  TempC        0.43976E+02      27   0.32080E-03   0.36758E+01 0.22737E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3316          9.0084          4.5729          4.5729
v  Velocity[Y]             -2.689          7.1927         0.22824         0.22824
v  Velocity[Z]         -9.86e-015     9.7127e-015    -1.4542e-017    -1.4542e-017
v  ǁVelocityǁ         0.0032057          9.0086          5.0333          5.0333
v  Pressure               -26.587          25.808        -0.75678        -0.75678
v  nu_tilda           4.3982e-007       0.0045367       0.0017839       0.0017839
v  TempC                       21          73.096          22.054          22.054
v  TurbVisc           3.2935e-014       0.0053467       0.0020973       0.0020973
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2851:        0.21640E+01

===============================================================


 INSTANT    0.285200000E+04   TIME STEP NUMBER            2852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12288E-01 0.89065E+00
   Friction velocity        uk    :  0.12288E-01 0.89065E+00
   Dimensionless distance   yplus :  0.98929E-01 0.71704E+01
   Friction thermal sca.    tstar : -0.21366E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73812E-01 0.53499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10475E-01      33   0.23799E-03   0.40421E+01 0.18817E+03 
c  Velocity[X]                                      0.19908E+01 
c  Velocity[Y]                                      0.20513E+01 
c  Velocity[Z]                                      0.95184E-30 
c  Pressure     0.10010E-06     538   0.93385E-08   0.97914E-01 0.19660E+04 
c  nu_tilda     0.84772E-05      33   0.12703E-04   0.73583E-06 0.21417E+03 
c  TempC        0.43975E+02      26   0.28515E-03   0.64925E+01 0.28547E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3313          9.0086          4.5729          4.5729
v  Velocity[Y]             -2.688          7.1658         0.22809         0.22809
v  Velocity[Z]       -9.7804e-015     9.9318e-015    -1.4535e-017    -1.4535e-017
v  ǁVelocityǁ         0.0021108          9.0088          5.0333          5.0333
v  Pressure               -26.657          25.594        -0.85185        -0.85185
v  nu_tilda           4.3987e-007       0.0045368       0.0017838       0.0017838
v  TempC                       21          73.096          22.054          22.054
v  TurbVisc           3.2921e-014       0.0053469       0.0020972       0.0020972
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2852:        0.22190E+01

===============================================================


 INSTANT    0.285300000E+04   TIME STEP NUMBER            2853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.46234E-02 0.88928E+00
   Friction velocity        uk    :  0.46234E-02 0.88928E+00
   Dimensionless distance   yplus :  0.37222E-01 0.71593E+01
   Friction thermal sca.    tstar : -0.56782E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.27772E-01 0.53416E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10474E-01      33   0.23486E-03   0.40149E+01 0.18804E+03 
c  Velocity[X]                                      0.19503E+01 
c  Velocity[Y]                                      0.20646E+01 
c  Velocity[Z]                                      0.95043E-30 
c  Pressure     0.83655E-07     554   0.95156E-08   0.80401E-01 0.17794E+04 
c  nu_tilda     0.84772E-05      33   0.25273E-05   0.73595E-06 0.21418E+03 
c  TempC        0.43974E+02      26   0.28663E-03   0.51412E+01 0.25171E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.331          9.0088          4.5729          4.5729
v  Velocity[Y]            -2.6869          7.1861         0.22794         0.22794
v  Velocity[Z]       -9.3234e-015     9.9438e-015    -1.4518e-017    -1.4518e-017
v  ǁVelocityǁ         0.0031985          9.0091          5.0334          5.0334
v  Pressure               -26.603          25.803        -0.77313        -0.77313
v  nu_tilda           4.3985e-007        0.004537       0.0017838       0.0017838
v  TempC                       21          73.095          22.054          22.054
v  TurbVisc           3.2935e-014       0.0053471       0.0020972       0.0020972
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2853:        0.22700E+01

===============================================================


 INSTANT    0.285400000E+04   TIME STEP NUMBER            2854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10051E-01 0.89011E+00
   Friction velocity        uk    :  0.10051E-01 0.89011E+00
   Dimensionless distance   yplus :  0.80917E-01 0.71660E+01
   Friction thermal sca.    tstar : -0.26118E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.60373E-01 0.53466E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10472E-01      33   0.25738E-03   0.40171E+01 0.18802E+03 
c  Velocity[X]                                      0.19623E+01 
c  Velocity[Y]                                      0.20548E+01 
c  Velocity[Z]                                      0.10409E-29 
c  Pressure     0.11062E-06     537   0.90568E-08   0.10668E+00 0.20683E+04 
c  nu_tilda     0.84772E-05      33   0.12697E-04   0.73615E-06 0.21420E+03 
c  TempC        0.43974E+02      27   0.27577E-03   0.43796E+01 0.23059E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3308           9.009          4.5729          4.5729
v  Velocity[Y]            -2.6859          7.1586         0.22779         0.22779
v  Velocity[Z]       -9.3074e-015     1.0199e-014    -1.4507e-017    -1.4507e-017
v  ǁVelocityǁ         0.0028735          9.0093          5.0335          5.0335
v  Pressure               -26.678          25.561        -0.87215        -0.87215
v  nu_tilda           4.3985e-007       0.0045372       0.0017837       0.0017837
v  TempC                       21          73.093          22.054          22.054
v  TurbVisc            3.293e-014       0.0053473       0.0020971       0.0020971
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2854:        0.22290E+01

===============================================================


 INSTANT    0.285500000E+04   TIME STEP NUMBER            2855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.47134E-02 0.88955E+00
   Friction velocity        uk    :  0.47134E-02 0.88955E+00
   Dimensionless distance   yplus :  0.37946E-01 0.71615E+01
   Friction thermal sca.    tstar : -0.25048E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.28312E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10471E-01      33   0.20546E-03   0.40279E+01 0.18801E+03 
c  Velocity[X]                                      0.19848E+01 
c  Velocity[Y]                                      0.20431E+01 
c  Velocity[Z]                                      0.93971E-30 
c  Pressure     0.10921E-06     538   0.99985E-08   0.10427E+00 0.17355E+04 
c  nu_tilda     0.84772E-05      33   0.25342E-05   0.73630E-06 0.21422E+03 
c  TempC        0.43973E+02      27   0.27284E-03   0.54634E+01 0.25772E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3305          9.0093          4.5729          4.5729
v  Velocity[Y]            -2.6849          7.1858         0.22764         0.22764
v  Velocity[Z]       -8.9047e-015     1.0219e-014    -1.4497e-017    -1.4497e-017
v  ǁVelocityǁ         0.0014436          9.0095          5.0335          5.0335
v  Pressure               -26.621          25.776        -0.79617        -0.79617
v  nu_tilda           4.3981e-007       0.0045374       0.0017837       0.0017837
v  TempC                       21           73.09          22.054          22.054
v  TurbVisc           3.2929e-014       0.0053475        0.002097        0.002097
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2855:        0.22340E+01

===============================================================


 INSTANT    0.285600000E+04   TIME STEP NUMBER            2856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.78581E-02 0.89081E+00
   Friction velocity        uk    :  0.78581E-02 0.89081E+00
   Dimensionless distance   yplus :  0.63263E-01 0.71716E+01
   Friction thermal sca.    tstar : -0.15514E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47201E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10469E-01      33   0.23777E-03   0.40002E+01 0.18790E+03 
c  Velocity[X]                                      0.19426E+01 
c  Velocity[Y]                                      0.20576E+01 
c  Velocity[Z]                                      0.10629E-29 
c  Pressure     0.93420E-07     553   0.92927E-08   0.89768E-01 0.12742E+04 
c  nu_tilda     0.84772E-05      33   0.12692E-04   0.73648E-06 0.21423E+03 
c  TempC        0.43972E+02      26   0.33876E-03   0.54673E+01 0.26769E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3302          9.0095          4.5729          4.5729
v  Velocity[Y]            -2.6839          7.1923         0.22748         0.22748
v  Velocity[Z]       -8.8359e-015     1.0496e-014    -1.4482e-017    -1.4482e-017
v  ǁVelocityǁ         0.0033171          9.0098          5.0336          5.0336
v  Pressure               -26.695          25.672        -0.86511        -0.86511
v  nu_tilda           4.3975e-007       0.0045375       0.0017835       0.0017835
v  TempC                       21          73.085          22.054          22.054
v  TurbVisc           3.2917e-014       0.0053477       0.0020969       0.0020969
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2856:        0.22520E+01

===============================================================


 INSTANT    0.285700000E+04   TIME STEP NUMBER            2857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10896E-01 0.89040E+00
   Friction velocity        uk    :  0.10896E-01 0.89040E+00
   Dimensionless distance   yplus :  0.87720E-01 0.71683E+01
   Friction thermal sca.    tstar : -0.14552E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65449E-01 0.53484E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10468E-01      33   0.23347E-03   0.40169E+01 0.18784E+03 
c  Velocity[X]                                      0.19741E+01 
c  Velocity[Y]                                      0.20428E+01 
c  Velocity[Z]                                      0.95940E-30 
c  Pressure     0.11499E-06     458   0.95967E-08   0.11056E+00 0.53513E+03 
c  nu_tilda     0.84772E-05      33   0.25327E-05   0.73660E-06 0.21425E+03 
c  TempC        0.43971E+02      26   0.26600E-03   0.58437E+01 0.28905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3299          9.0097          4.5729          4.5729
v  Velocity[Y]            -2.6828          7.1624         0.22733         0.22733
v  Velocity[Z]       -8.4251e-015     1.0503e-014    -1.4471e-017    -1.4471e-017
v  ǁVelocityǁ          0.002877            9.01          5.0336          5.0336
v  Pressure               -26.634          25.618        -0.84314        -0.84314
v  nu_tilda            4.398e-007       0.0045377       0.0017835       0.0017835
v  TempC                       21          73.082          22.054          22.054
v  TurbVisc           3.2899e-014        0.005348       0.0020968       0.0020968
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2857:        0.20300E+01

===============================================================


 INSTANT    0.285800000E+04   TIME STEP NUMBER            2858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54790E-02 0.88921E+00
   Friction velocity        uk    :  0.54790E-02 0.88921E+00
   Dimensionless distance   yplus :  0.44110E-01 0.71587E+01
   Friction thermal sca.    tstar : -0.11665E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32911E-01 0.53412E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10467E-01      33   0.23982E-03   0.40112E+01 0.18786E+03 
c  Velocity[X]                                      0.19726E+01 
c  Velocity[Y]                                      0.20386E+01 
c  Velocity[Z]                                      0.10168E-29 
c  Pressure     0.88312E-07     520   0.97453E-08   0.84919E-01 0.82858E+03 
c  nu_tilda     0.84771E-05      33   0.12690E-04   0.73677E-06 0.21426E+03 
c  TempC        0.43970E+02      26   0.24580E-03   0.45653E+01 0.23844E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3296            9.01          4.5729          4.5729
v  Velocity[Y]            -2.6817          7.1827         0.22717         0.22717
v  Velocity[Z]       -8.4234e-015     1.0809e-014    -1.4457e-017    -1.4457e-017
v  ǁVelocityǁ          0.003222          9.0103          5.0337          5.0337
v  Pressure               -26.711          25.629         -0.8915         -0.8915
v  nu_tilda           4.3986e-007       0.0045379       0.0017834       0.0017834
v  TempC                       21          73.078          22.054          22.054
v  TurbVisc           3.2914e-014       0.0053482       0.0020968       0.0020968
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2858:        0.21720E+01

===============================================================


 INSTANT    0.285900000E+04   TIME STEP NUMBER            2859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11111E-01 0.89030E+00
   Friction velocity        uk    :  0.11111E-01 0.89030E+00
   Dimensionless distance   yplus :  0.89448E-01 0.71675E+01
   Friction thermal sca.    tstar : -0.10936E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66738E-01 0.53478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10465E-01      33   0.24384E-03   0.40087E+01 0.18779E+03 
c  Velocity[X]                                      0.19576E+01 
c  Velocity[Y]                                      0.20511E+01 
c  Velocity[Z]                                      0.82158E-30 
c  Pressure     0.10975E-06     504   0.94011E-08   0.10654E+00 0.76100E+03 
c  nu_tilda     0.84771E-05      33   0.25404E-05   0.73691E-06 0.21428E+03 
c  TempC        0.43969E+02      27   0.39794E-03   0.29848E+01 0.21045E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3293          9.0102          4.5729          4.5729
v  Velocity[Y]            -2.6807          7.1626         0.22702         0.22702
v  Velocity[Z]       -8.1388e-015     1.0757e-014    -1.4445e-017    -1.4445e-017
v  ǁVelocityǁ           0.00279          9.0105          5.0337          5.0337
v  Pressure               -26.654          25.644        -0.85024        -0.85024
v  nu_tilda           4.3992e-007       0.0045381       0.0017834       0.0017834
v  TempC                       21          73.075          22.054          22.054
v  TurbVisc           3.2932e-014       0.0053484       0.0020967       0.0020967
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2859:        0.21520E+01

===============================================================


 INSTANT    0.286000000E+04   TIME STEP NUMBER            2860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14611E-01 0.88941E+00
   Friction velocity        uk    :  0.14611E-01 0.88941E+00
   Dimensionless distance   yplus :  0.11762E+00 0.71604E+01
   Friction thermal sca.    tstar : -0.10396E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87761E-01 0.53424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10464E-01      33   0.20679E-03   0.39927E+01 0.18769E+03 
c  Velocity[X]                                      0.19571E+01 
c  Velocity[Y]                                      0.20356E+01 
c  Velocity[Z]                                      0.97701E-30 
c  Pressure     0.10574E-06     522   0.94125E-08   0.10041E+00 0.12154E+04 
c  nu_tilda     0.84771E-05      33   0.12684E-04   0.73710E-06 0.21429E+03 
c  TempC        0.43968E+02      28   0.31291E-03   0.58496E+01 0.27101E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.329          9.0105          4.5729          4.5729
v  Velocity[Y]            -2.6797           7.182         0.22686         0.22686
v  Velocity[Z]       -8.1445e-015     1.1052e-014    -1.4435e-017    -1.4435e-017
v  ǁVelocityǁ         0.0030646          9.0108          5.0338          5.0338
v  Pressure               -26.726          25.567         -0.9178         -0.9178
v  nu_tilda           4.3997e-007       0.0045383       0.0017832       0.0017832
v  TempC                       21          73.073          22.054          22.054
v  TurbVisc            3.295e-014       0.0053486       0.0020966       0.0020966
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2860:        0.21950E+01

===============================================================


 INSTANT    0.286100000E+04   TIME STEP NUMBER            2861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.76467E-02 0.89111E+00
   Friction velocity        uk    :  0.76467E-02 0.89111E+00
   Dimensionless distance   yplus :  0.61561E-01 0.71741E+01
   Friction thermal sca.    tstar : -0.95982E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.45931E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10462E-01      33   0.25779E-03   0.39936E+01 0.18766E+03 
c  Velocity[X]                                      0.19668E+01 
c  Velocity[Y]                                      0.20267E+01 
c  Velocity[Z]                                      0.96957E-30 
c  Pressure     0.10486E-06     553   0.95552E-08   0.10114E+00 0.13647E+04 
c  nu_tilda     0.84771E-05      33   0.25365E-05   0.73725E-06 0.21431E+03 
c  TempC        0.43967E+02      27   0.29421E-03   0.37855E+01 0.22329E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3287          9.0107          4.5729          4.5729
v  Velocity[Y]            -2.6787          7.1949          0.2267          0.2267
v  Velocity[Z]       -8.1447e-015     1.0966e-014    -1.4419e-017    -1.4419e-017
v  ǁVelocityǁ         0.0032086           9.011          5.0338          5.0338
v  Pressure               -26.671          25.705         -0.8536         -0.8536
v  nu_tilda           4.3995e-007       0.0045385       0.0017833       0.0017833
v  TempC                       21          73.073          22.053          22.053
v  TurbVisc           3.2966e-014       0.0053488       0.0020965       0.0020965
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2861:        0.22660E+01

===============================================================


 INSTANT    0.286200000E+04   TIME STEP NUMBER            2862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13966E-01 0.89071E+00
   Friction velocity        uk    :  0.13966E-01 0.89071E+00
   Dimensionless distance   yplus :  0.11244E+00 0.71708E+01
   Friction thermal sca.    tstar : -0.89951E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83891E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10461E-01      33   0.23210E-03   0.40101E+01 0.18772E+03 
c  Velocity[X]                                      0.19662E+01 
c  Velocity[Y]                                      0.20440E+01 
c  Velocity[Z]                                      0.92591E-30 
c  Pressure     0.98970E-07     568   0.98551E-08   0.96363E-01 0.20062E+04 
c  nu_tilda     0.84770E-05      33   0.12679E-04   0.73743E-06 0.21433E+03 
c  TempC        0.43966E+02      27   0.23684E-03   0.44377E+01 0.23368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3284          9.0109          4.5729          4.5729
v  Velocity[Y]            -2.6776          7.1661         0.22654         0.22654
v  Velocity[Z]       -8.2193e-015     1.1202e-014    -1.4411e-017    -1.4411e-017
v  ǁVelocityǁ         0.0017256          9.0112          5.0339          5.0339
v  Pressure                -26.74          25.484        -0.94991        -0.94991
v  nu_tilda           4.3993e-007       0.0045386       0.0017831       0.0017831
v  TempC                       21          73.073          22.053          22.053
v  TurbVisc            3.296e-014       0.0053491       0.0020964       0.0020964
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2862:        0.24920E+01

===============================================================


 INSTANT    0.286300000E+04   TIME STEP NUMBER            2863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.82417E-02 0.88929E+00
   Friction velocity        uk    :  0.82417E-02 0.88929E+00
   Dimensionless distance   yplus :  0.66351E-01 0.71594E+01
   Friction thermal sca.    tstar : -0.85083E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49505E-01 0.53417E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10459E-01      33   0.23833E-03   0.39956E+01 0.18763E+03 
c  Velocity[X]                                      0.19596E+01 
c  Velocity[Y]                                      0.20359E+01 
c  Velocity[Z]                                      0.88880E-30 
c  Pressure     0.10578E-06     521   0.91112E-08   0.99656E-01 0.13923E+04 
c  nu_tilda     0.84770E-05      33   0.25452E-05   0.73756E-06 0.21434E+03 
c  TempC        0.43965E+02      26   0.23804E-03   0.36870E+01 0.22690E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3281          9.0112          4.5729          4.5729
v  Velocity[Y]            -2.6766          7.1828         0.22638         0.22638
v  Velocity[Z]       -8.2244e-015     1.1003e-014    -1.4396e-017    -1.4396e-017
v  ǁVelocityǁ         0.0030585          9.0115          5.0339          5.0339
v  Pressure               -26.685          25.635         -0.8859         -0.8859
v  nu_tilda           4.3994e-007       0.0045388       0.0017831       0.0017831
v  TempC                       21          73.073          22.053          22.053
v  TurbVisc           3.2953e-014       0.0053493       0.0020963       0.0020963
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2863:        0.24580E+01

===============================================================


 INSTANT    0.286400000E+04   TIME STEP NUMBER            2864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85958E-02 0.89043E+00
   Friction velocity        uk    :  0.85958E-02 0.89043E+00
   Dimensionless distance   yplus :  0.69202E-01 0.71685E+01
   Friction thermal sca.    tstar : -0.78668E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51633E-01 0.53485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10458E-01      33   0.25415E-03   0.40114E+01 0.18762E+03 
c  Velocity[X]                                      0.19889E+01 
c  Velocity[Y]                                      0.20225E+01 
c  Velocity[Z]                                      0.82384E-30 
c  Pressure     0.10564E-06     553   0.97012E-08   0.10316E+00 0.15520E+04 
c  nu_tilda     0.84769E-05      33   0.12676E-04   0.73774E-06 0.21436E+03 
c  TempC        0.43964E+02      26   0.30692E-03   0.38737E+01 0.22328E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3277          9.0114          4.5729          4.5729
v  Velocity[Y]            -2.6755          7.1607         0.22622         0.22622
v  Velocity[Z]       -8.2937e-015     1.1228e-014    -1.4386e-017    -1.4386e-017
v  ǁVelocityǁ         0.0028811          9.0117           5.034           5.034
v  Pressure                -26.76          25.473        -0.96507        -0.96507
v  nu_tilda           4.4003e-007        0.004539        0.001783        0.001783
v  TempC                       21          73.074          22.053          22.053
v  TurbVisc           3.2956e-014       0.0053495       0.0020963       0.0020963
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2864:        0.22610E+01

===============================================================


 INSTANT    0.286500000E+04   TIME STEP NUMBER            2865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11371E-01 0.88961E+00
   Friction velocity        uk    :  0.11371E-01 0.88961E+00
   Dimensionless distance   yplus :  0.91545E-01 0.71619E+01
   Friction thermal sca.    tstar : -0.79207E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68302E-01 0.53436E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10456E-01      33   0.23273E-03   0.39918E+01 0.18753E+03 
c  Velocity[X]                                      0.19558E+01 
c  Velocity[Y]                                      0.20360E+01 
c  Velocity[Z]                                      0.93822E-30 
c  Pressure     0.88362E-07     537   0.91294E-08   0.84721E-01 0.14930E+04 
c  nu_tilda     0.84769E-05      33   0.25409E-05   0.73789E-06 0.21437E+03 
c  TempC        0.43963E+02      26   0.30376E-03   0.72311E+01 0.30097E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3274          9.0116          4.5729          4.5729
v  Velocity[Y]            -2.6745          7.1863         0.22605         0.22605
v  Velocity[Z]       -8.3016e-015     1.0703e-014    -1.4373e-017    -1.4373e-017
v  ǁVelocityǁ          0.001415          9.0119           5.034           5.034
v  Pressure               -26.701          25.648        -0.89675        -0.89675
v  nu_tilda           4.4006e-007       0.0045392        0.001783        0.001783
v  TempC                       21          73.076          22.053          22.053
v  TurbVisc           3.2984e-014       0.0053497       0.0020962       0.0020962
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2865:        0.22340E+01

===============================================================


 INSTANT    0.286600000E+04   TIME STEP NUMBER            2866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.58746E-02 0.89077E+00
   Friction velocity        uk    :  0.58746E-02 0.89077E+00
   Dimensionless distance   yplus :  0.47295E-01 0.71713E+01
   Friction thermal sca.    tstar : -0.73735E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.35287E-01 0.53506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10455E-01      33   0.23428E-03   0.39596E+01 0.18737E+03 
c  Velocity[X]                                      0.19358E+01 
c  Velocity[Y]                                      0.20238E+01 
c  Velocity[Z]                                      0.10593E-29 
c  Pressure     0.10092E-06     538   0.93934E-08   0.96457E-01 0.13782E+04 
c  nu_tilda     0.84768E-05      33   0.12670E-04   0.73809E-06 0.21439E+03 
c  TempC        0.43962E+02      27   0.30754E-03   0.51122E+01 0.26592E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3271          9.0118          4.5729          4.5729
v  Velocity[Y]            -2.6735          7.1902         0.22589         0.22589
v  Velocity[Z]       -8.3692e-015      1.113e-014    -1.4362e-017    -1.4362e-017
v  ǁVelocityǁ         0.0029831          9.0121          5.0341          5.0341
v  Pressure               -26.774          25.523        -0.96967        -0.96967
v  nu_tilda           4.4003e-007       0.0045394       0.0017828       0.0017828
v  TempC                       21          73.078          22.053          22.053
v  TurbVisc           3.2993e-014         0.00535       0.0020961       0.0020961
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2866:        0.22220E+01

===============================================================


 INSTANT    0.286700000E+04   TIME STEP NUMBER            2867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.70095E-02 0.89052E+00
   Friction velocity        uk    :  0.70095E-02 0.89052E+00
   Dimensionless distance   yplus :  0.56431E-01 0.71693E+01
   Friction thermal sca.    tstar : -0.88510E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.42104E-01 0.53491E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10454E-01      33   0.27416E-03   0.39884E+01 0.18744E+03 
c  Velocity[X]                                      0.19724E+01 
c  Velocity[Y]                                      0.20160E+01 
c  Velocity[Z]                                      0.98229E-30 
c  Pressure     0.10961E-06     490   0.93678E-08   0.10619E+00 0.63705E+03 
c  nu_tilda     0.84767E-05      33   0.25473E-05   0.73823E-06 0.21441E+03 
c  TempC        0.43961E+02      27   0.27313E-03   0.50085E+01 0.26136E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3267          9.0121          4.5729          4.5729
v  Velocity[Y]            -2.6724          7.1645         0.22573         0.22573
v  Velocity[Z]       -8.3729e-015     1.0595e-014    -1.4356e-017    -1.4356e-017
v  ǁVelocityǁ         0.0028795          9.0124          5.0341          5.0341
v  Pressure               -26.714          25.524        -0.93543        -0.93543
v  nu_tilda           4.4007e-007       0.0045396       0.0017828       0.0017828
v  TempC                       21          73.079          22.053          22.053
v  TurbVisc           3.2983e-014       0.0053502        0.002096        0.002096
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2867:        0.21240E+01

===============================================================


 INSTANT    0.286800000E+04   TIME STEP NUMBER            2868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.92829E-02 0.88916E+00
   Friction velocity        uk    :  0.92829E-02 0.88916E+00
   Dimensionless distance   yplus :  0.74733E-01 0.71584E+01
   Friction thermal sca.    tstar : -0.69316E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55760E-01 0.53410E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10452E-01      33   0.24741E-03   0.40233E+01 0.18767E+03 
c  Velocity[X]                                      0.19851E+01 
c  Velocity[Y]                                      0.20382E+01 
c  Velocity[Z]                                      0.83736E-30 
c  Pressure     0.12210E-06     489   0.92749E-08   0.11717E+00 0.86477E+03 
c  nu_tilda     0.84767E-05      33   0.12669E-04   0.73841E-06 0.21442E+03 
c  TempC        0.43960E+02      26   0.23931E-03   0.54342E+01 0.27255E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3264          9.0123          4.5729          4.5729
v  Velocity[Y]            -2.6714           7.184         0.22556         0.22556
v  Velocity[Z]       -8.4364e-015     1.1104e-014    -1.4347e-017    -1.4347e-017
v  ǁVelocityǁ         0.0027402          9.0126          5.0342          5.0342
v  Pressure               -26.794          25.519        -0.98655        -0.98655
v  nu_tilda           4.4002e-007       0.0045398       0.0017827       0.0017827
v  TempC                       21          73.081          22.053          22.053
v  TurbVisc           3.2995e-014       0.0053504       0.0020959       0.0020959
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2868:        0.21130E+01

===============================================================


 INSTANT    0.286900000E+04   TIME STEP NUMBER            2869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.72308E-02 0.89037E+00
   Friction velocity        uk    :  0.72308E-02 0.89037E+00
   Dimensionless distance   yplus :  0.58213E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.85504E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43434E-01 0.53482E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10451E-01      33   0.22024E-03   0.39980E+01 0.18735E+03 
c  Velocity[X]                                      0.19840E+01 
c  Velocity[Y]                                      0.20141E+01 
c  Velocity[Z]                                      0.98894E-30 
c  Pressure     0.12272E-06     442   0.98704E-08   0.11801E+00 0.55224E+03 
c  nu_tilda     0.84766E-05      33   0.25466E-05   0.73856E-06 0.21444E+03 
c  TempC        0.43959E+02      26   0.35958E-03   0.49473E+01 0.25710E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3261          9.0125          4.5729          4.5729
v  Velocity[Y]            -2.6703          7.1593         0.22539         0.22539
v  Velocity[Z]       -8.4401e-015     1.0493e-014    -1.4337e-017    -1.4337e-017
v  ǁVelocityǁ         0.0027425          9.0128          5.0343          5.0343
v  Pressure                -26.73          25.467        -0.96351        -0.96351
v  nu_tilda           4.3998e-007         0.00454       0.0017827       0.0017827
v  TempC                       21          73.082          22.053          22.053
v  TurbVisc           3.2982e-014       0.0053506       0.0020958       0.0020958
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2869:        0.20060E+01

===============================================================


 INSTANT    0.287000000E+04   TIME STEP NUMBER            2870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.93617E-02 0.88973E+00
   Friction velocity        uk    :  0.93617E-02 0.88973E+00
   Dimensionless distance   yplus :  0.75368E-01 0.71629E+01
   Friction thermal sca.    tstar : -0.66148E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56233E-01 0.53443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10449E-01      33   0.19255E-03   0.39614E+01 0.18719E+03 
c  Velocity[X]                                      0.19559E+01 
c  Velocity[Y]                                      0.20055E+01 
c  Velocity[Z]                                      0.82192E-30 
c  Pressure     0.93953E-07     522   0.94391E-08   0.90641E-01 0.78018E+03 
c  nu_tilda     0.84765E-05      33   0.12663E-04   0.73875E-06 0.21446E+03 
c  TempC        0.43958E+02      27   0.26839E-03   0.79682E+01 0.30693E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3257          9.0127          4.5729          4.5729
v  Velocity[Y]            -2.6693          7.1845         0.22523         0.22523
v  Velocity[Z]       -8.5048e-015     1.1067e-014    -1.4321e-017    -1.4321e-017
v  ǁVelocityǁ         0.0027195           9.013          5.0343          5.0343
v  Pressure               -26.803          25.483         -1.0081         -1.0081
v  nu_tilda           4.3995e-007       0.0045402       0.0017825       0.0017825
v  TempC                       21          73.082          22.053          22.053
v  TurbVisc           3.2968e-014       0.0053508       0.0020957       0.0020957
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2870:        0.21860E+01

===============================================================


 INSTANT    0.287100000E+04   TIME STEP NUMBER            2871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.36101E-02 0.89124E+00
   Friction velocity        uk    :  0.36101E-02 0.89124E+00
   Dimensionless distance   yplus :  0.29064E-01 0.71751E+01
   Friction thermal sca.    tstar : -0.17087E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.21685E-01 0.53534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10448E-01      33   0.25921E-03   0.39515E+01 0.18715E+03 
c  Velocity[X]                                      0.19314E+01 
c  Velocity[Y]                                      0.20201E+01 
c  Velocity[Z]                                      0.86333E-30 
c  Pressure     0.96598E-07     537   0.94129E-08   0.92646E-01 0.12222E+04 
c  nu_tilda     0.84764E-05      33   0.25494E-05   0.73890E-06 0.21447E+03 
c  TempC        0.43957E+02      26   0.24201E-03   0.57080E+01 0.26550E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3254           9.013          4.5729          4.5729
v  Velocity[Y]            -2.6683          7.1955         0.22506         0.22506
v  Velocity[Z]       -8.5054e-015      1.045e-014    -1.4306e-017    -1.4306e-017
v  ǁVelocityǁ         0.0026543          9.0133          5.0344          5.0344
v  Pressure               -26.747          25.595        -0.94828        -0.94828
v  nu_tilda           4.3992e-007       0.0045404       0.0017825       0.0017825
v  TempC                       21          73.082          22.053          22.053
v  TurbVisc            3.296e-014       0.0053511       0.0020956       0.0020956
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2871:        0.22020E+01

===============================================================


 INSTANT    0.287200000E+04   TIME STEP NUMBER            2872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14556E-02 0.89079E+00
   Friction velocity        uk    :  0.14556E-02 0.89079E+00
   Dimensionless distance   yplus :  0.11719E-01 0.71715E+01
   Friction thermal sca.    tstar : -0.42404E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87436E-02 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10446E-01      33   0.23824E-03   0.39926E+01 0.18731E+03 
c  Velocity[X]                                      0.19819E+01 
c  Velocity[Y]                                      0.20107E+01 
c  Velocity[Z]                                      0.10605E-29 
c  Pressure     0.12554E-06     570   0.94122E-08   0.12007E+00 0.23167E+04 
c  nu_tilda     0.84763E-05      33   0.12658E-04   0.73908E-06 0.21449E+03 
c  TempC        0.43956E+02      27   0.31878E-03   0.47386E+01 0.24057E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.325          9.0132          4.5729          4.5729
v  Velocity[Y]            -2.6672          7.1634         0.22489         0.22489
v  Velocity[Z]       -8.5636e-015     1.1047e-014    -1.4296e-017    -1.4296e-017
v  ǁVelocityǁ         0.0023304          9.0135          5.0344          5.0344
v  Pressure               -26.815          25.319         -1.0552         -1.0552
v  nu_tilda           4.3996e-007       0.0045405       0.0017824       0.0017824
v  TempC                       21          73.082          22.053          22.053
v  TurbVisc           3.2951e-014       0.0053513       0.0020956       0.0020956
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2872:        0.22990E+01

===============================================================


 INSTANT    0.287300000E+04   TIME STEP NUMBER            2873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.82483E-02 0.88978E+00
   Friction velocity        uk    :  0.82483E-02 0.88978E+00
   Dimensionless distance   yplus :  0.66404E-01 0.71633E+01
   Friction thermal sca.    tstar : -0.59939E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.49545E-01 0.53446E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10445E-01      33   0.24473E-03   0.39772E+01 0.18725E+03 
c  Velocity[X]                                      0.19696E+01 
c  Velocity[Y]                                      0.20076E+01 
c  Velocity[Z]                                      0.89667E-30 
c  Pressure     0.97935E-07     537   0.95923E-08   0.94682E-01 0.21222E+04 
c  nu_tilda     0.84762E-05      33   0.25517E-05   0.73924E-06 0.21451E+03 
c  TempC        0.43955E+02      27   0.26358E-03   0.55746E+01 0.27976E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3247          9.0134          4.5729          4.5729
v  Velocity[Y]            -2.6662          7.1869         0.22472         0.22472
v  Velocity[Z]       -8.5628e-015     1.0366e-014    -1.4284e-017    -1.4284e-017
v  ǁVelocityǁ         0.0024599          9.0137          5.0345          5.0345
v  Pressure               -26.765          25.582        -0.96556        -0.96556
v  nu_tilda           4.3994e-007       0.0045407       0.0017824       0.0017824
v  TempC                       21          73.081          22.053          22.053
v  TurbVisc           3.2963e-014       0.0053515       0.0020955       0.0020955
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2873:        0.22200E+01

===============================================================


 INSTANT    0.287400000E+04   TIME STEP NUMBER            2874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.92735E-02 0.89059E+00
   Friction velocity        uk    :  0.92735E-02 0.89059E+00
   Dimensionless distance   yplus :  0.74658E-01 0.71699E+01
   Friction thermal sca.    tstar : -0.66399E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55703E-01 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10443E-01      33   0.24607E-03   0.39700E+01 0.18714E+03 
c  Velocity[X]                                      0.19552E+01 
c  Velocity[Y]                                      0.20148E+01 
c  Velocity[Z]                                      0.81802E-30 
c  Pressure     0.96848E-07     584   0.98265E-08   0.94172E-01 0.21958E+04 
c  nu_tilda     0.84761E-05      33   0.12654E-04   0.73944E-06 0.21453E+03 
c  TempC        0.43954E+02      26   0.30251E-03   0.52824E+01 0.24898E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3243          9.0136          4.5729          4.5729
v  Velocity[Y]            -2.6651          7.1641         0.22454         0.22454
v  Velocity[Z]       -8.6196e-015     1.1011e-014    -1.4267e-017    -1.4267e-017
v  ǁVelocityǁ         0.0024106          9.0139          5.0345          5.0345
v  Pressure               -26.832          25.335         -1.0688         -1.0688
v  nu_tilda           4.3993e-007       0.0045409       0.0017822       0.0017822
v  TempC                       21          73.081          22.053          22.053
v  TurbVisc           3.2957e-014       0.0053517       0.0020954       0.0020954
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2874:        0.23520E+01

===============================================================


 INSTANT    0.287500000E+04   TIME STEP NUMBER            2875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85685E-02 0.88978E+00
   Friction velocity        uk    :  0.85685E-02 0.88978E+00
   Dimensionless distance   yplus :  0.68983E-01 0.71633E+01
   Friction thermal sca.    tstar : -0.71896E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51469E-01 0.53446E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10442E-01      33   0.20606E-03   0.39643E+01 0.18702E+03 
c  Velocity[X]                                      0.19638E+01 
c  Velocity[Y]                                      0.20005E+01 
c  Velocity[Z]                                      0.82624E-30 
c  Pressure     0.11318E-06     538   0.98296E-08   0.10641E+00 0.15261E+04 
c  nu_tilda     0.84760E-05      33   0.25533E-05   0.73957E-06 0.21454E+03 
c  TempC        0.43953E+02      27   0.28051E-03   0.39123E+01 0.23801E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.324          9.0139          4.5729          4.5729
v  Velocity[Y]             -2.664           7.185         0.22437         0.22437
v  Velocity[Z]       -8.6163e-015     1.0328e-014     -1.425e-017     -1.425e-017
v  ǁVelocityǁ         0.0017582          9.0141          5.0346          5.0346
v  Pressure               -26.775          25.505        -0.99847        -0.99847
v  nu_tilda           4.3992e-007        0.004541       0.0017822       0.0017822
v  TempC                       21           73.08          22.053          22.053
v  TurbVisc           3.2953e-014       0.0053519       0.0020953       0.0020953
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2875:        0.22250E+01

===============================================================


 INSTANT    0.287600000E+04   TIME STEP NUMBER            2876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.78841E-02 0.89113E+00
   Friction velocity        uk    :  0.78841E-02 0.89113E+00
   Dimensionless distance   yplus :  0.63472E-01 0.71742E+01
   Friction thermal sca.    tstar : -0.77872E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.47358E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10440E-01      33   0.27147E-03   0.39683E+01 0.18706E+03 
c  Velocity[X]                                      0.19771E+01 
c  Velocity[Y]                                      0.19912E+01 
c  Velocity[Z]                                      0.85346E-30 
c  Pressure     0.10848E-06     505   0.96488E-08   0.10435E+00 0.10582E+04 
c  nu_tilda     0.84759E-05      33   0.12650E-04   0.73977E-06 0.21456E+03 
c  TempC        0.43952E+02      26   0.24329E-03   0.43496E+01 0.24284E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3236          9.0141          4.5729          4.5729
v  Velocity[Y]             -2.663          7.1928          0.2242          0.2242
v  Velocity[Z]       -8.6716e-015     1.0464e-014    -1.4233e-017    -1.4233e-017
v  ǁVelocityǁ         0.0023226          9.0143          5.0346          5.0346
v  Pressure               -26.848          25.435         -1.0577         -1.0577
v  nu_tilda           4.3988e-007       0.0045412       0.0017821       0.0017821
v  TempC                       21          73.079          22.053          22.053
v  TurbVisc           3.2949e-014       0.0053521       0.0020952       0.0020952
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2876:        0.21490E+01

===============================================================


 INSTANT    0.287700000E+04   TIME STEP NUMBER            2877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48376E-02 0.89070E+00
   Friction velocity        uk    :  0.48376E-02 0.89070E+00
   Dimensionless distance   yplus :  0.38946E-01 0.71707E+01
   Friction thermal sca.    tstar : -0.12707E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29058E-01 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10439E-01      33   0.23010E-03   0.39724E+01 0.18705E+03 
c  Velocity[X]                                      0.19626E+01 
c  Velocity[Y]                                      0.20098E+01 
c  Velocity[Z]                                      0.99973E-30 
c  Pressure     0.11005E-06     521   0.95836E-08   0.10732E+00 0.62095E+03 
c  nu_tilda     0.84758E-05      33   0.25584E-05   0.73994E-06 0.21458E+03 
c  TempC        0.43951E+02      27   0.34250E-03   0.37714E+01 0.23294E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3232          9.0143          4.5729          4.5729
v  Velocity[Y]             -2.662           7.167         0.22402         0.22402
v  Velocity[Z]       -8.6656e-015     1.0731e-014     -1.422e-017     -1.422e-017
v  ǁVelocityǁ         0.0022421          9.0146          5.0347          5.0347
v  Pressure               -26.787          25.425         -1.0245         -1.0245
v  nu_tilda           4.3988e-007       0.0045414       0.0017821       0.0017821
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc            3.294e-014       0.0053523       0.0020951       0.0020951
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2877:        0.21800E+01

===============================================================


 INSTANT    0.287800000E+04   TIME STEP NUMBER            2878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.77132E-02 0.88923E+00
   Friction velocity        uk    :  0.77132E-02 0.88923E+00
   Dimensionless distance   yplus :  0.62097E-01 0.71589E+01
   Friction thermal sca.    tstar : -0.75921E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46331E-01 0.53413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10437E-01      33   0.24976E-03   0.39515E+01 0.18696E+03 
c  Velocity[X]                                      0.19494E+01 
c  Velocity[Y]                                      0.20021E+01 
c  Velocity[Z]                                      0.90275E-30 
c  Pressure     0.10422E-06     521   0.98617E-08   0.99111E-01 0.10103E+04 
c  nu_tilda     0.84756E-05      33   0.12648E-04   0.74014E-06 0.21460E+03 
c  TempC        0.43949E+02      27   0.26994E-03   0.62177E+01 0.28655E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3228          9.0145          4.5729          4.5729
v  Velocity[Y]             -2.661          7.1823         0.22385         0.22385
v  Velocity[Z]       -8.7124e-015     1.0604e-014    -1.4204e-017    -1.4204e-017
v  ǁVelocityǁ         0.0015394          9.0148          5.0347          5.0347
v  Pressure               -26.863          25.381         -1.0833         -1.0833
v  nu_tilda           4.3986e-007       0.0045416       0.0017819       0.0017819
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc           3.2939e-014       0.0053525        0.002095        0.002095
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2878:        0.21780E+01

===============================================================


 INSTANT    0.287900000E+04   TIME STEP NUMBER            2879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.52574E-02 0.89054E+00
   Friction velocity        uk    :  0.52574E-02 0.89054E+00
   Dimensionless distance   yplus :  0.42325E-01 0.71695E+01
   Friction thermal sca.    tstar : -0.11677E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.31580E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10436E-01      33   0.25043E-03   0.39576E+01 0.18685E+03 
c  Velocity[X]                                      0.19741E+01 
c  Velocity[Y]                                      0.19835E+01 
c  Velocity[Z]                                      0.79382E-30 
c  Pressure     0.10748E-06     490   0.94486E-08   0.10433E+00 0.65875E+03 
c  nu_tilda     0.84755E-05      33   0.25581E-05   0.74028E-06 0.21461E+03 
c  TempC        0.43948E+02      26   0.22921E-03   0.59181E+01 0.27485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3224          9.0147          4.5729          4.5729
v  Velocity[Y]            -2.6599          7.1643         0.22367         0.22367
v  Velocity[Z]       -8.7034e-015     1.0149e-014    -1.4187e-017    -1.4187e-017
v  ǁVelocityǁ         0.0021065           9.015          5.0348          5.0348
v  Pressure               -26.802          25.395         -1.0479         -1.0479
v  nu_tilda           4.3989e-007       0.0045417       0.0017819       0.0017819
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc           3.2931e-014       0.0053527       0.0020949       0.0020949
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2879:        0.21210E+01

===============================================================


 INSTANT    0.288000000E+04   TIME STEP NUMBER            2880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.69013E-02 0.88965E+00
   Friction velocity        uk    :  0.69013E-02 0.88965E+00
   Dimensionless distance   yplus :  0.55560E-01 0.71623E+01
   Friction thermal sca.    tstar : -0.70954E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.41454E-01 0.53438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10434E-01      33   0.19724E-03   0.39511E+01 0.18685E+03 
c  Velocity[X]                                      0.19523E+01 
c  Velocity[Y]                                      0.19988E+01 
c  Velocity[Z]                                      0.73019E-30 
c  Pressure     0.95899E-07     536   0.97080E-08   0.92342E-01 0.78411E+03 
c  nu_tilda     0.84754E-05      33   0.12642E-04   0.74048E-06 0.21463E+03 
c  TempC        0.43947E+02      26   0.36925E-03   0.43052E+01 0.25432E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.322          9.0149          4.5729          4.5729
v  Velocity[Y]            -2.6588          7.1874         0.22349         0.22349
v  Velocity[Z]       -8.7513e-015     1.0397e-014     -1.417e-017     -1.417e-017
v  ǁVelocityǁ          0.002027          9.0152          5.0348          5.0348
v  Pressure               -26.876          25.394          -1.093          -1.093
v  nu_tilda            4.399e-007       0.0045419       0.0017818       0.0017818
v  TempC                       21          73.078          22.052          22.052
v  TurbVisc           3.2941e-014       0.0053529       0.0020948       0.0020948
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2880:        0.22220E+01

===============================================================


 INSTANT    0.288100000E+04   TIME STEP NUMBER            2881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.67092E-02 0.89110E+00
   Friction velocity        uk    :  0.67092E-02 0.89110E+00
   Dimensionless distance   yplus :  0.54014E-01 0.71740E+01
   Friction thermal sca.    tstar : -0.91428E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.40300E-01 0.53526E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10433E-01      33   0.25472E-03   0.39241E+01 0.18663E+03 
c  Velocity[X]                                      0.19423E+01 
c  Velocity[Y]                                      0.19817E+01 
c  Velocity[Z]                                      0.10266E-29 
c  Pressure     0.10386E-06     505   0.95086E-08   0.98689E-01 0.86716E+03 
c  nu_tilda     0.84752E-05      33   0.25651E-05   0.74063E-06 0.21465E+03 
c  TempC        0.43946E+02      26   0.26979E-03   0.70647E+01 0.31055E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3217          9.0151          4.5729          4.5729
v  Velocity[Y]            -2.6578          7.1941         0.22331         0.22331
v  Velocity[Z]       -8.7407e-015     1.0752e-014    -1.4151e-017    -1.4151e-017
v  ǁVelocityǁ         0.0012355          9.0154          5.0349          5.0349
v  Pressure               -26.814           25.45          -1.047          -1.047
v  nu_tilda           4.3988e-007       0.0045421       0.0017817       0.0017817
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc           3.2944e-014       0.0053531       0.0020947       0.0020947
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2881:        0.21450E+01

===============================================================


 INSTANT    0.288200000E+04   TIME STEP NUMBER            2882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.60760E-02 0.89079E+00
   Friction velocity        uk    :  0.60760E-02 0.89079E+00
   Dimensionless distance   yplus :  0.48916E-01 0.71715E+01
   Friction thermal sca.    tstar : -0.10075E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.36497E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10431E-01      33   0.25068E-03   0.39768E+01 0.18688E+03 
c  Velocity[X]                                      0.19958E+01 
c  Velocity[Y]                                      0.19810E+01 
c  Velocity[Z]                                      0.87339E-30 
c  Pressure     0.11594E-06     536   0.98644E-08   0.11329E+00 0.15502E+04 
c  nu_tilda     0.84751E-05      33   0.12639E-04   0.74083E-06 0.21467E+03 
c  TempC        0.43945E+02      26   0.25206E-03   0.50349E+01 0.24243E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3213          9.0153          4.5729          4.5729
v  Velocity[Y]            -2.6568          7.1674         0.22313         0.22313
v  Velocity[Z]       -8.7828e-015     1.0575e-014    -1.4133e-017    -1.4133e-017
v  ǁVelocityǁ          0.001851          9.0156          5.0349          5.0349
v  Pressure               -26.887          25.288         -1.1256         -1.1256
v  nu_tilda           4.3989e-007       0.0045422       0.0017816       0.0017816
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc           3.2938e-014       0.0053533       0.0020947       0.0020947
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2882:        0.22440E+01

===============================================================


 INSTANT    0.288300000E+04   TIME STEP NUMBER            2883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.94383E-02 0.88949E+00
   Friction velocity        uk    :  0.94383E-02 0.88949E+00
   Dimensionless distance   yplus :  0.75985E-01 0.71610E+01
   Friction thermal sca.    tstar : -0.64998E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.56693E-01 0.53429E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10430E-01      33   0.23402E-03   0.39556E+01 0.18683E+03 
c  Velocity[X]                                      0.19527E+01 
c  Velocity[Y]                                      0.20029E+01 
c  Velocity[Z]                                      0.84859E-30 
c  Pressure     0.90632E-07     505   0.96451E-08   0.86732E-01 0.14362E+04 
c  nu_tilda     0.84749E-05      33   0.25642E-05   0.74100E-06 0.21469E+03 
c  TempC        0.43943E+02      27   0.33669E-03   0.39137E+01 0.22193E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3209          9.0155          4.5729          4.5729
v  Velocity[Y]            -2.6557          7.1882         0.22295         0.22295
v  Velocity[Z]       -8.7703e-015      9.912e-015    -1.4114e-017    -1.4114e-017
v  ǁVelocityǁ         0.0018654          9.0158           5.035           5.035
v  Pressure               -26.829          25.456         -1.0602         -1.0602
v  nu_tilda           4.3987e-007       0.0045424       0.0017816       0.0017816
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc           3.2942e-014       0.0053535       0.0020945       0.0020945
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2883:        0.21630E+01

===============================================================


 INSTANT    0.288400000E+04   TIME STEP NUMBER            2884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16683E-02 0.89036E+00
   Friction velocity        uk    :  0.16683E-02 0.89036E+00
   Dimensionless distance   yplus :  0.13431E-01 0.71680E+01
   Friction thermal sca.    tstar : -0.11311E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10021E-01 0.53481E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10428E-01      33   0.24679E-03   0.39342E+01 0.18660E+03 
c  Velocity[X]                                      0.19561E+01 
c  Velocity[Y]                                      0.19781E+01 
c  Velocity[Z]                                      0.81642E-30 
c  Pressure     0.11116E-06     538   0.97677E-08   0.10683E+00 0.19080E+04 
c  nu_tilda     0.84748E-05      33   0.12633E-04   0.74120E-06 0.21471E+03 
c  TempC        0.43942E+02      27   0.28592E-03   0.46311E+01 0.24665E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3205          9.0157          4.5729          4.5729
v  Velocity[Y]            -2.6547            7.16         0.22277         0.22277
v  Velocity[Z]       -8.8123e-015     1.0359e-014    -1.4094e-017    -1.4094e-017
v  ǁVelocityǁ         0.0013704           9.016           5.035           5.035
v  Pressure               -26.899          25.236         -1.1514         -1.1514
v  nu_tilda           4.3983e-007       0.0045426       0.0017814       0.0017814
v  TempC                       21           73.08          22.052          22.052
v  TurbVisc           3.2936e-014       0.0053537       0.0020945       0.0020945
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2884:        0.22120E+01

===============================================================


 INSTANT    0.288500000E+04   TIME STEP NUMBER            2885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.44492E-02 0.88965E+00
   Friction velocity        uk    :  0.44492E-02 0.88965E+00
   Dimensionless distance   yplus :  0.35819E-01 0.71623E+01
   Friction thermal sca.    tstar : -0.58806E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.26725E-01 0.53439E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10427E-01      33   0.24513E-03   0.39415E+01 0.18659E+03 
c  Velocity[X]                                      0.19720E+01 
c  Velocity[Y]                                      0.19695E+01 
c  Velocity[Z]                                      0.11013E-29 
c  Pressure     0.91431E-07     553   0.96520E-08   0.87783E-01 0.16895E+04 
c  nu_tilda     0.84746E-05      33   0.25697E-05   0.74135E-06 0.21472E+03 
c  TempC        0.43941E+02      27   0.28730E-03   0.35917E+01 0.21867E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3201          9.0159          4.5729          4.5729
v  Velocity[Y]            -2.6536          7.1876         0.22258         0.22258
v  Velocity[Z]       -8.7987e-015     1.0643e-014    -1.4075e-017    -1.4075e-017
v  ǁVelocityǁ         0.0017452          9.0162           5.035           5.035
v  Pressure               -26.841          25.434         -1.0751         -1.0751
v  nu_tilda           4.3978e-007       0.0045427       0.0017814       0.0017814
v  TempC                       21           73.08          22.052          22.052
v  TurbVisc           3.2924e-014       0.0053539       0.0020944       0.0020944
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2885:        0.22440E+01

===============================================================


 INSTANT    0.288600000E+04   TIME STEP NUMBER            2886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.80622E-02 0.89081E+00
   Friction velocity        uk    :  0.80622E-02 0.89081E+00
   Dimensionless distance   yplus :  0.64906E-01 0.71717E+01
   Friction thermal sca.    tstar : -0.75803E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48427E-01 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        200

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10425E-01      33   0.23687E-03   0.39175E+01 0.18653E+03 
c  Velocity[X]                                      0.19334E+01 
c  Velocity[Y]                                      0.19842E+01 
c  Velocity[Z]                                      0.99411E-30 
c  Pressure     0.88958E-07     553   0.91261E-08   0.85446E-01 0.13041E+04 
c  nu_tilda     0.84744E-05      33   0.12629E-04   0.74154E-06 0.21474E+03 
c  TempC        0.43940E+02      26   0.25872E-03   0.43065E+01 0.22692E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3197          9.0161          4.5729          4.5729
v  Velocity[Y]            -2.6526           7.193          0.2224          0.2224
v  Velocity[Z]       -8.8384e-015     1.0243e-014    -1.4049e-017    -1.4049e-017
v  ǁVelocityǁ         0.0017439          9.0164          5.0351          5.0351
v  Pressure               -26.911          25.334         -1.1454         -1.1454
v  nu_tilda           4.3972e-007       0.0045429       0.0017813       0.0017813
v  TempC                       21           73.08          22.052          22.052
v  TurbVisc           3.2907e-014       0.0053541       0.0020943       0.0020943
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2886:        0.22520E+01

===============================================================


 INSTANT    0.288700000E+04   TIME STEP NUMBER            2887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13558E-01 0.89029E+00
   Friction velocity        uk    :  0.13558E-01 0.89029E+00
   Dimensionless distance   yplus :  0.10915E+00 0.71674E+01
   Friction thermal sca.    tstar : -0.61506E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81442E-01 0.53477E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10424E-01      33   0.24788E-03   0.39504E+01 0.18658E+03 
c  Velocity[X]                                      0.19714E+01 
c  Velocity[Y]                                      0.19790E+01 
c  Velocity[Z]                                      0.99303E-30 
c  Pressure     0.12329E-06     506   0.95444E-08   0.11849E+00 0.61610E+03 
c  nu_tilda     0.84743E-05      33   0.25703E-05   0.74172E-06 0.21476E+03 
c  TempC        0.43938E+02      26   0.29212E-03   0.53258E+01 0.25956E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3193          9.0163          4.5729          4.5729
v  Velocity[Y]            -2.6516           7.163         0.22221         0.22221
v  Velocity[Z]       -8.8244e-015     9.5996e-015     -1.404e-017     -1.404e-017
v  ǁVelocityǁ         0.0011775          9.0166          5.0351          5.0351
v  Pressure               -26.853          25.303         -1.1132         -1.1132
v  nu_tilda           4.3978e-007        0.004543       0.0017813       0.0017813
v  TempC                       21           73.08          22.052          22.052
v  TurbVisc            3.289e-014       0.0053542       0.0020942       0.0020942
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2887:        0.21490E+01

===============================================================


 INSTANT    0.288800000E+04   TIME STEP NUMBER            2888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.91921E-02 0.88910E+00
   Friction velocity        uk    :  0.91921E-02 0.88910E+00
   Dimensionless distance   yplus :  0.74003E-01 0.71579E+01
   Friction thermal sca.    tstar : -0.60268E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.55214E-01 0.53406E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10422E-01      33   0.25164E-03   0.39425E+01 0.18652E+03 
c  Velocity[X]                                      0.19806E+01 
c  Velocity[Y]                                      0.19619E+01 
c  Velocity[Z]                                      0.83593E-30 
c  Pressure     0.10575E-06     520   0.99542E-08   0.10142E+00 0.90381E+03 
c  nu_tilda     0.84741E-05      33   0.12628E-04   0.74195E-06 0.21478E+03 
c  TempC        0.43937E+02      27   0.30625E-03   0.46347E+01 0.24153E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3189          9.0165          4.5729          4.5729
v  Velocity[Y]            -2.6505          7.1837         0.22202         0.22202
v  Velocity[Z]       -8.8588e-015      1.048e-014    -1.4018e-017    -1.4018e-017
v  ǁVelocityǁ         0.0016431          9.0168          5.0352          5.0352
v  Pressure               -26.925          25.292         -1.1659         -1.1659
v  nu_tilda           4.3985e-007       0.0045432       0.0017811       0.0017811
v  TempC                       21          73.079          22.052          22.052
v  TurbVisc            3.291e-014       0.0053544       0.0020941       0.0020941
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2888:        0.22030E+01

===============================================================


 INSTANT    0.288900000E+04   TIME STEP NUMBER            2889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17437E-01 0.89037E+00
   Friction velocity        uk    :  0.17437E-01 0.89037E+00
   Dimensionless distance   yplus :  0.14038E+00 0.71681E+01
   Friction thermal sca.    tstar : -0.58565E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10474E+00 0.53482E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10421E-01      33   0.24415E-03   0.39354E+01 0.18646E+03 
c  Velocity[X]                                      0.19611E+01 
c  Velocity[Y]                                      0.19744E+01 
c  Velocity[Z]                                      0.10173E-29 
c  Pressure     0.10551E-06     505   0.95345E-08   0.10275E+00 0.74079E+03 
c  nu_tilda     0.84739E-05      33   0.25760E-05   0.74214E-06 0.21480E+03 
c  TempC        0.43936E+02      26   0.28095E-03   0.51686E+01 0.27052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3185          9.0168          4.5729          4.5729
v  Velocity[Y]            -2.6495          7.1628         0.22184         0.22184
v  Velocity[Z]       -8.8428e-015     9.3917e-015    -1.4002e-017    -1.4002e-017
v  ǁVelocityǁ         0.0016039           9.017          5.0352          5.0352
v  Pressure               -26.865          25.311         -1.1258         -1.1258
v  nu_tilda           4.3988e-007       0.0045434       0.0017811       0.0017811
v  TempC                       21          73.078          22.052          22.052
v  TurbVisc           3.2929e-014       0.0053546        0.002094        0.002094
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2889:        0.21510E+01

===============================================================


 INSTANT    0.289000000E+04   TIME STEP NUMBER            2890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12822E-01 0.88944E+00
   Friction velocity        uk    :  0.12822E-01 0.88944E+00
   Dimensionless distance   yplus :  0.10323E+00 0.71606E+01
   Friction thermal sca.    tstar : -0.59040E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77018E-01 0.53426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10419E-01      33   0.18224E-03   0.39135E+01 0.18631E+03 
c  Velocity[X]                                      0.19545E+01 
c  Velocity[Y]                                      0.19590E+01 
c  Velocity[Z]                                      0.94244E-30 
c  Pressure     0.10765E-06     537   0.95457E-08   0.10207E+00 0.10869E+04 
c  nu_tilda     0.84737E-05      33   0.12623E-04   0.74237E-06 0.21482E+03 
c  TempC        0.43935E+02      26   0.26379E-03   0.71501E+01 0.28452E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3181          9.0169          4.5729          4.5729
v  Velocity[Y]            -2.6484          7.1824         0.22165         0.22165
v  Velocity[Z]       -8.8853e-015     9.2106e-015    -1.3986e-017    -1.3986e-017
v  ǁVelocityǁ           0.00159          9.0172          5.0353          5.0353
v  Pressure               -26.938          25.253         -1.1877         -1.1877
v  nu_tilda           4.3993e-007       0.0045435       0.0017809       0.0017809
v  TempC                       21          73.075          22.052          22.052
v  TurbVisc           3.2939e-014       0.0053548       0.0020939       0.0020939
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2890:        0.22370E+01

===============================================================


 INSTANT    0.289100000E+04   TIME STEP NUMBER            2891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11292E-01 0.89112E+00
   Friction velocity        uk    :  0.11292E-01 0.89112E+00
   Dimensionless distance   yplus :  0.90912E-01 0.71741E+01
   Friction thermal sca.    tstar : -0.58848E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67831E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10418E-01      33   0.24836E-03   0.39078E+01 0.18624E+03 
c  Velocity[X]                                      0.19571E+01 
c  Velocity[Y]                                      0.19507E+01 
c  Velocity[Z]                                      0.91318E-30 
c  Pressure     0.98317E-07     568   0.99778E-08   0.94440E-01 0.13548E+04 
c  nu_tilda     0.84735E-05      33   0.25756E-05   0.74255E-06 0.21484E+03 
c  TempC        0.43933E+02      26   0.35713E-03   0.58570E+01 0.26734E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3177          9.0171          4.5729          4.5729
v  Velocity[Y]            -2.6473          7.1958         0.22146         0.22146
v  Velocity[Z]       -8.8834e-015     9.4017e-015    -1.3966e-017    -1.3966e-017
v  ǁVelocityǁ         0.0015651          9.0174          5.0353          5.0353
v  Pressure               -26.881          25.387         -1.1226         -1.1226
v  nu_tilda           4.3992e-007       0.0045436       0.0017809       0.0017809
v  TempC                       21          73.072          22.051          22.051
v  TurbVisc           3.2953e-014        0.005355       0.0020938       0.0020938
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2891:        0.26650E+01

===============================================================


 INSTANT    0.289200000E+04   TIME STEP NUMBER            2892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17640E-01 0.89070E+00
   Friction velocity        uk    :  0.17640E-01 0.89070E+00
   Dimensionless distance   yplus :  0.14202E+00 0.71707E+01
   Friction thermal sca.    tstar : -0.57962E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10596E+00 0.53502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10416E-01      33   0.23939E-03   0.39297E+01 0.18635E+03 
c  Velocity[X]                                      0.19624E+01 
c  Velocity[Y]                                      0.19673E+01 
c  Velocity[Z]                                      0.90889E-30 
c  Pressure     0.10976E-06     570   0.97295E-08   0.10688E+00 0.20402E+04 
c  nu_tilda     0.84733E-05      33   0.12619E-04   0.74276E-06 0.21486E+03 
c  TempC        0.43932E+02      26   0.26754E-03   0.66776E+01 0.30137E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3172          9.0173          4.5729          4.5729
v  Velocity[Y]            -2.6463          7.1663         0.22127         0.22127
v  Velocity[Z]       -8.9374e-015     8.8467e-015    -1.3952e-017    -1.3952e-017
v  ǁVelocityǁ         0.0015674          9.0176          5.0354          5.0354
v  Pressure                -26.95          25.157         -1.2202         -1.2202
v  nu_tilda           4.3994e-007       0.0045438       0.0017808       0.0017808
v  TempC                       21          73.069          22.051          22.051
v  TurbVisc            3.295e-014       0.0053552       0.0020937       0.0020937
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2892:        0.23980E+01

===============================================================


 INSTANT    0.289300000E+04   TIME STEP NUMBER            2893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16463E-01 0.88929E+00
   Friction velocity        uk    :  0.16463E-01 0.88929E+00
   Dimensionless distance   yplus :  0.13254E+00 0.71594E+01
   Friction thermal sca.    tstar : -0.58769E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98890E-01 0.53417E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10414E-01      33   0.23824E-03   0.39079E+01 0.18615E+03 
c  Velocity[X]                                      0.19582E+01 
c  Velocity[Y]                                      0.19498E+01 
c  Velocity[Z]                                      0.77695E-30 
c  Pressure     0.92341E-07     521   0.92097E-08   0.88228E-01 0.16347E+04 
c  nu_tilda     0.84731E-05      33   0.25821E-05   0.74290E-06 0.21488E+03 
c  TempC        0.43931E+02      26   0.25958E-03   0.49155E+01 0.25790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3168          9.0175          4.5729          4.5729
v  Velocity[Y]            -2.6453           7.184         0.22107         0.22107
v  Velocity[Z]       -8.9468e-015     8.8301e-015    -1.3936e-017    -1.3936e-017
v  ǁVelocityǁ         0.0015649          9.0178          5.0354          5.0354
v  Pressure               -26.892           25.34         -1.1449         -1.1449
v  nu_tilda           4.3995e-007        0.004544       0.0017808       0.0017808
v  TempC                       21          73.064          22.051          22.051
v  TurbVisc           3.2956e-014       0.0053553       0.0020936       0.0020936
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2893:        0.21890E+01

===============================================================


 INSTANT    0.289400000E+04   TIME STEP NUMBER            2894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16606E-01 0.89034E+00
   Friction velocity        uk    :  0.16606E-01 0.89034E+00
   Dimensionless distance   yplus :  0.13369E+00 0.71679E+01
   Friction thermal sca.    tstar : -0.60201E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99745E-01 0.53480E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10413E-01      33   0.28286E-03   0.39128E+01 0.18620E+03 
c  Velocity[X]                                      0.19706E+01 
c  Velocity[Y]                                      0.19422E+01 
c  Velocity[Z]                                      0.75699E-30 
c  Pressure     0.95915E-07     538   0.97055E-08   0.93277E-01 0.19614E+04 
c  nu_tilda     0.84729E-05      33   0.12616E-04   0.74309E-06 0.21490E+03 
c  TempC        0.43929E+02      26   0.29594E-03   0.45296E+01 0.23413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3163          9.0177          4.5729          4.5729
v  Velocity[Y]            -2.6443          7.1618         0.22088         0.22088
v  Velocity[Z]       -9.0081e-015     8.8405e-015    -1.3916e-017    -1.3916e-017
v  ǁVelocityǁ         0.0015978           9.018          5.0355          5.0355
v  Pressure               -26.959          25.123         -1.2391         -1.2391
v  nu_tilda           4.3997e-007       0.0045441       0.0017806       0.0017806
v  TempC                       21           73.06          22.051          22.051
v  TurbVisc           3.2959e-014       0.0053555       0.0020935       0.0020935
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2894:        0.22320E+01

===============================================================


 INSTANT    0.289500000E+04   TIME STEP NUMBER            2895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16267E-01 0.88969E+00
   Friction velocity        uk    :  0.16267E-01 0.88969E+00
   Dimensionless distance   yplus :  0.13096E+00 0.71626E+01
   Friction thermal sca.    tstar : -0.63194E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97710E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10411E-01      33   0.23750E-03   0.39464E+01 0.18633E+03 
c  Velocity[X]                                      0.19875E+01 
c  Velocity[Y]                                      0.19590E+01 
c  Velocity[Z]                                      0.86950E-30 
c  Pressure     0.11902E-06     552   0.99433E-08   0.11327E+00 0.19572E+04 
c  nu_tilda     0.84727E-05      33   0.25813E-05   0.74323E-06 0.21492E+03 
c  TempC        0.43928E+02      26   0.26391E-03   0.45921E+01 0.25334E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3159          9.0179          4.5729          4.5729
v  Velocity[Y]            -2.6432          7.1874         0.22068         0.22068
v  Velocity[Z]       -9.0247e-015     8.8268e-015    -1.3898e-017    -1.3898e-017
v  ǁVelocityǁ         0.0015981          9.0182          5.0355          5.0355
v  Pressure               -26.906          25.355         -1.1529         -1.1529
v  nu_tilda           4.3995e-007       0.0045443       0.0017806       0.0017806
v  TempC                       21          73.055          22.051          22.051
v  TurbVisc           3.2967e-014       0.0053557       0.0020934       0.0020934
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2895:        0.22590E+01

===============================================================


 INSTANT    0.289600000E+04   TIME STEP NUMBER            2896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14670E-01 0.89089E+00
   Friction velocity        uk    :  0.14670E-01 0.89089E+00
   Dimensionless distance   yplus :  0.11810E+00 0.71723E+01
   Friction thermal sca.    tstar : -0.63175E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88116E-01 0.53513E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10410E-01      33   0.22033E-03   0.38979E+01 0.18606E+03 
c  Velocity[X]                                      0.19559E+01 
c  Velocity[Y]                                      0.19420E+01 
c  Velocity[Z]                                      0.92821E-30 
c  Pressure     0.10339E-06     568   0.95721E-08   0.97788E-01 0.17176E+04 
c  nu_tilda     0.84725E-05      33   0.12610E-04   0.74341E-06 0.21494E+03 
c  TempC        0.43927E+02      26   0.31937E-03   0.50874E+01 0.25863E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3155          9.0181          4.5729          4.5729
v  Velocity[Y]            -2.6421          7.1891         0.22049         0.22049
v  Velocity[Z]       -9.0972e-015     8.8379e-015    -1.3875e-017    -1.3875e-017
v  ǁVelocityǁ         0.0016403          9.0184          5.0355          5.0355
v  Pressure               -26.972          25.186         -1.2389         -1.2389
v  nu_tilda           4.3991e-007       0.0045444       0.0017804       0.0017804
v  TempC                       21          73.052          22.051          22.051
v  TurbVisc            3.296e-014       0.0053559       0.0020933       0.0020933
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2896:        0.22990E+01

===============================================================


 INSTANT    0.289700000E+04   TIME STEP NUMBER            2897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12288E-01 0.89072E+00
   Friction velocity        uk    :  0.12288E-01 0.89072E+00
   Dimensionless distance   yplus :  0.98929E-01 0.71709E+01
   Friction thermal sca.    tstar : -0.65397E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.73812E-01 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10408E-01      33   0.23991E-03   0.38978E+01 0.18599E+03 
c  Velocity[X]                                      0.19648E+01 
c  Velocity[Y]                                      0.19330E+01 
c  Velocity[Z]                                      0.91596E-30 
c  Pressure     0.11216E-06     506   0.99289E-08   0.10973E+00 0.78151E+03 
c  nu_tilda     0.84722E-05      33   0.25873E-05   0.74356E-06 0.21496E+03 
c  TempC        0.43925E+02      27   0.26807E-03   0.45137E+01 0.24707E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3151          9.0183          4.5729          4.5729
v  Velocity[Y]            -2.6411          7.1663         0.22029         0.22029
v  Velocity[Z]       -9.1232e-015     8.8225e-015    -1.3853e-017    -1.3853e-017
v  ǁVelocityǁ         0.0016944          9.0186          5.0356          5.0356
v  Pressure               -26.912          25.209         -1.1963         -1.1963
v  nu_tilda           4.3997e-007       0.0045445       0.0017804       0.0017804
v  TempC                       21          73.052          22.051          22.051
v  TurbVisc           3.2948e-014        0.005356       0.0020932       0.0020932
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2897:        0.21530E+01

===============================================================


 INSTANT    0.289800000E+04   TIME STEP NUMBER            2898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.54626E-02 0.88936E+00
   Friction velocity        uk    :  0.54626E-02 0.88936E+00
   Dimensionless distance   yplus :  0.43978E-01 0.71600E+01
   Friction thermal sca.    tstar : -0.67938E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32812E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10407E-01      33   0.26129E-03   0.38983E+01 0.18603E+03 
c  Velocity[X]                                      0.19485E+01 
c  Velocity[Y]                                      0.19498E+01 
c  Velocity[Z]                                      0.11341E-29 
c  Pressure     0.97723E-07     504   0.99621E-08   0.93872E-01 0.79195E+03 
c  nu_tilda     0.84720E-05      33   0.12610E-04   0.74373E-06 0.21497E+03 
c  TempC        0.43924E+02      27   0.27320E-03   0.40694E+01 0.23976E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3146          9.0185          4.5729          4.5729
v  Velocity[Y]            -2.6401          7.1842         0.22009         0.22009
v  Velocity[Z]       -9.2008e-015     8.8373e-015    -1.3832e-017    -1.3832e-017
v  ǁVelocityǁ         0.0012163          9.0188          5.0356          5.0356
v  Pressure               -26.986          25.213          -1.242          -1.242
v  nu_tilda           4.3993e-007       0.0045447       0.0017803       0.0017803
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.2964e-014       0.0053562       0.0020931       0.0020931
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2898:        0.21610E+01

===============================================================


 INSTANT    0.289900000E+04   TIME STEP NUMBER            2899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.86770E-02 0.89043E+00
   Friction velocity        uk    :  0.86770E-02 0.89043E+00
   Dimensionless distance   yplus :  0.69856E-01 0.71686E+01
   Friction thermal sca.    tstar : -0.68678E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.52120E-01 0.53486E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10405E-01      33   0.24718E-03   0.39244E+01 0.18604E+03 
c  Velocity[X]                                      0.19884E+01 
c  Velocity[Y]                                      0.19360E+01 
c  Velocity[Z]                                      0.81095E-30 
c  Pressure     0.13432E-06     457   0.92567E-08   0.12770E+00 0.59261E+03 
c  nu_tilda     0.84718E-05      33   0.25875E-05   0.74386E-06 0.21499E+03 
c  TempC        0.43922E+02      26   0.35883E-03   0.57042E+01 0.26580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3142          9.0187          4.5729          4.5729
v  Velocity[Y]            -2.6391          7.1605         0.21988         0.21988
v  Velocity[Z]       -9.2338e-015     8.8187e-015    -1.3815e-017    -1.3815e-017
v  ǁVelocityǁ         0.0017933          9.0189          5.0357          5.0357
v  Pressure                -26.92          25.139         -1.2222         -1.2222
v  nu_tilda           4.3993e-007       0.0045448       0.0017803       0.0017803
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.2954e-014       0.0053563        0.002093        0.002093
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2899:        0.20580E+01

===============================================================


 INSTANT    0.290000000E+04   TIME STEP NUMBER            2900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15080E-01 0.88998E+00
   Friction velocity        uk    :  0.15080E-01 0.88998E+00
   Dimensionless distance   yplus :  0.12141E+00 0.71649E+01
   Friction thermal sca.    tstar : -0.73906E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90583E-01 0.53458E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10404E-01      33   0.19621E-03   0.39081E+01 0.18598E+03 
c  Velocity[X]                                      0.19814E+01 
c  Velocity[Y]                                      0.19267E+01 
c  Velocity[Z]                                      0.77370E-30 
c  Pressure     0.10158E-06     520   0.95400E-08   0.97811E-01 0.69864E+03 
c  nu_tilda     0.84715E-05      33   0.12605E-04   0.74405E-06 0.21501E+03 
c  TempC        0.43921E+02      26   0.27555E-03   0.66667E+01 0.29263E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3137          9.0189          4.5729          4.5729
v  Velocity[Y]             -2.638          7.1861         0.21968         0.21968
v  Velocity[Z]       -9.3196e-015     8.8337e-015    -1.3795e-017    -1.3795e-017
v  ǁVelocityǁ         0.0018031          9.0191          5.0357          5.0357
v  Pressure               -26.996          25.201         -1.2541         -1.2541
v  nu_tilda            4.399e-007        0.004545       0.0017801       0.0017801
v  TempC                       21          73.051          22.051          22.051
v  TurbVisc           3.2953e-014       0.0053565       0.0020929       0.0020929
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2900:        0.21810E+01

===============================================================


 INSTANT    0.290100000E+04   TIME STEP NUMBER            2901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17291E-01 0.89139E+00
   Friction velocity        uk    :  0.17291E-01 0.89139E+00
   Dimensionless distance   yplus :  0.13920E+00 0.71763E+01
   Friction thermal sca.    tstar : -0.73128E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10386E+00 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10402E-01      33   0.22991E-03   0.38806E+01 0.18584E+03 
c  Velocity[X]                                      0.19387E+01 
c  Velocity[Y]                                      0.19419E+01 
c  Velocity[Z]                                      0.10125E-29 
c  Pressure     0.75448E-07     505   0.98009E-08   0.72548E-01 0.95460E+03 
c  nu_tilda     0.84713E-05      33   0.25942E-05   0.74419E-06 0.21503E+03 
c  TempC        0.43919E+02      27   0.26382E-03   0.48078E+01 0.25677E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3133           9.019          4.5729          4.5729
v  Velocity[Y]            -2.6369          7.1979         0.21947         0.21947
v  Velocity[Z]        -9.354e-015     8.8171e-015    -1.3768e-017    -1.3768e-017
v  ǁVelocityǁ         0.0017287          9.0193          5.0357          5.0357
v  Pressure               -26.933          25.275         -1.2038         -1.2038
v  nu_tilda           4.3982e-007       0.0045451       0.0017801       0.0017801
v  TempC                       21          73.052          22.051          22.051
v  TurbVisc           3.2943e-014       0.0053567       0.0020928       0.0020928
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2901:        0.21690E+01

===============================================================


 INSTANT    0.290200000E+04   TIME STEP NUMBER            2902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13999E-01 0.89094E+00
   Friction velocity        uk    :  0.13999E-01 0.89094E+00
   Dimensionless distance   yplus :  0.11270E+00 0.71727E+01
   Friction thermal sca.    tstar : -0.77866E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.84090E-01 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10400E-01      33   0.24702E-03   0.38975E+01 0.18586E+03 
c  Velocity[X]                                      0.19683E+01 
c  Velocity[Y]                                      0.19292E+01 
c  Velocity[Z]                                      0.10156E-29 
c  Pressure     0.10928E-06     569   0.94307E-08   0.10560E+00 0.18444E+04 
c  nu_tilda     0.84710E-05      33   0.12602E-04   0.74437E-06 0.21505E+03 
c  TempC        0.43918E+02      26   0.30515E-03   0.50119E+01 0.23036E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3128          9.0192          4.5729          4.5729
v  Velocity[Y]            -2.6359          7.1648         0.21927         0.21927
v  Velocity[Z]       -9.4422e-015     8.8296e-015    -1.3755e-017    -1.3755e-017
v  ǁVelocityǁ         0.0018846          9.0195          5.0358          5.0358
v  Pressure               -27.001          25.061         -1.2922         -1.2922
v  nu_tilda           4.3984e-007       0.0045452       0.0017799       0.0017799
v  TempC                       21          73.052          22.051          22.051
v  TurbVisc           3.2921e-014       0.0053569       0.0020927       0.0020927
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2902:        0.22780E+01

===============================================================


 INSTANT    0.290300000E+04   TIME STEP NUMBER            2903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15640E-01 0.88962E+00
   Friction velocity        uk    :  0.15640E-01 0.88962E+00
   Dimensionless distance   yplus :  0.12591E+00 0.71620E+01
   Friction thermal sca.    tstar : -0.77804E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93944E-01 0.53437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10399E-01      33   0.27186E-03   0.39084E+01 0.18588E+03 
c  Velocity[X]                                      0.19903E+01 
c  Velocity[Y]                                      0.19181E+01 
c  Velocity[Z]                                      0.81497E-30 
c  Pressure     0.10474E-06     570   0.96667E-08   0.10017E+00 0.15982E+04 
c  nu_tilda     0.84708E-05      33   0.25926E-05   0.74451E-06 0.21507E+03 
c  TempC        0.43917E+02      27   0.26026E-03   0.44692E+01 0.26033E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3124          9.0194          4.5729          4.5729
v  Velocity[Y]            -2.6349          7.1886         0.21906         0.21906
v  Velocity[Z]       -9.4846e-015     8.8147e-015    -1.3733e-017    -1.3733e-017
v  ǁVelocityǁ         0.0015094          9.0197          5.0358          5.0358
v  Pressure                -26.94          25.248         -1.2187         -1.2187
v  nu_tilda           4.3988e-007       0.0045453       0.0017799       0.0017799
v  TempC                       21          73.054          22.051          22.051
v  TurbVisc           3.2928e-014        0.005357       0.0020926       0.0020926
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2903:        0.22920E+01

===============================================================


 INSTANT    0.290400000E+04   TIME STEP NUMBER            2904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13048E-01 0.89062E+00
   Friction velocity        uk    :  0.13048E-01 0.89062E+00
   Dimensionless distance   yplus :  0.10504E+00 0.71701E+01
   Friction thermal sca.    tstar : -0.84637E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.78374E-01 0.53497E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10397E-01      33   0.24844E-03   0.38985E+01 0.18584E+03 
c  Velocity[X]                                      0.19650E+01 
c  Velocity[Y]                                      0.19336E+01 
c  Velocity[Z]                                      0.79507E-30 
c  Pressure     0.10167E-06     536   0.98484E-08   0.98845E-01 0.16874E+04 
c  nu_tilda     0.84705E-05      33   0.12597E-04   0.74469E-06 0.21509E+03 
c  TempC        0.43915E+02      26   0.30216E-03   0.41217E+01 0.23798E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3119          9.0196          4.5729          4.5729
v  Velocity[Y]            -2.6338          7.1646         0.21885         0.21885
v  Velocity[Z]       -9.5783e-015     8.8268e-015    -1.3713e-017    -1.3713e-017
v  ǁVelocityǁ         0.0019843          9.0198          5.0359          5.0359
v  Pressure               -27.008          25.065         -1.3012         -1.3012
v  nu_tilda           4.3996e-007       0.0045455       0.0017798       0.0017798
v  TempC                       21          73.054           22.05           22.05
v  TurbVisc           3.2937e-014       0.0053572       0.0020925       0.0020925
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2904:        0.22200E+01

===============================================================


 INSTANT    0.290500000E+04   TIME STEP NUMBER            2905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12860E-01 0.88974E+00
   Friction velocity        uk    :  0.12860E-01 0.88974E+00
   Dimensionless distance   yplus :  0.10353E+00 0.71630E+01
   Friction thermal sca.    tstar : -0.86912E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77246E-01 0.53444E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10396E-01      33   0.25041E-03   0.38878E+01 0.18567E+03 
c  Velocity[X]                                      0.19694E+01 
c  Velocity[Y]                                      0.19184E+01 
c  Velocity[Z]                                      0.76184E-30 
c  Pressure     0.10409E-06     553   0.96894E-08   0.98412E-01 0.14564E+04 
c  nu_tilda     0.84702E-05      33   0.25998E-05   0.74481E-06 0.21510E+03 
c  TempC        0.43914E+02      27   0.32662E-03   0.41304E+01 0.23470E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3114          9.0198          4.5729          4.5729
v  Velocity[Y]            -2.6328          7.1866         0.21864         0.21864
v  Velocity[Z]       -9.6298e-015     8.8104e-015    -1.3689e-017    -1.3689e-017
v  ǁVelocityǁ         0.0020362            9.02          5.0359          5.0359
v  Pressure               -26.946          25.222         -1.2316         -1.2316
v  nu_tilda           4.3997e-007       0.0045456       0.0017797       0.0017797
v  TempC                       21          73.059           22.05           22.05
v  TurbVisc           3.2961e-014       0.0053573       0.0020924       0.0020924
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2905:        0.22620E+01

===============================================================


 INSTANT    0.290600000E+04   TIME STEP NUMBER            2906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.55066E-02 0.89111E+00
   Friction velocity        uk    :  0.55066E-02 0.89111E+00
   Dimensionless distance   yplus :  0.44332E-01 0.71740E+01
   Friction thermal sca.    tstar : -0.94136E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.33076E-01 0.53526E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10394E-01      33   0.24869E-03   0.38739E+01 0.18562E+03 
c  Velocity[X]                                      0.19633E+01 
c  Velocity[Y]                                      0.19106E+01 
c  Velocity[Z]                                      0.86277E-30 
c  Pressure     0.84291E-07     536   0.96876E-08   0.81233E-01 0.10247E+04 
c  nu_tilda     0.84700E-05      33   0.12594E-04   0.74500E-06 0.21512E+03 
c  TempC        0.43912E+02      26   0.27209E-03   0.61033E+01 0.25950E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3109          9.0199          4.5729          4.5729
v  Velocity[Y]            -2.6317          7.1949         0.21842         0.21842
v  Velocity[Z]       -9.7334e-015     8.8225e-015    -1.3666e-017    -1.3666e-017
v  ǁVelocityǁ        0.00096083          9.0202          5.0359          5.0359
v  Pressure               -27.016          25.161          -1.289          -1.289
v  nu_tilda           4.3987e-007       0.0045458       0.0017796       0.0017796
v  TempC                       21          73.061           22.05           22.05
v  TurbVisc           3.2966e-014       0.0053575       0.0020923       0.0020923
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2906:        0.22020E+01

===============================================================


 INSTANT    0.290700000E+04   TIME STEP NUMBER            2907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.53763E-02 0.89067E+00
   Friction velocity        uk    :  0.53763E-02 0.89067E+00
   Dimensionless distance   yplus :  0.43283E-01 0.71705E+01
   Friction thermal sca.    tstar : -0.95110E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.32294E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10392E-01      33   0.23895E-03   0.38943E+01 0.18569E+03 
c  Velocity[X]                                      0.19675E+01 
c  Velocity[Y]                                      0.19268E+01 
c  Velocity[Z]                                      0.10684E-29 
c  Pressure     0.11578E-06     490   0.95904E-08   0.11217E+00 0.63950E+03 
c  nu_tilda     0.84697E-05      33   0.25991E-05   0.74515E-06 0.21514E+03 
c  TempC        0.43911E+02      26   0.32829E-03   0.59367E+01 0.26129E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3104          9.0201          4.5729          4.5729
v  Velocity[Y]            -2.6307          7.1687         0.21821         0.21821
v  Velocity[Z]       -9.7899e-015     8.8057e-015    -1.3648e-017    -1.3648e-017
v  ǁVelocityǁ         0.0021032          9.0204           5.036           5.036
v  Pressure                -26.95           25.14         -1.2551         -1.2551
v  nu_tilda           4.3984e-007       0.0045459       0.0017796       0.0017796
v  TempC                       21          73.064           22.05           22.05
v  TurbVisc           3.2935e-014       0.0053577       0.0020922       0.0020922
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2907:        0.21320E+01

===============================================================


 INSTANT    0.290800000E+04   TIME STEP NUMBER            2908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10765E-01 0.88921E+00
   Friction velocity        uk    :  0.10765E-01 0.88921E+00
   Dimensionless distance   yplus :  0.86662E-01 0.71588E+01
   Friction thermal sca.    tstar : -0.10414E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.64660E-01 0.53412E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10391E-01      33   0.24844E-03   0.38690E+01 0.18555E+03 
c  Velocity[X]                                      0.19582E+01 
c  Velocity[Y]                                      0.19107E+01 
c  Velocity[Z]                                      0.11029E-29 
c  Pressure     0.10285E-06     505   0.95069E-08   0.97582E-01 0.89880E+03 
c  nu_tilda     0.84694E-05      33   0.12592E-04   0.74533E-06 0.21516E+03 
c  TempC        0.43909E+02      26   0.24898E-03   0.58663E+01 0.28252E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.31          9.0203          4.5729          4.5729
v  Velocity[Y]            -2.6296          7.1829         0.21799         0.21799
v  Velocity[Z]       -9.9066e-015     8.8175e-015    -1.3626e-017    -1.3626e-017
v  ǁVelocityǁ         0.0018178          9.0205           5.036           5.036
v  Pressure               -27.019          25.114         -1.3066         -1.3066
v  nu_tilda           4.3986e-007        0.004546       0.0017794       0.0017794
v  TempC                       21          73.067           22.05           22.05
v  TurbVisc           3.2926e-014       0.0053578       0.0020921       0.0020921
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2908:        0.21430E+01

===============================================================


 INSTANT    0.290900000E+04   TIME STEP NUMBER            2909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.80577E-02 0.89045E+00
   Friction velocity        uk    :  0.80577E-02 0.89045E+00
   Dimensionless distance   yplus :  0.64870E-01 0.71687E+01
   Friction thermal sca.    tstar : -0.11011E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48400E-01 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10389E-01      33   0.25666E-03   0.38942E+01 0.18561E+03 
c  Velocity[X]                                      0.19919E+01 
c  Velocity[Y]                                      0.19023E+01 
c  Velocity[Z]                                      0.91680E-30 
c  Pressure     0.11334E-06     522   0.99133E-08   0.11065E+00 0.74616E+03 
c  nu_tilda     0.84691E-05      33   0.26050E-05   0.74546E-06 0.21518E+03 
c  TempC        0.43908E+02      26   0.24588E-03   0.52865E+01 0.25568E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3095          9.0205          4.5729          4.5729
v  Velocity[Y]            -2.6286          7.1658         0.21777         0.21777
v  Velocity[Z]       -9.9717e-015     8.8008e-015    -1.3607e-017    -1.3607e-017
v  ǁVelocityǁ         0.0022006          9.0207           5.036           5.036
v  Pressure               -26.952          25.121         -1.2651         -1.2651
v  nu_tilda            4.399e-007       0.0045461       0.0017794       0.0017794
v  TempC                       21          73.067           22.05           22.05
v  TurbVisc           3.2932e-014        0.005358        0.002092        0.002092
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2909:        0.21920E+01

===============================================================


 INSTANT    0.291000000E+04   TIME STEP NUMBER            2910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15662E-01 0.88969E+00
   Friction velocity        uk    :  0.15662E-01 0.88969E+00
   Dimensionless distance   yplus :  0.12609E+00 0.71626E+01
   Friction thermal sca.    tstar : -0.12996E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.94079E-01 0.53441E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10388E-01      33   0.19009E-03   0.38805E+01 0.18556E+03 
c  Velocity[X]                                      0.19623E+01 
c  Velocity[Y]                                      0.19182E+01 
c  Velocity[Z]                                      0.11448E-29 
c  Pressure     0.95075E-07     488   0.96523E-08   0.91426E-01 0.70405E+03 
c  nu_tilda     0.84688E-05      33   0.12588E-04   0.74563E-06 0.21520E+03 
c  TempC        0.43906E+02      27   0.33115E-03   0.51493E+01 0.24106E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.309          9.0206          4.5729          4.5729
v  Velocity[Y]            -2.6276          7.1884         0.21755         0.21755
v  Velocity[Z]       -1.0092e-014     8.8131e-015    -1.3588e-017    -1.3588e-017
v  ǁVelocityǁ         0.0022111          9.0209          5.0361          5.0361
v  Pressure               -27.024          25.146         -1.3034         -1.3034
v  nu_tilda           4.3989e-007       0.0045463       0.0017792       0.0017792
v  TempC                       21          73.069           22.05           22.05
v  TurbVisc           3.2945e-014       0.0053581       0.0020919       0.0020919
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2910:        0.21150E+01

===============================================================


 INSTANT    0.291100000E+04   TIME STEP NUMBER            2911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17771E-01 0.89110E+00
   Friction velocity        uk    :  0.17771E-01 0.89110E+00
   Dimensionless distance   yplus :  0.14307E+00 0.71740E+01
   Friction thermal sca.    tstar : -0.12777E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10675E+00 0.53526E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10386E-01      33   0.24412E-03   0.38531E+01 0.18532E+03 
c  Velocity[X]                                      0.19514E+01 
c  Velocity[Y]                                      0.19016E+01 
c  Velocity[Z]                                      0.92224E-30 
c  Pressure     0.10921E-06     522   0.98255E-08   0.10349E+00 0.85931E+03 
c  nu_tilda     0.84685E-05      33   0.26059E-05   0.74578E-06 0.21522E+03 
c  TempC        0.43904E+02      27   0.29770E-03   0.58602E+01 0.27982E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3085          9.0208          4.5729          4.5729
v  Velocity[Y]            -2.6265          7.1944         0.21733         0.21733
v  Velocity[Z]       -1.0181e-014     8.7949e-015    -1.3567e-017    -1.3567e-017
v  ǁVelocityǁ         0.0015839          9.0211          5.0361          5.0361
v  Pressure               -26.956          25.193         -1.2562         -1.2562
v  nu_tilda           4.3985e-007       0.0045464       0.0017792       0.0017792
v  TempC                       21           73.07           22.05           22.05
v  TurbVisc           3.2941e-014       0.0053582       0.0020918       0.0020918
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2911:        0.22010E+01

===============================================================


 INSTANT    0.291200000E+04   TIME STEP NUMBER            2912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.13857E-01 0.89077E+00
   Friction velocity        uk    :  0.13857E-01 0.89077E+00
   Dimensionless distance   yplus :  0.11156E+00 0.71713E+01
   Friction thermal sca.    tstar : -0.16213E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83233E-01 0.53506E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10384E-01      33   0.24039E-03   0.38913E+01 0.18549E+03 
c  Velocity[X]                                      0.19944E+01 
c  Velocity[Y]                                      0.18969E+01 
c  Velocity[Z]                                      0.81401E-30 
c  Pressure     0.10234E-06     553   0.92949E-08   0.99997E-01 0.14706E+04 
c  nu_tilda     0.84682E-05      33   0.12585E-04   0.74597E-06 0.21524E+03 
c  TempC        0.43903E+02      26   0.31909E-03   0.49356E+01 0.26144E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3081           9.021          4.5729          4.5729
v  Velocity[Y]            -2.6254          7.1678         0.21711         0.21711
v  Velocity[Z]       -1.0314e-014     8.8058e-015    -1.3549e-017    -1.3549e-017
v  ǁVelocityǁ         0.0022888          9.0212          5.0361          5.0361
v  Pressure               -27.023          25.034         -1.3293         -1.3293
v  nu_tilda           4.3986e-007       0.0045465        0.001779        0.001779
v  TempC                       21          73.069           22.05           22.05
v  TurbVisc           3.2931e-014       0.0053584       0.0020917       0.0020917
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2912:        0.22620E+01

===============================================================


 INSTANT    0.291300000E+04   TIME STEP NUMBER            2913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16381E-01 0.88941E+00
   Friction velocity        uk    :  0.16381E-01 0.88941E+00
   Dimensionless distance   yplus :  0.13188E+00 0.71604E+01
   Friction thermal sca.    tstar : -0.15480E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98396E-01 0.53424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10383E-01      33   0.23565E-03   0.38637E+01 0.18536E+03 
c  Velocity[X]                                      0.19543E+01 
c  Velocity[Y]                                      0.19094E+01 
c  Velocity[Z]                                      0.88152E-30 
c  Pressure     0.88085E-07     585   0.93243E-08   0.84650E-01 0.15328E+04 
c  nu_tilda     0.84679E-05      33   0.26116E-05   0.74612E-06 0.21526E+03 
c  TempC        0.43901E+02      26   0.27020E-03   0.47962E+01 0.25124E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3076          9.0212          4.5729          4.5729
v  Velocity[Y]            -2.6244          7.1881         0.21688         0.21688
v  Velocity[Z]       -1.0393e-014     8.7894e-015     -1.353e-017     -1.353e-017
v  ǁVelocityǁ        0.00032029          9.0214          5.0362          5.0362
v  Pressure               -26.958           25.21         -1.2563         -1.2563
v  nu_tilda           4.3982e-007       0.0045466        0.001779        0.001779
v  TempC                       21          73.066           22.05           22.05
v  TurbVisc           3.2933e-014       0.0053585       0.0020915       0.0020915
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2913:        0.23490E+01

===============================================================


 INSTANT    0.291400000E+04   TIME STEP NUMBER            2914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.48995E-02 0.89027E+00
   Friction velocity        uk    :  0.48995E-02 0.89027E+00
   Dimensionless distance   yplus :  0.39444E-01 0.71673E+01
   Friction thermal sca.    tstar : -0.24359E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.29430E-01 0.53476E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10381E-01      33   0.25690E-03   0.38582E+01 0.18530E+03 
c  Velocity[X]                                      0.19637E+01 
c  Velocity[Y]                                      0.18946E+01 
c  Velocity[Z]                                      0.99535E-30 
c  Pressure     0.10708E-06     584   0.97224E-08   0.10284E+00 0.21775E+04 
c  nu_tilda     0.84676E-05      33   0.12581E-04   0.74630E-06 0.21528E+03 
c  TempC        0.43900E+02      26   0.26186E-03   0.54108E+01 0.24696E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.307          9.0213          4.5729          4.5729
v  Velocity[Y]            -2.6234          7.1602         0.21666         0.21666
v  Velocity[Z]       -1.0557e-014     8.7985e-015    -1.3505e-017    -1.3505e-017
v  ǁVelocityǁ         0.0023918          9.0216          5.0362          5.0362
v  Pressure               -27.018          24.952         -1.3556         -1.3556
v  nu_tilda           4.3982e-007       0.0045467       0.0017789       0.0017789
v  TempC                       21          73.065           22.05           22.05
v  TurbVisc           3.2921e-014       0.0053587       0.0020914       0.0020914
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2914:        0.23360E+01

===============================================================


 INSTANT    0.291500000E+04   TIME STEP NUMBER            2915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.65264E-02 0.88963E+00
   Friction velocity        uk    :  0.65264E-02 0.88963E+00
   Dimensionless distance   yplus :  0.52542E-01 0.71621E+01
   Friction thermal sca.    tstar : -0.40236E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.39202E-01 0.53438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10379E-01      33   0.20713E-03   0.38769E+01 0.18534E+03 
c  Velocity[X]                                      0.19895E+01 
c  Velocity[Y]                                      0.18874E+01 
c  Velocity[Z]                                      0.99403E-30 
c  Pressure     0.10884E-06     538   0.99784E-08   0.10366E+00 0.22577E+04 
c  nu_tilda     0.84673E-05      33   0.26108E-05   0.74644E-06 0.21530E+03 
c  TempC        0.43898E+02      26   0.35410E-03   0.54846E+01 0.25854E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3066          9.0215          4.5729          4.5729
v  Velocity[Y]            -2.6224          7.1877         0.21643         0.21643
v  Velocity[Z]        -1.063e-014     8.7851e-015    -1.3492e-017    -1.3492e-017
v  ǁVelocityǁ         0.0015879          9.0217          5.0362          5.0362
v  Pressure                -26.96          25.224         -1.2551         -1.2551
v  nu_tilda           4.3983e-007       0.0045468       0.0017789       0.0017789
v  TempC                       21          73.064           22.05           22.05
v  TurbVisc           3.2921e-014       0.0053588       0.0020913       0.0020913
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2915:        0.22200E+01

===============================================================


 INSTANT    0.291600000E+04   TIME STEP NUMBER            2916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.80340E-02 0.89094E+00
   Friction velocity        uk    :  0.80340E-02 0.89094E+00
   Dimensionless distance   yplus :  0.64679E-01 0.71727E+01
   Friction thermal sca.    tstar : -0.26605E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.48258E-01 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10378E-01      33   0.23967E-03   0.38494E+01 0.18523E+03 
c  Velocity[X]                                      0.19463E+01 
c  Velocity[Y]                                      0.19031E+01 
c  Velocity[Z]                                      0.10349E-29 
c  Pressure     0.90940E-07     522   0.93283E-08   0.87261E-01 0.12810E+04 
c  nu_tilda     0.84669E-05      33   0.12576E-04   0.74661E-06 0.21532E+03 
c  TempC        0.43897E+02      26   0.28481E-03   0.66193E+01 0.30444E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3061          9.0217          4.5729          4.5729
v  Velocity[Y]            -2.6213          7.1944          0.2162          0.2162
v  Velocity[Z]       -1.0827e-014     8.7947e-015    -1.3472e-017    -1.3472e-017
v  ǁVelocityǁ         0.0024443          9.0219          5.0363          5.0363
v  Pressure               -27.024          25.114         -1.3217         -1.3217
v  nu_tilda           4.3984e-007        0.004547       0.0017787       0.0017787
v  TempC                       21          73.063          22.049          22.049
v  TurbVisc           3.2924e-014       0.0053589       0.0020912       0.0020912
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2916:        0.21970E+01

===============================================================


 INSTANT    0.291700000E+04   TIME STEP NUMBER            2917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.95736E-02 0.89053E+00
   Friction velocity        uk    :  0.95736E-02 0.89053E+00
   Dimensionless distance   yplus :  0.77074E-01 0.71694E+01
   Friction thermal sca.    tstar : -0.27321E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57506E-01 0.53492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10376E-01      33   0.23607E-03   0.38661E+01 0.18516E+03 
c  Velocity[X]                                      0.19791E+01 
c  Velocity[Y]                                      0.18870E+01 
c  Velocity[Z]                                      0.85683E-30 
c  Pressure     0.11978E-06     504   0.97571E-08   0.11518E+00 0.64731E+03 
c  nu_tilda     0.84666E-05      33   0.26179E-05   0.74677E-06 0.21534E+03 
c  TempC        0.43895E+02      27   0.27022E-03   0.60707E+01 0.26137E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3055          9.0218          4.5729          4.5729
v  Velocity[Y]            -2.6202           7.164         0.21597         0.21597
v  Velocity[Z]       -1.0815e-014     8.7761e-015    -1.3454e-017    -1.3454e-017
v  ǁVelocityǁ         0.0025118          9.0221          5.0363          5.0363
v  Pressure               -26.954          25.076         -1.2892         -1.2892
v  nu_tilda           4.3994e-007       0.0045471       0.0017787       0.0017787
v  TempC                       21           73.06          22.049          22.049
v  TurbVisc           3.2928e-014       0.0053591       0.0020911       0.0020911
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2917:        0.21510E+01

===============================================================


 INSTANT    0.291800000E+04   TIME STEP NUMBER            2918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12948E-01 0.88929E+00
   Friction velocity        uk    :  0.12948E-01 0.88929E+00
   Dimensionless distance   yplus :  0.10424E+00 0.71594E+01
   Friction thermal sca.    tstar : -0.16489E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.77776E-01 0.53417E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10374E-01      33   0.24139E-03   0.38588E+01 0.18514E+03 
c  Velocity[X]                                      0.19788E+01 
c  Velocity[Y]                                      0.18800E+01 
c  Velocity[Z]                                      0.83205E-30 
c  Pressure     0.89037E-07     569   0.93756E-08   0.85759E-01 0.74401E+03 
c  nu_tilda     0.84663E-05      33   0.12576E-04   0.74696E-06 0.21536E+03 
c  TempC        0.43893E+02      26   0.29513E-03   0.48370E+01 0.23752E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.305           9.022          4.5729          4.5729
v  Velocity[Y]            -2.6192          7.1849         0.21574         0.21574
v  Velocity[Z]       -1.0815e-014      8.787e-015    -1.3436e-017    -1.3436e-017
v  ǁVelocityǁ         0.0017668          9.0222          5.0363          5.0363
v  Pressure                -27.02          25.085          -1.331          -1.331
v  nu_tilda           4.3995e-007       0.0045472       0.0017785       0.0017785
v  TempC                       21          73.059          22.049          22.049
v  TurbVisc           3.2955e-014       0.0053592        0.002091        0.002091
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2918:        0.22710E+01

===============================================================


 INSTANT    0.291900000E+04   TIME STEP NUMBER            2919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14763E-01 0.89043E+00
   Friction velocity        uk    :  0.14763E-01 0.89043E+00
   Dimensionless distance   yplus :  0.11885E+00 0.71686E+01
   Friction thermal sca.    tstar : -0.14692E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88675E-01 0.53486E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10373E-01      33   0.25097E-03   0.38561E+01 0.18511E+03 
c  Velocity[X]                                      0.19616E+01 
c  Velocity[Y]                                      0.18945E+01 
c  Velocity[Z]                                      0.88642E-30 
c  Pressure     0.10898E-06     537   0.94083E-08   0.10523E+00 0.86412E+03 
c  nu_tilda     0.84659E-05      33   0.26176E-05   0.74711E-06 0.21538E+03 
c  TempC        0.43892E+02      26   0.26369E-03   0.42704E+01 0.24859E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3045          9.0221          4.5729          4.5729
v  Velocity[Y]            -2.6182          7.1643          0.2155          0.2155
v  Velocity[Z]       -1.0656e-014     8.7704e-015    -1.3418e-017    -1.3418e-017
v  ǁVelocityǁ         0.0026303          9.0224          5.0363          5.0363
v  Pressure               -26.952          25.108         -1.2823         -1.2823
v  nu_tilda           4.3995e-007       0.0045473       0.0017785       0.0017785
v  TempC                       21          73.058          22.049          22.049
v  TurbVisc           3.2959e-014       0.0053594       0.0020909       0.0020909
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2919:        0.24650E+01

===============================================================


 INSTANT    0.292000000E+04   TIME STEP NUMBER            2920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16028E-01 0.88951E+00
   Friction velocity        uk    :  0.16028E-01 0.88951E+00
   Dimensionless distance   yplus :  0.12904E+00 0.71612E+01
   Friction thermal sca.    tstar : -0.12752E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.96276E-01 0.53430E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10371E-01      33   0.20838E-03   0.38412E+01 0.18501E+03 
c  Velocity[X]                                      0.19620E+01 
c  Velocity[Y]                                      0.18792E+01 
c  Velocity[Z]                                      0.11952E-29 
c  Pressure     0.10511E-06     537   0.92486E-08   0.99791E-01 0.10430E+04 
c  nu_tilda     0.84656E-05      33   0.12570E-04   0.74729E-06 0.21540E+03 
c  TempC        0.43890E+02      26   0.31194E-03   0.40983E+01 0.23834E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3039          9.0223          4.5729          4.5729
v  Velocity[Y]            -2.6172          7.1838         0.21527         0.21527
v  Velocity[Z]       -1.0675e-014     8.7803e-015    -1.3406e-017    -1.3406e-017
v  ǁVelocityǁ         0.0010557          9.0226          5.0364          5.0364
v  Pressure               -27.015          25.045         -1.3393         -1.3393
v  nu_tilda           4.3993e-007       0.0045474       0.0017783       0.0017783
v  TempC                       21          73.057          22.049          22.049
v  TurbVisc           3.2959e-014       0.0053595       0.0020908       0.0020908
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2920:        0.24730E+01

===============================================================


 INSTANT    0.292100000E+04   TIME STEP NUMBER            2921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.11436E-01 0.89120E+00
   Friction velocity        uk    :  0.11436E-01 0.89120E+00
   Dimensionless distance   yplus :  0.92066E-01 0.71748E+01
   Friction thermal sca.    tstar : -0.11690E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.68691E-01 0.53532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10369E-01      33   0.25632E-03   0.38431E+01 0.18499E+03 
c  Velocity[X]                                      0.19704E+01 
c  Velocity[Y]                                      0.18727E+01 
c  Velocity[Z]                                      0.79339E-30 
c  Pressure     0.10735E-06     568   0.98080E-08   0.10305E+00 0.13043E+04 
c  nu_tilda     0.84652E-05      33   0.26234E-05   0.74744E-06 0.21542E+03 
c  TempC        0.43888E+02      27   0.31825E-03   0.38317E+01 0.23348E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3035          9.0225          4.5729          4.5729
v  Velocity[Y]            -2.6161          7.1971         0.21503         0.21503
v  Velocity[Z]       -1.0501e-014     8.7641e-015    -1.3385e-017    -1.3385e-017
v  ǁVelocityǁ         0.0027345          9.0228          5.0364          5.0364
v  Pressure               -26.951           25.17         -1.2738         -1.2738
v  nu_tilda           4.3989e-007       0.0045476       0.0017783       0.0017783
v  TempC                       21          73.056          22.049          22.049
v  TurbVisc           3.2954e-014       0.0053596       0.0020907       0.0020907
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2921:        0.22970E+01

===============================================================


 INSTANT    0.292200000E+04   TIME STEP NUMBER            2922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17106E-01 0.89085E+00
   Friction velocity        uk    :  0.17106E-01 0.89085E+00
   Dimensionless distance   yplus :  0.13771E+00 0.71719E+01
   Friction thermal sca.    tstar : -0.10647E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10275E+00 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10368E-01      33   0.23432E-03   0.38596E+01 0.18505E+03 
c  Velocity[X]                                      0.19712E+01 
c  Velocity[Y]                                      0.18884E+01 
c  Velocity[Z]                                      0.83442E-30 
c  Pressure     0.10536E-06     554   0.98452E-08   0.10248E+00 0.16042E+04 
c  nu_tilda     0.84649E-05      33   0.12568E-04   0.74762E-06 0.21544E+03 
c  TempC        0.43887E+02      26   0.24558E-03   0.43920E+01 0.23751E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3029          9.0227          4.5729          4.5729
v  Velocity[Y]             -2.615          7.1677         0.21479         0.21479
v  Velocity[Z]       -1.0554e-014     8.7736e-015    -1.3371e-017    -1.3371e-017
v  ǁVelocityǁ        0.00077357           9.023          5.0364          5.0364
v  Pressure               -27.013          24.996          -1.351          -1.351
v  nu_tilda           4.3989e-007       0.0045477       0.0017781       0.0017781
v  TempC                       21          73.053          22.049          22.049
v  TurbVisc           3.2941e-014       0.0053598       0.0020906       0.0020906
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2922:        0.22660E+01

===============================================================


 INSTANT    0.292300000E+04   TIME STEP NUMBER            2923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.97896E-02 0.88937E+00
   Friction velocity        uk    :  0.97896E-02 0.88937E+00
   Dimensionless distance   yplus :  0.78813E-01 0.71600E+01
   Friction thermal sca.    tstar : -0.10235E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.58803E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10366E-01      33   0.24002E-03   0.38353E+01 0.18482E+03 
c  Velocity[X]                                      0.19644E+01 
c  Velocity[Y]                                      0.18709E+01 
c  Velocity[Z]                                      0.82566E-30 
c  Pressure     0.10650E-06     568   0.95987E-08   0.10051E+00 0.13357E+04 
c  nu_tilda     0.84645E-05      33   0.26242E-05   0.74778E-06 0.21546E+03 
c  TempC        0.43885E+02      27   0.33234E-03   0.43820E+01 0.23883E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3024          9.0229          4.5729          4.5729
v  Velocity[Y]             -2.614          7.1847         0.21455         0.21455
v  Velocity[Z]        -1.037e-014     8.7558e-015    -1.3352e-017    -1.3352e-017
v  ǁVelocityǁ         0.0028863          9.0232          5.0365          5.0365
v  Pressure               -26.946           25.13          -1.284          -1.284
v  nu_tilda           4.3988e-007       0.0045479       0.0017781       0.0017781
v  TempC                       21          73.054          22.049          22.049
v  TurbVisc           3.2941e-014         0.00536       0.0020905       0.0020905
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2923:        0.22870E+01

===============================================================


 INSTANT    0.292400000E+04   TIME STEP NUMBER            2924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16546E-01 0.89052E+00
   Friction velocity        uk    :  0.16546E-01 0.89052E+00
   Dimensionless distance   yplus :  0.13320E+00 0.71693E+01
   Friction thermal sca.    tstar : -0.91488E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99385E-01 0.53491E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10364E-01      33   0.25721E-03   0.38575E+01 0.18493E+03 
c  Velocity[X]                                      0.19927E+01 
c  Velocity[Y]                                      0.18648E+01 
c  Velocity[Z]                                      0.85396E-30 
c  Pressure     0.10317E-06     538   0.97671E-08   0.10014E+00 0.14067E+04 
c  nu_tilda     0.84642E-05      33   0.12565E-04   0.74799E-06 0.21548E+03 
c  TempC        0.43883E+02      27   0.31087E-03   0.57466E+01 0.28248E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3019          9.0231          4.5729          4.5729
v  Velocity[Y]             -2.613           7.163         0.21431         0.21431
v  Velocity[Z]       -1.0453e-014     8.7659e-015     -1.334e-017     -1.334e-017
v  ǁVelocityǁ         0.0007705          9.0234          5.0365          5.0365
v  Pressure               -27.009          24.979         -1.3531         -1.3531
v  nu_tilda           4.3993e-007        0.004548        0.001778        0.001778
v  TempC                       21          73.054          22.049          22.049
v  TurbVisc           3.2938e-014       0.0053601       0.0020904       0.0020904
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2924:        0.22320E+01

===============================================================


 INSTANT    0.292500000E+04   TIME STEP NUMBER            2925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96182E-02 0.88978E+00
   Friction velocity        uk    :  0.96182E-02 0.88978E+00
   Dimensionless distance   yplus :  0.77433E-01 0.71634E+01
   Friction thermal sca.    tstar : -0.90929E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57774E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10363E-01      33   0.23535E-03   0.38408E+01 0.18483E+03 
c  Velocity[X]                                      0.19616E+01 
c  Velocity[Y]                                      0.18792E+01 
c  Velocity[Z]                                      0.93433E-30 
c  Pressure     0.88238E-07     586   0.99348E-08   0.84587E-01 0.17386E+04 
c  nu_tilda     0.84638E-05      33   0.26299E-05   0.74813E-06 0.21550E+03 
c  TempC        0.43882E+02      27   0.32388E-03   0.53967E+01 0.26991E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3014          9.0232          4.5729          4.5729
v  Velocity[Y]             -2.612          7.1881         0.21407         0.21407
v  Velocity[Z]       -1.0243e-014     8.7502e-015    -1.3325e-017    -1.3325e-017
v  ǁVelocityǁ         0.0030453          9.0236          5.0365          5.0365
v  Pressure                -26.94          25.182           -1.27           -1.27
v  nu_tilda           4.3993e-007       0.0045481       0.0017779       0.0017779
v  TempC                       21          73.055          22.049          22.049
v  TurbVisc           3.2953e-014       0.0053603       0.0020903       0.0020903
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2925:        0.23470E+01

===============================================================


 INSTANT    0.292600000E+04   TIME STEP NUMBER            2926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17074E-01 0.89087E+00
   Friction velocity        uk    :  0.17074E-01 0.89087E+00
   Dimensionless distance   yplus :  0.13746E+00 0.71721E+01
   Friction thermal sca.    tstar : -0.84255E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10256E+00 0.53512E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10361E-01      33   0.23645E-03   0.38066E+01 0.18462E+03 
c  Velocity[X]                                      0.19411E+01 
c  Velocity[Y]                                      0.18655E+01 
c  Velocity[Z]                                      0.10938E-29 
c  Pressure     0.96937E-07     538   0.97451E-08   0.92405E-01 0.12285E+04 
c  nu_tilda     0.84634E-05      33   0.12561E-04   0.74831E-06 0.21552E+03 
c  TempC        0.43880E+02      26   0.28720E-03   0.61987E+01 0.27239E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3009          9.0234          4.5729          4.5729
v  Velocity[Y]            -2.6109           7.192         0.21383         0.21383
v  Velocity[Z]       -1.0371e-014     8.7604e-015    -1.3314e-017    -1.3314e-017
v  ǁVelocityǁ         0.0010267          9.0237          5.0365          5.0365
v  Pressure               -27.006          25.068         -1.3339         -1.3339
v  nu_tilda            4.399e-007       0.0045482       0.0017778       0.0017778
v  TempC                       21          73.054          22.049          22.049
v  TurbVisc           3.2953e-014       0.0053604       0.0020902       0.0020902
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2926:        0.22210E+01

===============================================================


 INSTANT    0.292700000E+04   TIME STEP NUMBER            2927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.10962E-01 0.89061E+00
   Friction velocity        uk    :  0.10962E-01 0.89061E+00
   Dimensionless distance   yplus :  0.88248E-01 0.71700E+01
   Friction thermal sca.    tstar : -0.86406E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.65843E-01 0.53496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10359E-01      33   0.27526E-03   0.38331E+01 0.18470E+03 
c  Velocity[X]                                      0.19762E+01 
c  Velocity[Y]                                      0.18568E+01 
c  Velocity[Z]                                      0.78572E-30 
c  Pressure     0.10627E-06     520   0.95192E-08   0.10312E+00 0.65986E+03 
c  nu_tilda     0.84630E-05      33   0.26300E-05   0.74847E-06 0.21554E+03 
c  TempC        0.43878E+02      26   0.24154E-03   0.58464E+01 0.26712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3003          9.0236          4.5729          4.5729
v  Velocity[Y]            -2.6098          7.1664         0.21358         0.21358
v  Velocity[Z]       -1.0147e-014      8.742e-015    -1.3294e-017    -1.3294e-017
v  ǁVelocityǁ         0.0024918          9.0239          5.0366          5.0366
v  Pressure               -26.933          25.052         -1.2995         -1.2995
v  nu_tilda           4.3996e-007       0.0045484       0.0017778       0.0017778
v  TempC                       21          73.055          22.049          22.049
v  TurbVisc           3.2945e-014       0.0053606         0.00209         0.00209
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2927:        0.21840E+01

===============================================================


 INSTANT    0.292800000E+04   TIME STEP NUMBER            2928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15611E-01 0.88926E+00
   Friction velocity        uk    :  0.15611E-01 0.88926E+00
   Dimensionless distance   yplus :  0.12568E+00 0.71592E+01
   Friction thermal sca.    tstar : -0.77788E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93769E-01 0.53415E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10358E-01      33   0.24937E-03   0.38616E+01 0.18487E+03 
c  Velocity[X]                                      0.19874E+01 
c  Velocity[Y]                                      0.18742E+01 
c  Velocity[Z]                                      0.84253E-30 
c  Pressure     0.12100E-06     490   0.93268E-08   0.11567E+00 0.76589E+03 
c  nu_tilda     0.84626E-05      33   0.12560E-04   0.74867E-06 0.21556E+03 
c  TempC        0.43876E+02      26   0.36741E-03   0.44275E+01 0.24408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2998          9.0238          4.5729          4.5729
v  Velocity[Y]            -2.6088          7.1861         0.21334         0.21334
v  Velocity[Z]       -1.0322e-014     8.7529e-015    -1.3277e-017    -1.3277e-017
v  ǁVelocityǁ         0.0017037          9.0241          5.0366          5.0366
v  Pressure               -26.997          25.046         -1.3426         -1.3426
v  nu_tilda           4.3996e-007       0.0045485       0.0017776       0.0017776
v  TempC                       21          73.056          22.049          22.049
v  TurbVisc           3.2961e-014       0.0053607       0.0020899       0.0020899
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2928:        0.21110E+01

===============================================================


 INSTANT    0.292900000E+04   TIME STEP NUMBER            2929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.14231E-01 0.89048E+00
   Friction velocity        uk    :  0.14231E-01 0.89048E+00
   Dimensionless distance   yplus :  0.11457E+00 0.71690E+01
   Friction thermal sca.    tstar : -0.75699E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85484E-01 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10356E-01      33   0.22249E-03   0.38459E+01 0.18463E+03 
c  Velocity[X]                                      0.19893E+01 
c  Velocity[Y]                                      0.18566E+01 
c  Velocity[Z]                                      0.13719E-29 
c  Pressure     0.12035E-06     506   0.98236E-08   0.11522E+00 0.78931E+03 
c  nu_tilda     0.84622E-05      33   0.26366E-05   0.74883E-06 0.21559E+03 
c  TempC        0.43875E+02      27   0.24384E-03   0.64994E+01 0.29194E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2992           9.024          4.5729          4.5729
v  Velocity[Y]            -2.6077           7.161         0.21309         0.21309
v  Velocity[Z]       -1.0074e-014     8.7361e-015    -1.3267e-017    -1.3267e-017
v  ǁVelocityǁ         0.0014694          9.0243          5.0366          5.0366
v  Pressure               -26.929          25.044         -1.2981         -1.2981
v  nu_tilda           4.3994e-007       0.0045486       0.0017776       0.0017776
v  TempC                       21          73.058          22.048          22.048
v  TurbVisc           3.2962e-014       0.0053609       0.0020898       0.0020898
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2929:        0.21580E+01

===============================================================


 INSTANT    0.293000000E+04   TIME STEP NUMBER            2930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.12483E-01 0.88981E+00
   Friction velocity        uk    :  0.12483E-01 0.88981E+00
   Dimensionless distance   yplus :  0.10050E+00 0.71636E+01
   Friction thermal sca.    tstar : -0.72814E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.74984E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10354E-01      33   0.19378E-03   0.38088E+01 0.18445E+03 
c  Velocity[X]                                      0.19610E+01 
c  Velocity[Y]                                      0.18478E+01 
c  Velocity[Z]                                      0.85723E-30 
c  Pressure     0.10068E-06     505   0.93850E-08   0.97159E-01 0.68195E+03 
c  nu_tilda     0.84618E-05      33   0.12556E-04   0.74902E-06 0.21561E+03 
c  TempC        0.43873E+02      26   0.23048E-03   0.43716E+01 0.23600E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2987          9.0242          4.5729          4.5729
v  Velocity[Y]            -2.6067          7.1868         0.21284         0.21284
v  Velocity[Z]        -1.026e-014     8.7458e-015    -1.3255e-017    -1.3255e-017
v  ǁVelocityǁ         0.0027585          9.0245          5.0366          5.0366
v  Pressure               -26.992          25.061          -1.335          -1.335
v  nu_tilda           4.3993e-007       0.0045487       0.0017774       0.0017774
v  TempC                       21          73.059          22.048          22.048
v  TurbVisc           3.2958e-014        0.005361       0.0020897       0.0020897
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2930:        0.21530E+01

===============================================================


 INSTANT    0.293100000E+04   TIME STEP NUMBER            2931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17143E-01 0.89139E+00
   Friction velocity        uk    :  0.17143E-01 0.89139E+00
   Dimensionless distance   yplus :  0.13801E+00 0.71763E+01
   Friction thermal sca.    tstar : -0.72661E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10297E+00 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10353E-01      33   0.26199E-03   0.37990E+01 0.18442E+03 
c  Velocity[X]                                      0.19360E+01 
c  Velocity[Y]                                      0.18630E+01 
c  Velocity[Z]                                      0.76589E-30 
c  Pressure     0.93987E-07     569   0.99843E-08   0.90015E-01 0.12303E+04 
c  nu_tilda     0.84614E-05      33   0.26372E-05   0.74918E-06 0.21563E+03 
c  TempC        0.43871E+02      27   0.32365E-03   0.40455E+01 0.22542E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2981          9.0243          4.5729          4.5729
v  Velocity[Y]            -2.6057          7.1975         0.21259         0.21259
v  Velocity[Z]       -1.0015e-014     8.7291e-015    -1.3237e-017    -1.3237e-017
v  ǁVelocityǁ        0.00094767          9.0246          5.0367          5.0367
v  Pressure               -26.926          25.173         -1.2715         -1.2715
v  nu_tilda           4.3987e-007       0.0045489       0.0017774       0.0017774
v  TempC                       21          73.057          22.048          22.048
v  TurbVisc           3.2954e-014       0.0053612       0.0020896       0.0020896
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2931:        0.22970E+01

===============================================================


 INSTANT    0.293200000E+04   TIME STEP NUMBER            2932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.57767E-02 0.89092E+00
   Friction velocity        uk    :  0.57767E-02 0.89092E+00
   Dimensionless distance   yplus :  0.46507E-01 0.71725E+01
   Friction thermal sca.    tstar : -0.69514E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.34699E-01 0.53515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10351E-01      33   0.24006E-03   0.38393E+01 0.18457E+03 
c  Velocity[X]                                      0.19877E+01 
c  Velocity[Y]                                      0.18516E+01 
c  Velocity[Z]                                      0.83569E-30 
c  Pressure     0.12430E-06     600   0.98281E-08   0.11911E+00 0.21459E+04 
c  nu_tilda     0.84610E-05      33   0.12552E-04   0.74937E-06 0.21565E+03 
c  TempC        0.43869E+02      27   0.30864E-03   0.55654E+01 0.28281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2975          9.0245          4.5729          4.5729
v  Velocity[Y]            -2.6047          7.1655         0.21234         0.21234
v  Velocity[Z]       -1.0231e-014     8.7376e-015    -1.3226e-017    -1.3226e-017
v  ǁVelocityǁ         0.0021832          9.0248          5.0367          5.0367
v  Pressure               -26.982          24.911         -1.3671         -1.3671
v  nu_tilda           4.3992e-007        0.004549       0.0017772       0.0017772
v  TempC                       21          73.059          22.048          22.048
v  TurbVisc           3.2935e-014       0.0053613       0.0020895       0.0020895
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2932:        0.23860E+01

===============================================================


 INSTANT    0.293300000E+04   TIME STEP NUMBER            2933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15308E-01 0.88990E+00
   Friction velocity        uk    :  0.15308E-01 0.88990E+00
   Dimensionless distance   yplus :  0.12324E+00 0.71643E+01
   Friction thermal sca.    tstar : -0.67001E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91951E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10349E-01      33   0.24727E-03   0.38147E+01 0.18441E+03 
c  Velocity[X]                                      0.19733E+01 
c  Velocity[Y]                                      0.18413E+01 
c  Velocity[Z]                                      0.86432E-30 
c  Pressure     0.99995E-07     568   0.92814E-08   0.96306E-01 0.22052E+04 
c  nu_tilda     0.84606E-05      33   0.26418E-05   0.74952E-06 0.21567E+03 
c  TempC        0.43868E+02      26   0.30002E-03   0.55717E+01 0.26461E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.297          9.0247          4.5729          4.5729
v  Velocity[Y]            -2.6036          7.1887         0.21209         0.21209
v  Velocity[Z]       -9.9568e-015     8.7236e-015    -1.3205e-017    -1.3205e-017
v  ǁVelocityǁ         0.0024351           9.025          5.0367          5.0367
v  Pressure                -26.92           25.18         -1.2681         -1.2681
v  nu_tilda            4.399e-007       0.0045491       0.0017772       0.0017772
v  TempC                       21          73.061          22.048          22.048
v  TurbVisc            3.295e-014       0.0053615       0.0020894       0.0020894
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2933:        0.23000E+01

===============================================================


 INSTANT    0.293400000E+04   TIME STEP NUMBER            2934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16291E-01 0.89068E+00
   Friction velocity        uk    :  0.16291E-01 0.89068E+00
   Dimensionless distance   yplus :  0.13116E+00 0.71705E+01
   Friction thermal sca.    tstar : -0.65557E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97857E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10348E-01      33   0.24871E-03   0.38187E+01 0.18442E+03 
c  Velocity[X]                                      0.19600E+01 
c  Velocity[Y]                                      0.18587E+01 
c  Velocity[Z]                                      0.11600E-29 
c  Pressure     0.90302E-07     570   0.99370E-08   0.87776E-01 0.19507E+04 
c  nu_tilda     0.84602E-05      33   0.12549E-04   0.74972E-06 0.21569E+03 
c  TempC        0.43866E+02      26   0.26091E-03   0.52221E+01 0.25146E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2964          9.0249          4.5729          4.5729
v  Velocity[Y]            -2.6025          7.1659         0.21183         0.21183
v  Velocity[Z]       -1.0207e-014     8.7313e-015    -1.3195e-017    -1.3195e-017
v  ǁVelocityǁ         0.0013428          9.0252          5.0367          5.0367
v  Pressure               -26.977          24.953         -1.3569         -1.3569
v  nu_tilda           4.3988e-007       0.0045492        0.001777        0.001777
v  TempC                       21          73.062          22.048          22.048
v  TurbVisc           3.2946e-014       0.0053616       0.0020893       0.0020893
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2934:        0.23060E+01

===============================================================


 INSTANT    0.293500000E+04   TIME STEP NUMBER            2935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.76602E-02 0.88989E+00
   Friction velocity        uk    :  0.76602E-02 0.88989E+00
   Dimensionless distance   yplus :  0.61670E-01 0.71642E+01
   Friction thermal sca.    tstar : -0.63813E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.46012E-01 0.53453E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10346E-01      33   0.20737E-03   0.38129E+01 0.18425E+03 
c  Velocity[X]                                      0.19699E+01 
c  Velocity[Y]                                      0.18430E+01 
c  Velocity[Z]                                      0.87282E-30 
c  Pressure     0.11101E-06     584   0.93867E-08   0.10445E+00 0.18306E+04 
c  nu_tilda     0.84598E-05      33   0.26436E-05   0.74990E-06 0.21572E+03 
c  TempC        0.43864E+02      26   0.25673E-03   0.43192E+01 0.24070E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2959          9.0251          4.5729          4.5729
v  Velocity[Y]            -2.6015           7.187         0.21158         0.21158
v  Velocity[Z]       -9.9475e-015      8.716e-015     -1.318e-017     -1.318e-017
v  ǁVelocityǁ         0.0015778          9.0253          5.0368          5.0368
v  Pressure               -26.911          25.157         -1.2699         -1.2699
v  nu_tilda           4.3984e-007       0.0045494        0.001777        0.001777
v  TempC                       21          73.062          22.048          22.048
v  TurbVisc           3.2939e-014       0.0053618       0.0020892       0.0020892
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2935:        0.23280E+01

===============================================================


 INSTANT    0.293600000E+04   TIME STEP NUMBER            2936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.42688E-02 0.89125E+00
   Friction velocity        uk    :  0.42688E-02 0.89125E+00
   Dimensionless distance   yplus :  0.34367E-01 0.71752E+01
   Friction thermal sca.    tstar : -0.63192E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.25641E-01 0.53535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10344E-01      33   0.27278E-03   0.38146E+01 0.18430E+03 
c  Velocity[X]                                      0.19807E+01 
c  Velocity[Y]                                      0.18339E+01 
c  Velocity[Z]                                      0.75443E-30 
c  Pressure     0.10418E-06     536   0.98078E-08   0.10007E+00 0.12760E+04 
c  nu_tilda     0.84594E-05      33   0.12546E-04   0.75010E-06 0.21574E+03 
c  TempC        0.43862E+02      27   0.37342E-03   0.45603E+01 0.23181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2953          9.0252          4.5729          4.5729
v  Velocity[Y]            -2.6005           7.195         0.21132         0.21132
v  Velocity[Z]       -1.0244e-014     8.7236e-015    -1.3164e-017    -1.3164e-017
v  ǁVelocityǁ          0.001919          9.0255          5.0368          5.0368
v  Pressure               -26.972          25.053         -1.3362         -1.3362
v  nu_tilda           4.3977e-007       0.0045494       0.0017768       0.0017768
v  TempC                       21          73.062          22.048          22.048
v  TurbVisc           3.2927e-014       0.0053619       0.0020891       0.0020891
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2936:        0.22350E+01

===============================================================


 INSTANT    0.293700000E+04   TIME STEP NUMBER            2937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.96378E-02 0.89084E+00
   Friction velocity        uk    :  0.96378E-02 0.89084E+00
   Dimensionless distance   yplus :  0.77591E-01 0.71719E+01
   Friction thermal sca.    tstar : -0.61364E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.57892E-01 0.53510E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10342E-01      33   0.23206E-03   0.38143E+01 0.18426E+03 
c  Velocity[X]                                      0.19660E+01 
c  Velocity[Y]                                      0.18483E+01 
c  Velocity[Z]                                      0.10070E-29 
c  Pressure     0.10581E-06     505   0.95368E-08   0.10321E+00 0.71577E+03 
c  nu_tilda     0.84589E-05      33   0.26488E-05   0.75025E-06 0.21576E+03 
c  TempC        0.43860E+02      27   0.26070E-03   0.55457E+01 0.26457E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2948          9.0254          4.5729          4.5729
v  Velocity[Y]            -2.5995          7.1691         0.21106         0.21106
v  Velocity[Z]        -9.945e-015     8.7065e-015    -1.3141e-017    -1.3141e-017
v  ǁVelocityǁ         0.0021933          9.0257          5.0368          5.0368
v  Pressure               -26.902          25.044         -1.2968         -1.2968
v  nu_tilda           4.3976e-007       0.0045496       0.0017768       0.0017768
v  TempC                       21          73.063          22.048          22.048
v  TurbVisc           3.2906e-014        0.005362       0.0020889       0.0020889
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2937:        0.22160E+01

===============================================================


 INSTANT    0.293800000E+04   TIME STEP NUMBER            2938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.39090E-02 0.88937E+00
   Friction velocity        uk    :  0.39090E-02 0.88937E+00
   Dimensionless distance   yplus :  0.31470E-01 0.71600E+01
   Friction thermal sca.    tstar : -0.59489E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.23480E-01 0.53422E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10341E-01      33   0.25222E-03   0.37856E+01 0.18407E+03 
c  Velocity[X]                                      0.19526E+01 
c  Velocity[Y]                                      0.18329E+01 
c  Velocity[Z]                                      0.13243E-29 
c  Pressure     0.10734E-06     520   0.92109E-08   0.10170E+00 0.72009E+03 
c  nu_tilda     0.84585E-05      33   0.12545E-04   0.75044E-06 0.21578E+03 
c  TempC        0.43858E+02      27   0.25089E-03   0.38263E+01 0.21573E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2942          9.0256          4.5729          4.5729
v  Velocity[Y]            -2.5984          7.1843         0.21081         0.21081
v  Velocity[Z]       -1.0228e-014     8.7172e-015    -1.3134e-017    -1.3134e-017
v  ǁVelocityǁ         0.0028922          9.0259          5.0368          5.0368
v  Pressure               -26.966          25.037         -1.3366         -1.3366
v  nu_tilda           4.3976e-007       0.0045497       0.0017767       0.0017767
v  TempC                       21          73.065          22.048          22.048
v  TurbVisc           3.2902e-014       0.0053621       0.0020888       0.0020888
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2938:        0.21800E+01

===============================================================


 INSTANT    0.293900000E+04   TIME STEP NUMBER            2939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85676E-02 0.89067E+00
   Friction velocity        uk    :  0.85676E-02 0.89067E+00
   Dimensionless distance   yplus :  0.68975E-01 0.71705E+01
   Friction thermal sca.    tstar : -0.59182E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51463E-01 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10339E-01      33   0.25293E-03   0.38032E+01 0.18408E+03 
c  Velocity[X]                                      0.19771E+01 
c  Velocity[Y]                                      0.18261E+01 
c  Velocity[Z]                                      0.76873E-30 
c  Pressure     0.11496E-06     536   0.94891E-08   0.11152E+00 0.86348E+03 
c  nu_tilda     0.84580E-05      33   0.26496E-05   0.75062E-06 0.21580E+03 
c  TempC        0.43857E+02      26   0.35682E-03   0.47559E+01 0.24763E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2937          9.0258          4.5729          4.5729
v  Velocity[Y]            -2.5974          7.1664         0.21055         0.21055
v  Velocity[Z]       -1.0011e-014     8.6998e-015     -1.312e-017     -1.312e-017
v  ǁVelocityǁ         0.0027442          9.0261          5.0368          5.0368
v  Pressure               -26.895          25.065          -1.288          -1.288
v  nu_tilda           4.3977e-007       0.0045498       0.0017766       0.0017766
v  TempC                       21          73.064          22.048          22.048
v  TurbVisc           3.2902e-014       0.0053623       0.0020887       0.0020887
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2939:        0.22130E+01

===============================================================


 INSTANT    0.294000000E+04   TIME STEP NUMBER            2940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15493E-01 0.88980E+00
   Friction velocity        uk    :  0.15493E-01 0.88980E+00
   Dimensionless distance   yplus :  0.12473E+00 0.71635E+01
   Friction thermal sca.    tstar : -0.59353E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93064E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10337E-01      33   0.19820E-03   0.37978E+01 0.18408E+03 
c  Velocity[X]                                      0.19562E+01 
c  Velocity[Y]                                      0.18416E+01 
c  Velocity[Z]                                      0.80679E-30 
c  Pressure     0.96252E-07     521   0.97246E-08   0.92616E-01 0.73328E+03 
c  nu_tilda     0.84576E-05      33   0.12541E-04   0.75082E-06 0.21583E+03 
c  TempC        0.43855E+02      26   0.23994E-03   0.59930E+01 0.29474E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2931          9.0259          4.5729          4.5729
v  Velocity[Y]            -2.5963          7.1897         0.21029         0.21029
v  Velocity[Z]       -1.0315e-014     8.7092e-015    -1.3107e-017    -1.3107e-017
v  ǁVelocityǁ         0.0030042          9.0262          5.0369          5.0369
v  Pressure               -26.957          25.061         -1.3287         -1.3287
v  nu_tilda           4.3978e-007       0.0045499       0.0017765       0.0017765
v  TempC                       21          73.064          22.048          22.048
v  TurbVisc           3.2906e-014       0.0053624       0.0020886       0.0020886
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2940:        0.22180E+01

===============================================================


 INSTANT    0.294100000E+04   TIME STEP NUMBER            2941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17094E-01 0.89126E+00
   Friction velocity        uk    :  0.17094E-01 0.89126E+00
   Dimensionless distance   yplus :  0.13762E+00 0.71752E+01
   Friction thermal sca.    tstar : -0.58488E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10268E+00 0.53535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10336E-01      33   0.25566E-03   0.37708E+01 0.18385E+03 
c  Velocity[X]                                      0.19461E+01 
c  Velocity[Y]                                      0.18247E+01 
c  Velocity[Z]                                      0.76861E-30 
c  Pressure     0.10160E-06     537   0.99179E-08   0.96630E-01 0.98732E+03 
c  nu_tilda     0.84571E-05      33   0.26560E-05   0.75098E-06 0.21585E+03 
c  TempC        0.43853E+02      27   0.29598E-03   0.33477E+01 0.22921E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2925          9.0261          4.5729          4.5729
v  Velocity[Y]            -2.5953          7.1958         0.21002         0.21002
v  Velocity[Z]       -9.7893e-015     8.6916e-015    -1.3088e-017    -1.3088e-017
v  ǁVelocityǁ         0.0030115          9.0264          5.0369          5.0369
v  Pressure               -26.888          25.131         -1.2752         -1.2752
v  nu_tilda           4.3976e-007         0.00455       0.0017764       0.0017764
v  TempC                       21          73.065          22.048          22.048
v  TurbVisc           3.2908e-014       0.0053626       0.0020885       0.0020885
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2941:        0.22410E+01

===============================================================


 INSTANT    0.294200000E+04   TIME STEP NUMBER            2942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16853E-01 0.89086E+00
   Friction velocity        uk    :  0.16853E-01 0.89086E+00
   Dimensionless distance   yplus :  0.13568E+00 0.71721E+01
   Friction thermal sca.    tstar : -0.58486E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10123E+00 0.53512E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10334E-01      33   0.25276E-03   0.38181E+01 0.18407E+03 
c  Velocity[X]                                      0.19976E+01 
c  Velocity[Y]                                      0.18205E+01 
c  Velocity[Z]                                      0.11540E-29 
c  Pressure     0.11159E-06     585   0.96906E-08   0.10850E+00 0.17234E+04 
c  nu_tilda     0.84567E-05      33   0.12540E-04   0.75119E-06 0.21587E+03 
c  TempC        0.43851E+02      27   0.27383E-03   0.47502E+01 0.24768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2919          9.0263          4.5729          4.5729
v  Velocity[Y]            -2.5943          7.1697         0.20976         0.20976
v  Velocity[Z]       -1.0057e-014     8.6994e-015    -1.3071e-017    -1.3071e-017
v  ǁVelocityǁ         0.0027628          9.0266          5.0369          5.0369
v  Pressure               -26.946          24.936         -1.3562         -1.3562
v  nu_tilda           4.3984e-007       0.0045501       0.0017763       0.0017763
v  TempC                       21          73.067          22.047          22.047
v  TurbVisc           3.2904e-014       0.0053627       0.0020884       0.0020884
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2942:        0.23430E+01

===============================================================


 INSTANT    0.294300000E+04   TIME STEP NUMBER            2943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15926E-01 0.88963E+00
   Friction velocity        uk    :  0.15926E-01 0.88963E+00
   Dimensionless distance   yplus :  0.12821E+00 0.71622E+01
   Friction thermal sca.    tstar : -0.63515E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95662E-01 0.53438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10332E-01      33   0.23621E-03   0.37891E+01 0.18390E+03 
c  Velocity[X]                                      0.19553E+01 
c  Velocity[Y]                                      0.18338E+01 
c  Velocity[Z]                                      0.10467E-29 
c  Pressure     0.91281E-07     586   0.98721E-08   0.87223E-01 0.21351E+04 
c  nu_tilda     0.84562E-05      33   0.26566E-05   0.75135E-06 0.21589E+03 
c  TempC        0.43849E+02      27   0.20456E-03   0.46770E+01 0.25408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2914          9.0264          4.5729          4.5729
v  Velocity[Y]            -2.5933            7.19          0.2095          0.2095
v  Velocity[Z]       -9.5908e-015     8.6853e-015    -1.3058e-017    -1.3058e-017
v  ǁVelocityǁ         0.0030658          9.0267          5.0369          5.0369
v  Pressure               -26.884           25.19         -1.2588         -1.2588
v  nu_tilda           4.3982e-007       0.0045502       0.0017763       0.0017763
v  TempC                       21          73.066          22.047          22.047
v  TurbVisc           3.2927e-014       0.0053628       0.0020883       0.0020883
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2943:        0.23510E+01

===============================================================


 INSTANT    0.294400000E+04   TIME STEP NUMBER            2944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.85179E-02 0.89045E+00
   Friction velocity        uk    :  0.85179E-02 0.89045E+00
   Dimensionless distance   yplus :  0.68575E-01 0.71687E+01
   Friction thermal sca.    tstar : -0.59537E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51164E-01 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10330E-01      33   0.24906E-03   0.37767E+01 0.18380E+03 
c  Velocity[X]                                      0.19581E+01 
c  Velocity[Y]                                      0.18186E+01 
c  Velocity[Z]                                      0.83932E-30 
c  Pressure     0.10251E-06     585   0.98391E-08   0.98521E-01 0.22591E+04 
c  nu_tilda     0.84557E-05      33   0.12535E-04   0.75155E-06 0.21592E+03 
c  TempC        0.43847E+02      26   0.33602E-03   0.32171E+01 0.22635E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2907          9.0266          4.5729          4.5729
v  Velocity[Y]            -2.5922          7.1625         0.20923         0.20923
v  Velocity[Z]        -9.944e-015     8.6917e-015    -1.3045e-017    -1.3045e-017
v  ǁVelocityǁ         0.0026844          9.0269          5.0369          5.0369
v  Pressure               -26.938          24.916         -1.3588         -1.3588
v  nu_tilda           4.3981e-007       0.0045504       0.0017761       0.0017761
v  TempC                       21          73.066          22.047          22.047
v  TurbVisc           3.2922e-014       0.0053629       0.0020882       0.0020882
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2944:        0.23480E+01

===============================================================


 INSTANT    0.294500000E+04   TIME STEP NUMBER            2945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.15462E-01 0.88984E+00
   Friction velocity        uk    :  0.15462E-01 0.88984E+00
   Dimensionless distance   yplus :  0.12448E+00 0.71638E+01
   Friction thermal sca.    tstar : -0.59868E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92878E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10329E-01      33   0.24792E-03   0.37853E+01 0.18377E+03 
c  Velocity[X]                                      0.19750E+01 
c  Velocity[Y]                                      0.18102E+01 
c  Velocity[Z]                                      0.85270E-30 
c  Pressure     0.93237E-07     569   0.97569E-08   0.89702E-01 0.21519E+04 
c  nu_tilda     0.84553E-05      33   0.26611E-05   0.75171E-06 0.21594E+03 
c  TempC        0.43845E+02      26   0.26886E-03   0.55298E+01 0.27869E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2902          9.0268          4.5729          4.5729
v  Velocity[Y]            -2.5911          7.1896         0.20896         0.20896
v  Velocity[Z]       -9.3352e-015     8.6775e-015     -1.303e-017     -1.303e-017
v  ǁVelocityǁ         0.0030064          9.0271           5.037           5.037
v  Pressure               -26.872          25.172         -1.2596         -1.2596
v  nu_tilda           4.3982e-007       0.0045505       0.0017761       0.0017761
v  TempC                       21          73.068          22.047          22.047
v  TurbVisc           3.2918e-014       0.0053631        0.002088        0.002088
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2945:        0.23600E+01

===============================================================


 INSTANT    0.294600000E+04   TIME STEP NUMBER            2946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.16831E-01 0.89094E+00
   Friction velocity        uk    :  0.16831E-01 0.89094E+00
   Dimensionless distance   yplus :  0.13550E+00 0.71726E+01
   Friction thermal sca.    tstar : -0.58715E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10110E+00 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10327E-01      33   0.23876E-03   0.37641E+01 0.18370E+03 
c  Velocity[X]                                      0.19382E+01 
c  Velocity[Y]                                      0.18259E+01 
c  Velocity[Z]                                      0.79059E-30 
c  Pressure     0.87449E-07     554   0.99326E-08   0.84048E-01 0.12526E+04 
c  nu_tilda     0.84548E-05      33   0.12533E-04   0.75191E-06 0.21596E+03 
c  TempC        0.43843E+02      26   0.24485E-03   0.53902E+01 0.25699E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2896          9.0269          4.5729          4.5729
v  Velocity[Y]            -2.5901          7.1958          0.2087          0.2087
v  Velocity[Z]       -9.4505e-015     8.6848e-015    -1.3014e-017    -1.3014e-017
v  ǁVelocityǁ         0.0031624          9.0272           5.037           5.037
v  Pressure               -26.933          25.065         -1.3245         -1.3245
v  nu_tilda           4.3981e-007       0.0045506       0.0017759       0.0017759
v  TempC                       21          73.069          22.047          22.047
v  TurbVisc            3.292e-014       0.0053632       0.0020879       0.0020879
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2946:        0.22550E+01

===============================================================


 INSTANT    0.294700000E+04   TIME STEP NUMBER            2947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.17818E-01 0.89049E+00
   Friction velocity        uk    :  0.17818E-01 0.89049E+00
   Dimensionless distance   yplus :  0.14345E+00 0.71691E+01
   Friction thermal sca.    tstar : -0.58565E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10703E+00 0.53489E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10325E-01      33   0.24686E-03   0.37829E+01 0.18364E+03 
c  Velocity[X]                                      0.19728E+01 
c  Velocity[Y]                                      0.18101E+01 
c  Velocity[Z]                                      0.10670E-29 
c  Pressure     0.11982E-06     521   0.94800E-08   0.11485E+00 0.70775E+03 
c  nu_tilda     0.84543E-05      33   0.26636E-05   0.75209E-06 0.21599E+03 
c  TempC        0.43841E+02      27   0.31200E-03   0.45909E+01 0.24181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.289          9.0271          4.5729          4.5729
v  Velocity[Y]            -2.5891           7.165         0.20843         0.20843
v  Velocity[Z]       -8.9925e-015     8.6669e-015    -1.2997e-017    -1.2997e-017
v  ǁVelocityǁ         0.0027297          9.0274           5.037           5.037
v  Pressure               -26.863           25.04         -1.2863         -1.2863
v  nu_tilda           4.3986e-007       0.0045506       0.0017759       0.0017759
v  TempC                       21          73.068          22.047          22.047
v  TurbVisc           3.2918e-014       0.0053633       0.0020878       0.0020878
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2947:        0.24780E+01

===============================================================


 INSTANT    0.294800000E+04   TIME STEP NUMBER            2948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15395E-01 0.88922E+00
   Friction velocity        uk    :  0.15395E-01 0.88922E+00
   Dimensionless distance   yplus :  0.12394E+00 0.71588E+01
   Friction thermal sca.    tstar : -0.59312E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92473E-01 0.53413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10323E-01      33   0.25412E-03   0.37867E+01 0.18369E+03 
c  Velocity[X]                                      0.19825E+01 
c  Velocity[Y]                                      0.18041E+01 
c  Velocity[Z]                                      0.87043E-30 
c  Pressure     0.11119E-06     536   0.99720E-08   0.10662E+00 0.68608E+03 
c  nu_tilda     0.84538E-05      33   0.12533E-04   0.75230E-06 0.21601E+03 
c  TempC        0.43840E+02      27   0.27031E-03   0.56341E+01 0.27124E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2884          9.0273          4.5729          4.5729
v  Velocity[Y]            -2.5881          7.1858         0.20816         0.20816
v  Velocity[Z]       -9.0067e-015     8.6763e-015    -1.2983e-017    -1.2983e-017
v  ǁVelocityǁ         0.0029849          9.0275           5.037           5.037
v  Pressure               -26.927          25.056         -1.3239         -1.3239
v  nu_tilda           4.3989e-007       0.0045507       0.0017757       0.0017757
v  TempC                       21          73.068          22.047          22.047
v  TurbVisc           3.2933e-014       0.0053634       0.0020877       0.0020877
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2948:        0.25020E+01

===============================================================


 INSTANT    0.294900000E+04   TIME STEP NUMBER            2949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17003E-01 0.89047E+00
   Friction velocity        uk    :  0.17003E-01 0.89047E+00
   Dimensionless distance   yplus :  0.13688E+00 0.71689E+01
   Friction thermal sca.    tstar : -0.58491E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10213E+00 0.53488E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10322E-01      33   0.24630E-03   0.37803E+01 0.18363E+03 
c  Velocity[X]                                      0.19625E+01 
c  Velocity[Y]                                      0.18178E+01 
c  Velocity[Z]                                      0.98475E-30 
c  Pressure     0.10155E-06     554   0.93972E-08   0.98800E-01 0.79187E+03 
c  nu_tilda     0.84533E-05      33   0.26680E-05   0.75245E-06 0.21603E+03 
c  TempC        0.43838E+02      26   0.30149E-03   0.55542E+01 0.25651E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2878          9.0274          4.5729          4.5729
v  Velocity[Y]             -2.587          7.1654         0.20789         0.20789
v  Velocity[Z]       -8.6202e-015     8.6587e-015    -1.2967e-017    -1.2967e-017
v  ǁVelocityǁ         0.0027611          9.0277           5.037           5.037
v  Pressure               -26.855          25.063         -1.2792         -1.2792
v  nu_tilda           4.3992e-007       0.0045508       0.0017757       0.0017757
v  TempC                       21           73.07          22.047          22.047
v  TurbVisc           3.2941e-014       0.0053635       0.0020876       0.0020876
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2949:        0.24760E+01

===============================================================


 INSTANT    0.295000000E+04   TIME STEP NUMBER            2950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15554E-01 0.88961E+00
   Friction velocity        uk    :  0.15554E-01 0.88961E+00
   Dimensionless distance   yplus :  0.12522E+00 0.71620E+01
   Friction thermal sca.    tstar : -0.59467E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93427E-01 0.53436E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10320E-01      33   0.18231E-03   0.37575E+01 0.18346E+03 
c  Velocity[X]                                      0.19544E+01 
c  Velocity[Y]                                      0.18032E+01 
c  Velocity[Z]                                      0.10812E-29 
c  Pressure     0.10506E-06     522   0.96354E-08   0.99837E-01 0.95154E+03 
c  nu_tilda     0.84528E-05      33   0.12528E-04   0.75266E-06 0.21605E+03 
c  TempC        0.43836E+02      27   0.26571E-03   0.54446E+01 0.24589E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2872          9.0276          4.5729          4.5729
v  Velocity[Y]            -2.5859          7.1845         0.20762         0.20762
v  Velocity[Z]       -8.6601e-015     8.6671e-015    -1.2949e-017    -1.2949e-017
v  ǁVelocityǁ         0.0029624          9.0278           5.037           5.037
v  Pressure               -26.913          25.018         -1.3309         -1.3309
v  nu_tilda           4.3988e-007        0.004551       0.0017755       0.0017755
v  TempC                       21           73.07          22.047          22.047
v  TurbVisc           3.2952e-014       0.0053636       0.0020875       0.0020875
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2950:        0.23630E+01

===============================================================


 INSTANT    0.295100000E+04   TIME STEP NUMBER            2951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16925E-01 0.89123E+00
   Friction velocity        uk    :  0.16925E-01 0.89123E+00
   Dimensionless distance   yplus :  0.13626E+00 0.71750E+01
   Friction thermal sca.    tstar : -0.62726E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10167E+00 0.53534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10318E-01      33   0.25051E-03   0.37517E+01 0.18339E+03 
c  Velocity[X]                                      0.19562E+01 
c  Velocity[Y]                                      0.17954E+01 
c  Velocity[Z]                                      0.73226E-30 
c  Pressure     0.92065E-07     553   0.99731E-08   0.88139E-01 0.14474E+04 
c  nu_tilda     0.84523E-05      33   0.26698E-05   0.75284E-06 0.21608E+03 
c  TempC        0.43834E+02      26   0.29432E-03   0.36771E+01 0.22577E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2866          9.0277          4.5729          4.5729
v  Velocity[Y]            -2.5849           7.198         0.20734         0.20734
v  Velocity[Z]       -8.3091e-015     8.6518e-015    -1.2929e-017    -1.2929e-017
v  ǁVelocityǁ          0.003044           9.028          5.0371          5.0371
v  Pressure               -26.848          25.157         -1.2582         -1.2582
v  nu_tilda           4.3979e-007        0.004551       0.0017755       0.0017755
v  TempC                       21          73.069          22.047          22.047
v  TurbVisc           3.2939e-014       0.0053638       0.0020874       0.0020874
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2951:        0.24650E+01

===============================================================


 INSTANT    0.295200000E+04   TIME STEP NUMBER            2952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17035E-01 0.89082E+00
   Friction velocity        uk    :  0.17035E-01 0.89082E+00
   Dimensionless distance   yplus :  0.13714E+00 0.71717E+01
   Friction thermal sca.    tstar : -0.59668E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10232E+00 0.53509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10316E-01      33   0.24162E-03   0.37755E+01 0.18349E+03 
c  Velocity[X]                                      0.19631E+01 
c  Velocity[Y]                                      0.18124E+01 
c  Velocity[Z]                                      0.94213E-30 
c  Pressure     0.10432E-06     552   0.96075E-08   0.10162E+00 0.17442E+04 
c  nu_tilda     0.84518E-05      33   0.12527E-04   0.75303E-06 0.21610E+03 
c  TempC        0.43832E+02      26   0.35726E-03   0.61484E+01 0.26890E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.286          9.0279          4.5729          4.5729
v  Velocity[Y]            -2.5839          7.1689         0.20707         0.20707
v  Velocity[Z]       -8.4705e-015     8.6591e-015     -1.291e-017     -1.291e-017
v  ǁVelocityǁ         0.0027587          9.0282          5.0371          5.0371
v  Pressure               -26.907          24.956         -1.3403         -1.3403
v  nu_tilda           4.3981e-007       0.0045511       0.0017753       0.0017753
v  TempC                       21           73.07          22.047          22.047
v  TurbVisc           3.2913e-014       0.0053639       0.0020873       0.0020873
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2952:        0.23500E+01

===============================================================


 INSTANT    0.295300000E+04   TIME STEP NUMBER            2953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15869E-01 0.88946E+00
   Friction velocity        uk    :  0.15869E-01 0.88946E+00
   Dimensionless distance   yplus :  0.12776E+00 0.71607E+01
   Friction thermal sca.    tstar : -0.59672E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95321E-01 0.53427E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10315E-01      33   0.24049E-03   0.37510E+01 0.18327E+03 
c  Velocity[X]                                      0.19560E+01 
c  Velocity[Y]                                      0.17950E+01 
c  Velocity[Z]                                      0.88976E-30 
c  Pressure     0.94236E-07     554   0.97121E-08   0.89857E-01 0.14964E+04 
c  nu_tilda     0.84513E-05      33   0.26748E-05   0.75321E-06 0.21613E+03 
c  TempC        0.43830E+02      26   0.26147E-03   0.81910E+01 0.32395E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2854          9.0281          4.5729          4.5729
v  Velocity[Y]            -2.5829           7.186         0.20679         0.20679
v  Velocity[Z]       -8.2769e-015      8.642e-015    -1.2896e-017    -1.2896e-017
v  ǁVelocityǁ         0.0029155          9.0283          5.0371          5.0371
v  Pressure               -26.838          25.119         -1.2666         -1.2666
v  nu_tilda           4.3985e-007       0.0045512       0.0017753       0.0017753
v  TempC                       21          73.071          22.047          22.047
v  TurbVisc           3.2918e-014        0.005364       0.0020871       0.0020871
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2953:        0.23030E+01

===============================================================


 INSTANT    0.295400000E+04   TIME STEP NUMBER            2954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16374E-01 0.89045E+00
   Friction velocity        uk    :  0.16374E-01 0.89045E+00
   Dimensionless distance   yplus :  0.13182E+00 0.71688E+01
   Friction thermal sca.    tstar : -0.58923E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98356E-01 0.53487E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10313E-01      33   0.28576E-03   0.37555E+01 0.18331E+03 
c  Velocity[X]                                      0.19681E+01 
c  Velocity[Y]                                      0.17874E+01 
c  Velocity[Z]                                      0.74396E-30 
c  Pressure     0.10024E-06     553   0.98931E-08   0.97359E-01 0.15460E+04 
c  nu_tilda     0.84508E-05      33   0.12525E-04   0.75343E-06 0.21615E+03 
c  TempC        0.43828E+02      27   0.30959E-03   0.42872E+01 0.25000E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2848          9.0282          4.5729          4.5729
v  Velocity[Y]            -2.5818          7.1643         0.20652         0.20652
v  Velocity[Z]       -8.4864e-015     8.6505e-015    -1.2884e-017    -1.2884e-017
v  ǁVelocityǁ         0.0027043          9.0285          5.0371          5.0371
v  Pressure               -26.897          24.943         -1.3401         -1.3401
v  nu_tilda           4.3991e-007       0.0045513       0.0017751       0.0017751
v  TempC                       21          73.072          22.046          22.046
v  TurbVisc           3.2931e-014       0.0053641        0.002087        0.002087
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2954:        0.22750E+01

===============================================================


 INSTANT    0.295500000E+04   TIME STEP NUMBER            2955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15614E-01 0.88986E+00
   Friction velocity        uk    :  0.15614E-01 0.88986E+00
   Dimensionless distance   yplus :  0.12570E+00 0.71640E+01
   Friction thermal sca.    tstar : -0.60254E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93789E-01 0.53452E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10311E-01      33   0.23972E-03   0.37902E+01 0.18344E+03 
c  Velocity[X]                                      0.19857E+01 
c  Velocity[Y]                                      0.18045E+01 
c  Velocity[Z]                                      0.92851E-30 
c  Pressure     0.11626E-06     600   0.93478E-08   0.11059E+00 0.18515E+04 
c  nu_tilda     0.84503E-05      33   0.26767E-05   0.75360E-06 0.21618E+03 
c  TempC        0.43826E+02      27   0.28404E-03   0.47451E+01 0.25468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2842          9.0284          4.5729          4.5729
v  Velocity[Y]            -2.5807          7.1895         0.20624         0.20624
v  Velocity[Z]       -8.2679e-015     8.6353e-015    -1.2865e-017    -1.2865e-017
v  ǁVelocityǁ          0.002979          9.0286          5.0371          5.0371
v  Pressure               -26.829          25.162         -1.2525         -1.2525
v  nu_tilda           4.3989e-007       0.0045514       0.0017751       0.0017751
v  TempC                       21          73.072          22.046          22.046
v  TurbVisc           3.2949e-014       0.0053642       0.0020869       0.0020869
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2955:        0.23790E+01

===============================================================


 INSTANT    0.295600000E+04   TIME STEP NUMBER            2956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16725E-01 0.89101E+00
   Friction velocity        uk    :  0.16725E-01 0.89101E+00
   Dimensionless distance   yplus :  0.13465E+00 0.71733E+01
   Friction thermal sca.    tstar : -0.58606E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10047E+00 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10309E-01      33   0.22268E-03   0.37401E+01 0.18315E+03 
c  Velocity[X]                                      0.19529E+01 
c  Velocity[Y]                                      0.17872E+01 
c  Velocity[Z]                                      0.13125E-29 
c  Pressure     0.10586E-06     552   0.96280E-08   0.10018E+00 0.14091E+04 
c  nu_tilda     0.84497E-05      33   0.12521E-04   0.75380E-06 0.21620E+03 
c  TempC        0.43824E+02      27   0.23813E-03   0.56066E+01 0.27393E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2836          9.0285          4.5729          4.5729
v  Velocity[Y]            -2.5797          7.1912         0.20596         0.20596
v  Velocity[Z]       -8.4795e-015     8.6429e-015     -1.285e-017     -1.285e-017
v  ǁVelocityǁ          0.002962          9.0288          5.0371          5.0371
v  Pressure               -26.891          25.023         -1.3237         -1.3237
v  nu_tilda           4.3988e-007       0.0045515       0.0017749       0.0017749
v  TempC                       21          73.072          22.046          22.046
v  TurbVisc           3.2941e-014       0.0053643       0.0020868       0.0020868
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2956:        0.22850E+01

===============================================================


 INSTANT    0.295700000E+04   TIME STEP NUMBER            2957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16892E-01 0.89084E+00
   Friction velocity        uk    :  0.16892E-01 0.89084E+00
   Dimensionless distance   yplus :  0.13599E+00 0.71719E+01
   Friction thermal sca.    tstar : -0.58591E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10146E+00 0.53510E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10308E-01      33   0.24275E-03   0.37408E+01 0.18306E+03 
c  Velocity[X]                                      0.19625E+01 
c  Velocity[Y]                                      0.17784E+01 
c  Velocity[Z]                                      0.92402E-30 
c  Pressure     0.11200E-06     522   0.95203E-08   0.10953E+00 0.92620E+03 
c  nu_tilda     0.84492E-05      33   0.26807E-05   0.75396E-06 0.21622E+03 
c  TempC        0.43822E+02      26   0.34133E-03   0.44588E+01 0.25491E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.283          9.0287          4.5729          4.5729
v  Velocity[Y]            -2.5787          7.1681         0.20568         0.20568
v  Velocity[Z]       -8.2339e-015      8.627e-015    -1.2834e-017    -1.2834e-017
v  ǁVelocityǁ         0.0027231          9.0289          5.0371          5.0371
v  Pressure               -26.821          25.058         -1.2717         -1.2717
v  nu_tilda           4.3991e-007       0.0045516       0.0017749       0.0017749
v  TempC                       21          73.073          22.046          22.046
v  TurbVisc           3.2939e-014       0.0053644       0.0020867       0.0020867
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2957:        0.22000E+01

===============================================================


 INSTANT    0.295800000E+04   TIME STEP NUMBER            2958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15321E-01 0.88949E+00
   Friction velocity        uk    :  0.15321E-01 0.88949E+00
   Dimensionless distance   yplus :  0.12335E+00 0.71610E+01
   Friction thermal sca.    tstar : -0.59656E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92029E-01 0.53429E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10306E-01      33   0.26425E-03   0.37391E+01 0.18310E+03 
c  Velocity[X]                                      0.19439E+01 
c  Velocity[Y]                                      0.17952E+01 
c  Velocity[Z]                                      0.93690E-30 
c  Pressure     0.95477E-07     505   0.98520E-08   0.91821E-01 0.72681E+03 
c  nu_tilda     0.84487E-05      33   0.12522E-04   0.75417E-06 0.21625E+03 
c  TempC        0.43820E+02      26   0.31943E-03   0.67917E+01 0.30453E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2823          9.0288          4.5729          4.5729
v  Velocity[Y]            -2.5777          7.1864          0.2054          0.2054
v  Velocity[Z]       -8.4524e-015     8.6357e-015    -1.2819e-017    -1.2819e-017
v  ǁVelocityǁ         0.0030143          9.0291          5.0372          5.0372
v  Pressure               -26.883          25.059         -1.3123         -1.3123
v  nu_tilda           4.3989e-007       0.0045517       0.0017747       0.0017747
v  TempC                       21          73.074          22.046          22.046
v  TurbVisc           3.2948e-014       0.0053645       0.0020866       0.0020866
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2958:        0.21730E+01

===============================================================


 INSTANT    0.295900000E+04   TIME STEP NUMBER            2959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17160E-01 0.89060E+00
   Friction velocity        uk    :  0.17160E-01 0.89060E+00
   Dimensionless distance   yplus :  0.13815E+00 0.71699E+01
   Friction thermal sca.    tstar : -0.62647E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10307E+00 0.53496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10304E-01      33   0.24876E-03   0.37665E+01 0.18309E+03 
c  Velocity[X]                                      0.19846E+01 
c  Velocity[Y]                                      0.17819E+01 
c  Velocity[Z]                                      0.74813E-30 
c  Pressure     0.13133E-06     505   0.97610E-08   0.12462E+00 0.66638E+03 
c  nu_tilda     0.84481E-05      33   0.26840E-05   0.75436E-06 0.21627E+03 
c  TempC        0.43817E+02      26   0.25856E-03   0.64289E+01 0.28081E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2817           9.029          4.5729          4.5729
v  Velocity[Y]            -2.5766          7.1633         0.20512         0.20512
v  Velocity[Z]       -8.2094e-015     8.6175e-015    -1.2804e-017    -1.2804e-017
v  ǁVelocityǁ         0.0025919          9.0292          5.0372          5.0372
v  Pressure               -26.808          25.003         -1.2827         -1.2827
v  nu_tilda           4.3991e-007       0.0045517       0.0017747       0.0017747
v  TempC                       21          73.072          22.046          22.046
v  TurbVisc           3.2942e-014       0.0053646       0.0020864       0.0020864
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2959:        0.21650E+01

===============================================================


 INSTANT    0.296000000E+04   TIME STEP NUMBER            2960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14559E-01 0.89015E+00
   Friction velocity        uk    :  0.14559E-01 0.89015E+00
   Dimensionless distance   yplus :  0.11721E+00 0.71663E+01
   Friction thermal sca.    tstar : -0.61329E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87453E-01 0.53468E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10302E-01      33   0.19801E-03   0.37473E+01 0.18302E+03 
c  Velocity[X]                                      0.19744E+01 
c  Velocity[Y]                                      0.17728E+01 
c  Velocity[Z]                                      0.74144E-30 
c  Pressure     0.96882E-07     522   0.99040E-08   0.93156E-01 0.65400E+03 
c  nu_tilda     0.84476E-05      33   0.12519E-04   0.75457E-06 0.21630E+03 
c  TempC        0.43815E+02      27   0.31312E-03   0.48661E+01 0.24616E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2811          9.0291          4.5729          4.5729
v  Velocity[Y]            -2.5756           7.189         0.20484         0.20484
v  Velocity[Z]       -8.1739e-015     8.6266e-015    -1.2786e-017    -1.2786e-017
v  ǁVelocityǁ         0.0028945          9.0294          5.0372          5.0372
v  Pressure               -26.871          25.037          -1.317          -1.317
v  nu_tilda           4.3995e-007       0.0045518       0.0017745       0.0017745
v  TempC                       21          73.072          22.046          22.046
v  TurbVisc           3.2949e-014       0.0053647       0.0020863       0.0020863
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2960:        0.22520E+01

===============================================================


 INSTANT    0.296100000E+04   TIME STEP NUMBER            2961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14721E-01 0.89158E+00
   Friction velocity        uk    :  0.14721E-01 0.89158E+00
   Dimensionless distance   yplus :  0.11851E+00 0.71778E+01
   Friction thermal sca.    tstar : -0.59554E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88423E-01 0.53555E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10300E-01      33   0.23143E-03   0.37216E+01 0.18286E+03 
c  Velocity[X]                                      0.19330E+01 
c  Velocity[Y]                                      0.17886E+01 
c  Velocity[Z]                                      0.91350E-30 
c  Pressure     0.81443E-07     601   0.98006E-08   0.78299E-01 0.14560E+04 
c  nu_tilda     0.84470E-05      33   0.26881E-05   0.75473E-06 0.21632E+03 
c  TempC        0.43813E+02      27   0.29864E-03   0.49302E+01 0.24418E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2804          9.0293          4.5729          4.5729
v  Velocity[Y]            -2.5745          7.1997         0.20455         0.20455
v  Velocity[Z]       -8.0606e-015     8.6116e-015    -1.2766e-017    -1.2766e-017
v  ǁVelocityǁ         0.0030238          9.0295          5.0372          5.0372
v  Pressure               -26.805          25.172         -1.2428         -1.2428
v  nu_tilda            4.399e-007       0.0045519       0.0017745       0.0017745
v  TempC                       21          73.071          22.046          22.046
v  TurbVisc            3.296e-014       0.0053648       0.0020862       0.0020862
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2961:        0.26330E+01

===============================================================


 INSTANT    0.296200000E+04   TIME STEP NUMBER            2962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16913E-01 0.89104E+00
   Friction velocity        uk    :  0.16913E-01 0.89104E+00
   Dimensionless distance   yplus :  0.13616E+00 0.71735E+01
   Friction thermal sca.    tstar : -0.59607E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10159E+00 0.53522E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10299E-01      33   0.24973E-03   0.37341E+01 0.18288E+03 
c  Velocity[X]                                      0.19601E+01 
c  Velocity[Y]                                      0.17740E+01 
c  Velocity[Z]                                      0.91510E-30 
c  Pressure     0.10793E-06     601   0.98399E-08   0.10401E+00 0.22116E+04 
c  nu_tilda     0.84465E-05      33   0.12517E-04   0.75494E-06 0.21634E+03 
c  TempC        0.43811E+02      26   0.23543E-03   0.46163E+01 0.22778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2798          9.0294          4.5729          4.5729
v  Velocity[Y]            -2.5735          7.1678         0.20427         0.20427
v  Velocity[Z]       -8.3799e-015     8.6162e-015    -1.2753e-017    -1.2753e-017
v  ǁVelocityǁ         0.0026785          9.0297          5.0372          5.0372
v  Pressure               -26.859           24.91         -1.3422         -1.3422
v  nu_tilda           4.3991e-007        0.004552       0.0017743       0.0017743
v  TempC                       21          73.068          22.046          22.046
v  TurbVisc           3.2945e-014       0.0053649       0.0020861       0.0020861
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2962:        0.23910E+01

===============================================================


 INSTANT    0.296300000E+04   TIME STEP NUMBER            2963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15469E-01 0.88983E+00
   Friction velocity        uk    :  0.15469E-01 0.88983E+00
   Dimensionless distance   yplus :  0.12453E+00 0.71637E+01
   Friction thermal sca.    tstar : -0.61971E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92916E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10297E-01      33   0.27531E-03   0.37471E+01 0.18288E+03 
c  Velocity[X]                                      0.19832E+01 
c  Velocity[Y]                                      0.17638E+01 
c  Velocity[Z]                                      0.80898E-30 
c  Pressure     0.10985E-06     601   0.96267E-08   0.10523E+00 0.20738E+04 
c  nu_tilda     0.84459E-05      33   0.26899E-05   0.75511E-06 0.21637E+03 
c  TempC        0.43809E+02      26   0.32958E-03   0.44367E+01 0.24058E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2792          9.0295          4.5729          4.5729
v  Velocity[Y]            -2.5725          7.1913         0.20398         0.20398
v  Velocity[Z]       -8.0589e-015     8.6025e-015    -1.2739e-017    -1.2739e-017
v  ǁVelocityǁ         0.0029048          9.0298          5.0372          5.0372
v  Pressure               -26.794          25.152         -1.2465         -1.2465
v  nu_tilda           4.3992e-007       0.0045521       0.0017743       0.0017743
v  TempC                       21          73.065          22.046          22.046
v  TurbVisc           3.2946e-014        0.005365        0.002086        0.002086
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2963:        0.23930E+01

===============================================================


 INSTANT    0.296400000E+04   TIME STEP NUMBER            2964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16351E-01 0.89081E+00
   Friction velocity        uk    :  0.16351E-01 0.89081E+00
   Dimensionless distance   yplus :  0.13163E+00 0.71716E+01
   Friction thermal sca.    tstar : -0.63189E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98214E-01 0.53508E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10295E-01      33   0.25137E-03   0.37383E+01 0.18283E+03 
c  Velocity[X]                                      0.19582E+01 
c  Velocity[Y]                                      0.17800E+01 
c  Velocity[Z]                                      0.10954E-29 
c  Pressure     0.10031E-06     600   0.93630E-08   0.97148E-01 0.17584E+04 
c  nu_tilda     0.84453E-05      33   0.12515E-04   0.75533E-06 0.21639E+03 
c  TempC        0.43807E+02      27   0.27837E-03   0.55750E+01 0.28858E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2786          9.0297          4.5729          4.5729
v  Velocity[Y]            -2.5714           7.167          0.2037          0.2037
v  Velocity[Z]       -8.0816e-015      8.609e-015    -1.2721e-017    -1.2721e-017
v  ǁVelocityǁ         0.0026995          9.0299          5.0372          5.0372
v  Pressure               -26.851          24.954         -1.3284         -1.3284
v  nu_tilda           4.3995e-007       0.0045521       0.0017741       0.0017741
v  TempC                       21          73.061          22.046          22.046
v  TurbVisc            3.295e-014       0.0053651       0.0020859       0.0020859
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2964:        0.23820E+01

===============================================================


 INSTANT    0.296500000E+04   TIME STEP NUMBER            2965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15549E-01 0.88990E+00
   Friction velocity        uk    :  0.15549E-01 0.88990E+00
   Dimensionless distance   yplus :  0.12518E+00 0.71643E+01
   Friction thermal sca.    tstar : -0.64207E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93396E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10293E-01      33   0.25312E-03   0.37246E+01 0.18265E+03 
c  Velocity[X]                                      0.19607E+01 
c  Velocity[Y]                                      0.17640E+01 
c  Velocity[Z]                                      0.11325E-29 
c  Pressure     0.10592E-06     585   0.96657E-08   0.10039E+00 0.17276E+04 
c  nu_tilda     0.84448E-05      33   0.26944E-05   0.75552E-06 0.21642E+03 
c  TempC        0.43805E+02      26   0.35197E-03   0.38693E+01 0.24107E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.278          9.0298          4.5729          4.5729
v  Velocity[Y]            -2.5704          7.1887         0.20341         0.20341
v  Velocity[Z]       -7.9217e-015     8.5936e-015    -1.2712e-017    -1.2712e-017
v  ǁVelocityǁ         0.0028863          9.0301          5.0372          5.0372
v  Pressure               -26.785          25.143         -1.2454         -1.2454
v  nu_tilda           4.3991e-007       0.0045522       0.0017741       0.0017741
v  TempC                       21          73.055          22.045          22.045
v  TurbVisc           3.2961e-014       0.0053652       0.0020857       0.0020857
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2965:        0.23530E+01

===============================================================


 INSTANT    0.296600000E+04   TIME STEP NUMBER            2966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16220E-01 0.89123E+00
   Friction velocity        uk    :  0.16220E-01 0.89123E+00
   Dimensionless distance   yplus :  0.13058E+00 0.71750E+01
   Friction thermal sca.    tstar : -0.65794E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.97429E-01 0.53534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10292E-01      33   0.25136E-03   0.37120E+01 0.18258E+03 
c  Velocity[X]                                      0.19544E+01 
c  Velocity[Y]                                      0.17577E+01 
c  Velocity[Z]                                      0.81644E-30 
c  Pressure     0.94710E-07     553   0.99331E-08   0.90989E-01 0.11107E+04 
c  nu_tilda     0.84442E-05      33   0.12513E-04   0.75572E-06 0.21645E+03 
c  TempC        0.43803E+02      27   0.29669E-03   0.58547E+01 0.27778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2773            9.03          4.5729          4.5729
v  Velocity[Y]            -2.5693          7.1976         0.20312         0.20312
v  Velocity[Z]       -8.2547e-015      8.601e-015    -1.2697e-017    -1.2697e-017
v  ǁVelocityǁ         0.0030472          9.0302          5.0372          5.0372
v  Pressure               -26.845          25.058         -1.3044         -1.3044
v  nu_tilda            4.398e-007       0.0045523       0.0017739       0.0017739
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc           3.2948e-014       0.0053652       0.0020856       0.0020856
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2966:        0.22710E+01

===============================================================


 INSTANT    0.296700000E+04   TIME STEP NUMBER            2967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.30659E-02 0.89087E+00
   Friction velocity        uk    :  0.30659E-02 0.89087E+00
   Dimensionless distance   yplus :  0.24682E-01 0.71721E+01
   Friction thermal sca.    tstar : -0.65528E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.18416E-01 0.53512E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10290E-01      33   0.24244E-03   0.37311E+01 0.18264E+03 
c  Velocity[X]                                      0.19588E+01 
c  Velocity[Y]                                      0.17723E+01 
c  Velocity[Z]                                      0.10060E-29 
c  Pressure     0.11190E-06     537   0.97686E-08   0.10871E+00 0.82131E+03 
c  nu_tilda     0.84436E-05      33   0.26971E-05   0.75590E-06 0.21647E+03 
c  TempC        0.43801E+02      27   0.27694E-03   0.46275E+01 0.25063E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2767          9.0301          4.5729          4.5729
v  Velocity[Y]            -2.5683          7.1705         0.20283         0.20283
v  Velocity[Z]       -7.9345e-015     8.5844e-015    -1.2681e-017    -1.2681e-017
v  ǁVelocityǁ         0.0027705          9.0304          5.0372          5.0372
v  Pressure               -26.773          25.075         -1.2579         -1.2579
v  nu_tilda           4.3976e-007       0.0045524       0.0017739       0.0017739
v  TempC                       21          73.052          22.045          22.045
v  TurbVisc           3.2913e-014       0.0053653       0.0020855       0.0020855
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2967:        0.22640E+01

===============================================================


 INSTANT    0.296800000E+04   TIME STEP NUMBER            2968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15619E-01 0.88930E+00
   Friction velocity        uk    :  0.15619E-01 0.88930E+00
   Dimensionless distance   yplus :  0.12575E+00 0.71595E+01
   Friction thermal sca.    tstar : -0.68618E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93821E-01 0.53418E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10288E-01      33   0.25168E-03   0.37049E+01 0.18249E+03 
c  Velocity[X]                                      0.19484E+01 
c  Velocity[Y]                                      0.17565E+01 
c  Velocity[Z]                                      0.91592E-30 
c  Pressure     0.10165E-06     554   0.96060E-08   0.96163E-01 0.99646E+03 
c  nu_tilda     0.84430E-05      33   0.12513E-04   0.75610E-06 0.21649E+03 
c  TempC        0.43799E+02      27   0.25980E-03   0.38511E+01 0.23499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.276          9.0302          4.5729          4.5729
v  Velocity[Y]            -2.5673          7.1854         0.20254         0.20254
v  Velocity[Z]       -7.8773e-015     8.5917e-015     -1.267e-017     -1.267e-017
v  ǁVelocityǁ         0.0028748          9.0305          5.0372          5.0372
v  Pressure               -26.832          25.017         -1.3122         -1.3122
v  nu_tilda           4.3978e-007       0.0045524       0.0017737       0.0017737
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc           3.2902e-014       0.0053654       0.0020854       0.0020854
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2968:        0.22950E+01

===============================================================


 INSTANT    0.296900000E+04   TIME STEP NUMBER            2969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16466E-01 0.89062E+00
   Friction velocity        uk    :  0.16466E-01 0.89062E+00
   Dimensionless distance   yplus :  0.13256E+00 0.71701E+01
   Friction thermal sca.    tstar : -0.70825E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98904E-01 0.53497E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10286E-01      33   0.26024E-03   0.37299E+01 0.18254E+03 
c  Velocity[X]                                      0.19811E+01 
c  Velocity[Y]                                      0.17488E+01 
c  Velocity[Z]                                      0.77972E-30 
c  Pressure     0.11755E-06     552   0.97804E-08   0.11442E+00 0.10007E+04 
c  nu_tilda     0.84424E-05      33   0.26999E-05   0.75627E-06 0.21652E+03 
c  TempC        0.43796E+02      27   0.25036E-03   0.44694E+01 0.24709E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2754          9.0304          4.5729          4.5729
v  Velocity[Y]            -2.5663          7.1676         0.20225         0.20225
v  Velocity[Z]       -7.8126e-015     8.5761e-015     -1.266e-017     -1.266e-017
v  ǁVelocityǁ         0.0026869          9.0306          5.0373          5.0373
v  Pressure               -26.764          25.064         -1.2567         -1.2567
v  nu_tilda           4.3986e-007       0.0045525       0.0017737       0.0017737
v  TempC                       21          73.052          22.045          22.045
v  TurbVisc           3.2908e-014       0.0053655       0.0020853       0.0020853
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2969:        0.22770E+01

===============================================================


 INSTANT    0.297000000E+04   TIME STEP NUMBER            2970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.71831E-02 0.88983E+00
   Friction velocity        uk    :  0.71831E-02 0.88983E+00
   Dimensionless distance   yplus :  0.57829E-01 0.71637E+01
   Friction thermal sca.    tstar : -0.73327E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.43147E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10284E-01      33   0.19278E-03   0.37160E+01 0.18248E+03 
c  Velocity[X]                                      0.19513E+01 
c  Velocity[Y]                                      0.17647E+01 
c  Velocity[Z]                                      0.82670E-30 
c  Pressure     0.95558E-07     521   0.97058E-08   0.91660E-01 0.76458E+03 
c  nu_tilda     0.84418E-05      33   0.12510E-04   0.75650E-06 0.21655E+03 
c  TempC        0.43794E+02      27   0.34212E-03   0.47143E+01 0.24554E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2747          9.0305          4.5729          4.5729
v  Velocity[Y]            -2.5652          7.1903         0.20195         0.20195
v  Velocity[Z]       -8.2229e-015     8.5841e-015    -1.2644e-017    -1.2644e-017
v  ǁVelocityǁ         0.0030185          9.0308          5.0373          5.0373
v  Pressure               -26.824          25.062         -1.2997         -1.2997
v  nu_tilda           4.3989e-007       0.0045525       0.0017735       0.0017735
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc           3.2931e-014       0.0053656       0.0020851       0.0020851
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2970:        0.22460E+01

===============================================================


 INSTANT    0.297100000E+04   TIME STEP NUMBER            2971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11254E-02 0.89125E+00
   Friction velocity        uk    :  0.11254E-02 0.89125E+00
   Dimensionless distance   yplus :  0.90605E-02 0.71751E+01
   Friction thermal sca.    tstar : -0.74804E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.67601E-02 0.53535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10282E-01      33   0.24741E-03   0.36901E+01 0.18223E+03 
c  Velocity[X]                                      0.19403E+01 
c  Velocity[Y]                                      0.17498E+01 
c  Velocity[Z]                                      0.11145E-29 
c  Pressure     0.11184E-06     552   0.97285E-08   0.10582E+00 0.12163E+04 
c  nu_tilda     0.84412E-05      33   0.27045E-05   0.75669E-06 0.21658E+03 
c  TempC        0.43792E+02      26   0.26263E-03   0.66675E+01 0.29934E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2741          9.0307          4.5729          4.5729
v  Velocity[Y]            -2.5641          7.1973         0.20166         0.20166
v  Velocity[Z]       -7.8849e-015     8.5686e-015    -1.2635e-017    -1.2635e-017
v  ǁVelocityǁ         0.0029949          9.0309          5.0373          5.0373
v  Pressure               -26.756          25.157         -1.2352         -1.2352
v  nu_tilda           4.3989e-007       0.0045526       0.0017735       0.0017735
v  TempC                       21          73.052          22.045          22.045
v  TurbVisc           3.2942e-014       0.0053656        0.002085        0.002085
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2971:        0.22510E+01

===============================================================


 INSTANT    0.297200000E+04   TIME STEP NUMBER            2972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16795E-01 0.89094E+00
   Friction velocity        uk    :  0.16795E-01 0.89094E+00
   Dimensionless distance   yplus :  0.13521E+00 0.71727E+01
   Friction thermal sca.    tstar : -0.75374E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10088E+00 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10281E-01      33   0.24235E-03   0.37249E+01 0.18239E+03 
c  Velocity[X]                                      0.19820E+01 
c  Velocity[Y]                                      0.17429E+01 
c  Velocity[Z]                                      0.75362E-30 
c  Pressure     0.99955E-07     601   0.98135E-08   0.97327E-01 0.18940E+04 
c  nu_tilda     0.84406E-05      33   0.12509E-04   0.75690E-06 0.21660E+03 
c  TempC        0.43790E+02      27   0.21691E-03   0.49507E+01 0.24216E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2734          9.0308          4.5729          4.5729
v  Velocity[Y]            -2.5631            7.17         0.20137         0.20137
v  Velocity[Z]       -7.8931e-015     8.5744e-015    -1.2623e-017    -1.2623e-017
v  ǁVelocityǁ         0.0027024           9.031          5.0373          5.0373
v  Pressure               -26.812          24.942         -1.3232         -1.3232
v  nu_tilda           4.3992e-007       0.0045527       0.0017733       0.0017733
v  TempC                       21          73.051          22.045          22.045
v  TurbVisc           3.2943e-014       0.0053657       0.0020849       0.0020849
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2972:        0.24780E+01

===============================================================


 INSTANT    0.297300000E+04   TIME STEP NUMBER            2973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13210E-01 0.88956E+00
   Friction velocity        uk    :  0.13210E-01 0.88956E+00
   Dimensionless distance   yplus :  0.10635E+00 0.71616E+01
   Friction thermal sca.    tstar : -0.79680E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.79347E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10279E-01      33   0.23905E-03   0.36986E+01 0.18225E+03 
c  Velocity[X]                                      0.19428E+01 
c  Velocity[Y]                                      0.17558E+01 
c  Velocity[Z]                                      0.99813E-30 
c  Pressure     0.85790E-07     569   0.92905E-08   0.82515E-01 0.19528E+04 
c  nu_tilda     0.84400E-05      33   0.27067E-05   0.75707E-06 0.21662E+03 
c  TempC        0.43788E+02      26   0.33535E-03   0.31422E+01 0.20597E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2728          9.0309          4.5729          4.5729
v  Velocity[Y]            -2.5621          7.1903         0.20107         0.20107
v  Velocity[Z]       -7.7824e-015     8.5603e-015    -1.2607e-017    -1.2607e-017
v  ǁVelocityǁ         0.0029696          9.0312          5.0373          5.0373
v  Pressure               -26.746          25.168         -1.2317         -1.2317
v  nu_tilda           4.3986e-007       0.0045528       0.0017733       0.0017733
v  TempC                       21          73.052          22.045          22.045
v  TurbVisc           3.2949e-014       0.0053658       0.0020848       0.0020848
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2973:        0.24650E+01

===============================================================


 INSTANT    0.297400000E+04   TIME STEP NUMBER            2974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16647E-01 0.89041E+00
   Friction velocity        uk    :  0.16647E-01 0.89041E+00
   Dimensionless distance   yplus :  0.13402E+00 0.71684E+01
   Friction thermal sca.    tstar : -0.83584E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.99992E-01 0.53484E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10277E-01      33   0.26003E-03   0.36936E+01 0.18217E+03 
c  Velocity[X]                                      0.19519E+01 
c  Velocity[Y]                                      0.17417E+01 
c  Velocity[Z]                                      0.12015E-29 
c  Pressure     0.10619E-06     570   0.97454E-08   0.10159E+00 0.19855E+04 
c  nu_tilda     0.84394E-05      33   0.12507E-04   0.75727E-06 0.21665E+03 
c  TempC        0.43786E+02      27   0.24994E-03   0.46423E+01 0.24440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2721          9.0311          4.5729          4.5729
v  Velocity[Y]            -2.5611          7.1632         0.20077         0.20077
v  Velocity[Z]       -8.3369e-015     8.5661e-015      -1.26e-017      -1.26e-017
v  ǁVelocityǁ          0.002678          9.0313          5.0373          5.0373
v  Pressure               -26.801          24.931         -1.3216         -1.3216
v  nu_tilda           4.3985e-007       0.0045528       0.0017731       0.0017731
v  TempC                       21          73.052          22.045          22.045
v  TurbVisc           3.2933e-014       0.0053659       0.0020847       0.0020847
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2974:        0.26280E+01

===============================================================


 INSTANT    0.297500000E+04   TIME STEP NUMBER            2975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15465E-01 0.88982E+00
   Friction velocity        uk    :  0.15465E-01 0.88982E+00
   Dimensionless distance   yplus :  0.12450E+00 0.71637E+01
   Friction thermal sca.    tstar : -0.87230E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92892E-01 0.53449E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10275E-01      33   0.20940E-03   0.37090E+01 0.18220E+03 
c  Velocity[X]                                      0.19746E+01 
c  Velocity[Y]                                      0.17343E+01 
c  Velocity[Z]                                      0.82025E-30 
c  Pressure     0.10578E-06     618   0.98183E-08   0.10063E+00 0.18591E+04 
c  nu_tilda     0.84388E-05      33   0.27098E-05   0.75746E-06 0.21667E+03 
c  TempC        0.43783E+02      27   0.28642E-03   0.36855E+01 0.21204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2714          9.0312          4.5729          4.5729
v  Velocity[Y]              -2.56          7.1906         0.20047         0.20047
v  Velocity[Z]       -7.9102e-015     8.5514e-015    -1.2584e-017    -1.2584e-017
v  ǁVelocityǁ         0.0029232          9.0314          5.0373          5.0373
v  Pressure               -26.732          25.151         -1.2341         -1.2341
v  nu_tilda           4.3986e-007       0.0045529       0.0017731       0.0017731
v  TempC                       21          73.056          22.045          22.045
v  TurbVisc           3.2929e-014        0.005366       0.0020845       0.0020845
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2975:        0.25310E+01

===============================================================


 INSTANT    0.297600000E+04   TIME STEP NUMBER            2976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16442E-01 0.89112E+00
   Friction velocity        uk    :  0.16442E-01 0.89112E+00
   Dimensionless distance   yplus :  0.13237E+00 0.71741E+01
   Friction thermal sca.    tstar : -0.95776E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98765E-01 0.53527E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10273E-01      33   0.24253E-03   0.36853E+01 0.18209E+03 
c  Velocity[X]                                      0.19343E+01 
c  Velocity[Y]                                      0.17510E+01 
c  Velocity[Z]                                      0.81838E-30 
c  Pressure     0.88365E-07     553   0.97486E-08   0.84707E-01 0.90366E+03 
c  nu_tilda     0.84381E-05      33   0.12505E-04   0.75769E-06 0.21670E+03 
c  TempC        0.43781E+02      27   0.27993E-03   0.42493E+01 0.23598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2708          9.0313          4.5729          4.5729
v  Velocity[Y]            -2.5589          7.1957         0.20017         0.20017
v  Velocity[Z]       -7.9473e-015       8.56e-015    -1.2569e-017    -1.2569e-017
v  ǁVelocityǁ         0.0031007          9.0316          5.0373          5.0373
v  Pressure               -26.796          25.093         -1.2837         -1.2837
v  nu_tilda           4.3985e-007       0.0045529       0.0017729       0.0017729
v  TempC                       21          73.057          22.044          22.044
v  TurbVisc           3.2931e-014        0.005366       0.0020844       0.0020844
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2976:        0.22740E+01

===============================================================


 INSTANT    0.297700000E+04   TIME STEP NUMBER            2977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.17520E-01 0.89062E+00
   Friction velocity        uk    :  0.17520E-01 0.89062E+00
   Dimensionless distance   yplus :  0.14104E+00 0.71701E+01
   Friction thermal sca.    tstar : -0.89889E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10523E+00 0.53497E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10272E-01      33   0.23884E-03   0.36996E+01 0.18201E+03 
c  Velocity[X]                                      0.19651E+01 
c  Velocity[Y]                                      0.17345E+01 
c  Velocity[Z]                                      0.10168E-29 
c  Pressure     0.11502E-06     505   0.97966E-08   0.11024E+00 0.67078E+03 
c  nu_tilda     0.84375E-05      33   0.27133E-05   0.75788E-06 0.21673E+03 
c  TempC        0.43779E+02      26   0.31795E-03   0.46850E+01 0.25048E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2701          9.0314          4.5729          4.5729
v  Velocity[Y]            -2.5579          7.1667         0.19987         0.19987
v  Velocity[Z]       -7.8421e-015     8.5418e-015    -1.2554e-017    -1.2554e-017
v  ǁVelocityǁ         0.0026878          9.0317          5.0373          5.0373
v  Pressure                -26.72          25.032         -1.2557         -1.2557
v  nu_tilda           4.3991e-007        0.004553       0.0017729       0.0017729
v  TempC                       21           73.06          22.044          22.044
v  TurbVisc            3.293e-014       0.0053661       0.0020843       0.0020843
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2977:        0.21450E+01

===============================================================


 INSTANT    0.297800000E+04   TIME STEP NUMBER            2978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15099E-01 0.88947E+00
   Friction velocity        uk    :  0.15099E-01 0.88947E+00
   Dimensionless distance   yplus :  0.12156E+00 0.71609E+01
   Friction thermal sca.    tstar : -0.10208E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.90697E-01 0.53428E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10270E-01      33   0.24430E-03   0.36918E+01 0.18198E+03 
c  Velocity[X]                                      0.19643E+01 
c  Velocity[Y]                                      0.17275E+01 
c  Velocity[Z]                                      0.97465E-30 
c  Pressure     0.91066E-07     521   0.94620E-08   0.87630E-01 0.63594E+03 
c  nu_tilda     0.84369E-05      33   0.12506E-04   0.75808E-06 0.21676E+03 
c  TempC        0.43777E+02      27   0.33161E-03   0.55889E+01 0.26323E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2694          9.0316          4.5729          4.5729
v  Velocity[Y]            -2.5569          7.1877         0.19957         0.19957
v  Velocity[Z]       -8.3701e-015     8.5512e-015    -1.2547e-017    -1.2547e-017
v  ǁVelocityǁ         0.0029768          9.0318          5.0373          5.0373
v  Pressure               -26.783           25.06         -1.2889         -1.2889
v  nu_tilda           4.3991e-007        0.004553       0.0017727       0.0017727
v  TempC                       21          73.059          22.044          22.044
v  TurbVisc           3.2948e-014       0.0053661       0.0020842       0.0020842
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2978:        0.21630E+01

===============================================================


 INSTANT    0.297900000E+04   TIME STEP NUMBER            2979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16986E-01 0.89064E+00
   Friction velocity        uk    :  0.16986E-01 0.89064E+00
   Dimensionless distance   yplus :  0.13675E+00 0.71703E+01
   Friction thermal sca.    tstar : -0.10410E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10203E+00 0.53498E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10268E-01      33   0.24899E-03   0.36896E+01 0.18193E+03 
c  Velocity[X]                                      0.19476E+01 
c  Velocity[Y]                                      0.17420E+01 
c  Velocity[Z]                                      0.91551E-30 
c  Pressure     0.10438E-06     554   0.94711E-08   0.10048E+00 0.81423E+03 
c  nu_tilda     0.84362E-05      33   0.27170E-05   0.75826E-06 0.21678E+03 
c  TempC        0.43775E+02      27   0.26011E-03   0.56328E+01 0.25840E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2688          9.0317          4.5729          4.5729
v  Velocity[Y]            -2.5559          7.1662         0.19927         0.19927
v  Velocity[Z]       -7.8588e-015     8.5347e-015    -1.2534e-017    -1.2534e-017
v  ǁVelocityǁ         0.0027291          9.0319          5.0373          5.0373
v  Pressure                -26.71          25.072         -1.2427         -1.2427
v  nu_tilda           4.3991e-007       0.0045531       0.0017727       0.0017727
v  TempC                       21          73.061          22.044          22.044
v  TurbVisc           3.2947e-014       0.0053662       0.0020841       0.0020841
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2979:        0.22590E+01

===============================================================


 INSTANT    0.298000000E+04   TIME STEP NUMBER            2980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15401E-01 0.88966E+00
   Friction velocity        uk    :  0.15401E-01 0.88966E+00
   Dimensionless distance   yplus :  0.12399E+00 0.71624E+01
   Friction thermal sca.    tstar : -0.11634E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.92510E-01 0.53440E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10266E-01      33   0.21191E-03   0.36742E+01 0.18182E+03 
c  Velocity[X]                                      0.19476E+01 
c  Velocity[Y]                                      0.17267E+01 
c  Velocity[Z]                                      0.81660E-30 
c  Pressure     0.10522E-06     554   0.98362E-08   0.99845E-01 0.86162E+03 
c  nu_tilda     0.84356E-05      33   0.12503E-04   0.75847E-06 0.21681E+03 
c  TempC        0.43772E+02      27   0.32999E-03   0.42406E+01 0.24396E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2681          9.0318          4.5729          4.5729
v  Velocity[Y]            -2.5548          7.1861         0.19897         0.19897
v  Velocity[Z]       -7.8606e-015     8.5425e-015     -1.252e-017     -1.252e-017
v  ǁVelocityǁ         0.0028524          9.0321          5.0373          5.0373
v  Pressure               -26.772          25.034         -1.2912         -1.2912
v  nu_tilda           4.3991e-007       0.0045532       0.0017725       0.0017725
v  TempC                       21          73.059          22.044          22.044
v  TurbVisc           3.2947e-014       0.0053663       0.0020839       0.0020839
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2980:        0.22720E+01

===============================================================


 INSTANT    0.298100000E+04   TIME STEP NUMBER            2981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16363E-01 0.89139E+00
   Friction velocity        uk    :  0.16363E-01 0.89139E+00
   Dimensionless distance   yplus :  0.13173E+00 0.71763E+01
   Friction thermal sca.    tstar : -0.11850E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98288E-01 0.53543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10264E-01      33   0.26309E-03   0.36770E+01 0.18179E+03 
c  Velocity[X]                                      0.19569E+01 
c  Velocity[Y]                                      0.17201E+01 
c  Velocity[Z]                                      0.87740E-30 
c  Pressure     0.10861E-06     600   0.98198E-08   0.10411E+00 0.13770E+04 
c  nu_tilda     0.84349E-05      33   0.27191E-05   0.75867E-06 0.21684E+03 
c  TempC        0.43770E+02      26   0.27427E-03   0.52645E+01 0.27440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2675          9.0319          4.5729          4.5729
v  Velocity[Y]            -2.5537          7.2001         0.19866         0.19866
v  Velocity[Z]       -7.6541e-015     8.5271e-015    -1.2509e-017    -1.2509e-017
v  ǁVelocityǁ         0.0029749          9.0322          5.0373          5.0373
v  Pressure               -26.701          25.164         -1.2202         -1.2202
v  nu_tilda           4.3988e-007       0.0045532       0.0017725       0.0017725
v  TempC                       21          73.059          22.044          22.044
v  TurbVisc           3.2947e-014       0.0053664       0.0020838       0.0020838
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2981:        0.23830E+01

===============================================================


 INSTANT    0.298200000E+04   TIME STEP NUMBER            2982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16676E-01 0.89105E+00
   Friction velocity        uk    :  0.16676E-01 0.89105E+00
   Dimensionless distance   yplus :  0.13425E+00 0.71736E+01
   Friction thermal sca.    tstar : -0.12531E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10017E+00 0.53523E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10262E-01      33   0.23714E-03   0.36916E+01 0.18185E+03 
c  Velocity[X]                                      0.19560E+01 
c  Velocity[Y]                                      0.17356E+01 
c  Velocity[Z]                                      0.80697E-30 
c  Pressure     0.10305E-06     553   0.99320E-08   0.10034E+00 0.16995E+04 
c  nu_tilda     0.84343E-05      33   0.12502E-04   0.75890E-06 0.21687E+03 
c  TempC        0.43768E+02      26   0.27919E-03   0.55936E+01 0.25514E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2668           9.032          4.5729          4.5729
v  Velocity[Y]            -2.5527          7.1701         0.19836         0.19836
v  Velocity[Z]       -8.1983e-015     8.5336e-015    -1.2495e-017    -1.2495e-017
v  ǁVelocityǁ         0.0027716          9.0323          5.0373          5.0373
v  Pressure               -26.759          24.973         -1.3005         -1.3005
v  nu_tilda           4.3992e-007       0.0045532       0.0017723       0.0017723
v  TempC                       21          73.057          22.044          22.044
v  TurbVisc           3.2939e-014       0.0053664       0.0020837       0.0020837
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2982:        0.22670E+01

===============================================================


 INSTANT    0.298300000E+04   TIME STEP NUMBER            2983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15968E-01 0.88955E+00
   Friction velocity        uk    :  0.15968E-01 0.88955E+00
   Dimensionless distance   yplus :  0.12855E+00 0.71615E+01
   Friction thermal sca.    tstar : -0.13739E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.95913E-01 0.53433E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10261E-01      33   0.24292E-03   0.36676E+01 0.18160E+03 
c  Velocity[X]                                      0.19493E+01 
c  Velocity[Y]                                      0.17182E+01 
c  Velocity[Z]                                      0.12538E-29 
c  Pressure     0.10772E-06     584   0.97326E-08   0.10123E+00 0.14827E+04 
c  nu_tilda     0.84336E-05      33   0.27236E-05   0.75909E-06 0.21689E+03 
c  TempC        0.43765E+02      27   0.30286E-03   0.44316E+01 0.23090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2661          9.0322          4.5729          4.5729
v  Velocity[Y]            -2.5517          7.1871         0.19805         0.19805
v  Velocity[Z]       -7.6004e-015     8.5174e-015    -1.2479e-017    -1.2479e-017
v  ǁVelocityǁ         0.0028443          9.0324          5.0373          5.0373
v  Pressure               -26.687          25.127          -1.226          -1.226
v  nu_tilda           4.3994e-007       0.0045533       0.0017723       0.0017723
v  TempC                       21          73.057          22.044          22.044
v  TurbVisc           3.2952e-014       0.0053665       0.0020836       0.0020836
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2983:        0.23520E+01

===============================================================


 INSTANT    0.298400000E+04   TIME STEP NUMBER            2984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14614E-01 0.89071E+00
   Friction velocity        uk    :  0.14614E-01 0.89071E+00
   Dimensionless distance   yplus :  0.11766E+00 0.71709E+01
   Friction thermal sca.    tstar : -0.18051E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.87784E-01 0.53503E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10259E-01      33   0.25999E-03   0.36888E+01 0.18171E+03 
c  Velocity[X]                                      0.19763E+01 
c  Velocity[Y]                                      0.17126E+01 
c  Velocity[Z]                                      0.96130E-30 
c  Pressure     0.10479E-06     554   0.98456E-08   0.10180E+00 0.14579E+04 
c  nu_tilda     0.84330E-05      33   0.12501E-04   0.75929E-06 0.21692E+03 
c  TempC        0.43763E+02      27   0.26390E-03   0.36351E+01 0.23121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2654          9.0323          4.5729          4.5729
v  Velocity[Y]            -2.5507          7.1657         0.19774         0.19774
v  Velocity[Z]       -7.6077e-015     8.5246e-015    -1.2471e-017    -1.2471e-017
v  ǁVelocityǁ         0.0026689          9.0325          5.0373          5.0373
v  Pressure               -26.747           24.97         -1.2975         -1.2975
v  nu_tilda           4.3998e-007       0.0045534       0.0017721       0.0017721
v  TempC                       21          73.054          22.044          22.044
v  TurbVisc           3.2955e-014       0.0053666       0.0020835       0.0020835
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2984:        0.22630E+01

===============================================================


 INSTANT    0.298500000E+04   TIME STEP NUMBER            2985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13888E-01 0.88991E+00
   Friction velocity        uk    :  0.13888E-01 0.88991E+00
   Dimensionless distance   yplus :  0.11180E+00 0.71644E+01
   Friction thermal sca.    tstar : -0.18996E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.83419E-01 0.53454E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10257E-01      33   0.23791E-03   0.36713E+01 0.18159E+03 
c  Velocity[X]                                      0.19447E+01 
c  Velocity[Y]                                      0.17266E+01 
c  Velocity[Z]                                      0.88452E-30 
c  Pressure     0.89378E-07     570   0.95739E-08   0.85299E-01 0.17240E+04 
c  nu_tilda     0.84323E-05      33   0.27256E-05   0.75948E-06 0.21694E+03 
c  TempC        0.43761E+02      27   0.24756E-03   0.32767E+01 0.21326E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2647          9.0324          4.5729          4.5729
v  Velocity[Y]            -2.5496          7.1913         0.19743         0.19743
v  Velocity[Z]       -7.3667e-015     8.5091e-015    -1.2455e-017    -1.2455e-017
v  ǁVelocityǁ          0.002908          9.0326          5.0373          5.0373
v  Pressure               -26.677          25.164         -1.2139         -1.2139
v  nu_tilda           4.4001e-007       0.0045534       0.0017721       0.0017721
v  TempC                       21          73.054          22.044          22.044
v  TurbVisc            3.297e-014       0.0053666       0.0020833       0.0020833
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2985:        0.23060E+01

===============================================================


 INSTANT    0.298600000E+04   TIME STEP NUMBER            2986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.85683E-02 0.89108E+00
   Friction velocity        uk    :  0.85683E-02 0.89108E+00
   Dimensionless distance   yplus :  0.68981E-01 0.71738E+01
   Friction thermal sca.    tstar : -0.30788E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.51468E-01 0.53524E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10255E-01      33   0.25660E-03   0.36374E+01 0.18138E+03 
c  Velocity[X]                                      0.19245E+01 
c  Velocity[Y]                                      0.17129E+01 
c  Velocity[Z]                                      0.88058E-30 
c  Pressure     0.10624E-06     554   0.92720E-08   0.10075E+00 0.11484E+04 
c  nu_tilda     0.84316E-05      33   0.12498E-04   0.75970E-06 0.21697E+03 
c  TempC        0.43759E+02      26   0.36078E-03   0.53540E+01 0.25110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.264          9.0325          4.5729          4.5729
v  Velocity[Y]            -2.5486           7.193         0.19713         0.19713
v  Velocity[Z]       -7.9603e-015     8.5166e-015     -1.244e-017     -1.244e-017
v  ǁVelocityǁ         0.0030038          9.0328          5.0373          5.0373
v  Pressure               -26.738          25.065         -1.2741         -1.2741
v  nu_tilda           4.4001e-007       0.0045535       0.0017719       0.0017719
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc           3.2978e-014       0.0053667       0.0020832       0.0020832
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2986:        0.22710E+01

===============================================================


 INSTANT    0.298700000E+04   TIME STEP NUMBER            2987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.11097E-01 0.89078E+00
   Friction velocity        uk    :  0.11097E-01 0.89078E+00
   Dimensionless distance   yplus :  0.89342E-01 0.71714E+01
   Friction thermal sca.    tstar : -0.23776E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.66659E-01 0.53507E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10253E-01      33   0.24870E-03   0.36704E+01 0.18147E+03 
c  Velocity[X]                                      0.19653E+01 
c  Velocity[Y]                                      0.17051E+01 
c  Velocity[Z]                                      0.10190E-29 
c  Pressure     0.11759E-06     520   0.94157E-08   0.11402E+00 0.73636E+03 
c  nu_tilda     0.84309E-05      33   0.27297E-05   0.75990E-06 0.21700E+03 
c  TempC        0.43756E+02      26   0.27419E-03   0.92658E+01 0.33816E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2633          9.0326          4.5729          4.5729
v  Velocity[Y]            -2.5476          7.1697         0.19681         0.19681
v  Velocity[Z]       -7.3068e-015      8.499e-015    -1.2429e-017    -1.2429e-017
v  ǁVelocityǁ         0.0026634          9.0329          5.0373          5.0373
v  Pressure               -26.661          25.053          -1.234          -1.234
v  nu_tilda           4.4002e-007       0.0045536       0.0017718       0.0017718
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc           3.2977e-014       0.0053668       0.0020831       0.0020831
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2987:        0.21890E+01

===============================================================


 INSTANT    0.298800000E+04   TIME STEP NUMBER            2988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.90793E-02 0.88939E+00
   Friction velocity        uk    :  0.90793E-02 0.88939E+00
   Dimensionless distance   yplus :  0.73095E-01 0.71602E+01
   Friction thermal sca.    tstar : -0.29059E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.54537E-01 0.53423E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10251E-01      33   0.26685E-03   0.36560E+01 0.18144E+03 
c  Velocity[X]                                      0.19336E+01 
c  Velocity[Y]                                      0.17224E+01 
c  Velocity[Z]                                      0.79332E-30 
c  Pressure     0.88480E-07     537   0.94941E-08   0.84718E-01 0.76233E+03 
c  nu_tilda     0.84302E-05      33   0.12500E-04   0.76012E-06 0.21703E+03 
c  TempC        0.43754E+02      26   0.28230E-03   0.49422E+01 0.25549E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2626          9.0328          4.5729          4.5729
v  Velocity[Y]            -2.5466          7.1889          0.1965          0.1965
v  Velocity[Z]       -7.3666e-015     8.5071e-015    -1.2411e-017    -1.2411e-017
v  ǁVelocityǁ         0.0028854          9.0331          5.0373          5.0373
v  Pressure               -26.722          25.047         -1.2771         -1.2771
v  nu_tilda           4.3999e-007       0.0045537       0.0017717       0.0017717
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc           3.2982e-014       0.0053669        0.002083        0.002083
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2988:        0.22170E+01

===============================================================


 INSTANT    0.298900000E+04   TIME STEP NUMBER            2989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.13561E-01 0.89059E+00
   Friction velocity        uk    :  0.13561E-01 0.89059E+00
   Dimensionless distance   yplus :  0.10918E+00 0.71698E+01
   Friction thermal sca.    tstar : -0.19452E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.81459E-01 0.53495E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10249E-01      33   0.24986E-03   0.36746E+01 0.18135E+03 
c  Velocity[X]                                      0.19694E+01 
c  Velocity[Y]                                      0.17053E+01 
c  Velocity[Z]                                      0.81037E-30 
c  Pressure     0.13202E-06     536   0.98679E-08   0.12611E+00 0.84870E+03 
c  nu_tilda     0.84296E-05      33   0.27323E-05   0.76031E-06 0.21706E+03 
c  TempC        0.43752E+02      26   0.33721E-03   0.45964E+01 0.25259E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2619          9.0329          4.5729          4.5729
v  Velocity[Y]            -2.5455          7.1657         0.19619         0.19619
v  Velocity[Z]       -7.0636e-015     8.4919e-015    -1.2395e-017    -1.2395e-017
v  ǁVelocityǁ         0.0025811          9.0332          5.0373          5.0373
v  Pressure               -26.651          25.048         -1.2288         -1.2288
v  nu_tilda           4.3995e-007       0.0045538       0.0017716       0.0017716
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc            3.297e-014        0.005367       0.0020828       0.0020828
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2989:        0.22480E+01

===============================================================


 INSTANT    0.299000000E+04   TIME STEP NUMBER            2990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14161E-01 0.89005E+00
   Friction velocity        uk    :  0.14161E-01 0.89005E+00
   Dimensionless distance   yplus :  0.11401E+00 0.71655E+01
   Friction thermal sca.    tstar : -0.16889E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.85061E-01 0.53463E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10248E-01      33   0.18982E-03   0.36494E+01 0.18123E+03 
c  Velocity[X]                                      0.19513E+01 
c  Velocity[Y]                                      0.16981E+01 
c  Velocity[Z]                                      0.10463E-29 
c  Pressure     0.10700E-06     522   0.92808E-08   0.10305E+00 0.64608E+03 
c  nu_tilda     0.84289E-05      33   0.12498E-04   0.76052E-06 0.21708E+03 
c  TempC        0.43749E+02      26   0.25173E-03   0.76601E+01 0.28187E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2612           9.033          4.5729          4.5729
v  Velocity[Y]            -2.5445          7.1905         0.19588         0.19588
v  Velocity[Z]       -7.2172e-015        8.5e-015    -1.2384e-017    -1.2384e-017
v  ǁVelocityǁ         0.0029439          9.0333          5.0373          5.0373
v  Pressure               -26.712          25.083         -1.2628         -1.2628
v  nu_tilda           4.3992e-007       0.0045538       0.0017715       0.0017715
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc           3.2961e-014       0.0053671       0.0020827       0.0020827
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2990:        0.21680E+01

===============================================================


 INSTANT    0.299100000E+04   TIME STEP NUMBER            2991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14847E-01 0.89142E+00
   Friction velocity        uk    :  0.14847E-01 0.89142E+00
   Dimensionless distance   yplus :  0.11953E+00 0.71765E+01
   Friction thermal sca.    tstar : -0.17771E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89181E-01 0.53545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10246E-01      33   0.25741E-03   0.36289E+01 0.18111E+03 
c  Velocity[X]                                      0.19159E+01 
c  Velocity[Y]                                      0.17131E+01 
c  Velocity[Z]                                      0.80728E-30 
c  Pressure     0.85920E-07     569   0.97899E-08   0.82361E-01 0.12306E+04 
c  nu_tilda     0.84282E-05      33   0.27373E-05   0.76072E-06 0.21711E+03 
c  TempC        0.43747E+02      26   0.33815E-03   0.50451E+01 0.25961E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2605          9.0332          4.5729          4.5729
v  Velocity[Y]            -2.5434          7.2012         0.19556         0.19556
v  Velocity[Z]       -7.4435e-015     8.4842e-015     -1.237e-017     -1.237e-017
v  ǁVelocityǁ         0.0029767          9.0335          5.0373          5.0373
v  Pressure               -26.639          25.183         -1.1968         -1.1968
v  nu_tilda           4.3986e-007       0.0045539       0.0017714       0.0017714
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc            3.295e-014       0.0053671       0.0020826       0.0020826
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2991:        0.22990E+01

===============================================================


 INSTANT    0.299200000E+04   TIME STEP NUMBER            2992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16705E-01 0.89094E+00
   Friction velocity        uk    :  0.16705E-01 0.89094E+00
   Dimensionless distance   yplus :  0.13449E+00 0.71727E+01
   Friction thermal sca.    tstar : -0.14466E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10034E+00 0.53516E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10244E-01      33   0.24019E-03   0.36582E+01 0.18120E+03 
c  Velocity[X]                                      0.19575E+01 
c  Velocity[Y]                                      0.17007E+01 
c  Velocity[Z]                                      0.11356E-29 
c  Pressure     0.11256E-06     602   0.99291E-08   0.10751E+00 0.20647E+04 
c  nu_tilda     0.84275E-05      33   0.12497E-04   0.76094E-06 0.21714E+03 
c  TempC        0.43745E+02      26   0.26865E-03   0.54238E+01 0.29249E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2598          9.0333          4.5729          4.5729
v  Velocity[Y]            -2.5424           7.169         0.19525         0.19525
v  Velocity[Z]       -7.1529e-015     8.4895e-015    -1.2355e-017    -1.2355e-017
v  ǁVelocityǁ         0.0025815          9.0336          5.0373          5.0373
v  Pressure               -26.693          24.935         -1.2902         -1.2902
v  nu_tilda           4.3991e-007       0.0045539       0.0017712       0.0017712
v  TempC                       21          73.051          22.043          22.043
v  TurbVisc           3.2934e-014       0.0053672       0.0020825       0.0020825
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2992:        0.23920E+01

===============================================================


 INSTANT    0.299300000E+04   TIME STEP NUMBER            2993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14860E-01 0.88983E+00
   Friction velocity        uk    :  0.14860E-01 0.88983E+00
   Dimensionless distance   yplus :  0.11964E+00 0.71638E+01
   Friction thermal sca.    tstar : -0.12642E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.89262E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10242E-01      33   0.24633E-03   0.36282E+01 0.18098E+03 
c  Velocity[X]                                      0.19383E+01 
c  Velocity[Y]                                      0.16899E+01 
c  Velocity[Z]                                      0.10029E-29 
c  Pressure     0.93453E-07     618   0.93510E-08   0.90248E-01 0.22243E+04 
c  nu_tilda     0.84268E-05      33   0.27376E-05   0.76115E-06 0.21717E+03 
c  TempC        0.43742E+02      27   0.26728E-03   0.46584E+01 0.24687E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2592          9.0335          4.5729          4.5729
v  Velocity[Y]            -2.5414          7.1923         0.19493         0.19493
v  Velocity[Z]       -6.9287e-015     8.4765e-015    -1.2343e-017    -1.2343e-017
v  ǁVelocityǁ         0.0029179          9.0338          5.0373          5.0373
v  Pressure               -26.625          25.202         -1.1874         -1.1874
v  nu_tilda            4.399e-007        0.004554       0.0017712       0.0017712
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc           3.2947e-014       0.0053673       0.0020823       0.0020823
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2993:        0.24270E+01

===============================================================


 INSTANT    0.299400000E+04   TIME STEP NUMBER            2994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16382E-01 0.89062E+00
   Friction velocity        uk    :  0.16382E-01 0.89062E+00
   Dimensionless distance   yplus :  0.13189E+00 0.71701E+01
   Friction thermal sca.    tstar : -0.11741E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.98405E-01 0.53497E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10240E-01      33   0.26863E-03   0.36451E+01 0.18108E+03 
c  Velocity[X]                                      0.19367E+01 
c  Velocity[Y]                                      0.17084E+01 
c  Velocity[Z]                                      0.76983E-30 
c  Pressure     0.92594E-07     601   0.97373E-08   0.89760E-01 0.19550E+04 
c  nu_tilda     0.84261E-05      33   0.12495E-04   0.76137E-06 0.21720E+03 
c  TempC        0.43740E+02      26   0.31423E-03   0.41853E+01 0.22962E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2584          9.0336          4.5729          4.5729
v  Velocity[Y]            -2.5403          7.1684         0.19461         0.19461
v  Velocity[Z]       -6.9287e-015     8.4816e-015     -1.233e-017     -1.233e-017
v  ǁVelocityǁ         0.0026845          9.0339          5.0373          5.0373
v  Pressure               -26.681          24.973         -1.2774         -1.2774
v  nu_tilda           4.3991e-007       0.0045541        0.001771        0.001771
v  TempC                       21           73.05          22.043          22.043
v  TurbVisc           3.2945e-014       0.0053674       0.0020822       0.0020822
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2994:        0.23790E+01

===============================================================


 INSTANT    0.299500000E+04   TIME STEP NUMBER            2995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15494E-01 0.88979E+00
   Friction velocity        uk    :  0.15494E-01 0.88979E+00
   Dimensionless distance   yplus :  0.12474E+00 0.71634E+01
   Friction thermal sca.    tstar : -0.11032E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.93068E-01 0.53447E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10238E-01      33   0.21759E-03   0.36534E+01 0.18099E+03 
c  Velocity[X]                                      0.19613E+01 
c  Velocity[Y]                                      0.16922E+01 
c  Velocity[Z]                                      0.83948E-30 
c  Pressure     0.12126E-06     632   0.99896E-08   0.11424E+00 0.19199E+04 
c  nu_tilda     0.84253E-05      33   0.27442E-05   0.76157E-06 0.21723E+03 
c  TempC        0.43737E+02      27   0.27223E-03   0.36111E+01 0.23802E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2577          9.0338          4.5729          4.5729
v  Velocity[Y]            -2.5393          7.1891         0.19429         0.19429
v  Velocity[Z]       -6.9287e-015     8.4678e-015    -1.2311e-017    -1.2311e-017
v  ǁVelocityǁ         0.0028547           9.034          5.0373          5.0373
v  Pressure               -26.611          25.186         -1.1846         -1.1846
v  nu_tilda           4.3984e-007       0.0045541        0.001771        0.001771
v  TempC                       21          73.051          22.043          22.043
v  TurbVisc           3.2946e-014       0.0053674       0.0020821       0.0020821
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2995:        0.24510E+01

===============================================================


 INSTANT    0.299600000E+04   TIME STEP NUMBER            2996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.23080E-02 0.89118E+00
   Friction velocity        uk    :  0.23080E-02 0.89118E+00
   Dimensionless distance   yplus :  0.18581E-01 0.71746E+01
   Friction thermal sca.    tstar : -0.10885E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.13864E-01 0.53530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10236E-01      33   0.26049E-03   0.36456E+01 0.18097E+03 
c  Velocity[X]                                      0.19623E+01 
c  Velocity[Y]                                      0.16833E+01 
c  Velocity[Z]                                      0.10746E-29 
c  Pressure     0.10475E-06     553   0.94571E-08   0.10046E+00 0.12781E+04 
c  nu_tilda     0.84246E-05      33   0.12494E-04   0.76178E-06 0.21725E+03 
c  TempC        0.43735E+02      26   0.35557E-03   0.42126E+01 0.24780E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.257          9.0339          4.5729          4.5729
v  Velocity[Y]            -2.5382          7.1981         0.19397         0.19397
v  Velocity[Z]       -7.2708e-015     8.4735e-015      -1.23e-017      -1.23e-017
v  ǁVelocityǁ         0.0029629          9.0342          5.0373          5.0373
v  Pressure               -26.667          25.079         -1.2507         -1.2507
v  nu_tilda           4.3939e-007       0.0045542       0.0017708       0.0017708
v  TempC                       21          73.052          22.043          22.043
v  TurbVisc           3.2927e-014       0.0053675        0.002082        0.002082
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2996:        0.22650E+01

===============================================================


 INSTANT    0.299700000E+04   TIME STEP NUMBER            2997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16888E-01 0.89085E+00
   Friction velocity        uk    :  0.16888E-01 0.89085E+00
   Dimensionless distance   yplus :  0.13596E+00 0.71719E+01
   Friction thermal sca.    tstar : -0.10109E+03 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10144E+00 0.53511E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10234E-01      33   0.23907E-03   0.36449E+01 0.18089E+03 
c  Velocity[X]                                      0.19458E+01 
c  Velocity[Y]                                      0.16991E+01 
c  Velocity[Z]                                      0.84736E-30 
c  Pressure     0.11089E-06     538   0.92634E-08   0.10795E+00 0.94670E+03 
c  nu_tilda     0.84239E-05      33   0.27447E-05   0.76199E-06 0.21728E+03 
c  TempC        0.43733E+02      26   0.29055E-03   0.70259E+01 0.30462E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2563           9.034          4.5729          4.5729
v  Velocity[Y]            -2.5372          7.1716         0.19365         0.19365
v  Velocity[Z]       -6.9287e-015     8.4584e-015    -1.2286e-017    -1.2286e-017
v  ǁVelocityǁ         0.0027059          9.0343          5.0373          5.0373
v  Pressure               -26.594          25.106         -1.1967         -1.1967
v  nu_tilda           4.3898e-007       0.0045542       0.0017708       0.0017708
v  TempC                       21          73.052          22.042          22.042
v  TurbVisc           3.2793e-014       0.0053676       0.0020818       0.0020818
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2997:        0.22610E+01

===============================================================


 INSTANT    0.299800000E+04   TIME STEP NUMBER            2998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421569E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.15211E-01 0.88941E+00
   Friction velocity        uk    :  0.15211E-01 0.88941E+00
   Dimensionless distance   yplus :  0.12246E+00 0.71603E+01
   Friction thermal sca.    tstar : -0.94318E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.91366E-01 0.53424E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10233E-01      33   0.23986E-03   0.36128E+01 0.18070E+03 
c  Velocity[X]                                      0.19294E+01 
c  Velocity[Y]                                      0.16834E+01 
c  Velocity[Z]                                      0.83106E-30 
c  Pressure     0.10282E-06     522   0.98278E-08   0.97207E-01 0.88250E+03 
c  nu_tilda     0.84232E-05      33   0.12495E-04   0.76221E-06 0.21731E+03 
c  TempC        0.43730E+02      26   0.21147E-03   0.56103E+01 0.24973E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2556          9.0342          4.5729          4.5729
v  Velocity[Y]            -2.5362          7.1862         0.19333         0.19333
v  Velocity[Z]       -6.9287e-015     8.4653e-015     -1.227e-017     -1.227e-017
v  ǁVelocityǁ         0.0029088          9.0345          5.0373          5.0373
v  Pressure               -26.652          25.073         -1.2458         -1.2458
v  nu_tilda           4.3863e-007       0.0045543       0.0017706       0.0017706
v  TempC                       21          73.051          22.042          22.042
v  TurbVisc           3.2671e-014       0.0053676       0.0020817       0.0020817
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2998:        0.21930E+01

===============================================================


 INSTANT    0.299900000E+04   TIME STEP NUMBER            2999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421571E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.16660E-01 0.89066E+00
   Friction velocity        uk    :  0.16660E-01 0.89066E+00
   Dimensionless distance   yplus :  0.13412E+00 0.71705E+01
   Friction thermal sca.    tstar : -0.90782E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.10007E+00 0.53500E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10231E-01      33   0.25261E-03   0.36286E+01 0.18067E+03 
c  Velocity[X]                                      0.19527E+01 
c  Velocity[Y]                                      0.16759E+01 
c  Velocity[Z]                                      0.10040E-29 
c  Pressure     0.11233E-06     521   0.95994E-08   0.10886E+00 0.99331E+03 
c  nu_tilda     0.84224E-05      33   0.27504E-05   0.76241E-06 0.21734E+03 
c  TempC        0.43728E+02      27   0.29944E-03   0.31956E+01 0.20152E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2548          9.0343          4.5729          4.5729
v  Velocity[Y]            -2.5352          7.1686         0.19301         0.19301
v  Velocity[Z]       -6.9287e-015     8.4502e-015     -1.226e-017     -1.226e-017
v  ǁVelocityǁ         0.0026498          9.0346          5.0372          5.0372
v  Pressure               -26.576          25.107          -1.189          -1.189
v  nu_tilda           4.3828e-007       0.0045544       0.0017706       0.0017706
v  TempC                       21          73.051          22.042          22.042
v  TurbVisc           3.2567e-014       0.0053677       0.0020816       0.0020816
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             2999:        0.21870E+01

===============================================================


 INSTANT    0.300000000E+04   TIME STEP NUMBER            3000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.263421570E-03
Smooth wall               5        1720         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      312800         0.000000000E+00
Free outlet               3         200         0.263421570E-03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00-0.00000E+00
   Friction velocity        uet   :  0.14765E-01 0.88984E+00
   Friction velocity        uk    :  0.14765E-01 0.88984E+00
   Dimensionless distance   yplus :  0.11887E+00 0.71638E+01
   Friction thermal sca.    tstar : -0.86358E+02 0.00000E+00
   Rough dim-less th. sca.  tplus :  0.88691E-01 0.53450E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1720
   Total number of wall faces                   :       1720
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration       3000, Physical time    0.30000E+04


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint\main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint\main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint\auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.33200E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10229E-01      33   0.19784E-03   0.36219E+01 0.18066E+03 
c  Velocity[X]                                      0.19292E+01 
c  Velocity[Y]                                      0.16927E+01 
c  Velocity[Z]                                      0.82310E-30 
c  Pressure     0.10355E-06     521   0.95796E-08   0.99243E-01 0.75831E+03 
c  nu_tilda     0.84217E-05      33   0.12493E-04   0.76264E-06 0.21737E+03 
c  TempC        0.43725E+02      27   0.29314E-03   0.44694E+01 0.23744E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  nu_tilda
a  TempC   


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2541          9.0344          4.5729          4.5729
v  Velocity[Y]            -2.5341          7.1914         0.19268         0.19268
v  Velocity[Z]       -6.9287e-015     8.4571e-015    -1.2247e-017    -1.2247e-017
v  ǁVelocityǁ         0.0028914          9.0347          5.0372          5.0372
v  Pressure               -26.635          25.099         -1.2317         -1.2317
v  nu_tilda           4.3796e-007       0.0045544       0.0017704       0.0017704
v  TempC                       21          73.051          22.042          22.042
v  TurbVisc           3.2461e-014       0.0053678       0.0020815       0.0020815
v  total_pressure      1.013e+005     1.0135e+005     1.0132e+005     1.0132e+005


 TIME FOR THE TIME STEP             3000:        0.26230E+01

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.20000E-02
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  CPU time:                7188.531 s
  Total CPU time:         21565.593 s

  Elapsed time:            7188.531 s
  CPU / elapsed time          1.000

Memory use summary:

  Theoretical instrumented dynamic memory:       347.406 MiB
                             local minimum:      103.401 MiB  (rank 2)
                             local maximum:      140.205 MiB  (rank 0)
